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["ECSS Source Reference","ECSS Req. Indentifier","Type","IE PUID","Original requirement","Text of Note of Original Requirement","4. Applicability\n(A/M/D/N)","5. Modified or New requirement\n(full text)","6. Justification\n(only in case of M, D or N in colum 4)","Active or superseded ECSS","ECSS Discipline","Level 1 or Level 2 Standard"]
["ECSS-Q-ST-30-11C","4a","Requirement","ECSS-Q-ST-30-11_0140001","The user of this Standard shall verify that the ordered assurance level of procured components is compatible with the intended application.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2a","Requirement","ECSS-Q-ST-30-11_0140002","Derating shall be applied in consideration of temperature limits recommended.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2b","Requirement","ECSS-Q-ST-30-11_0140003","The derating requirements of this Standard shall not be used as a justification to upgrade the quality level of components.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2c","Requirement","ECSS-Q-ST-30-11_0140004","The derating requirements shall be taken into account at the beginning of the design cycle of an equipment for any consequential design trade-off to be made. Specific attention shall be paid to, for example, breadboards and engineering models where parameter derating was not considered.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2d","Requirement","ECSS-Q-ST-30-11_0140005","Component families and groups excluded in this Standard are due to the lack of experimental data and failure history. For these components, the user shall consult a component design and reliability specialist to apply the requirements of this Standard.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2e","Requirement","ECSS-Q-ST-30-11_0140006","Components may be excluded from this Standard if they are used for short durations of less than one month provided the device ratings are not exceeded; for example, components used in solar generator deployment systems, redundancy commutation and launchers (except in some specific cases, noted family by family). In these cases, the designer shall ensure that the applied stress level does not exceed the component maximum rating. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2f","Requirement","ECSS-Q-ST-30-11_0140007","In the same way, during a test (e.g. qualification and EMC), derating requirements are applied on operating conditions and not on test conditions, even if during some periods, the temperature range reached is higher than the derated value. However, the specified maximum ratings shall not be exceeded. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2g","Requirement","ECSS-Q-ST-30-11_0140008","Derating shall be applied on normal operating conditions and not on the fault condition. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.3.2h","Requirement","ECSS-Q-ST-30-11_0140009","Where components are required to operate in protection mode or in fail-safe mode in order to prevent failure propagation (e.g. short-circuit protection), the components concerned shall meet the derating requirements and application rules when performing the protection or fail-safe function under the worst failure case (i.e. highest stress applied to the components that can last throughout the mission).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.4.2a","Requirement","ECSS-Q-ST-30-11_0140010","If ratings are provided for transients or surge conditions, the same derating figures as for steady-state equivalent parameters shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.4.2b","Requirement","ECSS-Q-ST-30-11_0140011","If ratings are not provided for transient or surge conditions, then it shall be assured that the transient or surge values are below the steady-state specified maximum ratings.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.4.2c","Requirement","ECSS-Q-ST-30-11_0140012","Repetitive transients, e.g. in a switching DC/DC converter operation, and clock transmission lines, shall not exceed the derated steady-state values, superseded by no more than 90 % of the rated manufacturer values if not compatible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.4.2d","Requirement","ECSS-Q-ST-30-11_0140013","Where radiation sensitive components are identified, it is the user’s responsibility that the chosen component technologies are suitable and that the mitigation factors, such as shielding, meet the customer’s requirement. The electrical derating shall be in accordance with this Standard.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","5.5.2a","Requirement","ECSS-Q-ST-30-11_0140014","For hybrids, individual components shall be in conformance with their respective derating rules.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.2.1a","Requirement","ECSS-Q-ST-30-11_0140015","The capacitor stress sum value of steady-state voltage, AC voltage shall not exceed the load ratios specified hereunder. For transients refer to clause 5.4.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.2.1b","Permission","ECSS-Q-ST-30-11_0140079","Multilayer capacitors with a DC voltage rating less than 100 V may be used in low voltage (less than 10 V) continuous applications provided they have been submitted to a low voltage (1,5 V) 85 % humidity at 85 °C test or other approved method. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.2.1c","Recommendation","ECSS-Q-ST-30-11_0140080","Physical limitation for type II: maximum surge dV/dt approximate to 100 V/ms. This should be verified with the manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.2.1d","Recommendation","ECSS-Q-ST-30-11_0140081","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1a","Requirement","ECSS-Q-ST-30-11_0140019","The capacitor stress sum value of steady-state voltage and AC voltage shall not exceed the load ratio specified hereunder. For transients refer to clause 5.4.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1b","Requirement","ECSS-Q-ST-30-11_0140020","100 % surge current screening shall be applied for all surface mounted capacitors types.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1c","Requirement","ECSS-Q-ST-30-11_0140021","Surge current shall be derated to 75 % of the Isurge max. Isurge max is defined as Vrated/(ESR+Rs). Vrated is the maximum rated voltage, ESR is the maximum specified value and Rs is the value of series resistance specified in the circuit for surge current testing as defined in the applicable procurement specification.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1d","Requirement","ECSS-Q-ST-30-11_0140022","Reverse voltage shall not exceed 75 % of the manufacturer’s specified maximum value for the reverse voltage.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1e","Requirement","ECSS-Q-ST-30-11_0140023","Ripple power shall never exceed 50 % of the manufacturer’s specified maximum value.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.3.1f","Recommendation","ECSS-Q-ST-30-11_0140082","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.4.1a","Requirement","ECSS-Q-ST-30-11_0140025","Reverse voltage shall not exceed 75 % of the manufacturer’s specified maximum value for the reverse voltage.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.4.1b","Requirement","ECSS-Q-ST-30-11_0140026","Manufacturer’s ratings for ripple power or current shall never be exceeded. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.4.1c","Recommendation","ECSS-Q-ST-30-11_0140083","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.5.1a","Requirement","ECSS-Q-ST-30-11_0140028","Self healing requirements for polyethylene terepthalate (PET, polyester) film:\n    1. To have a clearing process in any case, the minimum energy available shall be greater than the manufacturer’s specified value (typical self healing energy is 5 mJ minimum).\n    2. To prevent any risk of destruction during self healing, capacitor banks shall not provide energy greater than 15 J.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.5.1b","Requirement","ECSS-Q-ST-30-11_0140029","For other films, clearing recommendations from manufacturers shall be followed.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.5.1c","Recommendation","ECSS-Q-ST-30-11_0140084","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.6.1a","Recommendation","ECSS-Q-ST-30-11_0140085","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.7.1a","Recommendation","ECSS-Q-ST-30-11_0140086","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.8.1a","Recommendation","ECSS-Q-ST-30-11_0140087","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.9.1a","Recommendation","ECSS-Q-ST-30-11_0140088","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.10.1a","Recommendation","ECSS-Q-ST-30-11_0140089","Internal heating due to ESR can increase ageing and should be taken into account by applying a margin in temperature. Where ESR is not known at the frequency of a ripple current, an extrapolation of the ESR value and resonance (from manufacturer’s or test data) should be made where possible.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.11.1a","Requirement","ECSS-Q-ST-30-11_0140036","For power connectors, power and return lines shall be separated by at least one unassigned contact to reduce the short-circuit risk.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.11.1b","Requirement","ECSS-Q-ST-30-11_0140037","Connector savers shall be used during testing of equipment to minimize number of mating and demating cycles.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.11.1c","Requirement","ECSS-Q-ST-30-11_0140038","When multi-pin connectors are close to one another, they shall be configured such that mating with a wrong connector is not possible or the contact assignments shall be chosen such that mating with a wrong connector does not cause damage to the unit itself nor to any other element of the system.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.11.1d","Requirement","ECSS-Q-ST-30-11_0140039","The connector and its constituent parts shall be from the same manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.12.1a","Requirement","ECSS-Q-ST-30-11_0140040","Connector savers shall be used during testing of equipment to minimize number of mating and demating cycles.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.14.1a","Requirement","ECSS-Q-ST-30-11_0140041","Some diodes can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60. Where power cycling is critical this should be considered.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.15.1a","Requirement","ECSS-Q-ST-30-11_0140042","Some diodes can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.17.1a","Requirement","ECSS-Q-ST-30-11_0140043","Fuses shall be avoided whenever possible. The derating requirements in 6.17.2 (below) are only applicable to Cermet types. The application and the deratings of other fuse technologies shall be justified.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.17.1b","Requirement","ECSS-Q-ST-30-11_0140044","The largest fuse rating compatible with the source capability shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.17.1c","Requirement","ECSS-Q-ST-30-11_0140045","The power supply shall be capable of delivering three times the specified fuse rated current in order to obtain short fusing times.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.18.1a","Requirement","ECSS-Q-ST-30-11_0140046","For custom-made inductors and transformers, the maximum rated temperature shall be evaluated taking into consideration the temperature characteristics of the materials used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.19.1a","Requirement","ECSS-Q-ST-30-11_0140047","Some devices can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.20.1a","Requirement","ECSS-Q-ST-30-11_0140048","Some devices can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.21.1a","Requirement","ECSS-Q-ST-30-11_0140049","Some linear circuits can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.21.1b","Requirement","ECSS-Q-ST-30-11_0140050","Additional margins can be applied for radiation effects.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.22.1a","Requirement","ECSS-Q-ST-30-11_0140051","Some linear circuits can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.23.1a","Requirement","ECSS-Q-ST-30-11_0140052","Some MMICs can be radiation sensitive: the choice of MMICs shall be based on suitability and application. Justification shall be in accordance with ECSS-Q-ST-60 and provided in accordance with this Standard, and at the design reviews.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.23.2a","Requirement","ECSS-Q-ST-30-11_0140053","Each discrete cell (capacitors, resistors, diodes and transistors) constituting analogue custom MMICs shall be derated in accordance with this document’s requirements for the applicable family. For digital cells, apply the derating rules applicable to integrated circuits.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.23.2b","Requirement","ECSS-Q-ST-30-11_0140054","When operational reliability data is available, the compression level shall be derated to 2 dB under the highest compression level showing no drift. MMICs having no compression data shall not be submitted to more than 1 dB of compression.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.24.1a","Requirement","ECSS-Q-ST-30-11_0140055","For all ICs not considered in the previous subgroups, the following derating rules shall be followed:\n    1. Manufacturer’s derating values.\n    2. Maximum junction temperature: 110 °C or Tj max - 40 °C, whichever is lower.\n    3. For the part of the IC similar to logic ICs, apply the derating rules for logic subgroups, for the part similar to linear ICs, apply the derating rules for linear subgroups and so forth.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.24.1b","Requirement","ECSS-Q-ST-30-11_0140056","Some integrated circuits can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1a","Requirement","ECSS-Q-ST-30-11_0140057","The coil supply voltage shall be within the specified voltage range or between the specified rated and the maximum coil voltage.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1b","Requirement","ECSS-Q-ST-30-11_0140058","The minimum coil pulse duration for latching relays shall be 10 times the sum of latch time (tL) and bounce time (tB) or 30 ms, whichever is greater.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1c","Requirement","ECSS-Q-ST-30-11_0140059","Current derating does not apply to contacts that only carry current and do not switch it or to contacts that switch at zero current. In the latter case, the number of operations is limited to the qualified number of operations.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1d","Requirement","ECSS-Q-ST-30-11_0140060","Rated contact load voltage should not be exceeded since it has a strong impact on the contact current: this shall be recorded and approved in accordance with ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1e","Requirement","ECSS-Q-ST-30-11_0140061","A double throw contact shall not be used to switch a load (movable contact) between a power supply and ground (stationary contacts). This type of configuration may be accepted in the following conditions:\n    1. when switching off the power supply the other stationary contact is not connected to ground, or\n    2. the potential difference between stationary contacts is less than 10 V and the switched current less than 0,1 A.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1f","Requirement","ECSS-Q-ST-30-11_0140062","Paralleled relays shall not be used to increase current switching capabilities of contacts. When relays are paralleled for redundancy, in order to increase the system’s reliability, the sum of the paralleled currents shall not exceed the contact current rating. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.25.1g","Requirement","ECSS-Q-ST-30-11_0140063","Suppression diodes shall not be used inside relays. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.26.1.1a","Requirement","ECSS-Q-ST-30-11_0140064","The mentioned temperatures cited below refer to case temperatures.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.26.1.9a","Requirement","ECSS-Q-ST-30-11_0140065","Average power < 50 % of nominal rating\n \nwhere\nVp\tis the pulse amplitude\nR\tis the resistance\ntp\tis the pulse width\nT\tis the cycle duration",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.26.1.10a","Requirement","ECSS-Q-ST-30-11_0140066","If ratings are provided for transient or surge condition, the same derating figures as for steady-state equivalent parameters shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.26.1.10b","Requirement","ECSS-Q-ST-30-11_0140067","If ratings are not provided for transient or surge condition, then it shall be assured that the transient or surge values are below the steady-state specified ratings.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.26.2a","Requirement","ECSS-Q-ST-30-11_0140068","Actual rated power shall be specified in the applicable heater design drawing. It shall be determined from the specified heating area (s) in cm2 taking into account the thermal properties of the mounted heater in the application.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.28.1a","Requirement","ECSS-Q-ST-30-11_0140069","Some transistors can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.29.1a","Requirement","ECSS-Q-ST-30-11_0140070","Only SEE radiation characterized MOSFETs shall be used in space applications.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.29.1b","Requirement","ECSS-Q-ST-30-11_0140071","The user shall consider power cycling when this is critical to his application.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.30.1a","Requirement","ECSS-Q-ST-30-11_0140072","Some transistors can be radiation sensitive: the issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.31.1a","Requirement","ECSS-Q-ST-30-11_0140073","Some transistors can be radiation sensitive: this issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.33.1a","Requirement","ECSS-Q-ST-30-11_0140074","Light emitting diodes can be radiation sensitive, in particular, there is a high sensitivity to proton displacement damage: this issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.33.1b","Requirement","ECSS-Q-ST-30-11_0140075","Opto-couplers can be radiation sensitive, in particular, operation at low diode currents increases radiation sensitivity: this issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.33.1c","Requirement","ECSS-Q-ST-30-11_0140076","Photo-transistors can be radiation sensitive: this issue shall be recorded in the design file and the components selection shall be reviewed and approved as described in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.34.1a","Requirement","ECSS-Q-ST-30-11_0140077","For connectorized components, connector savers shall be used during testing of equipment to minimize number of mating and demating cycles.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-30-11C","6.36a","Requirement","ECSS-Q-ST-30-11_0140078","For hybrids, individual components shall be in conformance with their respective derating rules.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.1a","Requirement","ECSS-Q-ST-70-13_0610001","The supplier shall identify, manage and process materials and parts with hazardous characteristics according to ECSS-Q-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.1b","Requirement","ECSS-Q-ST-70-13_0610002","The supplier shall keep the health and safety precautions according to the supplier’s national safety regulations.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1a","Requirement","ECSS-Q-ST-70-13_0610003","The supplier shall prepare the material samples according to the process specifications or manufacturer’s data.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1b","Requirement","ECSS-Q-ST-70-13_0610004","The material samples shall be representative of batch variance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1c","Requirement","ECSS-Q-ST-70-13_0610005","If it is not practicable to test completed assemblies, the supplier shall submit samples made from the same materials and by the same processes as those used in the manufacture of the assemblies.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1d","Requirement","ECSS-Q-ST-70-13_0610006","The sample for testing shall have clean flat surfaces which do not overlap the sample holder described in clause 5.1.4.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1e","Requirement","ECSS-Q-ST-70-13_0610007","The width of the test sample surface face shall be at least equal to the width of the tape used in the test procedure.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1f","Requirement","ECSS-Q-ST-70-13_0610008","The nominal tape width shall be 20 mm.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1g","Requirement","ECSS-Q-ST-70-13_0610009","The supplier shall specify the number of samples to be taken from a qualification batch, test programme, or production batch at the start of the test in conformance with the DRD in Annex A..",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1h","Requirement","ECSS-Q-ST-70-13_0610010","The supplier shall test at least ten test samples.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1i","Requirement","ECSS-Q-ST-70-13_0610011","If it is not practicable to obtain test samples from the finished article, the supplier shall furnish bonded test samples for the test.\n    ","NOTE These samples are not used for any other purpose than the designated test.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1j","Requirement","ECSS-Q-ST-70-13_0610012","The supplier shall furnish a certificate of conformity for the purpose of traceability.\n    ","NOTE This certificate of conformity is delivered by the manufacturer in order to provide evidence that the product is compliant with the manufacturer’s process.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.1k","Requirement","ECSS-Q-ST-70-13_0610013","The supplier shall mark all test samples with identification to maintain traceability but in such a way as not to degrade the quality of the sample during testing.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.2a","Requirement","ECSS-Q-ST-70-13_0610014","The suppler shall perform the same cleaning and other treatments of the sample as that applied to the finished article, which the sample is intended to represent, prior to integration into the spacecraft.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.2b","Requirement","ECSS-Q-ST-70-13_0610015","The supplier shall not carry out further cleaning or other treatments.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.3a","Requirement","ECSS-Q-ST-70-13_0610016","The supplier shall handle the samples only with clean nylon or lint-free gloves.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.3b","Requirement","ECSS-Q-ST-70-13_0610017","The supplier shall store the samples in a controlled area, with an ambient temperature of (22 ± 3) °C and relative humidity of (55 ± 10) %.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.3c","Requirement","ECSS-Q-ST-70-13_0610018","The supplier shall shield coated surfaces from contact by using polyethylene or polypropylene bags or sheets.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.3d","Requirement","ECSS-Q-ST-70-13_0610019","The supplier shall avoid physical damage by packing the polyethylene or polypropylene-wrapped workpieces in clean, dust- and lint-free material.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.3e","Requirement","ECSS-Q-ST-70-13_0610020","The supplier shall label limited-life materials with their shelf lives and dates of manufacture, or date of delivery if date of manufacture is not known.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.4.1a","Requirement","ECSS-Q-ST-70-13_0610021","The supplier shall identify materials submitted for testing in conformance to annex A of ECSS-Q-ST-70-02.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.2.4.2a","Requirement","ECSS-Q-ST-70-13_0610022","The supplier shall identify assemblies submitted for testing, as a minimum, by:\n    1. trade name and batch number;\n    2. name of manufacturer or supplier through whom the purchase was made;\n    3. configuration control status of the assembly.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.3.1a","Requirement","ECSS-Q-ST-70-13_0610023","The work area shall be clean and free of dust.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.3.1b","Requirement","ECSS-Q-ST-70-13_0610024","The supplier shall filter the air used for ventilation to prevent contamination of the sample.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.3.2a","Requirement","ECSS-Q-ST-70-13_0610025","The supplier shall environmentally condition the sample for a nominal 24 hour period at (22 ± 3) °C with a relative humidity of (55 ± 10) %.\n    ","NOTE 1 The humidity requirement can be achieved either in a conditioning room, or by dessicators filled with silica gel or a saturated salt solution.\nNOTE 2 A saturated salt solution of calcium nitrate gives approximately 51 % relative humidity at the testing temperature.\n",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.1a","Requirement","ECSS-Q-ST-70-13_0610026","The supplier shall use the equipment as detailed in clauses 5.1.4.2 and 5.1.4.3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.2a","Requirement","ECSS-Q-ST-70-13_0610027","The supplier shall employ a power-driven machine capable of maintaining a specified constant rate of loading and able to be used for both tensile and compressive testing.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.2b","Requirement","ECSS-Q-ST-70-13_0610028","The machine shall have a fixed or essentially stationary member supporting a load cell and the tape holder.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.2c","Requirement","ECSS-Q-ST-70-13_0610029","A movable member shall carry the sample holder.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.2d","Requirement","ECSS-Q-ST-70-13_0610030","The applied compressive and tensile loads, as measured and recorded, shall be accurate within 1 percent of the load.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.2e","Requirement","ECSS-Q-ST-70-13_0610031","The rate of travel of the sample holder shall be at a nominal rate of 0,2 cm/min.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.3a","Recommendation","ECSS-Q-ST-70-13_0610074","The tape holder should be of a design similar to that depicted in Figure 5-1.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.3b","Requirement","ECSS-Q-ST-70-13_0610033","The part shall be screwed into the fixed member of the testing machine or be located firmly on it.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.3c","Requirement","ECSS-Q-ST-70-13_0610034","The supplier shall clamp a length of pressure-sensitive tape from one tape holder over the rubber block to the other tape holder.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.3d","Requirement","ECSS-Q-ST-70-13_0610035","The surface of the pressure-sensitive tape in contact with the flat surface of the rubber block shall be 4 cm2 ± 5 %.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.4a","Requirement","ECSS-Q-ST-70-13_0610036","The sample holder shall be firmly located beneath the tape holder on the movable member of the testing machine.\n    ","NOTE 1 A suitable design is seen in Figure 5-1.\nNOTE 2 This preferred system utilizes “top hat” supports onto which individual samples can be mechanically clamped or bonded in such a way that there is no relative movement between the support and the test sample at any time during the test cycle.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.4b","Requirement","ECSS-Q-ST-70-13_0610037","In case a “top hat” sample support is used, it shall slide into a horizontal fixture slot in such a way that its top surface is parallel to and directly beneath the rubber face of the tape holder.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.1.4.5a","Requirement","ECSS-Q-ST-70-13_0610038","The supplier shall employ a range of pressure-sensitive tapes for the tests with peel adhesion strengths of 220, 330, 440 and 670 g/cm, all with a tolerance of ± 10 %.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.1.1a","Requirement","ECSS-Q-ST-70-13_0610039","The supplier shall locate the test sample on the sample holder in conformance with the requirements stated in clause 5.1.4.3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.1.1b","Requirement","ECSS-Q-ST-70-13_0610040","If an adhesive bond is used between the sample and the sample support, this shall in no way interfere with the area under test.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.1.1c","Requirement","ECSS-Q-ST-70-13_0610041","The supplier shall ensure that there is no physical or chemical interaction between any adhesive employed during sample preparation and the sample materials.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.1.2a","Requirement","ECSS-Q-ST-70-13_0610042","The supplier shall condition the loaded sample support for a nominal 24 hours in conformance with the requirements stated in clause 5.1.3.2 before the test starts.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.2a","Recommendation","ECSS-Q-ST-70-13_0610076","The supplier should run the peel and pull-off test as described in Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.2b","Requirement","ECSS-Q-ST-70-13_0610044","If the supplier uses a different procedure, the supplier shall submit it for customer approval.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.2.3a","Requirement","ECSS-Q-ST-70-13_0610045","The supplier shall apply the conditions specified in clause 5.1.2.3 unless other post test disposal instructions are given.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3a","Requirement","ECSS-Q-ST-70-13_0610046","The supplier shall classify samples which have been tested and are not seen to be disturbed in any way by the processing described in clause 5.2.2 as having passed this test.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3b","Requirement","ECSS-Q-ST-70-13_0610047","The supplier shall examine samples in detail, which have been disturbed during the test sequence.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3c","Requirement","ECSS-Q-ST-70-13_0610048","The supplier shall carry out a visual examination for sample defects at ×7 magnification.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3d","Recommendation","ECSS-Q-ST-70-13_0610077","In case defects are detected at ×7 magnification, the supplier should use higher magnifications during further analysis for locating microscopic defects on any fracture surfaces.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3e","Requirement","ECSS-Q-ST-70-13_0610050","The supplier shall report defects and the appearance of the fracture.\n    ","NOTE 1 Defects for instance can be air bubbles or material inclusions.\nNOTE 2 Appearance of the fracture for instance can be rough, ductile, smooth or brittle.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3f","Requirement","ECSS-Q-ST-70-13_0610051","The supplier shall state the particular material or interface along which the fracture path has propagated through the test sample.\n    ","NOTE This can be wholly or partly an adhesion fracture, a cohesive separation or an adherent fracture as schematically drawn in Figure C-1.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3g","Requirement","ECSS-Q-ST-70-13_0610052","The supplier shall take a photographic record of the tested samples at appropriate level of magnification.\n    ","NOTE Typical topographical features are recorded at ×2, ×20, ×50, ×100, ×250, ×500 or ×1000 magnifications.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3h","Requirement","ECSS-Q-ST-70-13_0610053","The supplier shall agree with the customer on the granularity level of failure analysis to be performed on failed samples, prior to the test.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.3i","Requirement","ECSS-Q-ST-70-13_0610054","The supplier shall perform the failure analysis as agreed with the customer.\n    ","NOTE This failure analysis can include metallographic studies, chemical analysis or scanning electronic microscopy.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.1a","Requirement","ECSS-Q-ST-70-13_0610055","The supplier shall retain the quality records for at least ten years or in conformance with project business agreement requirements, and in conformance with the Test result sheet - DRD in Annex A.\n    ","NOTE Example of such quality records are logbooks.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.2a","Requirement","ECSS-Q-ST-70-13_0610056","The supplier shall disposition any nonconformance which is observed in respect of the test process in conformance with the quality assurance requirements specified in ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.3a","Requirement","ECSS-Q-ST-70-13_0610057","The supplier shall use only measuring equipment calibrated to traceable reference standard.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.3b","Requirement","ECSS-Q-ST-70-13_0610058","The supplier shall record any suspected or actual equipment failure as a project nonconformance report according to ECSS-Q-ST-20.\n    ","NOTE This is to ensure that previous results can be examined to ascertain whether or not re-inspection and retesting is required.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.3c","Requirement","ECSS-Q-ST-70-13_0610059","The supplier shall notify the customer of the nonconformance details.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","5.4.4a","Requirement","ECSS-Q-ST-70-13_0610060","The supplier shall maintain traceability throughout the process from incoming inspection to final test, including details of test equipment and personnel employed in performing the task.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1a","Requirement","ECSS-Q-ST-70-13_0610061","The test result sheet shall contain the trade names of the materials under test.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1b","Requirement","ECSS-Q-ST-70-13_0610062","The test result sheet shall contain the batch numbers of the materials under test.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1c","Requirement","ECSS-Q-ST-70-13_0610063","The test result sheet shall contain name of manufacturer or supplier through whom the purchase was made.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1d","Requirement","ECSS-Q-ST-70-13_0610064","The test result sheet shall contain summary of the preparation and conditioning schedule.\n    ","NOTE This can be for instance the mixing proportions, coating thickness, cure time and temperature, post-cure or cleaning procedure.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1e","Requirement","ECSS-Q-ST-70-13_0610065","The test result sheet shall contain details of the testing room environment conditions and test equipment.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1f","Requirement","ECSS-Q-ST-70-13_0610066","The test result sheet shall contain details of the test parameters outlined in Annex B.\n    ","NOTE This also includes any variation in testing environment conditions.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1g","Requirement","ECSS-Q-ST-70-13_0610067","The test result sheet shall contain details of equipment used for visual, mechanical, chemical and physical property measurement or inspection, as outlined in Annex B and test specifications where they exist.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1h","Requirement","ECSS-Q-ST-70-13_0610068","The test result sheet shall contain the number of sample tests.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1i","Requirement","ECSS-Q-ST-70-13_0610069","The test result sheet shall contain the results of the values obtained for peel or pull-off strength.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1j","Requirement","ECSS-Q-ST-70-13_0610070","The test result sheet shall contain the peel strength indicated by the manufacturer of the pressure-sensitive tape used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1k","Requirement","ECSS-Q-ST-70-13_0610071","The test result sheet shall contain the results of any failure analysis carried out according to clause 5.3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1l","Requirement","ECSS-Q-ST-70-13_0610072","The test result sheet shall contain the mode of fracture and any photographic records.\n    ","NOTE An indication of the various fracture line is given in Figure C-1.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C","A.2.1m","Requirement","ECSS-Q-ST-70-13_0610073","In case of failures, the test result sheet shall contain the following details of failure mode:\n    1. deficient design;\n    2. poor workmanship;\n    3. wrong fabrication or application procedure;\n    4. wrong choice of materials;\n    5. others.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-13C",null,"Permission","ECSS-Q-ST-70-13_0610078","The supplier may use the template given in Figure A-1.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-60C Rev. 1","4.1.1a","Requirement","ECSS-Q-ST-60_0480001","The supplier shall establish and implement throughout the duration of the business agreement a component programme which ensures that the requirements of the project as defined by the customer and the supplier in the related business agreement are in compliance with this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.2.1a","Requirement","ECSS-Q-ST-60_0480002","The supplier shall identify the organization responsible for the management of the component programme, and describe the organization’s approaches (including the procurement system and its rationale) and capability to efficiently implement, manage, and control the component requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.2.1b","Requirement","ECSS-Q-ST-60_0480003","The supplier’s organization shall comply with all the requirements of ECSS-M-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.2.2a","Requirement","ECSS-Q-ST-60_0480004","The supplier shall prepare a Component Control Plan (CCP) in conformance with its DRD in Annex A.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.2.2b","Permission","ECSS-Q-ST-60_0480446","The CCP may be part of the overall project PA plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.2.2c","Requirement","ECSS-Q-ST-60_0480006","The supplier shall submit the CCP to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.3a","Requirement","ECSS-Q-ST-60_0480007","At supplier's level, the Parts Control Board (PCB) shall be chaired by a member of the supplier’s PA team with designated responsibility for components management. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.3b","Requirement","ECSS-Q-ST-60_0480008","The composition of the PCB shall as a minimum include additionally the suppliers’ parts engineer, the customer’s representative and the lower tier subcontractor parts engineers.\n    ","NOTE The approval of the selection and usage of EEE parts are implemented through Parts Control Boards (PCBs) held between the customer and the supplier (or lower tier subcontractor).",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.3c","Permission","ECSS-Q-ST-60_0480447","Other pertinent experts from the customer or suppliers may also participate, on request.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.3d","Requirement","ECSS-Q-ST-60_0480010","Depending on the progress of the program, the main PCB activities shall be:\n    1. Review and approval of the supplier's EEE component control plan and any associated documents,\n    2. Parts type reduction and standardization,\n    3. Parts approval including evaluation activities,\n    4. Problem assessment (e.g. alerts, nonconformances, RFD, RFW and delivery delays).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4a","Requirement","ECSS-Q-ST-60_0480011","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4b","Requirement","ECSS-Q-ST-60_0480012","This list shall be kept under configuration control (issue and identification of changes). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4c","Requirement","ECSS-Q-ST-60_0480013","The DCL shall be issued as a minimum at PDR and CDR (as designed) and at flight hardware delivery (as built).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4d","Requirement","ECSS-Q-ST-60_0480014","After equipment CDR, all modifications affecting the PAD information shall be implemented, in the \"as design\" DCL, through the CN / CR process and submitted to the customer for approval.\n    ","NOTE For PAD generation, see 4.2.4d.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4e","Requirement","ECSS-Q-ST-60_0480015","The “as design” DCL shall be sent to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4f","Requirement","ECSS-Q-ST-60_0480016","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4g","Requirement","ECSS-Q-ST-60_0480017","The “as built” DCL reflecting the actual EEE parts assembled into the flight hardware and their date code, shall be provided to the customer for review at the delivery of the flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.4h","Requirement","ECSS-Q-ST-60_0480018","The content of the DCL shall be in conformance with its DRD in Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.5a","Requirement","ECSS-Q-ST-60_0480019","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.1.5b","Requirement","ECSS-Q-ST-60_0480020","Flight hardware connectors interfaces to GSE shall be protected by connector savers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.1a","Requirement","ECSS-Q-ST-60_0480021","The supplier shall ensure that the following requirements are met during his selection process:\n    1. Project requirements (e.g. quality levels, component policy, manufacturing and delivery schedules and budgets, quantities),\n    2. Design requirements (e.g. component type, case, dimensions, materials),\n    3. Production requirements (e.g. packaging, thermal and storage constraints, component mounting process),\n    4. Operational requirements (e.g. electrical, mechanical, radiation, reliability, assembly, and lifetime).\n        ","NOTE The supplier of each product is responsible for the selection of components, which enable the performance, lifetime, environmental, material, safety, quality and reliability requirements of the product of which they form a part, to be satisfied in all respects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1a","Requirement","ECSS-Q-ST-60_0480022","The supplier shall establish and maintain in his own facility, and ensure that his suppliers also establish and maintain, procedures for selecting and controlling all components intended for use in deliverable products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1b","Requirement","ECSS-Q-ST-60_0480023","Components shall be selected on the basis of proven qualification, characterization, and previous space experience and data, relevant with regard to the requirements for the programme, from manufacturers or sources (preferably European) employing effective Product Assurance Programmes in manufacturing and test.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1c","Requirement","ECSS-Q-ST-60_0480024","Preference shall be given to components which necessitate the least evaluation or qualification effort. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1d","Requirement","ECSS-Q-ST-60_0480025","Starting with the design phase of the project the supplier shall ensure maximum use of preferred (see 4.2.2.3) and qualified components to achieve an effective component reduction and standardization. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1e","Requirement","ECSS-Q-ST-60_0480026","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.1f","Requirement","ECSS-Q-ST-60_0480027","The supplier shall implement a type reduction activity.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2a","Requirement","ECSS-Q-ST-60_0480028","The supplier shall ensure that non-hermetically sealed materials of components meet the requirements of ECSS-Q-ST-70 regarding off-gassing, out-gassing, flammability, toxicity and any other criteria specified for the intended use. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2b","Requirement","ECSS-Q-ST-60_0480029","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2c","Requirement","ECSS-Q-ST-60_0480030","With respect to health and safety, beryllium oxide (except if identified in the procurement specification), cadmium, lithium, magnesium, mercury, zinc, radioactive material and all material which may cause safety hazards shall not be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2d","Requirement","ECSS-Q-ST-60_0480031","For limited life duration, known instability, safety hazards or reliability risk reasons, EEE components listed below shall not be used:\n    1. EEE components with pure tin (less than 3% Pb in case of SnPb alloy) used as a finish on the leads, terminations and external surfaces of components and packages.\n    2. Hollow core resistors,\n    3. Potentiometers (except for mechanism position monitoring),\n    4. Non-metallurgically bonded diodes,\n    5. Semiconductor dice with unglassivated active area,\n    6. Wet slug tantalum capacitors other than capacitor construction using double seals and a tantalum case,\n    7. Any component whose internal construction uses metallurgic bonding with a melting temperature not compatible with the end-application mounting conditions,\n    8. Wire link fuses < 5A,\n    9. TO5 relays without double welding of the mechanism to the header or with any type of integrated diodes inside,",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2e","Requirement","ECSS-Q-ST-60_0480032","For limited life duration, known instability, safety hazards or reliability risk reasons, EEE components listed below shall not be used for new designs:\n    1. RNC90 > 100 kW,\n    2. TO3 and DO4/DO5 packages.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2f","Permission","ECSS-Q-ST-60_0480448","The use of pure tin in internal cavities may be authorized, on a case-by-case basis, based on the demonstration that there is no alternative product and there is no risk (supported by a technical justification).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2g","Requirement","ECSS-Q-ST-60_0480034","As per clause 4.2.2.2e, the justification of the use of pure tin shall be presented during a PCB for customer’s approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.2h","Requirement","ECSS-Q-ST-60_0480035","The use of pure tin (inside or outside the part) shall be declared in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.3a","Requirement","ECSS-Q-ST-60_0480036","Parts shall be chosen from the EPPL part I.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.3b","Requirement","ECSS-Q-ST-60_0480037","For parts not selected from the EPPL part I, the following sources shall be considered in the following order of precedence:\n    1. EPPL part II (when compatible with the project requirements)\n    2. ESCC QPL and QML, \n    3. NPSL level 1 (with disposition of the associated application notes) and level 2 or 3 (when compatible with the project requirements),\n    4. MIL QPL's and QML's.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.3c","Requirement","ECSS-Q-ST-60_0480038","Parts subject to export restrictions or regulations shall not be preferred. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4a","Requirement","ECSS-Q-ST-60_0480039","The radiation requirements for EEE components are project specific.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4b","Requirement","ECSS-Q-ST-60_0480040","The supplier who is responsible for the design of the piece of hardware shall demonstrate the compliance of its components selection with the radiation constraints of the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4c","Requirement","ECSS-Q-ST-60_0480041","For this demonstration, the supplier shall consider all types of radiation including cosmic (Heavy Ions), electromagnetic, trapped (charged particles - electrons, protons - in radiation belts) and solar (flares). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4d","Requirement","ECSS-Q-ST-60_0480042","Due consideration shall be given to the mission orbit and trajectory, the duration, the associated spatial and temporal variations of the radiation environment as well as all protective factors such as shielding. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4e","Requirement","ECSS-Q-ST-60_0480043","The supplier shall assess the actual radiation tolerance of the selected components for compliance with the radiation requirements in term of total dose, displacement damage and Single Events Effects (SEE). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4f","Requirement","ECSS-Q-ST-60_0480044","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4g","Requirement","ECSS-Q-ST-60_0480045","The supplier shall implement a Radiation Hardness Assurance Programme, documented by a plan to be approved by the customer, for radiation sensitive components, covering the collection of all relevant information and specifying the necessary actions in terms of evaluation and procurement testing, planning and control. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4h","Requirement","ECSS-Q-ST-60_0480046","The supplier shall issue an Equipment Radiation Analysis document identifying all sensitive components w.r.t. the relevant radiation effects, possibly their impact and giving an adequate engineering solution (e.g. local shielding, design solution, specific test, and RVT) for the relevant equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.4i","Requirement","ECSS-Q-ST-60_0480047","The Equipment Radiation Analysis document shall be submitted to the customer for approval.\n    ","NOTE More detailed information about the above requirements is given in ECSS-E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.5a","Requirement","ECSS-Q-ST-60_0480048","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.2.5b","Requirement","ECSS-Q-ST-60_0480049","For wire link fuses, the current derating factor shall be 50 % with an additional derating of 0,2 %/°C for an increase in the temperature of fuse body above 25 °C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1a","Requirement","ECSS-Q-ST-60_0480050","The supplier shall perform a component evaluation in absence of an approved demonstration that a component has the ability to conform to the requirements for functional performance, quality, dependability, and environmental resistance as required for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1b","Requirement","ECSS-Q-ST-60_0480051","The supplier shall plan and carry out the evaluation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1c","Requirement","ECSS-Q-ST-60_0480052","The scope and planning of the component evaluation shall be derived from the results of an assessment of the design and intended application of the component. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1d","Requirement","ECSS-Q-ST-60_0480053","An evaluation plan shall be sent to the customer for approval, and include the following elements:\n    1. Component Manufacturer Assessment,\n    2. Constructional Analysis,\n    3. Evaluation Testing,\n    4. Radiation Hardness. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1e","Requirement","ECSS-Q-ST-60_0480054","In the definition of the evaluation programme any information including pertinent reliability, analysis and test data from the manufacturer of the component and previous use in comparable applications shall be considered.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1f","Requirement","ECSS-Q-ST-60_0480055","Omission of any of these elements, or the introduction of alternative activities, shall be justified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1g","Requirement","ECSS-Q-ST-60_0480056","All tests and inspections shall be carried out on representative samples of the component type from the current production of the manufacturer selected for the component procurement for the flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1h","Requirement","ECSS-Q-ST-60_0480057","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1i","Requirement","ECSS-Q-ST-60_0480058","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.1j","Requirement","ECSS-Q-ST-60_0480059","The supplier shall summarize the evaluation results in the evaluation report and send it to the customer for approval.\n    ","NOTE For guidance for the assessment of the space environmental aspects refer to ECSS-E-ST-10-04 and ECSS-E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.2.2a","Requirement","ECSS-Q-ST-60_0480060","The supplier shall perform an evaluation against the ESCC basic specification no. 20200 and the ancillary specifications for dedicated component families and shall include, but not necessarily be limited to, a survey of:\n    1. The overall manufacturing facility and its organization and management,\n    2. The manufacturer’s system for inspection and manufacturing control including all relevant specifications, procedures, and internal documents,\n    3. The production line used for the component.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.2.2b","Requirement","ECSS-Q-ST-60_0480061","The complete manufacturer assessment, including the survey report and the associated corrective actions, shall be part of the evaluation report.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.3a","Requirement","ECSS-Q-ST-60_0480062","Constructional analysis shall be carried out on representative components. \n    ","NOTE The primary aim is to provide an early indication of a component’s constructional suitability for meeting the specified performances of the space project application.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.3b","Requirement","ECSS-Q-ST-60_0480063","The Constructional Analysis shall comprise destructive and non-destructive inspections, analyses, and testing, to identify:\n    1. Design and construction technology,\n    2. Materials used,\n    3. Inherent reliability aspects,\n    4. Quality of workmanship,\n    5. Potential hazards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.3c","Requirement","ECSS-Q-ST-60_0480064","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.4a","Requirement","ECSS-Q-ST-60_0480065","The evaluation shall determine which inspections or tests are required to provide the confidence that the component type under evaluation, when assembled and tested in accordance with the procurement specification, successfully meets the project requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.3.4b","Requirement","ECSS-Q-ST-60_0480066","The supplier shall review the already existing data in order to adapt and minimize the content of the evaluation testing while ensuring that there are inputs and pertinent results covering the following topics:\n    1. Endurance test (operating at elevated temperature and electrical stress),\n    2. Mechanical stress (shock, vibration, constant acceleration),\n    3. Environmental stress (thermal shock, temperature cycling, high and low temperature storage, humidity),\n    4. Assembly capability testing,\n    5. Radiation testing, for total dose and single event effects sensitivity.\n        ","NOTE For guidance refer to ESCC basic specification no. 22600 and the ancillary specifications for dedicated component families. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.4a","Requirement","ECSS-Q-ST-60_0480067","The supplier shall document the procedure for approval of each component type intended for use in flight products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.4b","Requirement","ECSS-Q-ST-60_0480068","The approval of components shall be based on consideration of all pertinent data including both the electrical and environmental performance as well as the established quality and the dependability assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.4c","Requirement","ECSS-Q-ST-60_0480069","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.4d","Requirement","ECSS-Q-ST-60_0480070","The approval process by the customer shall be organized as follows:\n    1. All space qualified parts by listing them in the DCL,\n    2. A PAD in conformance with Annex D is required for any other part,\n    3. A PAD in conformance with Annex D is required for space qualified parts when:\n        (a) additional controls are required (e.g. precap, buy-off, LAT or LVT, RVT, DPA),\n        (b) used outside the specified limits,\n        (c) specific tests are required during procurement as per Table 7-1,\n        (d) pure tin is used inside or outside the part.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.2.4e","Requirement","ECSS-Q-ST-60_0480071","When a PAD is required, the customer’s approval process shall include 2 steps:\n    1. step 1: approval of the part type and attached action plan, through the PAD process for the PDR.\n    2. step 2: approval of the results of the action plan defined during step 1 through the final approval of the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1a","Requirement","ECSS-Q-ST-60_0480072","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1b","Requirement","ECSS-Q-ST-60_0480073","Class 1 components shall meet the quality levels ands supplementary conditions specified in Table 7-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1c","Requirement","ECSS-Q-ST-60_0480074","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1d","Requirement","ECSS-Q-ST-60_0480075","For non qualified parts, the supplier shall put in place a configuration control system to ensure that any change of the product (e.g. mask, manufacturing and assembly process) affecting evaluation, performance, quality, reliability and interchangeability is communicated to him by the manufacturer (e.g. PCN).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1e","Requirement","ECSS-Q-ST-60_0480076","The supplier shall ensure the compatibility of the change with its application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1f","Requirement","ECSS-Q-ST-60_0480077","The change shall be submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.1g","Requirement","ECSS-Q-ST-60_0480078","To reduce the risk of procuring counterfeit components, when parts are not directly procured from the manufacturer, the supplier shall procure parts only from distributors duly franchised by the parts manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2a","Requirement","ECSS-Q-ST-60_0480079","The supplier shall procure EEE components according to controlled specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2b","Requirement","ECSS-Q-ST-60_0480080","International specifications systems, recognized as suitable for space applications (e.g. ESCC, MIL), shall be used by the supplier. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2c","Requirement","ECSS-Q-ST-60_0480081","Any new specification shall be prepared and designed by the supplier as per existing international specification systems (ESCC, MIL). Preference shall be given to ESCC format when agreed to by the manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2d","Requirement","ECSS-Q-ST-60_0480082","The content of any new specification shall be in conformance with Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2e","Requirement","ECSS-Q-ST-60_0480083","The use of any new specification shall be submitted to the customer for approval through the approval process (see clause 4.2.4) ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2f","Requirement","ECSS-Q-ST-60_0480084","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.2g","Requirement","ECSS-Q-ST-60_0480085","The supplier shall keep each procurement specification under configuration control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.3a","Requirement","ECSS-Q-ST-60_0480086","All components to be incorporated into flight standard hardware shall be subjected to screening. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.3b","Requirement","ECSS-Q-ST-60_0480087","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.3c","Requirement","ECSS-Q-ST-60_0480088","All screening tests shall be performed at the component manufacturer’s premises or at a facility approved either by the qualification approval authority, where applicable (e.g. ESCC), or otherwise by the supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.3d","Requirement","ECSS-Q-ST-60_0480089","The applicable quality levels defined in Table 7-1 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.3e","Requirement","ECSS-Q-ST-60_0480090","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.4a","Requirement","ECSS-Q-ST-60_0480091","The procurement entity shall carry out, at the manufacturer’s premises, a customer precap inspection for non-space qualified parts listed below:\n    1. Capacitors (ceramic, mica and plastic film)\n    2. Crystals\n    3. Oscillators\n    4. Discrete semiconductors (including diodes and transistors)\n    5. Filters\n    6. Fuses (cermet)\n    7. Inductors, coils (not applicable to in-house products)\n    8. Monolithic microcircuits (including MMICs)\n    9. Hybrid circuits\n    10. Relays\n    11. Resistors (high precision, fixed, metal foil - RNC90)\n    12. Switches (including mechanical and thermal)\n    13. Optoelectronic devices (e.g. opto-couplers, LEDs, CCDs and sensors).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.4b","Requirement","ECSS-Q-ST-60_0480092","The procurement entity shall carry out, at the manufacturer’s premises, a customer precap inspection on critical space qualified parts , including as a minimum relays, crystals, oscillators and hybrids.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.4c","Requirement","ECSS-Q-ST-60_0480093","When not covered by MIL or ESCC specifications, methods and accept/reject criteria for customer’s precap inspection shall be documented by a procedure to be presented to the customer, on request, for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.5a","Requirement","ECSS-Q-ST-60_0480094","The supplier shall ensure that any lot or datecode of EEE parts is submitted to a lot acceptance procedure (in line with applied normative systems) according to the following rules:\n    1. Space qualified parts: \n        (a) ESCC: user’s lot acceptance on the procured lot is not required due to periodic lot validation testing performed by the manufacturer.\n        (b) MIL: QCI or TCI performed by the manufacturer is in accordance with the quality level of the MIL specification.\n    2. Non-space qualified parts: \n        (a) The content of the lot acceptance is ESCC level LAT1 or level LAT2 or LVT (subgroups 1, 2 and 3) or comparable QCI. \n        (b) The lot acceptance may be replaced by the review of available data less than 2 years old and provided there have been no changes to the manufacturing process and no changes to the part design and construction.\n        (c) In case of partial available data, any complementary lot acceptance content is defined by the supplier within the PCB.\n        (d) The PCB documents and justifies any reduced lot acceptance based on available data for customer approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.5b","Requirement","ECSS-Q-ST-60_0480095","The sample size for lot acceptance which may be reduced in some cases, shall be submitted to the customer for approval through the approval process (see clause 4.2.4). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.6a","Requirement","ECSS-Q-ST-60_0480096","The procurement entity shall carry out, at the manufacturer’s premises, a final customer source inspection for non-space qualified parts, based on inspections, tests and review activities to verify that the requirements of the purchase order are met prior to shipment of the flight parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.6b","Requirement","ECSS-Q-ST-60_0480097","The buy-off shall include:\n    1. External visual inspection,\n    2. Witnessing electrical measurements,\n    3. Verifying mechanical dimensions,\n    4. Review and verification of the data-package.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.6c","Permission","ECSS-Q-ST-60_0480449","The buy-off may be replaced by an incoming inspection at the procurement entity's facilities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.6d","Requirement","ECSS-Q-ST-60_0480099","If the buy-off is replaced by an incoming inspection at the procurement entity's facilities, it shall be reported in the PAD submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.7a","Requirement","ECSS-Q-ST-60_0480100","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.7b","Requirement","ECSS-Q-ST-60_0480101","The incoming inspection shall include the following items:\n    1. Marking control,\n    2. Quantity verification,\n    3. Packing checking,\n    4. Review of the manufacturer delivered documentation,\n    5. Additional tests based on the type of component, criticality and heritage with the manufacturer (e.g. solderability tests, electrical tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.7c","Requirement","ECSS-Q-ST-60_0480102","The incoming inspection shall be documented by a procedure to be sent, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.7d","Requirement","ECSS-Q-ST-60_0480103","If the parts have passed successfully a final CSI (or buy-off), the incoming inspection may be reduced. The minimum shall be:\n    1. Verification of the manufacturer’s CoC\n    2. Packing checking,\n    3. Quantity verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.7e","Requirement","ECSS-Q-ST-60_0480104","In case the incoming inspection has been performed by a procurement agent, the incoming inspection performed by the end-user, may be reduced. The minimum shall be:\n    1. Packing checking,\n    2. Quantity verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.8a","Requirement","ECSS-Q-ST-60_0480105","Radiation sensitive components, as defined in clause 4.2.2.4, and for which applicable existing test data is insufficient shall be subjected to RVT.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.8b","Requirement","ECSS-Q-ST-60_0480106","RVT shall be performed in accordance with internationally recognized standards, such as ESCC Basic Specifications No. 22900 and No 25100.\n    ","NOTE Additional information on test methods is given in MIL-STD-750 Test Method 1080, MIL-STD-883 Test Method 1019 and JEDEC JESD57.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.8c","Requirement","ECSS-Q-ST-60_0480107","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 4.2.4.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.8d","Requirement","ECSS-Q-ST-60_0480108","The results of RVT shall be documented by a report. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.8e","Requirement","ECSS-Q-ST-60_0480109","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9a","Requirement","ECSS-Q-ST-60_0480110","The DPA shall be performed on 3 samples per lot for non-space qualified parts belonging to the following categories:\n    1. Capacitors (ceramic, tantalum and variable)\n    2. Crystals\n    3. Oscillators\n    4. Discrete semiconductors (including diodes and transistors)\n    5. Filters\n    6. Monolithic microcircuits (including MMICs)\n    7. Hybrid circuits\n    8. Relays\n    9. Switches (including mechanical and thermal)\n    10. Optoelectronic devices (e.g. opto-couplers, LED’s, CCD’s and sensors)\n    11. Passive microwave devices (e.g. mixers, couplers, isolators and switches)",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9b","Requirement","ECSS-Q-ST-60_0480111","The DPA shall be performed on 3 samples per lot on critical space qualified parts, including as a minimum relays and oscillators. For other space qualified parts families, DPA is not required.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9c","Requirement","ECSS-Q-ST-60_0480112","DPA may be carried out on representative samples of the components families when procured from the same manufacturer and same package without major change in the process, with a limited datecode range of 13 weeks. Such reductions shall be submitted to the customer for approval through the PAD process.\n    ","NOTE In complement of above conditions, for series of integrated circuits, series of thermal switches, series of active discrete and series of passive components (e.g. 54xxxx, 1N63xx, …), representative samples can be from the same family considering technology limit and their complexity.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9d","Requirement","ECSS-Q-ST-60_0480113","The DPA sample size may be reduced in some cases which shall be submitted to the customer for approval through the PAD process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9e","Requirement","ECSS-Q-ST-60_0480114","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9f","Requirement","ECSS-Q-ST-60_0480115","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9g","Permission","ECSS-Q-ST-60_0480450","Independent laboratories may perform DPA when approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9h","Permission","ECSS-Q-ST-60_0480451","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9i","Requirement","ECSS-Q-ST-60_0480118","For health and safety reasons, any test producing beryllium oxide dust shall be omitted.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.9j","Requirement","ECSS-Q-ST-60_0480119","The results of DPA shall be documented by a report sent to the customer, on request, for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.10a","Permission","ECSS-Q-ST-60_0480452","Components from a supplier’s or parts procurement agent’s stock may be used provided the following criteria are met:\n    1. The parts are stored according to the minimum conditions given in clause 4.4 ,\n    2. The minimum overall requirements (including screening) are in accordance with the project requirements, \n    3. The lot homogeneity and traceability can be demonstrated, \n    4. The EEE parts documentation is available and the content is acceptable in accordance with the project requirements (including radiation data, if necessary), \n    5. There are no open NCR’s and no unresolved alerts with respect to their date code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.10b","Requirement","ECSS-Q-ST-60_0480121","For components meeting the above criteria, and which have a lot / date code exceeding the period defined in ECSS-Q-ST-60-14 clause 5, the relifing procedure ECSS-Q-ST-60-14 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.11a","Requirement","ECSS-Q-ST-60_0480122","The manufacturer’s CoC shall be delivered to the parts procurer. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.11b","Requirement","ECSS-Q-ST-60_0480123","Any other data (i.e. LAT or LVT, QCI orTCI), defined in the applicable procurement documents, shall be available at the manufacturer’s facilities or delivered to the parts’ procurer in line with the purchase order. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.3.11c","Requirement","ECSS-Q-ST-60_0480124","For non qualified parts, the documentation minimum storage period shall be 10 years after delivery of components by the manufacturer. \n    ","NOTE For qualified parts, the documentation storage period is under the responsibility of the manufacturer and the qualifying authority.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.4a","Requirement","ECSS-Q-ST-60_0480125","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.4b","Requirement","ECSS-Q-ST-60_0480126","The procedures shall be applicable at any facility dealing with components for flight application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.4c","Requirement","ECSS-Q-ST-60_0480127","On request, handling and storage procedures shall be sent to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.4d","Requirement","ECSS-Q-ST-60_0480128","As a minimum, the following areas shall be covered:\n    1. Control of the environment in accordance with ESCC Basic Specification No. 24900.\n    2. Measures and facilities to segregate and protect components during receiving inspection, storage, and delivery to manufacturing. \n    3. Control measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.1a","Requirement","ECSS-Q-ST-60_0480129","The supplier shall establish and implement the requirements of this document including methods, organizations and documents used to control the selection and procurement of components in accordance with the requirements of ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.2a","Requirement","ECSS-Q-ST-60_0480130","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.2b","Requirement","ECSS-Q-ST-60_0480131","Any observed deviation of EEE components from requirements as laid down in applicable specifications, procedures and drawings shall be controlled by the nonconformance control system.\n    ","NOTE This includes failures, malfunctions, deficiencies and defects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.2c","Requirement","ECSS-Q-ST-60_0480132","The nonconformance control system shall handle all nonconformances occurring on EEE components during:\n    1. Manufacture (if available), screening and acceptance tests, \n    2. Incoming inspection,\n    3. Integration and test of equipment,\n    4. Storage and handling.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.2d","Requirement","ECSS-Q-ST-60_0480133","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.3a","Requirement","ECSS-Q-ST-60_0480134","The supplier shall take into account all received alerts from international alert systems, from manufacturers or sent by the customer and shall validate that there are no alerts on the proposed parts with respect to the batch information (including date-code). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.3b","Requirement","ECSS-Q-ST-60_0480135","If alerts become available at a later stage, the supplier shall analyse the alerts, analyse the project risk and propose an action plan for customer approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.3c","Requirement","ECSS-Q-ST-60_0480136","The supplier shall initiate and distribute within the project notifications for all major problems arising on EEE parts during procurement, incoming inspection or during all levels of equipment manufacturing or testing, which are of general concern.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.4a","Requirement","ECSS-Q-ST-60_0480137","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.4b","Requirement","ECSS-Q-ST-60_0480138","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.4c","Requirement","ECSS-Q-ST-60_0480139","In any case, the traceability requirements imposed by the supplier on the EEE parts manufacturer or distributor shall allow managing the adequacy of the tests performed by the supplier (i.e. evaluation, lot validation, any additional test or inspection). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.4d","Requirement","ECSS-Q-ST-60_0480140","The traceability of EEE parts during installation in equipment, shall be ensured by the supplier through maintaining the traceability to the manufacturer’s lot/datecode number of the EEE parts actually mounted. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.4e","Requirement","ECSS-Q-ST-60_0480141","If the as built DCL has not yet been delivered, the supplier shall be able to provide this information (part type actually installed with its relevant lot/datecode number) within one week.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.5a","Requirement","ECSS-Q-ST-60_0480142","If tests are performed by sampling, the sampled parts shall be selected so that they are representative of the lot distribution. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.5.5b","Requirement","ECSS-Q-ST-60_0480143","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.1a","Requirement","ECSS-Q-ST-60_0480144","For the specific component types identified in clauses 4.6.2, 4.6.3, 4.6.4 and 4.6.5 reference shall be made to applicable standards, in addition to the requirements of this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.2a","Requirement","ECSS-Q-ST-60_0480145","ECSS-Q-ST-60-02 shall apply for the design development.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.3a","Requirement","ECSS-Q-ST-60_0480146","ECSS-Q-ST-60-05 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4a","Requirement","ECSS-Q-ST-60_0480147","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4b","Requirement","ECSS-Q-ST-60_0480148","The PAD shall allow traceability to the information related to the procurement of blank parts, the programming process and the acceptance of the programmed parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4c","Permission","ECSS-Q-ST-60_0480453","The programming process and the acceptance of the programmed parts may be part of PCB, for customer approval, if not indicated in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4d","Requirement","ECSS-Q-ST-60_0480150","One time programmable components shall be submitted to a post-programming sequence. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4e","Requirement","ECSS-Q-ST-60_0480151","A dynamic post-programming burn-in shall be applied to FPGA’s, in conformance with ESCC9000 subclause 8.21, except for the duration, that is 160 h minimum.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4f","Requirement","ECSS-Q-ST-60_0480152","The supplier shall prepare a post-programming procedure for customer’s approval, depending on part types (including when necessary electrical tests, programming conditions and equipment, burn-in conditions, additional screening tests and specific marking after programming). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4g","Requirement","ECSS-Q-ST-60_0480153","The lot acceptance procedure, as defined in clause 4.3.5, shall be performed on devices coming from the flight lot and programmed using on the same kind of the hardware tools and compatible software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.4h","Permission","ECSS-Q-ST-60_0480454","In case of several designs based on the same lot of blank parts, the lot acceptance procedure, as defined in clause,4.3.5, may be limited to one representative flight programmed design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.6.5a","Requirement","ECSS-Q-ST-60_0480155","ECSS-Q-ST-60-12 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","4.7a","Requirement","ECSS-Q-ST-60_0480156","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.1a","Requirement","ECSS-Q-ST-60_0480157","The supplier shall establish and implement throughout the duration of the business agreement a component programme which ensures that the requirements of the project as defined by the customer and the supplier in the related business agreement are in compliance with this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.2.1a","Requirement","ECSS-Q-ST-60_0480158","The supplier shall identify the organization responsible for the management of the component programme, and describe the organization’s approaches (including the procurement system and its rationale) and capability to efficiently implement, manage, and control the component requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.2.2a","Requirement","ECSS-Q-ST-60_0480159","The supplier shall prepare a compliance matrix to the clauses of this standard. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.2.2b","Requirement","ECSS-Q-ST-60_0480160","The supplier shall submit his compliance matrix to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.3a","Requirement","ECSS-Q-ST-60_0480161","At supplier's level, the Parts Control Board (PCB) shall be chaired by a member of the supplier’s PA team with designated responsibility for components management. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.3b","Requirement","ECSS-Q-ST-60_0480162","The composition of the PCB shall as a minimum include additionally the suppliers’ parts engineer, the customer’s representative and the lower tier subcontractor parts engineers.\n    ","NOTE The approval of the selection and usage of EEE parts are implemented through Parts Control Boards (PCBs) held between the customer and the supplier (or lower tier subcontractor). ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.3c","Permission","ECSS-Q-ST-60_0480455","Other pertinent experts from the customer or suppliers may also participate, on request.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.3d","Requirement","ECSS-Q-ST-60_0480164","Depending on the progress of the program, the main PCB activities shall be:\n    1. Review and approval of the supplier's EEE component control plan and any associated documents\n    2. Parts approval including evaluation activities,\n    3. Problem assessment (e.g. alerts, nonconformances, RFD, RFW and delivery delays).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4a","Requirement","ECSS-Q-ST-60_0480165","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4b","Requirement","ECSS-Q-ST-60_0480166","This list shall be kept under configuration control (issue and identification of changes). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4c","Requirement","ECSS-Q-ST-60_0480167","The DCL shall be issued as a minimum at PDR and CDR (as designed) and at flight hardware delivery (as built).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4d","Requirement","ECSS-Q-ST-60_0480168","After equipment CDR, all modifications affecting the PAD information shall be implemented, in the \"as design\" DCL, through the CN / CR process and submitted to the customer for approval.\n    ","NOTE For PAD generation, see 5.2.4.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4e","Requirement","ECSS-Q-ST-60_0480169","The “as design” DCL shall be sent to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4f","Requirement","ECSS-Q-ST-60_0480170","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4g","Requirement","ECSS-Q-ST-60_0480171","The “as built” DCL reflecting the actual EEE parts assembled into the flight hardware and their date code, shall be provided to the customer for review at the delivery of the flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.4h","Requirement","ECSS-Q-ST-60_0480172","The content of the DCL shall be in conformance with its DRD in Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.5a","Requirement","ECSS-Q-ST-60_0480173","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.1.5b","Requirement","ECSS-Q-ST-60_0480174","Flight hardware connectors interfaces to GSE shall be protected by connector savers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.1a","Requirement","ECSS-Q-ST-60_0480175","The supplier shall ensure that the following requirements are met during his selection process:\n    1. Project requirements (e.g. quality levels, component policy, manufacturing and delivery schedules and budgets, and quantities), \n    2. Design requirements (e.g. component type, case, dimensions, and materials), \n    3. Production requirements (e.g. packaging, thermal and storage constraints, component mounting and process), \n    4. Operational requirements (e.g. electrical, mechanical, radiation, reliability, assembly, and lifetime).\n        ","NOTE The supplier of each product is responsible for the selection of components, which enable the performance, lifetime, environmental, material, safety, quality and reliability requirements of the product of which they forms a part, to be satisfied in all respects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.1a","Requirement","ECSS-Q-ST-60_0480176","The supplier shall establish and maintain in his own facility, and ensure that his suppliers also establish and maintain, procedures for selecting and controlling all components intended for use in deliverable products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.1b","Requirement","ECSS-Q-ST-60_0480177","Components shall be selected on the basis of proven qualification, characterization, and previous space experience and data, relevant with regard to the requirements for the programme, from manufacturers or sources (preferably European) employing effective Product Assurance Programmes in manufacturing and test. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.1c","Requirement","ECSS-Q-ST-60_0480178","Preference shall be given to components which necessitate the least evaluation or qualification effort. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.1d","Requirement","ECSS-Q-ST-60_0480179","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2a","Requirement","ECSS-Q-ST-60_0480180","The supplier shall ensure that non-hermetically sealed materials of components meet the requirements of ECSS-Q-ST-70 regarding off-gassing, out-gassing, flammability, toxicity and any other criteria specified for the intended use. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2b","Requirement","ECSS-Q-ST-60_0480181","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2c","Requirement","ECSS-Q-ST-60_0480182","With respect to health and safety, beryllium oxide (except if identified in the procurement specification), cadmium, lithium, magnesium, mercury, zinc, radioactive material and all material which may cause safety hazard shall not be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2d","Requirement","ECSS-Q-ST-60_0480183","For limited life duration, known instability, safety hazard or reliability risk reasons, the use of EEE components listed below shall not be used:\n    1. EEE components with pure tin (less than 3% Pb in case of SnPb alloy) used as a finish on the leads, terminations and external surfaces of components and packages. \n    2. Hollow core resistors,\n    3. Potentiometers (except for mechanism position monitoring),\n    4. Non-metallurgically bonded diodes,\n    5. Semiconductor dice with unglassivated on active area,\n    6. Wet slug tantalum capacitors other than capacitor construction using double seals and a tantalum case,\n    7. Any component whose internal construction uses metallurgic bonding with a melting temperature not compatible with the end-application mounting conditions,\n    8. Wire link fuses < 5A,\n    9. TO5 relays without double welding of the mechanism to the header or with any type of integrated diodes inside.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2e","Requirement","ECSS-Q-ST-60_0480184","For limited life duration, known instability, safety hazards or reliability risk reasons, EEE components listed below shall not be used for new designs:\n    1. RNC90 > 100 kW,\n    2. TO3 and DO4/DO5 packages.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2f","Permission","ECSS-Q-ST-60_0480456","The use of pure tin in internal cavities may be authorized, on a case-by-case basis, based on the demonstration that there is no alternative product and there is no risk (supported by a technical justification).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2g","Requirement","ECSS-Q-ST-60_0480186","As per 5.2.2.2e., the justification of the use of pure tin shall be presented during a PCB for customer’s approval,",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.2h","Requirement","ECSS-Q-ST-60_0480187","The use of pure tin (inside or outside the part) shall be declared in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3a","Requirement","ECSS-Q-ST-60_0480188","The radiation requirements for EEE components are project specific.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3b","Requirement","ECSS-Q-ST-60_0480189","The supplier who is responsible for the design of the piece of hardware shall demonstrate the compliance of its components selection with the radiation constraints of the project. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3c","Requirement","ECSS-Q-ST-60_0480190","For this demonstration, the supplier shall consider all types of radiation including cosmic (Heavy Ions), electromagnetic, trapped (charged particles - electrons, protons - in radiation belts) and solar (flares). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3d","Requirement","ECSS-Q-ST-60_0480191","Due consideration shall be given to the mission orbit and trajectory, the duration, the associated spatial and temporal variations of the radiation environment as well as all protective factors such as shielding. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3e","Requirement","ECSS-Q-ST-60_0480192","The supplier shall assess the actual radiation tolerance of the selected components for compliance with the radiation requirements in term of total dose, displacement damage and Single Events Effects (SEE). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3f","Requirement","ECSS-Q-ST-60_0480193","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3g","Requirement","ECSS-Q-ST-60_0480194","The supplier shall implement a Radiation Hardness Assurance Programme, documented by a plan to be approved by the customer, for radiation sensitive components, covering the collection of all relevant information and specifying the necessary actions in terms of evaluation and procurement testing, planning and control. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3h","Requirement","ECSS-Q-ST-60_0480195","The supplier shall issue an Equipment Radiation Analysis document identifying all sensitive components w.r.t. the relevant radiation effects, possibly their impact and giving an adequate engineering solution (e.g. local shielding, design solution, specific test, RVT) for the relevant equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.3i","Requirement","ECSS-Q-ST-60_0480196","The Equipment Radiation Analysis document shall be submitted to the customer for approval.\n    ","NOTE More detailed information about the above requirements is given in ECSS-E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.4a","Requirement","ECSS-Q-ST-60_0480197","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.2.4b","Requirement","ECSS-Q-ST-60_0480198","For wire link fuses, the current derating factor shall be 50% with an additional derating of 0,2%/°C for an increase in the temperature of fuse body above 25°C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1a","Requirement","ECSS-Q-ST-60_0480199","The supplier shall perform a component evaluation in absence of an approved demonstration that a component has the ability to conform to the requirements for functional performance, quality, dependability, and environmental resistance as required for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1b","Requirement","ECSS-Q-ST-60_0480200","The supplier shall plan and carry out the evaluation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1c","Requirement","ECSS-Q-ST-60_0480201","The scope and planning of the component evaluation actions shall be derived from the results of an assessment of the design and intended application of the component. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1d","Requirement","ECSS-Q-ST-60_0480202","An evaluation plan shall be sent to the customer for approval, and include the following elements:\n    1. Constructional Analysis,\n    2. Evaluation Testing,\n    3. Radiation Hardness. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1e","Requirement","ECSS-Q-ST-60_0480203","In the definition of the evaluation programme any information including pertinent reliability, analysis and test data from the manufacturer of the component and previous use in comparable application shall be considered.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1f","Requirement","ECSS-Q-ST-60_0480204","Omission of any of these elements, or the introduction of alternative activities, shall be justified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1g","Requirement","ECSS-Q-ST-60_0480205","All tests and inspections shall be carried out on representative samples of the component type from the current production of the manufacturer selected for the component procurement for the flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1h","Requirement","ECSS-Q-ST-60_0480206","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1i","Requirement","ECSS-Q-ST-60_0480207","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.1j","Requirement","ECSS-Q-ST-60_0480208","The supplier shall summarize the evaluation results in the evaluation report and sent it to the customer for approval.\n    ","NOTE For guidance for the assessment of the environmental aspects refer to ECSS-E-ST-10-04 and ECSS-E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.2a","Requirement","ECSS-Q-ST-60_0480209","A component manufacturer assessment is not required. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.3a","Requirement","ECSS-Q-ST-60_0480210","Constructional analysis shall be carried out on representative components. \n    ","NOTE The primary aim of constructional analysis is to provide an early indication of a component’s constructional suitability for meeting the specified performances of the space project application.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.3b","Requirement","ECSS-Q-ST-60_0480211","The Constructional Analysis shall comprise destructive and non-destructive inspections, analyses, and testing, to identify:\n    1. Design and construction technology,\n    2. Materials used,\n    3. Inherent reliability aspects,\n    4. Quality of workmanship,\n    5. Potential hazards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.3c","Requirement","ECSS-Q-ST-60_0480212","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.4a","Requirement","ECSS-Q-ST-60_0480213","The evaluation shall determine which inspections or tests are required to provide the confidence that the component type under evaluation, when assembled and tested in accordance with the procurement specification, successfully meets the project requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.3.4b","Requirement","ECSS-Q-ST-60_0480214","The supplier shall review the already existing data in order to adapt and minimize the content of the evaluation testing while ensuring that there are inputs and pertinent results covering the following topics:\n    1. Endurance test (operating at elevated temperature and electrical stress),\n    2. Mechanical stress (shock, vibration, constant acceleration),\n    3. Environmental stress (thermal shock, temperature cycling, high and low temperature storage, humidity),\n    4. Assembly capability testing,\n    5. Radiation testing, for total dose and single event effects sensitivity.\n        ","NOTE For guidance refer to ESCC basic specification no. 22600 and the ancillary specifications for dedicated component families. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.4a","Requirement","ECSS-Q-ST-60_0480215","The supplier shall document the procedure for approval of each component type intended for use in flight products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.4b","Requirement","ECSS-Q-ST-60_0480216","The approval of components shall be based on consideration of all pertinent data including both the electrical and environmental performances as well as the established quality and the dependability assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.4c","Requirement","ECSS-Q-ST-60_0480217","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.4d","Requirement","ECSS-Q-ST-60_0480218","The approval process by the customer shall be organized as follows:\n    1. All parts belonging to EPPL, NPSL or qualified according to quality levels defined in Table 7-2 are approved by listing them in the DCL,\n    2. A PAD in conformance with Annex D is required for any other part (including CECC parts),\n    3. A PAD in conformance with Annex D is also required for EPPL, NPSL or qualified parts when:\n        (a) additional controls are required (e.g. precap, buy-off, LAT or LVT, RVT, DPA),\n        (b) used outside the specified limits,\n        (c) specific tests are required during procurement as per Table 7-2,\n        (d) pure tin is used inside or outside the part.\n    4. A Justification Document is required for any commercial part, instead of PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.2.4e","Requirement","ECSS-Q-ST-60_0480219","When a PAD or a Justification Document is required, the customer’s approval process shall include 2 steps:\n    1. step 1: approval of the part type and attached action plan, through the PAD or Justification Document process for the PDR.\n    2. step 2: approval of the results of the action plan defined during step 1 through the final approval of the PAD or the Justification Document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1a","Requirement","ECSS-Q-ST-60_0480220","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1b","Requirement","ECSS-Q-ST-60_0480221","Class 2 components shall meet the quality levels and supplementary conditions specified in Table 7-2.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1c","Requirement","ECSS-Q-ST-60_0480222","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1d","Requirement","ECSS-Q-ST-60_0480223","For non qualified parts, the supplier shall put in place a configuration control system to ensure that any change of the product (e.g. mask, manufacturing and assembly process) affecting evaluation, performance, quality, reliability and interchangeability is communicated to him by the manufacturer (e.g. PCN).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1e","Requirement","ECSS-Q-ST-60_0480224","The supplier shall ensure the compatibility of the change with its application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1f","Requirement","ECSS-Q-ST-60_0480225","The change shall be submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.1g","Requirement","ECSS-Q-ST-60_0480226","To reduce the risk of procuring counterfeit components, when parts are not directly procured from the manufacturer, the supplier shall procure parts only from distributors duly franchised by the parts manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2a","Requirement","ECSS-Q-ST-60_0480227","The supplier shall procure EEE components according to controlled specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2b","Requirement","ECSS-Q-ST-60_0480228","International specifications systems, new specifications or manufacturer’s datasheets under configuration shall be used by the supplier. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2c","Requirement","ECSS-Q-ST-60_0480229","Any new specification shall be prepared and designed by the supplier as per existing international specification systems (ESCC, MIL). Preference shall be given to ESCC format when agreed to by the manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2d","Requirement","ECSS-Q-ST-60_0480230","The content of any new specification shall be in conformance with Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2e","Requirement","ECSS-Q-ST-60_0480231","The use of any new specification or datasheet shall be submitted to the customer for approval through the approval process (see clause 5.2.4).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2f","Requirement","ECSS-Q-ST-60_0480232","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.2g","Requirement","ECSS-Q-ST-60_0480233","The supplier shall keep each procurement specification or manufacturer’s datasheet under configuration control. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.3a","Requirement","ECSS-Q-ST-60_0480234","All components to be incorporated into flight standard hardware shall be subjected to screening. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.3b","Requirement","ECSS-Q-ST-60_0480235","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.3c","Requirement","ECSS-Q-ST-60_0480236","All screening tests shall be performed at the component manufacturer’s premises or at facility approved either by the qualification approval authority, where applicable (e.g. ESCC), or otherwise by the supplier..",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.3d","Requirement","ECSS-Q-ST-60_0480237","The applicable quality levels defined in Table 7-2 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.3e","Requirement","ECSS-Q-ST-60_0480238","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s review. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.4a","Requirement","ECSS-Q-ST-60_0480239","The procurement entity shall carry out, at the manufacturer’s premises, a customer precap inspection for the following non-space qualified parts types: relays, crystals, oscillators and hybrids.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.4b","Requirement","ECSS-Q-ST-60_0480240","When not covered by MIL or ESCC specifications, methods and accept/reject criteria for customer’s precap inspection shall be documented by a procedure to be presented to the customer, on request, for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.5a","Requirement","ECSS-Q-ST-60_0480241","The supplier shall ensure that any lot or datecode of EEE parts is submitted to a lot acceptance procedure (in line with applied normative systems) according to the following rules:\n    1. Space qualified parts: \n        (a) ESCC: user’s lot acceptance on the procured lot is not required due to periodic lot validation testing performed by the manufacturer.\n        (b) MIL: QCI or TCI performed by the manufacturer is in accordance with the quality level of the MIL specification.\n    2. Non-space qualified parts: \n        (a) The content of the lot acceptance is defined according to the available data. \n        (b) The proposed lot acceptance is approved through the approval process (see clause 5.2.4). \n    3. Commercial parts:\n        (a) The content of the lot acceptance is defined according to information provided by the justification document. \n        (b) The proposed lot acceptance is approved through the approval process (see clause 5.2.4). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.5b","Permission","ECSS-Q-ST-60_0480457","The sample size for lot acceptance which may be reduced in some cases is submitted to the customer for approval through the approval process (see clause 5.2.4).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.6a","Requirement","ECSS-Q-ST-60_0480243","The procurement entity shall carry out, at the manufacturer’s premises, a final customer source inspection for non-space qualified parts based on inspections, tests and review activities to verify that the requirements of the purchase order are met prior to shipment of the flight parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.6b","Requirement","ECSS-Q-ST-60_0480244","The buy-off shall include:\n    1. External visual inspection,\n    2. Witnessing electrical measurements,\n    3. Verifying mechanical dimensions,\n    4. Review and verification of the data-package.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.6c","Permission","ECSS-Q-ST-60_0480458","The buy-off may be replaced by an incoming inspection at the procurement entity's facilities; ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.6d","Requirement","ECSS-Q-ST-60_0480246","If the buy-off is replaced by an incoming inspection at the procurement entity's facilities; it shall be reported in the PAD which is submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.7a","Requirement","ECSS-Q-ST-60_0480247","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.7b","Requirement","ECSS-Q-ST-60_0480248","The incoming inspection shall include the following items:\n    1. Marking control,\n    2. Quantity verification,\n    3. Packing checking,\n    4. Review of the manufacturer delivered documentation,\n    5. Additional tests based on the type of component, criticality and heritage with the manufacturer (e.g. solderability tests, electrical tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.7c","Requirement","ECSS-Q-ST-60_0480249","The incoming inspection shall be documented by a procedure to be presented, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.7d","Requirement","ECSS-Q-ST-60_0480250","If the parts have passed successfully a final CSI (or buy-off), the incoming inspection may be reduced. The minimum shall be:\n    1. Verification of the manufacturer’s CoC,\n    2. Packing checking,\n    3. Quantity verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.7e","Requirement","ECSS-Q-ST-60_0480251","In case the incoming inspection has been performed by a procurement agent, the incoming inspection performed by the end-user, may be reduced. The minimum shall be:\n    1. Packing checking,\n    2. Quantity verification",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.8a","Requirement","ECSS-Q-ST-60_0480252","Radiation sensitive components, as defined in clause, 5.2.2.3 and for which applicable existing test data is insufficient shall be subjected to RVT.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.8b","Requirement","ECSS-Q-ST-60_0480253","RVT shall be performed in accordance with internationally recognized standards, such as ESCC Basic Specifications No. 22900 and No.25100.\n    ","NOTE Additional information on test methods is given in MIL-STD-750 Test Method 1080, MIL-STD-883 Test Method 1019 and JEDEC JESD57.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.8c","Requirement","ECSS-Q-ST-60_0480254","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 5.2.4. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.8d","Requirement","ECSS-Q-ST-60_0480255","The results of RVT shall be documented by a report. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.8e","Requirement","ECSS-Q-ST-60_0480256","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9a","Requirement","ECSS-Q-ST-60_0480257","The DPA shall be performed on 3 samples per lot for the following non-space qualified parts types: as a minimum relays, oscillators and commercial parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9b","Requirement","ECSS-Q-ST-60_0480258","DPA may be carried out on representative samples of the components families when procured from the same manufacturer and same package without major change in the process, with a limited datecode range of 13 weeks. Such reductions shall be submitted to the customer for approval through the PAD (or Justification document) process.\n    ","NOTE In complement of above conditions, for series of integrated circuits, series of thermal switches, series of active discrete and series of passive components (e.g. 54xxxx, 1N63xx, …), representative samples can be from the same family considering technology limit and their complexity.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9c","Requirement","ECSS-Q-ST-60_0480259","The DPA sample size may be reduced in some cases which shall be submitted to the customer for approval through the PAD (or Justification document) process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9d","Requirement","ECSS-Q-ST-60_0480260","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9e","Requirement","ECSS-Q-ST-60_0480261","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9f","Permission","ECSS-Q-ST-60_0480459","Independent laboratories may perform DPA when approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9g","Permission","ECSS-Q-ST-60_0480460","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9h","Requirement","ECSS-Q-ST-60_0480264","For health and safety reasons, any test producing beryllium oxide dust shall be omitted.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.9i","Requirement","ECSS-Q-ST-60_0480265","The results of DPA shall be documented by a report sent to the customer, on request, for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.10a","Permission","ECSS-Q-ST-60_0480461","Components from a supplier’s or parts procurement agent’s stock may be used provided the following criteria are met:\n    1. The parts are stored according to the minimum conditions given in clause 5.4,\n    2. The minimum overall requirements (including screening) are in accordance with the project requirements, \n    3. The lot homogeneity and traceability can be demonstrated, \n    4. The EEE parts documentation is available and the content is acceptable in accordance with the project requirements (including radiation data, if necessary), \n    5. There are no open NCR’s and no unresolved alerts with respect to their date code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.10b","Requirement","ECSS-Q-ST-60_0480267","For components meeting the above criteria, and which have a lot / date code exceeding the period defined in ECSS-Q-ST-60-14 clause 5, the relifing procedure ECSS-Q-ST-60-14 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.11a","Requirement","ECSS-Q-ST-60_0480268","The manufacturer’s CoC shall be delivered to the parts procurer. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.11b","Requirement","ECSS-Q-ST-60_0480269","Any other data (i.e. LAT or LVT, QCI or TCI), defined in the applicable procurement documents, shall be available at the manufacturer’s facilities or delivered to the parts’ procurer in line with the purchase order. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.3.11c","Requirement","ECSS-Q-ST-60_0480270","For non qualified parts, the documentation minimum storage period shall be 10 years after delivery of components by the manufacturer. \n    ","NOTE For qualified parts, the documentation storage period is under the responsibility of the manufacturer and the qualifying authority.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.4a","Requirement","ECSS-Q-ST-60_0480271","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.4b","Requirement","ECSS-Q-ST-60_0480272","The procedures shall be applicable at any facility dealing with components for flight application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.4c","Requirement","ECSS-Q-ST-60_0480273","On request, handling and storage procedures shall be sent to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.4d","Requirement","ECSS-Q-ST-60_0480274","As a minimum, the following areas shall be covered:\n    1. Control of the environment in accordance with ESCC Basic Specification No. 24900.\n    2. Measures and facilities to segregate and protect components during receiving inspection, storage, and delivery to manufacturing. \n    3. Control measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.1a","Requirement","ECSS-Q-ST-60_0480275","The supplier shall establish and implement the requirements of this document including methods, organizations and documents used to control the selection and procurement of components in accordance with the requirements of ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.2a","Requirement","ECSS-Q-ST-60_0480276","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.2b","Requirement","ECSS-Q-ST-60_0480277","Any observed deviation of EEE components from requirements as laid down in applicable specifications, procedures and drawings shall be controlled by the nonconformance control system.\n    ","NOTE This includes failures, malfunctions, deficiencies and defects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.2c","Requirement","ECSS-Q-ST-60_0480278","The nonconformance control system shall handle all nonconformances occurring on EEE components during: \n    1. Manufacture (if available), screening and acceptance tests, \n    2. Incoming inspection,\n    3. Integration and test of equipment,\n    4. Storage and handling.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.2d","Requirement","ECSS-Q-ST-60_0480279","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.3a","Requirement","ECSS-Q-ST-60_0480280","The supplier shall take into account all received alerts from international alert systems, from manufacturers or sent by the customer and shall validate that there are no alert on the proposed parts with respect to the batch information (including date-code). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.3b","Requirement","ECSS-Q-ST-60_0480281","If alerts become available at a later stage, the supplier shall analyse the alerts, analyse the project risk and propose an action plan for customer approval. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.4a","Requirement","ECSS-Q-ST-60_0480282","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.4b","Requirement","ECSS-Q-ST-60_0480283","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.4c","Requirement","ECSS-Q-ST-60_0480284","In any case, the traceability requirements imposed by the supplier on the EEE parts manufacturer or distributor shall allow managing the adequacy of the tests performed by the supplier (i.e. evaluation, lot validation, any additional test or inspection). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.4d","Requirement","ECSS-Q-ST-60_0480285","The traceability of EEE parts during installation in equipment, shall be ensured by the supplier through maintaining traceability to the manufacturer lot/datecode number of the EEE parts actually mounted. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.4e","Requirement","ECSS-Q-ST-60_0480286","If the as built DCL has not yet been delivered, the supplier shall be able to provide this information (part type actually installed with its relevant lot/datecode number) within one week. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.5.5a","Requirement","ECSS-Q-ST-60_0480287","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.1a","Requirement","ECSS-Q-ST-60_0480288","For the specific component types identified in clauses, 5.6.2, 5.6.3, 5.6.4 and 5.6.5 reference shall be made to applicable standards, in addition to the requirements of this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.2a","Requirement","ECSS-Q-ST-60_0480289","ECSS-Q-ST-60-02 shall apply for the design development. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.3a","Requirement","ECSS-Q-ST-60_0480290","ECSS-Q-ST-60-05 shall apply. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4a","Requirement","ECSS-Q-ST-60_0480291","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4b","Requirement","ECSS-Q-ST-60_0480292","The PAD shall allow traceability to the information related to the procurement of blank parts, the programming and the acceptance of the programmed parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4c","Permission","ECSS-Q-ST-60_0480462","The programming and the acceptance of the programmed parts may be part of PCB, for customer approval, if not indicated in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4d","Requirement","ECSS-Q-ST-60_0480294","One time programmable components shall be submitted to a post-programming sequence. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4e","Requirement","ECSS-Q-ST-60_0480295","A dynamic post-programming burn-in shall be applied to FPGA’s, in conformance with ESCC9000 subclause 8.21, except for the duration, that is 160 h minimum.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4f","Requirement","ECSS-Q-ST-60_0480296","The supplier shall prepare a post-programming procedure for customer’s approval, depending on part types (including when necessary electrical tests, programming conditions and equipment, burn-in conditions, additional screening tests and specific marking after programming).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4g","Requirement","ECSS-Q-ST-60_0480297","The lot acceptance procedure, as defined in clause 5.3.5, shall be performed on devices coming from the flight lot and programmed using on the same kind of hardware tools and compatible software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.4h","Permission","ECSS-Q-ST-60_0480463","In case of several designs based on the same lot of blank parts, the lot acceptance procedure, as defined in clause 5.3.5, may be limited to one representative flight programmed design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.6.5a","Requirement","ECSS-Q-ST-60_0480299","ECSS-Q-ST-60-12 shall apply. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","5.7a","Requirement","ECSS-Q-ST-60_0480300","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.1a","Requirement","ECSS-Q-ST-60_0480301","The supplier shall establish and implement throughout the duration of the business agreement a component programme which ensures that the requirements of the project as defined by the customer and the supplier in the related business agreement are in compliance with this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.2.1a","Requirement","ECSS-Q-ST-60_0480302","The supplier shall identify the organization responsible for the management of the component programme, and describe the organization’s approaches (including the procurement system and its rationale) and capability to efficiently implement, manage, and control the component requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.2.2a","Requirement","ECSS-Q-ST-60_0480303","The supplier shall prepare a compliance matrix to the clauses of this standard. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.2.2b","Requirement","ECSS-Q-ST-60_0480304","The supplier shall submit his compliance matrix to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.3a","Requirement","ECSS-Q-ST-60_0480305","A PCB is not required.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4a","Requirement","ECSS-Q-ST-60_0480306","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4b","Requirement","ECSS-Q-ST-60_0480307","The DCL shall be kept under configuration control (issue and identification of changes). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4c","Requirement","ECSS-Q-ST-60_0480308","The DCL shall be issued as a minimum at PDR and CDR (as designed) .",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4d","Requirement","ECSS-Q-ST-60_0480309","After equipment CDR, all modifications affecting the PAD information shall be implemented, in the \"as design\" DCL, through the CN / CR process and submitted to the customer for approval.\n    ","NOTE For PAD generation, see 6.2.4d.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4e","Requirement","ECSS-Q-ST-60_0480310","The “as design” DCL shall be sent to the customer for approval. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4f","Requirement","ECSS-Q-ST-60_0480311","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.4g","Requirement","ECSS-Q-ST-60_0480312","The content of the DCL shall be in conformance with the DRD in Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.5a","Requirement","ECSS-Q-ST-60_0480313","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.1.5b","Requirement","ECSS-Q-ST-60_0480314","Flight hardware connectors interfaces to GSE shall be protected by connector savers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.1a","Requirement","ECSS-Q-ST-60_0480315","The supplier shall ensure that the following requirements are met during his selection process:\n    1. Project requirements (e.g. quality levels, component policy, manufacturing and delivery schedules and budgets, quantities),\n    2. Design requirements (e.g. component type, case, dimensions, materials),\n    3. Production requirements (e.g. packaging, thermal and storage constraints, component mounting process),\n    4. Operational requirements (e.g. electrical, mechanical, radiation, reliability, assembly, lifetime).\n        ","NOTE The supplier of each product is responsible for the selection of components, which enable the performance, lifetime, environmental, material, safety, quality and reliability requirements of the product of which they form a part, to be satisfied in all respects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.1a","Requirement","ECSS-Q-ST-60_0480316","The supplier shall establish and maintain in his own facility, and ensure that his suppliers also establish and maintain, procedures for selecting and controlling all components intended for use in deliverable products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.1b","Requirement","ECSS-Q-ST-60_0480317","Components shall be selected on the basis of proven qualification, characterization, and previous space experience and data, relevant with regard to the requirements for the programme, from manufacturers or sources (preferably European) employing effective Product Assurance Programmes in manufacturing and test. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.1c","Requirement","ECSS-Q-ST-60_0480318","Preference shall be given to components which necessitate the least evaluation or qualification effort. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.1d","Requirement","ECSS-Q-ST-60_0480319","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2a","Requirement","ECSS-Q-ST-60_0480320","The supplier shall ensure that non-hermetically sealed materials of components meet the requirements of ECSS-Q-ST-70 regarding off-gassing, out-gassing, flammability, toxicity and any other criteria specified for the intended use. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2b","Requirement","ECSS-Q-ST-60_0480321","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2c","Requirement","ECSS-Q-ST-60_0480322","With respect to health and safety, beryllium oxide (except if identified in the procurement specification), cadmium, lithium, magnesium, mercury, zinc, radioactive material and all material which may cause safety hazard shall not be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2d","Requirement","ECSS-Q-ST-60_0480323","For limited life duration , known instability, safety hazard or reliability risk reasons, the use of EEE components listed below shall not be used:\n    1. EEE components with pure tin (less than 3% Pb in case of SnPb alloy) used as a finish on the leads, terminations and external surfaces of components and packages,\n    2. Hollow core resistors,\n    3. Potentiometers (except for mechanism position monitoring),\n    4. Non-metallurgically bonded diodes,\n    5. Semiconductor dice with unglassivated active area,\n    6. Wet slug tantalum capacitors other than capacitor construction using double seals and a tantalum case,\n    7. Any component whose internal construction uses metallurgic bonding with a melting temperature not compatible with the end-application mounting conditions,\n    8. Wire link fuses < 5 A,\n    9. TO5 relays without double welding of the mechanism to the header or with any type of integrated diodes inside.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2e","Requirement","ECSS-Q-ST-60_0480324","For limited life duration, known instability, safety hazard or reliability risk reasons, the use of EEE components listed below shall not be used for new designs:\n    1. RNC90 > 100 kW,\n    2. TO3 and DO4/DO5 packages.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2f","Permission","ECSS-Q-ST-60_0480464","The use of pure tin in internal cavities may be authorized, on a case-by-case basis, based on the demonstration that there is no alternative product and there is no risk (supported by a technical justification).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2g","Requirement","ECSS-Q-ST-60_0480326","As per 6.2.2.2e, the justification of the use of pure tin shall be presented during a PCB for customer’s approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.2h","Requirement","ECSS-Q-ST-60_0480327","The use of pure tin (inside or outside the part) shall be declared in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.3a","Requirement","ECSS-Q-ST-60_0480328","Reference documents for the selection of components are not prescribed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4a","Requirement","ECSS-Q-ST-60_0480329","The radiation requirements for EEE components are project specific.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4b","Requirement","ECSS-Q-ST-60_0480330","The supplier who is responsible for the design of the piece of hardware shall demonstrate the compliance of its components selection with the radiation constraints of the project. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4c","Requirement","ECSS-Q-ST-60_0480331","For this demonstration, the supplier shall consider all types of radiation including cosmic (Heavy Ions), electromagnetic, trapped (charged particles - electrons, protons - in radiation belts) and solar (flares). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4d","Requirement","ECSS-Q-ST-60_0480332","Due consideration shall be given to the mission orbit and trajectory, the duration, the associated spatial and temporal variations of the radiation environment as well as all protective factors such as shielding. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4e","Requirement","ECSS-Q-ST-60_0480333","The supplier shall assess the actual radiation tolerance of the selected components for compliance with the radiation requirements in term of total dose, displacement damage and Single Events Effects (SEE). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4f","Requirement","ECSS-Q-ST-60_0480334","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4g","Requirement","ECSS-Q-ST-60_0480335","The supplier shall implement a Radiation Hardness Assurance Programme, documented by a plan to be approved by the customer, for radiation sensitive components, covering the collection of all relevant information and specifying the necessary actions in terms of evaluation and procurement testing, planning and control. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4h","Requirement","ECSS-Q-ST-60_0480336","The supplier shall issue an Equipment Radiation Analysis document identifying all sensitive components w.r.t. the relevant radiation effects, possibly their impact and giving an adequate engineering solution (e.g. shielding, design solution, specific test, and RVT) or the relevant equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.4i","Requirement","ECSS-Q-ST-60_0480337","The Equipment Radiation Analysis document shall be submitted to the customer for approval.\n    ","NOTE More detailed information about the above requirements is given in ECSS-E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.5a","Requirement","ECSS-Q-ST-60_0480338","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.2.5b","Requirement","ECSS-Q-ST-60_0480339","For wire link fuses, the current derating factor shall be 50% with an additional derating of 0,2%/°C for an increase in the temperature of fuse body above 25°C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1a","Requirement","ECSS-Q-ST-60_0480340","The supplier shall perform a component evaluation in absence of an approved demonstration that a component has the ability to conform to the requirements for functional performance, quality, dependability, and environmental resistance as required for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1b","Requirement","ECSS-Q-ST-60_0480341","The supplier shall plan and carry out the evaluation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1c","Requirement","ECSS-Q-ST-60_0480342","The scope and planning of the component evaluation actions shall be derived from the results of an assessment of the design and intended application of the needed component. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1d","Requirement","ECSS-Q-ST-60_0480343","An evaluation plan shall be sent to the customer for approval, and include the following elements:\n    1. Constructional Analysis,\n    2. Evaluation Testing,\n    3. Radiation Hardness. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1e","Requirement","ECSS-Q-ST-60_0480344","In the definition of the evaluation programme any information including pertinent reliability, analysis and test data from the manufacturer of the component and previous use in comparable application shall be considered.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1f","Requirement","ECSS-Q-ST-60_0480345","Omission of any of these elements, or the introduction of alternative activities, shall be justified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1g","Requirement","ECSS-Q-ST-60_0480346","All tests and inspections shall be carried out on representative samples of the component type from the current production of the manufacturer selected for the component procurement for the flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1h","Requirement","ECSS-Q-ST-60_0480347","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1i","Requirement","ECSS-Q-ST-60_0480348","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1j","Requirement","ECSS-Q-ST-60_0480349","The supplier shall summarize the evaluation results in the evaluation report and sent it to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.1k","Requirement","ECSS-Q-ST-60_0480350","It shall be reviewed to determine if they will have an impact on the content of the procurement specification.\n    ","NOTE For guidance for the assessment of the environmental aspects refer to ECSS-E-ST-10-04 and ECSS E-ST-10-12.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.2a","Requirement","ECSS-Q-ST-60_0480351","A component manufacturer assessment is not required. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.3a","Requirement","ECSS-Q-ST-60_0480352","Constructional analysis shall be carried out on representative components.\n    ","NOTE The primary aim is to provide an early indication of a component’s constructional suitability for meeting the specified performances of the space project application.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.3b","Requirement","ECSS-Q-ST-60_0480353","The Constructional Analysis shall comprise destructive and non-destructive inspections, analyses, and testing, to identify:\n    1. Design and construction technology,\n    2. Materials used,\n    3. Inherent reliability aspects,\n    4. Quality of workmanship,\n    5. Potential hazards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.3c","Requirement","ECSS-Q-ST-60_0480354","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.4a","Requirement","ECSS-Q-ST-60_0480355","The evaluation shall determine which inspections or tests are required to provide the confidence that the component type under evaluation, when assembled and tested in accordance with the procurement specification, successfully meets the project requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.3.4b","Requirement","ECSS-Q-ST-60_0480356","The supplier shall review the already existing data in order to adapt and minimize the content of the evaluation testing while ensuring that there are inputs and pertinent results covering the following topics:\n    1. Endurance test (operating at elevated temperature and electrical stress),\n    2. Mechanical stress (shock, vibration, constant acceleration),\n    3. Environmental stress (thermal shock, temperature cycling, high and low temperature storage, humidity),\n    4. Assembly capability testing,\n    5. Radiation testing, for total dose and single event effects sensitivity.\n        ","NOTE For guidance refer to ESCC basic specification no. 22600 and the ancillary specifications for dedicated component families. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.4a","Requirement","ECSS-Q-ST-60_0480357","The supplier shall document the procedure for approval of each component type intended for use in flight products. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.4b","Requirement","ECSS-Q-ST-60_0480358","The approval of components shall be based on consideration of all pertinent data including both the electrical and environmental performances as well as the established quality and the dependability assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.4c","Requirement","ECSS-Q-ST-60_0480359","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.4d","Requirement","ECSS-Q-ST-60_0480360","The approval process by the customer shall be organized as follows:\n    1. All parts are approved by listing then in the DCL,\n    2. A PAD in conformance with Annex D is required for parts when:\n        (a) additional controls are required (e.g. precap, buy-off, LAT or LVT, RVT, DPA),\n        (b) used outside the specified limits,\n        (c) specific tests are required during procurement as per Table 7-3.\n        (d) pure tin is used inside or outside the part\n    3. Justification Document is required for any commercial part, instead of PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.2.4e","Requirement","ECSS-Q-ST-60_0480361","When a PAD or a Justification Document is required, the customer’s approval process shall include 2 steps:\n    1. step 1: approval of the part type and attached action plan, through the PAD or Justification Document process for the PDR.\n    2. step 2: approval of the results of the action plan defined during step 1 through the final approval of the PAD or the Justification Document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.1a","Requirement","ECSS-Q-ST-60_0480362","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.1b","Requirement","ECSS-Q-ST-60_0480363","Class 3 components shall meet the quality levels and supplementary conditions specified in Table 7-3.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.1c","Requirement","ECSS-Q-ST-60_0480364","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.1d","Requirement","ECSS-Q-ST-60_0480365","To reduce the risk of procuring counterfeit components, when parts are not directly procured from the manufacturer, the supplier shall procure parts only from distributors duly franchised by the parts manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2a","Requirement","ECSS-Q-ST-60_0480366","The supplier shall procure EEE components according to controlled specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2b","Requirement","ECSS-Q-ST-60_0480367","International specifications systems, new specifications or manufacturer’s datasheets under configuration shall be used by the supplier. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2c","Requirement","ECSS-Q-ST-60_0480368","Any new specification shall be prepared and designed by the supplier as per existing international specification systems (ESCC, MIL). Preference shall be given to ESCC format when agreed to by the manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2d","Requirement","ECSS-Q-ST-60_0480369","The content of any new specification shall be in conformance with the procurement specification DRD in Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2e","Requirement","ECSS-Q-ST-60_0480370","The use of any new specification or datasheet shall be submitted to the customer for review through the approval process (see clause 6.2.4).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2f","Requirement","ECSS-Q-ST-60_0480371","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.2g","Requirement","ECSS-Q-ST-60_0480372","The supplier shall keep each procurement specification or manufacturer’s datasheet under configuration control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.3a","Requirement","ECSS-Q-ST-60_0480373","All components to be incorporated into flight standard hardware shall be subjected to screening.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.3b","Requirement","ECSS-Q-ST-60_0480374","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.3c","Requirement","ECSS-Q-ST-60_0480375","All screening tests shall be performed at the component manufacturer’s premises or at a facility approved either by the qualification approval authority, where applicable (e.g. ESCC), or otherwise by the supplier .",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.3d","Requirement","ECSS-Q-ST-60_0480376","The applicable quality levels defined in Table 7-3 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.3e","Requirement","ECSS-Q-ST-60_0480377","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s review. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.4a","Requirement","ECSS-Q-ST-60_0480378","A customer precap is not required.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.5a","Requirement","ECSS-Q-ST-60_0480379","The supplier shall ensure that any lot or datecode of EEE parts is submitted to a lot acceptance procedure (in line with applied normative systems) according to the following rules:\n    1. Space qualified parts: \n        (a) ESCC: user’s lot acceptance on the procured lot is not required due to periodic lot validation testing performed by the manufacturer.\n        (b) MIL: QCI or TCI performed by the manufacturer is in accordance with the quality level of the MIL specification.\n    2. Non-space qualified parts: \n        (a) The content of the lot acceptance is defined according to the available data. \n        (b) The proposed lot acceptance is approved through the approval process (see clause 6.2.4).\n    3. Commercial parts:\n        (a) The content of the lot acceptance is defined according to information provided by the justification document.\n        (b) The proposed lot acceptance is approved through the approval process (see clause 6.2.4).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.5b","Requirement","ECSS-Q-ST-60_0480380","The sample size for lot acceptance which may be reduced in some cases, shall be submitted to the customer approval through the approval process (see clause 6.2.4)",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.6a","Requirement","ECSS-Q-ST-60_0480381","A buy-off is not required.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.7a","Requirement","ECSS-Q-ST-60_0480382","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.7b","Requirement","ECSS-Q-ST-60_0480383","The incoming inspection shall include the following items:\n    1. Marking control,\n    2. Quantity verification,\n    3. Packing checking,\n    4. Review of the manufacturer delivered documentation,\n    5. Additional tests based on the type of component, criticality and heritage with the manufacturer (e.g. solderability tests, electrical tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.7c","Requirement","ECSS-Q-ST-60_0480384","The incoming inspection shall be documented by a procedure to be presented, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.7d","Requirement","ECSS-Q-ST-60_0480385","If the parts have passed successfully a final CSI (or buy-off), the incoming inspection may be reduced. The minimum shall be :\n    1. Verification of the manufacturer’s CoC,\n    2. Packing checking,\n    3. Quantity verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.7e","Requirement","ECSS-Q-ST-60_0480386","In case the incoming inspection has been performed by a procurement agent, the incoming inspection performed by the end-user, may be reduced. The minimum shall be : :\n    1. Packing checking,\n    2. Quantity verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.8a","Requirement","ECSS-Q-ST-60_0480387","Radiation sensitive components, as defined in clause 6.2.2.4 and for which applicable existing test data is insufficient shall be subjected to RVT.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.8b","Requirement","ECSS-Q-ST-60_0480388","RVT shall be performed in accordance with internationally recognized standards, such as ESCC Basic Specifications No. 22900 and No.25100. \n    ","NOTE Additional information on test methods is given in MIL-STD-750 Test Method 1080, MIL-STD-883 Test Method 1019 and JEDEC JESD57.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.8c","Requirement","ECSS-Q-ST-60_0480389","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 6.2.4.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.8d","Requirement","ECSS-Q-ST-60_0480390","The results of RVT shall be documented by a report. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.8e","Requirement","ECSS-Q-ST-60_0480391","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9a","Requirement","ECSS-Q-ST-60_0480392","The DPA shall be performed on 3 samples per lot for the following non-space qualified part types, as a minimum relays and commercial parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9b","Requirement","ECSS-Q-ST-60_0480393","DPA may be carried out on representative samples of the components families when procured from the same manufacturer and same package without major change in the process, with a limited datecode range of 13 weeks. Such reductions shall be submitted to the customer for approval through the PAD (or Justification document) process.\n    ","NOTE In complement of above conditions, for series of integrated circuits, series of thermal switches, series of active discrete and series of passive components (e.g. 54xxxx, 1N63xx, …), representative samples can be from the same family considering technology limit and their complexity.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9c","Requirement","ECSS-Q-ST-60_0480394","The DPA sample size may be reduced in some cases which shall be submitted to the customer for approval through the PAD process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9d","Requirement","ECSS-Q-ST-60_0480395","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9e","Requirement","ECSS-Q-ST-60_0480396","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9f","Permission","ECSS-Q-ST-60_0480465","Independent laboratories may perform DPA when approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9g","Permission","ECSS-Q-ST-60_0480466","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9h","Requirement","ECSS-Q-ST-60_0480399","Methods and accept/reject criteria for inspection component (material, design, construction, workmanship) shall be documented by a procedure to be presented to the customer, on request, for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9i","Requirement","ECSS-Q-ST-60_0480400","For health and safety reasons, any test producing beryllium oxide dust shall be omitted.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.9j","Requirement","ECSS-Q-ST-60_0480401","The results of DPA shall be documented by a report sent to the customer, on request, for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.10a","Permission","ECSS-Q-ST-60_0480467","Components from a supplier’s or parts procurement agent’s stock may be used provided the following criteria are met:\n    1. The parts are stored according to the minimum conditions given in clause 6.4, \n    2. The minimum overall requirements (including screening) are in accordance with the project requirements, \n    3. The lot homogeneity and traceability can be demonstrated, \n    4. The EEE parts documentation is available and the content is acceptable in accordance with the project requirements (including radiation data, if necessary), \n    5. There are no open NCR’s and no unresolved alerts with respect to their date code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.10b","Requirement","ECSS-Q-ST-60_0480403","For components meeting the above criteria, and which have a lot / date code exceeding the period defined in ECSS-Q-ST-60-14 clause 5, the relifing procedure ECSS-Q-ST-60-14 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.11a","Requirement","ECSS-Q-ST-60_0480404","The manufacturer’s CoC shall be delivered to the parts procurer. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.11b","Requirement","ECSS-Q-ST-60_0480405","Any other data (i.e. LAT or LVT, QCI or TCI), defined in the applicable procurement documents, shall be available at the manufacturer’s facilities or delivered to the parts’ procurer in line with the purchase order. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.3.11c","Requirement","ECSS-Q-ST-60_0480406","For non qualified parts, the documentation minimum storage period shall be 10 years after delivery of components by the manufacturer. \n    ","NOTE For qualified parts, the documentation storage period is under the responsibility of the manufacturer and the qualifying authority.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.4a","Requirement","ECSS-Q-ST-60_0480407","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.4b","Requirement","ECSS-Q-ST-60_0480408","The procedures shall be applicable at any facility dealing with components for flight application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.4c","Requirement","ECSS-Q-ST-60_0480409","On request, these procedures shall be sent to the customer for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.4d","Requirement","ECSS-Q-ST-60_0480410","As a minimum, the following areas shall be covered:\n    1. Control of the environment in accordance with ESCC Basic Specification No. 24900.\n    2. Measures and facilities to segregate and protect components during receiving inspection, storage, and delivery to manufacturing. \n    3. Control measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.1a","Requirement","ECSS-Q-ST-60_0480411","The supplier shall establish and implement the requirements of this document including methods, organizations and documents used to control the selection and procurement of components in accordance with the requirements of ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.2a","Requirement","ECSS-Q-ST-60_0480412","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.2b","Requirement","ECSS-Q-ST-60_0480413","Any observed deviation of EEE components from requirements as laid down in applicable specifications, procedures and drawings shall be controlled by the nonconformance control system.\n    ","NOTE This includes failures, malfunctions, deficiencies and defects.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.2c","Requirement","ECSS-Q-ST-60_0480414","The nonconformance control system shall handle all nonconformances occurring on EEE components during: \n    1. Manufacture (if available), screening and acceptance tests, \n    2. Incoming inspection,\n    3. Integration and test of equipment,\n    4. Storage and handling.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.2d","Requirement","ECSS-Q-ST-60_0480415","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.3a","Requirement","ECSS-Q-ST-60_0480416","The supplier shall take into account all received alerts from international alert systems, from manufacturers or sent by the customer and shall validate that there are no alerts on the proposed parts with respect to the batch information (including date-code). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.3b","Requirement","ECSS-Q-ST-60_0480417","If alerts become available at a later stage, the supplier shall analyse the alerts, analyse the project risk and propose an action plan for customer approval. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.4a","Requirement","ECSS-Q-ST-60_0480418","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.4b","Requirement","ECSS-Q-ST-60_0480419","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.4c","Requirement","ECSS-Q-ST-60_0480420","In any case, the traceability requirements imposed by the supplier on the EEE parts manufacturer or distributor shall allow managing the adequacy of the tests performed by the supplier (i.e. evaluation, lot validation, any additional test or inspection). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.4d","Requirement","ECSS-Q-ST-60_0480421","The traceability of EEE parts during installation in equipment, shall be ensured by the supplier through maintaining the traceability to the manufacturer’s lot/datecode number of the EEE parts actually mounted. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.4e","Requirement","ECSS-Q-ST-60_0480422","The supplier shall be able to provide these information (part type actually installed with its relevant lot/datecode number) within one working day (when the flight system is on launch pad) or within one week (in the other cases).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.5.5a","Requirement","ECSS-Q-ST-60_0480423","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.1a","Requirement","ECSS-Q-ST-60_0480424","For the specific component types identified in clauses 6.6.2, 6.6.3, 6.6.4, and 6.6.5 reference shall be made to applicable standards, in addition to the requirements of this standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.2a","Requirement","ECSS-Q-ST-60_0480425","ECSS-Q-60-02 shall apply for the design development.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.3a","Requirement","ECSS-Q-ST-60_0480426","ECSS-Q-ST-60-05 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4a","Requirement","ECSS-Q-ST-60_0480427","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4b","Requirement","ECSS-Q-ST-60_0480428","The PAD shall allow traceability to the information related to the procurement of blank parts, the programming and the acceptance of the programmed parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4c","Permission","ECSS-Q-ST-60_0480468","The programming and the acceptance of the programmed parts may be part of a separate document, for customer approval, if not indicated in the PAD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4d","Requirement","ECSS-Q-ST-60_0480430","One time programmable components shall be submitted to a post-programming sequence. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4e","Requirement","ECSS-Q-ST-60_0480431","A dynamic post-programming burn-in shall be applied to FPGA’s, in conformance with ESCC9000 subclause 8.21, except for the duration, that is 160 h minimum.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4f","Requirement","ECSS-Q-ST-60_0480432","The supplier shall prepare a post-programming procedure for customer’s approval, depending on part types (including when necessary electrical tests, programming conditions and equipment, burn-in conditions, additional screening tests and specific marking after programming).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4g","Requirement","ECSS-Q-ST-60_0480433","The lot acceptance procedure, as defined in clause 6.3.5, shall be performed on devices coming from the flight lot and programmed using on the same kind of hardware tools and compatible software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.4h","Permission","ECSS-Q-ST-60_0480469","In case of several designs based on the same lot of blank parts, the lot acceptance procedure, as defined in clause 6.3.5, may be limited to one representative flight programmed design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.6.5a","Requirement","ECSS-Q-ST-60_0480435","ECSS-Q-ST-60-12 shall apply. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","6.7a","Requirement","ECSS-Q-ST-60_0480436","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","A.2.1a","Requirement","ECSS-Q-ST-60_0480437","The CCP shall include or refer to the following information:\n    1. A description of the purpose, content and the reason prompting its preparation,\n    2. A list of the applicable and reference documents,\n    3. Any additional terms, definitions and abbreviations,\n    4. The organizational breakdown structure, responsibility descriptions, management approach and concurrent engineering,\n    5. Control of lower level suppliers, procurement agents (if any) and manufacturers,\n    6. Procurement system,\n    7. Radiation control programme,\n    8. Component selection and standardization,\n    9. Component data acquisition and assessment,\n    10. Component evaluation and related testing approach,\n    11. Component approval,\n    12. Component testing, inspection and storage,\n    13. Component quality assurance activities,\n    14. Assessment of problem notifications and alerts,\n    15. Programme planning with schedule of tasks linked to programme milestones,\n    16. Specific components control and back-up plans whenever there is evidence of possible schedule, quality or technical problems,\n    17. Reporting and deliverables, \n    18. Compliance matrix to the clauses of this standard. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","A.2.2a","Permission","ECSS-Q-ST-60_0480470","In conformance with 4.2.2.1b the CCP may be part of the overall project PA plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","B.2.1a","Requirement","ECSS-Q-ST-60_0480439","The DCL shall include or refer to the following information:\n    1. A description of the purpose, content and the reason prompting its preparation, \n    2. A list of the applicable and reference documents,\n    3. Any additional terms, definitions or abbreviations,\n    4. Component number (commercial equivalent designation),\n    5. Family (ESCC group code),\n    6. Package,\n    7. Value or range of values with tolerance for non qualified parts,\n    8. Component manufacturer (name, country),\n    9. Generic procurement specification, \n    10. Detail procurement specification (with issue and revision for non qualified parts),\n    11. Specification amendment (including issue and revision),\n    12. Name of the procurement agent (CPPA, supplier, distributor),\n    13. Quality level and lot test (ESCC LAT or LVT, MIL TCI or QCI or CI),\n    14. Space qualified status (yes or no),\n    15. RVT (yes or no),\n    16. Reference of the PAD or Justification Document, where required,\n    17. Approval status of the part,\n    18. Change identification between each DCL issue,\n    19. Date-code (only for “as built” DCL).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","C.2.1a","Requirement","ECSS-Q-ST-60_0480440","The procurement specification shall include or refer to the following information:\n    1. A description of the purpose, content and the reason prompting its preparation, \n    2. A list of the applicable and reference documents,\n    3. Any additional terms, definitions or abbreviations,\n    4. Absolute maximum ratings,\n    5. Electrical and mechanical parameters and limits,\n    6. Screening, burn-in, and acceptance requirements,\n    7. Package material and lead finish,\n    8. Documentation/data requirements,\n    9. Delta limits when applicable,\n    10. Criteria for percent defective allowable,\n    11. LAT or LVT, QCI or TCI,\n    12. Marking,\n    13. Storage requirements,\n    14. Requirements for lot homogeneity,\n    15. Serialization (when applicable),\n    16. Protective packaging and handling requirements,\n    17. Radiation Verification Testing requirements, when applicable.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 1","D.2a","Requirement","ECSS-Q-ST-60_0480441","The information given in Table D-1 shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.1a","Requirement","ECSS-Q-ST-20_0380001","The supplier shall prepare, maintain and implement a QA plan in conformance with the DRD in Annex A.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.1b","Requirement","ECSS-Q-ST-20_0380002","The QA plan shall be submitted to the customer for approval.\n    NOTE Information on the schedule for delivery of the QA plan is given in Annex I.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.2a","Requirement","ECSS-Q-ST-20_0380003","The supplier shall establish a documented training programme for the personnel whose performance determines or affects product quality.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.2b","Requirement","ECSS-Q-ST-20_0380004","Personnel performing special processes shall be trained and certified by internal or external training programmes.\n    NOTE The term “special process” is defined in ECSS-S-ST-00-01, Note 3 of the definition of “process”.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.2c","Requirement","ECSS-Q-ST-20_0380005","Personnel inspecting or controlling special processes, or performing non-destructive testing and evaluation, shall be trained and certified according to training programmes and standards accepted by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.1.2d","Requirement","ECSS-Q-ST-20_0380006","The supplier shall maintain records of the training.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.1a","Requirement","ECSS-Q-ST-20_0380007","The supplier shall implement Critical-items control in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.2a","Requirement","ECSS-Q-ST-20_0380008","The supplier shall implement a nonconformance control system in conformance with ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.3a","Requirement","ECSS-Q-ST-20_0380009","The supplier shall manage alerts in conformance with ECSS-Q-ST-10, clause 5.2.9.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4a","Requirement","ECSS-Q-ST-20_0380010","The supplier shall establish and maintain a documented stamp control system to ensure the correct and legitimate use of all fabrication and inspection stamps.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4b","Requirement","ECSS-Q-ST-20_0380011","Stamps shall be used to:\n    1. signify the completion of operations and processes, and\n    2. indicate inspection performance at source and incoming inspection, in process inspection and tests, final inspection, end point testing, storage and shipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4c","Requirement","ECSS-Q-ST-20_0380012","The use of stamps shall be restricted to authorized personnel as identified in the stamp control system.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4d","Requirement","ECSS-Q-ST-20_0380013","Stamps shall be traceable to individuals responsible for their use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4e","Requirement","ECSS-Q-ST-20_0380014","Stamps shall be applied directly to parts and materials, when specified by engineering drawings and specifications, and associated documents, records, labels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4f","Requirement","ECSS-Q-ST-20_0380015","Stamping materials and methods shall be compatible with the articles and their use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.4g","Permission","ECSS-Q-ST-20_0380225","Signatures instead of stamps may be used provided that similar traceability and responsibility records are maintained and available.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.5a","Requirement","ECSS-Q-ST-20_0380017","The supplier shall ensure that a bidirectional and unequivocal relationship between parts, materials or products and associated documentation or records is established and maintained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.5b","Requirement","ECSS-Q-ST-20_0380018","The supplier shall be capable to trace data, personnel and equipment related to procurement, manufacturing, inspection, test, assembly, integration and operations activities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.5c","Requirement","ECSS-Q-ST-20_0380019","The supplier shall be capable to trace backward the locations of materials, parts, sub-assemblies.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.5d","Requirement","ECSS-Q-ST-20_0380020","The supplier shall be capable to trace forward the locations of materials from raw stock.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.5e","Requirement","ECSS-Q-ST-20_0380021","The supplier shall establish controls to ensure that:\n    1. identification numbers are assigned in a systematic and consecutive manner,\n    2. identification numbers of scrapped or destroyed items are not used again,\n    3. identification numbers, once allocated, are not changed, unless the change is authorized by the customer.\n        NOTE Requirements for identification are addressed in ECSS-M-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6a","Requirement","ECSS-Q-ST-20_0380022","The supplier shall control, calibrate and maintain inspection, measuring and test equipment, whether owned by the supplier, on loan, or provided by the customer to demonstrate the conformance of product to the specified requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6b","Requirement","ECSS-Q-ST-20_0380023","The supplier shall use equipment in a manner which ensures that measurement uncertainty is known and is consistent with the specified measurement capability.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6c","Requirement","ECSS-Q-ST-20_0380024","The supplier shall include in the calculations of all measurements the total error in the measurement process attributable to the cumulative error from the calibration chain, measuring equipment and those contributed by personnel, procedures and the environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6d","Requirement","ECSS-Q-ST-20_0380025","The supplier shall record the basis for the calculation of the cumulative errors as specified in requirement 5.2.6c.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6e","Requirement","ECSS-Q-ST-20_0380026","The supplier shall select inspection, measuring and test equipment in conformance with the required measurement accuracy and precision.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6f","Requirement","ECSS-Q-ST-20_0380027","The supplier shall identify, calibrate and adjust all inspection, measuring and test equipment and devices that can affect product quality at prescribed intervals, or prior to use, against certified equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6g","Requirement","ECSS-Q-ST-20_0380028","The supplier shall establish, document and maintain calibration procedures, including details of equipment type, identification number, location, frequency of checks, check method, acceptance criteria and the action to be taken when results exceed the specified accuracy.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6h","Requirement","ECSS-Q-ST-20_0380029","The supplier shall ensure that the inspection, measuring and test equipment is capable of the specified accuracy and precision.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6i","Requirement","ECSS-Q-ST-20_0380030","The supplier shall identify inspection, measuring and test equipment with a suitable indicator or approved identification record to show the calibration status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6j","Requirement","ECSS-Q-ST-20_0380031","The supplier shall maintain calibration records for inspection, measuring and test equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6k","Requirement","ECSS-Q-ST-20_0380032","The supplier shall assess and document the validity of previous inspection and test results when inspection, measuring or test equipment is found to be out of calibration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6l","Requirement","ECSS-Q-ST-20_0380033","The supplier shall ensure that the environmental conditions are suitable for the calibrations, inspections, measurements and tests being carried out.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6m","Requirement","ECSS-Q-ST-20_0380034","The supplier shall ensure that inspection, measuring and test facilities, including both test hardware and test software are protected against adjustments, which can invalidate the calibration setting.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6n","Requirement","ECSS-Q-ST-20_0380035","The supplier shall ensure that the inspection, measuring and test equipment is handled, preserved and stored such that the accuracy and fitness for use is maintained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6o","Requirement","ECSS-Q-ST-20_0380036","The supplier shall check the test hardware or test software used for inspection to prove that it is capable of verifying the acceptability of the product prior to release for use during production and installation, and recheck it at specified intervals. \n    NOTE 1 Examples of test hardware are: jigs, fixtures, templates and patterns. \n    NOTE 2 Test aids such as test leads, break-out boxes, mains leads and similar items are not subject to the entire set of requirements defined in this clause, but are validated in a way appropriate to their usage.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6p","Requirement","ECSS-Q-ST-20_0380037","The supplier shall establish the extent and frequency of such checks and shall maintain records as evidence of control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.6q","Requirement","ECSS-Q-ST-20_0380038","The supplier shall make the measurement design data available to the customer upon request.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.1a","Requirement","ECSS-Q-ST-20_0380039","The supplier shall prevent handling damage during all phases of manufacturing, assembly, integration, testing, storage, transportation and operation.\n    NOTE Possible prevention measures are:\n\ta. protection of items during handling,\n\tb. handling devices, or\n\tc. procedures and instructions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.2a","Requirement","ECSS-Q-ST-20_0380040","The supplier shall place the following items in secure storage areas:\n    1. incoming materials,\n    2. intermediate items needing temporary storage, and\n    3. end items before shipping.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.2b","Requirement","ECSS-Q-ST-20_0380041","The supplier shall place the following items in designated segregated areas:\n    1. limited life materials,\n    2. suspended limited life materials,\n    3. nonconforming items awaiting NRB disposition,\n    4. scraped items,\n    5. items designated to be stored separately for health or safety reasons.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.2c","Requirement","ECSS-Q-ST-20_0380042","Each segregated area shall be identified and labelled for its intended use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.2d","Requirement","ECSS-Q-ST-20_0380043","The supplier shall maintain control over acceptance into and withdrawal from storage areas.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.2e","Requirement","ECSS-Q-ST-20_0380044","The supplier shall maintain records to ensure that all stored items are within the usable life limits, controlled and retested, and to provide traceability within the storage or segregated area.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.7.3a","Requirement","ECSS-Q-ST-20_0380045","The supplier shall ensure that items subject to deterioration, corrosion or contamination through exposure to any environmental elements are preserved by methods that ensure maximum protection consistent with life and usage.\n    NOTE Examples of such environmental elements are: air and moisture.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.8.1a","Requirement","ECSS-Q-ST-20_0380046","Statistical quality control and analysis methods shall be used to maintain or improve the specified control of quality, when statistically significant with respect to the product characteristics and to quantities produced.\n    NOTE Examples of statistical quality control and analysis methods are sample inspection plans, determination of quality levels, statistical process control and process capabilities studies.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.8.1b","Requirement","ECSS-Q-ST-20_0380047","When employing statistical quality control and analysis methods, the supplier shall ensure that all the conditions for use are enforced.\n    NOTE Example of such conditions are sample significance, recording and elaboration of data, and formulation of clear decision rules.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.8.1c","Requirement","ECSS-Q-ST-20_0380048","Statistical quality control applications, when used by the supplier for acceptance of materials, parts, processes and products, shall be submitted to the customer for approval. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.8.2a","Requirement","ECSS-Q-ST-20_0380049","When sampling plans are used the supplier shall define and justify the following:\n    1. sample size, sample selection methods and criteria for inspection severity, \n    2. acceptance / rejection criteria, and \n    3. screening of rejected lots.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.2.8.2b","Requirement","ECSS-Q-ST-20_0380050","The supplier shall maintain records of the sampling tests, together with the identification of the characteristics to which sampling is applied.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.1.1a","Requirement","ECSS-Q-ST-20_0380051","The supplier shall ensure that the product is designed such that it can be produced with the specified level of quality.\n    NOTE Produceability includes provisions for the following aspects:\n\t· Design simplification and standardization, reduction in part types and part number.\n\t· Guidelines for selection of preferred parts, materials and processes.\n\t· Unambiguous definitions of the requirements and limits to be used.\n\t· Definition of tolerance build-up methods, in order to simplify manufacturing, assembly, inspection.\n\t· Standardization of interfaces.\n\t· Part accessibility for assembly and inspection.\n\t· Definition of design criteria consistent with the capability of manufacturing processes.\n\t· Definition of design methods to ensure that the cleanliness requirements are compatible with the capability of related cleanliness procedures and facilities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.1.2a","Requirement","ECSS-Q-ST-20_0380052","The supplier shall ensure that the product is designed such that its performances and characteristics can be reproduced over different models and serial production.\n    NOTE Repeatability includes provisions for the following aspects:\n\t• Definition of standard tolerances generally applicable.\n\t• Recommended design concepts and solutions to ensure repeatability.\n\t• Recommended manufacturing processes having proven repeatability.\n\t• Design criteria that optimize implementation of automated manufacturing methods, or computer-aided manufacturing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.1.3a","Requirement","ECSS-Q-ST-20_0380053","The supplier shall ensure that the product is designed such that it can be inspected and tested under representative conditions, for production, AIV and operational environment.\n    NOTE Inspectability and testability include provisions for the following aspects:\n\t• Definition of inspection and test requirements, including acceptance or rejection criteria, expressed in an unambiguous and quantified manner.\n\t• Part and component accessibility for inspection and test.\n\t• Definition of tolerance methods for dimensional inspection performance (e.g. functional tolerances).\n\t• Definition of recommended design techniques to facilitate fault detection, identification and location (e.g. test points, modularity, built-in test software, and feedback loops).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.1.4a","Requirement","ECSS-Q-ST-20_0380054","The supplier shall ensure that the product is designed such that it can be operated in accordance with programme constraints and requirements, throughout its whole life cycle including handling, storage, transportation, integration and operations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.1a","Requirement","ECSS-Q-ST-20_0380055","The supplier shall ensure that requirement verification is performed progressively, as each stage of the project is completed, and provides the organized base of data upon which qualification and acceptance is incrementally declared.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.1b","Requirement","ECSS-Q-ST-20_0380056","The supplier shall ensure that top-down requirement allocations and bottom-up requirement verifications are complete and consistent.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.1c","Requirement","ECSS-Q-ST-20_0380057","The supplier shall ensure that a system for tracking requirements and verification of results is established and maintained during the whole project life cycle.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.1d","Requirement","ECSS-Q-ST-20_0380058","The supplier shall ensure that verification methods are adequate and consistent with the type and criticality of the requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.1e","Requirement","ECSS-Q-ST-20_0380059","The supplier shall ensure that appropriate reference to the verification documentation is recorded and status updated at project reviews up to final acceptance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.2a","Requirement","ECSS-Q-ST-20_0380060","The supplier shall ensure that the objectives of the analysis are defined in relation with the development logic defined in the verification plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.2b","Requirement","ECSS-Q-ST-20_0380061","The following items shall be identified:\n    1. reference of the configuration item definition under analysis;\n    2. environmental constraints considered in the analysis;\n    3. basic assumptions, analysis methods, mathematical models.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.3a","Requirement","ECSS-Q-ST-20_0380062","The supplier shall ensure that design reviews are conducted in accordance with project requirements and written procedures.\n    NOTE Design reviews address the following items:\n\t• Quality requirements and criteria for design, produceability, repeatability, testability and operability are adequately considered in design documentation.\n\t• Methods and data required for procurement, manufacturing, inspection and test are available and validated.\n\t• Risks of not achieving requirements are highlighted and adequately controlled.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.1a","Requirement","ECSS-Q-ST-20_0380063","The supplier shall ensure that all configuration items and their constituent items, either off-the-shelf or specifically designed, are properly qualified with margins commensurate with the application and use environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.1b","Requirement","ECSS-Q-ST-20_0380064","The supplier QA shall review and approve the qualification plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.1c","Requirement","ECSS-Q-ST-20_0380065","The supplier QA shall review and approve the qualification results.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.2a","Requirement","ECSS-Q-ST-20_0380066","Qualification by similarity with an identical or similar product shall be justified by providing evidence that the new application is within the limits of the previously qualified design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.2b","Requirement","ECSS-Q-ST-20_0380067","Any difference in definition with respect to the reference product and any difference in the required qualification tests shall be identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.2c","Requirement","ECSS-Q-ST-20_0380068","The need for complementary qualification tests shall be analysed and the decision justified and submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.2d","Requirement","ECSS-Q-ST-20_0380069","For this purpose the supplier shall:\n    1. evaluate the as-designed or as-built configuration and related nonconformances,\n    2. ensure that qualification requirements and qualification ranges are compatible with project requirements,\n    3. ensure that qualification test results meet the requirements and any nonconformances are available for evaluation, and\n    4. ensure that a logbook of the selected model is available for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.3a","Requirement","ECSS-Q-ST-20_0380070","The product used for qualification testing shall be produced in accordance with a full and clearly identified manufacturing and inspection file. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.3b","Requirement","ECSS-Q-ST-20_0380071","To obtain authorization to initiate qualification tests the supplier shall demonstrate that:\n    1. the qualification model is fully representative of the flight model and any differences have been analysed to evaluate their effect on the qualification status;\n    2. inspection and test requirements are expressed in an unambiguous and quantified manner including:\n        (a) test sequence;\n        (b) test conditions;\n        (c) test standards, if any;\n        (d) applicable test levels, durations and tolerances;\n        (e) accuracy in measurement.\n    3. the qualification test procedures and facilities are defined, available and conforming to requirements of clause 5.6.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.4a","Requirement","ECSS-Q-ST-20_0380072","The supplier shall report the qualification status in conformance with the “Qualification status list” DRD as defined in ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.4.5a","Requirement","ECSS-Q-ST-20_0380073","Once the design is qualified, the supplier shall assess all subsequent changes, deviations and anomalies for their impact on the qualification status and shall perform requalification as necessary.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.3.2.5a","Requirement","ECSS-Q-ST-20_0380074","The supplier shall ensure that all design changes and modifications are identified, documented, reviewed and approved before their implementation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.1.1a","Requirement","ECSS-Q-ST-20_0380075","The supplier QA shall participate in the approval and the selection of procurement sources.\n    NOTE The selection of procurement sources for EEE components is defined in ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.1.2a","Requirement","ECSS-Q-ST-20_0380076","The supplier shall select its suppliers on the basis of one of the following criteria:\n    1. The supplier has been certified by the final customer, and has a current approval to furnish items or services of the type and quality level being procured.\n        NOTE Third party certification (for instance against ISO 9001) can be also considered.\n    2. The supplier is furnishing, or has furnished within the past two years, items or services of the type and quality level being procured under other contracts with the final customer.\n    3. The supplier has demonstrated continuous capability to furnish items or services of the type and quality level being procured, supported by objective documentation.\n        NOTE This criterion does not apply if the supplier has not furnished items or services of the type being procured for more than two years.\n    4. Supplier’s capability of satisfying business agreement requirements is demonstrated by a pre-award audit by the relevant customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.1.2b","Requirement","ECSS-Q-ST-20_0380077","The supplier shall document and maintain on file results of supplier selection process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.1.3a","Requirement","ECSS-Q-ST-20_0380078","The supplier shall establish and maintain records of all procurement sources involved in business agreement performance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.1.3b","Requirement","ECSS-Q-ST-20_0380079","The supplier shall submit to the customer, upon request, the list of procurement sources, including all the information in the records 5.4.1.3a, for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.2a","Requirement","ECSS-Q-ST-20_0380080","The supplier shall ensure that supplies are identified and that all applicable requirements are defined in the procurement documents.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.2b","Requirement","ECSS-Q-ST-20_0380081","The supplier shall ensure that requirements to those contained in lower tier procurement documents are traceable.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.2c","Requirement","ECSS-Q-ST-20_0380082","The procurement documents shall contain, by statement or reference:\n    1. comprehensive technical descriptions of the items and services to be procured,\n    2. details of the applicable requirements, such as requirements for preservation, packaging, marking, shipping, accompanying documentation and provisions for limited-life items,\n    3. details of QA activities to be performed, such as inspection and test characteristics, records and reports,\n    4. details of supplier’s QA activities at source, and\n    5. special acceptance conditions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.2d","Requirement","ECSS-Q-ST-20_0380083","The supplier’s quality assurance organization shall review procurement documents prior to release, to verify the correct selection of procurement sources and appropriateness of their content.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.3a","Requirement","ECSS-Q-ST-20_0380084","The supplier shall exercise surveillance over all the activities carried out by lower level suppliers during business agreement performance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.3b","Requirement","ECSS-Q-ST-20_0380085","The surveillance programme shall include audits, reviews, mandatory inspection points, as well as direct supervision by supplier’s resident personnel at his suppliers’ facilities and source inspection.\n    NOTE Example of review is the manufacturing readiness review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.3c","Requirement","ECSS-Q-ST-20_0380086","The supplier shall select among the following criteria to define the type and extent of surveillance:\n    1. Testing or inspections cannot be accomplished by the supplier.\n        NOTE For example, environments or test equipment not available at supplier’s facility.\n    2. Verification tests are destructive in nature and the quality cannot be verified solely by inspection or test at supplier’s facility.\n    3. Supplies are designated for direct shipment from source to a customer site or the using site.\n    4. Manufacturing and AIV of complex equipment or subsystems.\n        NOTE For example, payloads.\n    5. Past performance or quality history of the lower level supplier is marginal.\n    6. Functional criticality and technical complexity of the supplies.\n    7. The degree of responsibility placed on the procurement source.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.3d","Requirement","ECSS-Q-ST-20_0380087","The supplier shall ensure that each of his suppliers implements surveillance on their lower level suppliers, in accordance with the same criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.3e","Permission","ECSS-Q-ST-20_0380226","Surveillance may be delegated by the customer to third parties.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.1a","Requirement","ECSS-Q-ST-20_0380089","The supplier shall ensure that all incoming supplies, including documentation and packaging, whether delivered on his own premises or elsewhere, conform to the requirements of the procurement documents.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.1b","Requirement","ECSS-Q-ST-20_0380090","The supplier shall perform inspections in accordance with established procedures and instructions, to ensure that quality level is properly determined. \n    NOTE 1 Sampling plans in receiving inspection are defined in 5.2.8.2\n    NOTE 2 Receiving inspection of components is defined in ECSS-Q-ST-60.\n    NOTE 3 Lot or batch acceptance of materials and mechanical parts is defined in ECSS-Q-ST-70.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.1c","Requirement","ECSS-Q-ST-20_0380091","Receiving inspectors shall have available the procurement documents, specifications, drawings and any other document relevant to incoming supplies as required in the procurement documents.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.2a","Requirement","ECSS-Q-ST-20_0380092","Receiving inspection activities shall include:\n    1. verification of the packaging conditions and of the status of environmental sensors,\n    2. visual inspection of the delivered items,\n    3. verification of correct identification and, where appropriate, configuration identification for conformance to the ordering data,\n    4. verification of the evidence of inspection and tests performed by the supplier and associated documentation,\n    5. verification of the performance of supplier’s source inspection, when required,\n    6. performance of inspections and tests on selected characteristics of incoming supplies or test specimens submitted with the supplies,\n    7. identification of the shelf life of limited-life items,\n    8. identification of the inspection status and physical separation of the supplies in the receiving inspection area according to the following categories:\n        (a) items for which the receiving inspection has not been completed;\n        (b) conforming items;\n        (c) nonconforming items.\n    9. prevention of unauthorized use of uninspected items,\n    10. identification of the items to be released for production with conformance status and traceability data to be recorded in manufacturing documents,\n    11. maintenance of receiving inspection records in conformance with 5.4.4.4.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.3a","Requirement","ECSS-Q-ST-20_0380093","Receiving inspection of items supplied by the customer shall consist of the verification of identity and integrity after transportation.\n    NOTE Additional inspections and tests, if any, are specified in the business agreement.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.4.4.4a","Requirement","ECSS-Q-ST-20_0380094","The supplier shall maintain receiving inspection records to ensure traceability and the availability of historical data to monitor supplier performance and quality trends.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1a","Requirement","ECSS-Q-ST-20_0380095","The supplier shall document the planning of manufacturing, assembly and integration operations and inspections in the manufacturing plan or flow chart for the product, including the sequence of operations and associated inspections and tests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1b","Requirement","ECSS-Q-ST-20_0380096","The planning shall include the identification of MIPs in conformance with 5.5.8, together with the reference to the procedures by which the various activities are performed and the required cleanliness levels and temperature and humidity requirements of the facilities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1c","Requirement","ECSS-Q-ST-20_0380097","Instructions shall direct the actual performance of manufacturing, assembly and integration operations and inspections, to ensure that the activities proceed in an orderly manner and according to the planned sequence.\n    NOTE For example: shop travellers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1d","Requirement","ECSS-Q-ST-20_0380098","The supplier shall issue and maintain manufacturing, assembly and integration documents in accordance with established and formal procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1e","Requirement","ECSS-Q-ST-20_0380099","The QA organization shall review and approve such documents, and any modifications thereof, to ensure that they include or refer to:\n    1. Identification of the item to be manufactured or equipment to be used.\n    2. Configuration data, including parts lists, drawings, changes and specifications.\n    3. Identification of the production and inspection equipment to be used for the manufacturing, assembly and integration of the item.\n        NOTE Examples of production and inspection equipment are tools, jigs and fixtures.\n    4. Identification of critical characteristics.\n        NOTE Critical characteristics are defined in ECSS-Q-ST-30.\n    5. Detailed definition, by description or reference, of manufacturing, assembly, integration, inspections and test operations to be performed, and special conditions to be maintained.\n    6. Provisions for inspections and tests to be witnessed by customer representative.\n    7. Accept or reject criteria (with tolerances) and workmanship standards.\n    8. Details of sampling inspection procedures to be used, if any.\n    9. Detailed procedures for the activities to be performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1f","Requirement","ECSS-Q-ST-20_0380100","Only “first off” shop travellers shall be reviewed unless subsequent travellers incorporate a significant change of inspection requirements or order of events.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.1g","Requirement","ECSS-Q-ST-20_0380101","The supplier shall also provide for detail support documents and instructions, such as drawings, procedure and instruction sheets, to enable operations to be correctly performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.2a","Requirement","ECSS-Q-ST-20_0380102","The supplier shall perform an internal review of the readiness for manufacturing, prior to starting the manufacture of the first flight-standard product.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.2b","Requirement","ECSS-Q-ST-20_0380103","The manufacturing readiness review shall evaluate the following aspects:\n    1. status of product definition and requirements, differences with the status of the qualification model, and impacts of these differences;\n    2. status of manufacturing, assembly, inspection and test documentation, differences with the status of the qualification model, and impacts of these differences;\n    3. validation status of manufacturing processes, with particular emphasis on critical processes;\n    4. implementation of dispositions for risk reduction, as defined by risk assessment, into the manufacturing, assembly, integration, inspection and test procedures;\n    5. availability of specified production, measuring and inspection equipment, and calibration status, when relevant;\n    6. cleanliness of facilities, with respect to the specified cleanliness levels;\n    7. facility temperature and humidity with respect to requirements.\n",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.1a","Requirement","ECSS-Q-ST-20_0380104","The supplier shall monitor all processes used for manufacturing, assembly and integration, and enforce all applicable process requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.1b","Requirement","ECSS-Q-ST-20_0380105","The supplier shall ensure that all manufacturing processes are covered by documented process specifications or standards.\n    NOTE Manufacturing process specifications are defined in ECSS-Q-ST-70.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.1c","Requirement","ECSS-Q-ST-20_0380106","Process specifications shall include QA provisions, methods for inspection and test, number of samples, accept or reject criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.1d","Requirement","ECSS-Q-ST-20_0380107","Process witness samples shall be stored in controlled conditions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.2a","Requirement","ECSS-Q-ST-20_0380108","The supplier shall establish and implement procedures and controls for special processes, to ensure that:\n    1. Special processes are validated for the intended application.\n        NOTE Validation of special processes is defined in ECSS-Q-ST-70.\n    2. Personnel who perform special processes or evaluate the process performance are trained and certified or can demonstrate their proficiency through their regular activity.\n    3. Materials, equipment, computer systems and software, and procedures involved in the performance of the special process are validated and monitored.\n    4. Coordination is maintained with the cognizant engineering function to ensure proper selection of the non-destructive or destructive methods for the evaluation of process performance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.3.3a","Recommendation","ECSS-Q-ST-20_0380227","Statistical methods for process control should be used for early detection of significant variations in manufacturing processes, in order to determine, analyse and eliminate the causes of undesirable variations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.4a","Requirement","ECSS-Q-ST-20_0380110","The supplier shall employ workmanship standards throughout all phases of manufacturing, assembly and integration, to ensure acceptable and consistent workmanship quality levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.4b","Requirement","ECSS-Q-ST-20_0380111","Workmanship standards shall identify acceptance or rejection criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.4c","Requirement","ECSS-Q-ST-20_0380112","Physical samples or visual aids shall be reviewed and agreed by the customer when they are used for the purpose of acceptance or rejection of items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.5a","Requirement","ECSS-Q-ST-20_0380113","The supplier shall ensure that only conforming items are released and used, and that those not required for the operation involved are removed from work operation areas.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.5b","Requirement","ECSS-Q-ST-20_0380114","Items having limited-life or definite characteristics of quality degradation or drift with age or use shall be marked to indicate the dates, test times or cycles at which life was initiated and at which the useful life expires.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.5c","Requirement","ECSS-Q-ST-20_0380115","Sensitive items shall be processed or manufactured, inspected and tested in a controlled environment to prevent any degradation.\n    NOTE Requirements for the selection and control of materials and parts are defined in ECSS-Q-ST-70.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1a","Requirement","ECSS-Q-ST-20_0380116","The supplier shall make provisions for accountability, identification and maintenance of manufacture, assembly and integration tooling.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1b","Requirement","ECSS-Q-ST-20_0380117","Manufacture, assembly and integration tooling shall be checked for its dimensional accuracy, regarding the product drawings, and correct function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1c","Requirement","ECSS-Q-ST-20_0380118","The QA organization shall approve tooling prior to use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1d","Requirement","ECSS-Q-ST-20_0380119","The approval shall be stamped in conformance with 5.2.4, and recorded.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1e","Requirement","ECSS-Q-ST-20_0380120","Tools shall be checked for accuracy during the production life at adequate intervals.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1f","Requirement","ECSS-Q-ST-20_0380121","Tools shall be submitted to re-approval following modification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1g","Requirement","ECSS-Q-ST-20_0380122","Tools shall be properly stored to prevent misuse, damage and deterioration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1h","Requirement","ECSS-Q-ST-20_0380123","Unnecessary tools shall be removed from working areas.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.1i","Requirement","ECSS-Q-ST-20_0380124","Records shall be kept of all manufacturing equipment. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.2a","Requirement","ECSS-Q-ST-20_0380125","The supplier shall ensure that computer-aided techniques and data for processing and machining are validated prior to use and controlled during their use in manufacturing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.6.2b","Requirement","ECSS-Q-ST-20_0380126","The supplier shall ensure that provisions are made for the testing, approval and configuration control of the software involved and prevention of its being tampered with.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.1a","Requirement","ECSS-Q-ST-20_0380127","The supplier shall establish controls for cleanliness of spacecraft hardware and facilities, and the limitation of sources of contamination.\n    NOTE Cleanliness and contamination control methods and processes are detailed in ECSS-Q-ST-70-01.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.2a","Requirement","ECSS-Q-ST-20_0380128","Contamination-sensitive items shall be cleaned, controlled and maintained to the required cleanliness levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.2b","Requirement","ECSS-Q-ST-20_0380129","The required cleanliness levels for all levels of flight hardware shall be indicated on drawings, specifications, procedures, or other documents controlling the manufacture, assembly, integration and test of the items. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.3a","Requirement","ECSS-Q-ST-20_0380130","The supplier shall develop detailed methods for attaining the cleanliness levels specified for the hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.4a","Requirement","ECSS-Q-ST-20_0380131","Contamination shall be minimized by operating in clean working areas and by proper handling, preservation, packaging and storage.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.4b","Requirement","ECSS-Q-ST-20_0380132","Contamination-sensitive items fabricated or processed in contamination-controlled environments shall be inspected, tested, modified or repaired in identical or cleaner environments, unless specific precautions are taken to protect the items concerned from contamination.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.4c","Requirement","ECSS-Q-ST-20_0380133","Specific protection measures, such as protective dust covers, shall be implemented to protect contamination-sensitive items when they are integrated in a higher level of assembly.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.7.5a","Requirement","ECSS-Q-ST-20_0380134","Fabrication, assembly and integration of contamination sensitive items shall be conducted in facilities that provide cleanliness levels compatible with the specified product cleanliness.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8a","Requirement","ECSS-Q-ST-20_0380135","Inspection and tests shall be planned at the points of the manufacturing, assembly and integration flow where maximum assurance for correct processing and prevention of unrecoverable or costly nonconformances can be obtained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8b","Requirement","ECSS-Q-ST-20_0380136","All identified critical characteristics shall be inspected as defined in the critical-item control programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8c","Requirement","ECSS-Q-ST-20_0380137","Self-inspection by the operators performing the associated manufacturing, assembly and integration activities shall not be considered sufficient for critical characteristics.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8d","Requirement","ECSS-Q-ST-20_0380138","Among the inspections and tests as part of the manufacturing, assembly and integration flow, mandatory inspection points (MIPs) shall be performed with participation of the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8e","Requirement","ECSS-Q-ST-20_0380139","MIPs shall be agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8f","Requirement","ECSS-Q-ST-20_0380140","MIPs shall be selected in accordance with the criteria as defined below, when one or more of the following conditions apply:\n    1. When maximum visibility of quality is given.\n    2. When critical processes are performed.\n    3. Where the next step of the manufacturing sequence:\n        (a) is irreversible, or\n        (b) makes the item difficult and costly to disassemble for inspection, or\n        (c) renders the location inaccessible for inspection.\n    4. When the item, once installed in the next higher assembly damages by its failure the higher assembly.\n    5. When previous failure history of the item indicates a need for inspection.\n    6. When a potential adverse impact on the properties and integrity of the end product could result, owing to the criticality or complexity of the manufacturing step.\n    7. When testing or critical inspections cannot be accomplished by the supplier.\n        NOTE For example, environments or test equipment not available at supplier’s facility.\n    8. When verification tests are destructive in nature and the quality cannot be verified solely by inspection or test at the supplier’s facility.\n    9. When manufacturing and AIV of complex equipment or subsystems is planned.\n        NOTE For example, for payloads.\n    10. When past performance or quality history of the lower level supplier is marginal.\n    11. When an item is going to final inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8g","Requirement","ECSS-Q-ST-20_0380141","Criteria 5.5.8f.7 to 10 shall be considered together with the criticality and complexity of the supplies and the supplier’s experience with the lower level supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8h","Requirement","ECSS-Q-ST-20_0380142","A MIP shall require an invitation with the agreed notice before the event, and the participation of the customer, or their written agreement to proceed without their participation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.8i","Requirement","ECSS-Q-ST-20_0380143","The supplier shall make provisions for a positive identification of the inspection and test status of any items at any stage of the manufacturing, assembly and integration cycle, starting from the incoming inspection up to shipping of the end item.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.1a","Requirement","ECSS-Q-ST-20_0380144","The supplier shall ensure the control of flight items which are temporarily removed or non-flight items which are temporarily installed to facilitate assembly, integration, testing, handling or preservation of the end item.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.1b","Requirement","ECSS-Q-ST-20_0380145","The control shall be initiated upon installation or removal of the first temporarily installed or removed item and be maintained through delivery and use of the end item.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.1c","Requirement","ECSS-Q-ST-20_0380146","The supplier shall establish and maintain records of temporary installations and removals.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.1d","Requirement","ECSS-Q-ST-20_0380147","Temporarily installed items shall be accounted for to prevent their being incorporated in the final flight configuration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.2a","Requirement","ECSS-Q-ST-20_0380148","The supplier shall prepare and maintain system, subsystem and equipment logbooks in conformance with the DRD in Annex C for all operations and tests performed on the item during the period to be covered by the logbook.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.2b","Requirement","ECSS-Q-ST-20_0380149","Equipment logbooks shall start with the first qualification or acceptance test after assembly.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.2c","Requirement","ECSS-Q-ST-20_0380150","Subsystem and system logbooks shall follow-on from the individual equipment logbooks to form a full record.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.2d","Requirement","ECSS-Q-ST-20_0380151","The logbook shall accompany the hardware whenever it is placed in the custody of another organization",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.9.2e","Requirement","ECSS-Q-ST-20_0380152","The receiving organization shall maintain the logbook up-to-date.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.5.10a","Requirement","ECSS-Q-ST-20_0380153","The supplier shall establish and maintain manufacturing, assembly and integration records to provide all manufacturing, assembly, integration and inspection data required for traceability.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.1a","Requirement","ECSS-Q-ST-20_0380154","The supplier shall ensure that test facilities, either internal or external, conform to specified requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.2a","Requirement","ECSS-Q-ST-20_0380155","The supplier shall ensure that computer-aided testing techniques and data are validated prior to use and controlled during their use in testing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.2b","Requirement","ECSS-Q-ST-20_0380156","The supplier shall ensure that provisions are made for testing, approval and configuration control of the software involved and prevention of its being tampered with.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.2c","Requirement","ECSS-Q-ST-20_0380157","The supplier shall ensure that test equipment are designed such that their correct operation can be verified without having to apply them to the test item.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.3.1a","Requirement","ECSS-Q-ST-20_0380158","The supplier shall ensure that tests are performed in accordance with documented procedures, which shall include, as a minimum:\n    1. scope of the test, including the identification of the requirement being verified,\n    2. identification of the test object,\n    3. applicable documents, with their revision status,\n    4. test flow,\n    5. test organization,\n    6. test conditions,\n    7. test equipment and set-up,\n    8. step-by-step procedure, including definition of specific steps to be witnessed by QA personnel,\n    9. recording of data,\n    10. pass or fail criteria and test data evaluation requirements, and\n    11. guidelines or criteria for deviation from test procedure and for retest.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.3.1b","Requirement","ECSS-Q-ST-20_0380159","The QA organization shall review and approve test procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.3.2a","Requirement","ECSS-Q-ST-20_0380160","The supplier shall ensure that all tests are comprehensively documented in test reports, and that they include, as a minimum:\n    1. reference to the applicable test procedure, and description of the deviations from it during the actual testing,\n    2. test data records and evaluation, and\n    3. summary of test results.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.3.2b","Requirement","ECSS-Q-ST-20_0380161","The QA organization shall review and approve test reports.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4a","Requirement","ECSS-Q-ST-20_0380162","On the basis of an analysis of the test plan, the QA organization shall define within the test plan the most appropriate way to monitor the performance of test activities, to ensure the adherence to the test procedures, and that any deviations are properly documented and treated.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4b","Requirement","ECSS-Q-ST-20_0380163","Test witnessing by QA personnel shall be considered when manual intervention is performed, at the setting-up, start and end of continuous fully automated test sequences, or when no automatic recording of test parameters or results is available.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4c","Requirement","ECSS-Q-ST-20_0380164","All testing activities related to critical characteristics as identified in the critical-items control programme shall be certified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4d","Requirement","ECSS-Q-ST-20_0380165","Self-certification by the operators performing the test activities shall not be considered sufficient for critical characteristics.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4e","Requirement","ECSS-Q-ST-20_0380166","Testing activities or results to be subject to QA certification shall be identified as such in the relevant test procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4f","Requirement","ECSS-Q-ST-20_0380167","Testing shall be subject to the requirements for the control of hazardous operations.\n    NOTE Definition of hazardous operations is given in ECSS-Q-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.4g","Requirement","ECSS-Q-ST-20_0380168","Where safety of personnel or damage to items or associated test equipment is possible, QA personnel shall have the authority to stop the test.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.5a","Requirement","ECSS-Q-ST-20_0380169","The supplier shall ensure that formal reviews are performed before and after major portions of qualification or acceptance tests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.6.5b","Requirement","ECSS-Q-ST-20_0380170","The QA organization shall be represented in the formal boards established for the review of readiness for testing and testing accomplishment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.1a","Requirement","ECSS-Q-ST-20_0380171","The supplier shall establish a formal acceptance process for all deliverable items, at any contractual level, to ensure that conformance of the items to be delivered is fully assessed and documented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.1b","Requirement","ECSS-Q-ST-20_0380172","The supplier shall ensure that the preparation of the items for delivery and the physical delivery itself are performed in such a way that quality degradation is prevented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.2a","Requirement","ECSS-Q-ST-20_0380173","The supplier shall provide an EIDP for each deliverable end item in conformance with the DRD in Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.2b","Requirement","ECSS-Q-ST-20_0380174","The EIDP shall constitute the basis for formal acceptance reviews.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.2c","Requirement","ECSS-Q-ST-20_0380175","EIDPs shall be maintained and integrated into higher level EIDPs during subsystem or system integration and testing. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3a","Requirement","ECSS-Q-ST-20_0380176","The supplier shall ensure that a DRB is convened prior to the delivery of equipment, separately assembled subsystems, test equipment or handling equipment for higher level activities.\n    NOTE “Acceptance Review Board” (ARB) defined in ECSS-M-ST-10 is referred to as “Delivery Review Board” (DRB) in this document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3b","Requirement","ECSS-Q-ST-20_0380177","The DRB functions at system level shall be fulfilled by the final acceptance review and chaired by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3c","Requirement","ECSS-Q-ST-20_0380178","The DRB shall be composed, at least, of the following members:\n    1. Representatives of the receiving organization:\n        (a) Project manager, or authorized representative, as chairman;\n        (b) PA manager, or authorized representative;\n        (c) Engineering or design manager, or authorized representative.\n    2. Submitting supplier’s representatives:\n        (a) Project manager, or authorized representative;\n        (b) PA manager, or authorized representative;\n        (c) Engineering or design manager, or authorized representative.\n    3. Higher level customers’ representative(s), as observers (not required for separate subsystems).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3d","Requirement","ECSS-Q-ST-20_0380179","If the final customer reserves the right to attend DRBs at any lower level as an observer, he shall be given due notice of such a DRB meeting.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3e","Requirement","ECSS-Q-ST-20_0380180","The DRB shall be responsible for authorising the shipment of the items under acceptance, and certifying in writing that:\n    1. the items conform to the contractual requirements and to an approved design configuration;\n    2. the items are free from material and workmanship deficiencies;\n    3. all nonconformances are closed-out, or corresponding plans, compatible with the delivery, are accepted;\n    4. the relevant EIDP is complete and accurate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3f","Requirement","ECSS-Q-ST-20_0380181","Delivery shall only be authorized by the unanimous agreement of the DRB members.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.3g","Requirement","ECSS-Q-ST-20_0380182","For the delivery a certificate of conformity, in conformance with Annex D, shall be made available and signed by the supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.4.1a","Requirement","ECSS-Q-ST-20_0380183","The supplier shall ensure that packaging materials, methods, procedures and instructions provide for protection of items while at the supplier’s plant, during transportation, and after their arrival at destination.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.4.2a","Requirement","ECSS-Q-ST-20_0380184","The supplier shall ensure that appropriate marking and labelling for packaging, storage, transportation and shipping of items are performed in accordance with the applicable specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.5.1a","Requirement","ECSS-Q-ST-20_0380185","The supplier shall ensure that the items to be shipped from his plant are inspected before release and found to be complete, adequately preserved and packaged, correctly marked and accompanied by all the required documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.5.1b","Requirement","ECSS-Q-ST-20_0380186","Accompanying documentation shall include the EIDP and, attached to the outside of the shipping container, the handling and packing or unpacking procedure and any relevant safety procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.7.5.2a","Requirement","ECSS-Q-ST-20_0380187","The supplier shall make provisions for the prevention of damage to items during transportation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.1.1.1a","Requirement","ECSS-Q-ST-20_0380188","The supplier shall ensure that internal design and verification standards are used or developed corresponding with the techniques to be used and fitting with the level of complexity of the items to be developed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.1.1.1b","Requirement","ECSS-Q-ST-20_0380189","The supplier shall ensure that development risks are identified and appropriate back-up solutions are identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.1.1.1c","Requirement","ECSS-Q-ST-20_0380190","The supplier shall ensure that the verification method and process are tailored to the:\n    1. complexity of the item to be verified;\n    2. criticality of the function to be implemented by the GSE item;\n    3. inherent criticality of the item itself.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.2a","Requirement","ECSS-Q-ST-20_0380191","The supplier shall ensure that GSE is configuration controlled.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.3.1a","Requirement","ECSS-Q-ST-20_0380192","The supplier shall ensure that selected GSE suppliers have a demonstrated ability to conform to requirements, through:\n    1. previous supply of items similar or more complex in the same field of techniques and technologies,\n    2. certification covering similar design, development and production as applicable for similar items in conformance with 5.4.1.2, or\n    3. evidence, documented by existing design, development, production and quality standards, of having similar experience associated with known success.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.3.1b","Requirement","ECSS-Q-ST-20_0380193","Procurement documents shall identify validation and receiving inspection requirements, and conform to the requirements in clause 5.4.2.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.3.2a","Recommendation","ECSS-Q-ST-20_0380228","The supplier and his lower level suppliers should not deviate from their standard practices when these are already documented and recognized for similar items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.4.1a","Requirement","ECSS-Q-ST-20_0380195","The acceptance data package shall include :\n    1. information regarding interfaces,\n    2. deviations from contractual requirements,\n    3. certification of conformance to an identified baseline,\n    4. description of the functioning of the item, and instructions to operate and maintain it, and\n    5. safety data or safety certification(s).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.5a","Requirement","ECSS-Q-ST-20_0380196","Acceptance shall be achieved through a formal review process \n    NOTE Review process is defined in ECSS-M-ST-10-01.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.5b","Requirement","ECSS-Q-ST-20_0380197","The acceptance process shall include:\n    1. acceptance plan,\n    2. inspection and test procedures, and\n    3. inspection and test reports.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.5c","Permission","ECSS-Q-ST-20_0380229","Acceptance may be achieved through a simple inspection process if agreed between customer and supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.6a","Requirement","ECSS-Q-ST-20_0380199","The supplier shall propose GSE elements for which acceptance is granted by a delivery board and agree these with his customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.6b","Requirement","ECSS-Q-ST-20_0380200","The delivery board shall include QA representatives from the supplier and the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.7a","Requirement","ECSS-Q-ST-20_0380201","The requirements of the following clauses shall be applied to the delivery of ground items and handling, storage, packing and shipping activities:\n    1. preparation for delivery, in conformance with 5.7.4,\n    2. delivery, in conformance with 5.7.5, and\n    3. handling, storage and preservation, in conformance with 5.2.7.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.8a","Requirement","ECSS-Q-ST-20_0380202","The following requirements shall be tailored in accordance with the complexity and criticality of the GSE item:\n    1. traceability requirements in 5.2.5, and\n    2. metrology and calibration requirements in 5.2.6.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.9a","Requirement","ECSS-Q-ST-20_0380203","The supplier shall ensure that maintenance activities are planned.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","5.8.9b","Requirement","ECSS-Q-ST-20_0380204","The supplier shall ensure that maintenance demonstration is performed in order to prove that maintainability requirements are satisfied in the real operational environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<1>a","Requirement","ECSS-Q-ST-20_0380205","The Quality Assurance Plan shall introduce the purpose, objective and the reason prompting its preparation ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<2>a","Requirement","ECSS-Q-ST-20_0380206","The Quality Assurance Plan shall list the applicable and reference documents in support of the generation of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<3>a","Requirement","ECSS-Q-ST-20_0380207","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable quality assurance general requirements defined in ECSS-Q-ST-20 clause 5.1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<4>a","Requirement","ECSS-Q-ST-20_0380208","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for design and verification defined in ECSS-Q-ST-20 clause 5.3.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<5>a","Requirement","ECSS-Q-ST-20_0380209","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for procurement defined in ECSS-Q-ST-20 clause 5.4",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<6>a","Requirement","ECSS-Q-ST-20_0380210","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for manufacturing, assembly and integration defined in ECSS-Q-ST-20 clause 5.5.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<7>a","Requirement","ECSS-Q-ST-20_0380211","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for testing defined in ECSS-Q-ST-20 clause 5.6.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.1<8>a","Requirement","ECSS-Q-ST-20_0380212","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for acceptance and delivery defined in ECSS-Q-ST-20 clause 5.7.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","A.2.2a","Permission","ECSS-Q-ST-20_0380230","The response to this DRD may be combined with the response to the product assurance plan, as defined in ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","B.2.1a","Requirement","ECSS-Q-ST-20_0380214","The EIDP shall include the following information and documentation:\n    1. The DRB minutes\n    2. The customer acceptance certificate if not covered in DRB minutes\n    3. Cover page\n        NOTE An example is given in Annex F.\n    4. Table of contents\n        NOTE An example is given in Annex G.\n    5. Change record\n    6. The product certificate of conformity in conformance with Annex D.\n    7. NCR list\n    8. ABCL\n    9. Summary and status of RFDs and RFWs raised and processed on the product\n    10. The product logbook\n    11. Product definition documents to be used for further integration, testing and operation in higher level assemblies including the software used to operate the item and the product user or operating manuals.\n    12. Procedures to be used for the proper handling of the product after its final delivery, including procedures for:\n        (a) packing,\n        (b) handling,\n        (c) storage,\n        (d) transportation,\n        (e) safety, and\n        (f) cleanliness.\n    13. Copies of the product test reports, or as a minimum the list of the documents with the identification of their location.\n    14. List of delivered ground support equipment (e.g.: MGSE, EGSE, FGSE, OGSE) with the reference to their corresponding EIDPs and software product.\n    15. List of EIDPs or logbooks of units and subsystem supplied by lower tier suppliers.\n    16. List of the loose items and not installed items supplied with the product.\n    17. Any additional useful information or data relevant to the product.\n        NOTE For example, cleanliness certification when cleanliness is a requirement.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1a","Requirement","ECSS-Q-ST-20_0380215","The logbook cover page shall contain the following:\n    1. general information,\n    2. contents,\n    3. approvals of the relevant authorities (QA, PA, PM), and\n    4. customer acceptance (if required by the business agreement).\n        NOTE An example of a logbook cover page is given in Annex E.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1b","Requirement","ECSS-Q-ST-20_0380216","The logbook shall contain the “hardware configuration and traceability” table, which reports all the identification references of single elements composing the CI. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1c","Requirement","ECSS-Q-ST-20_0380217","The logbook shall contain the “hardware configuration change and status” table, which reports for each singe element of the CI all the events relevant to integration, removal and replacement on the higher level.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1d","Requirement","ECSS-Q-ST-20_0380218","The logbook shall contain the summary list of the integration and test instructions, including for each entry, the action start date, action performed date and action close-out date shall also be reported.\n    NOTE Example: shop traveller",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1e","Requirement","ECSS-Q-ST-20_0380219","The logbook shall contain the summary list of nonconformances with relevant identification references, issue date, closure dates, and status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1f","Requirement","ECSS-Q-ST-20_0380220","The logbook shall contain all the electrical connector (or other limited cycles items) mate and demate cycles in order to ensure the conformance with the project requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1g","Requirement","ECSS-Q-ST-20_0380221","The logbook shall contain the records of total operating hours for each limited-life element identified in the test procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1h","Requirement","ECSS-Q-ST-20_0380222","The logbook shall contain, in chronological order, the events related to the integration and test activities performed on the relevant item (i.e. system, subsystem, and equipment), including the following:\n    1. Action requested form, reporting all the operations performed with the references to the applicable documents or procedures, start date, completion date and quality inspection stamps.\n    2. Step-by-step procedures and results, in which copies of the as-run procedures are included in a suitable format.\n    3. Procedures variation form, in which copies of modified procedures (red marked) identified with a procedure variation number and duly approved by responsible authorities, are included. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","C.2.1i","Requirement","ECSS-Q-ST-20_0380223","The logbook shall contain the list of open action or open test at the time of the product shipment to the customer, test facility or launch pad.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C","D.2.1a","Requirement","ECSS-Q-ST-20_0380224","The DoC shall contain the following elements:\n    1. Title including references to identify the product and the relevant applicable documents\n        NOTE Examples for references are item name, project, serial number, part number, customer, contract number.\n    2. Document no. in accordance with project configuration control rules;\n    3. EIDP reference number;\n    4. Intended use, specifying the item objective (i.e. BB, QM, FM)\n    5. Reference of conformity, calling for example the following documents:\n        (a) Business agreement requirements: reference number of design spec., ICD or other contractual documents;\n        (b) Operational documents: reference number of drawings, procedures, and electrical schemes;\n        (c) Deliverable documents: reference number of EIDP, logbooks, and manuals.\n    6. Statement of conformity.\n    7. List of waivers or deviations or other remarks.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.1.2a","Requirement","ECSS-Q-ST-70_0490001","The supplier shall prepare, maintain and implement a MMPP plan, as part of the overall PA plan in conformance to ECSS-Q-ST-10 and this Standard or as a separate document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.1.2b","Requirement","ECSS-Q-ST-70_0490002","The MMPP plan shall be submitted to the customer for approval.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.1.3a","Requirement","ECSS-Q-ST-70_0490003","To obtain the validation status for materials and qualification status for parts and verification status for processes, the MMPP manager shall present to the customer those activities which were performed in order to comply with this Standard together with results obtained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.1.3b","Requirement","ECSS-Q-ST-70_0490004","The MMPP manager shall organize technical review meetings with his suppliers at all levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2a","Requirement","ECSS-Q-ST-70_0490005","Each supplier and sub-supplier shall establish, collect, review and deliver the declared materials, mechanical parts and processes lists including all the items intended for use in the flight equipment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2b","Requirement","ECSS-Q-ST-70_0490006","The lists shall reflect the current design at the time of issue.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2c","Requirement","ECSS-Q-ST-70_0490007","These lists shall contain the materials, mechanical parts and processes used in the current design in order to: \n    1. demonstrate compliance with all requirements of the programme;\n    2. verify the results of equipment supplier activities;\n    3. control and monitor the status of materials, mechanical parts and processes in accordance with programme milestones.\n        NOTE See Annex F.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2d","Recommendation","ECSS-Q-ST-70_0490194","The following constraints should apply:\n    1. maximum use of the materials and processes described in approved data sources and items already approved on similar projects;\n        NOTE For approved data sources see for example ECSS-Q-ST-70-71.\n    2. use of project related preferred lists, if available.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2e","Requirement","ECSS-Q-ST-70_0490009","The following constraints shall be taken into account: \n    1. requirements originating from the initial technical specification;\n    2. programmatic project requirements and conditions;",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2f","Requirement","ECSS-Q-ST-70_0490010","An analysis of the criticality of these preliminary lists shall, after checking the conformity of the materials, mechanical parts and processes, against all the project requirements, allow them to be classified into three categories:\n    1. Critical items, subject to evaluation, validation, qualification, or verification programmes.\n    2. Items that are not critical but which do not conform to one or more project requirements (a justified deviation request should be drafted for this category).\n    3. Non-critical items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.2g","Requirement","ECSS-Q-ST-70_0490011","For critical items a request for approval shall be submitted in conformance with Annex D.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3a","Requirement","ECSS-Q-ST-70_0490012","The supplier shall document all materials in the Declared materials list in conformance with Annex A.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3b","Requirement","ECSS-Q-ST-70_0490013","The supplier shall document all mechanical parts in the Declared mechanical parts list in conformance with Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3c","Requirement","ECSS-Q-ST-70_0490014","The supplier shall document all processes in the Declared process list in conformance with Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3d","Requirement","ECSS-Q-ST-70_0490015","The supplier shall process the lists of lower level suppliers to ensure exchangeabililty, searchability, sortability, storability and retrievability for that set of lists, before submitting it to the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3e","Requirement","ECSS-Q-ST-70_0490016","These lists shall be updated during the course of the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3f","Requirement","ECSS-Q-ST-70_0490017","The preliminary lists shall include the items from suppliers’ preliminary needs.\n    NOTE They are used to identify critical items (available for the PDR).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3g","Requirement","ECSS-Q-ST-70_0490018","The as-designed lists shall include the items from the baselines various design files (available for the CDR).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.3h","Requirement","ECSS-Q-ST-70_0490019","Any change after CDR or QR shall be reflected in the list and shall be in accordance with Figure 4-1 (Part 2).\n    NOTE 1 The MMPP manager is responsible within the programme to ensure that all the information needed is given and that the approval status is consistent with technical and scheduling objectives and data is exchangeable.\n    NOTE 2 Where no project requirements exist for a separate DMPL, the mechanical parts can be entered into a separate section of the DML.\n    NOTE 3 The materials of, for example, screws and nuts that are made up of a few materials can be listed in the DMPL. The materials (metals and plastics) of complex parts can be listed in the DML with, for example, outgassing, toxicity, flammability, corrosion and stress corrosion values and reference to the DMPL item.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.4a","Requirement","ECSS-Q-ST-70_0490020","The supplier shall perform the following tasks:\n    1. obtaining the correct and complete lists from lower level suppliers;\n    2. providing provisional and, later, definitive approval for each list;\n    3. submitting the project declared lists for approval prior to initiation of the hardware phase (before critical design review).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.4b","Requirement","ECSS-Q-ST-70_0490021","The lists established by the suppliers shall include all the information described in this Standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.4c","Requirement","ECSS-Q-ST-70_0490022","Amendments to the lists shall be implemented only through established change procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.4d","Requirement","ECSS-Q-ST-70_0490023","The following documentation shall be delivered to the customer upon request:\n    1. RFA (reference and issue);\n    2. evaluation reports;\n    3. deviation requests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.2.4e","Requirement","ECSS-Q-ST-70_0490024","The material, mechanical parts or process justification files shall be made available to the customer upon request either on the supplier site, or by any other process agreed by both parties.\n    NOTE For example, by non-disclosure agreement.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.3a","Requirement","ECSS-Q-ST-70_0490025","Parts and materials shall satisfy the mission’s functional constraints.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.3b","Requirement","ECSS-Q-ST-70_0490026","Parts and materials shall satisfy both ground environment constraints and flight constraints.\n    NOTE Examples are:\n        · Ground environment constraints: manufacture, tests, storage, maintenance, transport and integration\n        · Flight constraints: launch and orbit.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.3c","Requirement","ECSS-Q-ST-70_0490027","The technical criteria from clause 5.1 shall be taken into account, according to the mission.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.3d","Requirement","ECSS-Q-ST-70_0490028","The estimated availability of the parts and products obtained from materials and processes used shall be compatible with the final system’s life cycle (tests, storage and mission).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.4a","Requirement","ECSS-Q-ST-70_0490029","The supplier shall establish and maintain a contamination and cleanliness control programme including, as a minimum:\n    1. cleaning procedures, and\n    2. cleanliness monitoring procedures or methods.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.4b","Requirement","ECSS-Q-ST-70_0490030","The risks of chemical or particle pollution generated by parts, materials or processes used shall be identified and reduced in accordance with mission requirements (cleanliness or contamination analysis).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.4c","Requirement","ECSS-Q-ST-70_0490031","For cleanliness- or contamination-critical applications, a requirement specification (chemical and particle) and a specific cleanliness control plan and shall be established in conformance with Annex A (CRS DRD) and Annex B (C&CCP DRD) of ECSS-Q-ST-70-01.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.5a","Requirement","ECSS-Q-ST-70_0490032","Parts and materials with hazardous characteristics shall be identified, managed and processed in conformance with ECSS-Q-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","4.6a","Requirement","ECSS-Q-ST-70_0490033","When optical, mechanical or electrical GSE materials are used in thermal vacuum or interfacing with flight hardware, possible degradation shall be taken into account.\n    NOTE For example, contamination, surface degradation, electro-mechanical and chemical effects.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.2a","Requirement","ECSS-Q-ST-70_0490034","Material properties shall be compatible with the thermal environment to which they are exposed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.3a","Requirement","ECSS-Q-ST-70_0490035","Materials subject to thermal cycling shall be assessed for their ability to withstand induced thermal stress.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.3b","Requirement","ECSS-Q-ST-70_0490036","The following materials shall be tested in conformance with ECSS-Q-ST-70-04:\n    1. Materials susceptible to thermal vacuum effect.\n        NOTE For a non-exhaustive list of such materials, see ECSS-Q-ST-70-04 Clause 1.\n    2. Materials of unknown characteristics in respect to thermal vacuum.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.3c","Requirement","ECSS-Q-ST-70_0490037","Materials subject to thermal cycling other than those covered by 5.1.3b, shall be tested in accordance with a procedure approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.4a","Requirement","ECSS-Q-ST-70_0490038","Materials selection shall be made in conformance with ECSS-Q-ST-70-71.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.4b","Requirement","ECSS-Q-ST-70_0490039","Outgassing tests shall be carried out in conformance with ECSS-Q-ST-70-02.\n    NOTE The need for retest of materials used for an extended period of time at a temperature higher than 50 °C should be mutually agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.5a","Requirement","ECSS-Q-ST-70_0490040","Spacecraft and associated equipment shall be manufactured from materials and by processes that do not cause a hazard to personnel or hardware, whether on the ground or in space.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.5b","Requirement","ECSS-Q-ST-70_0490041","ECSS-Q-ST-70-29 shall apply for the characterization of offgassing products.\n    NOTE MAPTIS and MIL-HDBK-454 test method is not space relevant.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.6a","Requirement","ECSS-Q-ST-70_0490042","The materials flammability resistance shall be evaluated in conformance with ECSS-Q-ST-70-21 for the most hazardous environment envisaged for their use.\n    NOTE For NASA STS payloads see NASA STD-6001.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.7a","Requirement","ECSS-Q-ST-70_0490043","Materials used on the spacecraft external surfaces shall be assessed in conformance with ECSS-Q-ST-70-06 in order to determine their resistance to the radiation dosage expected during the mission.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.8a","Requirement","ECSS-Q-ST-70_0490044","External surfaces of the spacecraft shall be sufficiently conductive, interconnected and grounded to the spacecraft structure to avoid the build-up of differential charges in conformance with ECSS-E-ST-20-06.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.9a","Requirement","ECSS-Q-ST-70_0490045","For all materials that come into contact with atmospheric gases, cleaning fluids or other chemicals, it shall be demonstrated that the degradation of properties during their anticipated service-life is acceptable in terms of the performance and integrity requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.10a","Requirement","ECSS-Q-ST-70_0490046","Materials used for structural and load-bearing applications (subject to tensile stress) shall be chosen in conformance with ECSS-Q-ST-70-36.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.10b","Requirement","ECSS-Q-ST-70_0490047","Any material not covered by standard ECSS-Q-ST-70-36 shall be tested in conformance with ECSS-Q-ST-70-37.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.11a","Requirement","ECSS-Q-ST-70_0490048","Materials within the system exposed to liquid oxygen (LOX), gaseous oxygen (GOX) or other reactive fluids, both directly and as a result of single point failures when failure propagation effects cause hazardous operation of interfacing hardware shall be compatible with that fluid in their application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.11b","Requirement","ECSS-Q-ST-70_0490049","The possibility of hydrogen embrittlement occurring during component manufacture or use shall be assessed, and an material evaluation be undertaken, including the assessment of adequate protection and control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.12a","Requirement","ECSS-Q-ST-70_0490050","When bimetallic contacts are used, the choice of the pair of metallic materials used shall be agreed with the customer. \n    NOTE This also includes metal-to-conductive fibre-reinforced materials contacts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.12b","Requirement","ECSS-Q-ST-70_0490051","Galvanic compatibilities shall be selected in conformance with Table 5-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.12c","Requirement","ECSS-Q-ST-70_0490052","Materials not listed in Table 5-1 shall be evaluated in a flight-simulated configuration using an accelerated environment to be agreed by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.13a","Requirement","ECSS-Q-ST-70_0490053","All materials considered for use on the external surfaces of spacecraft intended for use in Low Earth Orbit (LEO) altitudes (between 200 km and 700 km) shall be evaluated for their resistance to atomic oxygen (ATOX).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.13b","Requirement","ECSS-Q-ST-70_0490054","Test procedures shall be subject to the approval of the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.14a","Requirement","ECSS-Q-ST-70_0490055","The effect of impacts by micrometeoroids and debris on materials shall\n    1. be reviewed and assessed on a case by case basis, and\n    2. their use comply with safety evaluation and assessment results concerning design and application criteria or details.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.15a","Requirement","ECSS-Q-ST-70_0490056","Precautions shall be taken to avoid moisture absorption during manufacture and storage of CFRP-type materials in conformance with ECSS-Q-ST-70-01 and ECSS-Q-ST-70-22.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.16a","Requirement","ECSS-Q-ST-70_0490057","For all solid surfaces in moving contact with other solid surfaces, it shall be demonstrated that the degradation of surface properties over the complete mission is acceptable from a performance point of view.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.1.17a","Requirement","ECSS-Q-ST-70_0490058","Materials shall be selected to ensure sufficient life with respect to the intended application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.2.1a","Requirement","ECSS-Q-ST-70_0490059","Materials shall be chosen giving preference to the following:\n    1. those successfully used for an identical application in other space programmes similar with respect to environment constraints and lifetime to the proposed application;\n    2. those for which satisfactory evaluation results are obtained on samples representative of the application with a sufficient margin as regards conditions of use;\n    3. those included in approved data sources.\n        NOTE For example: ECSS-Q-ST-70-71, ESA and NASA data banks.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.2.1b","Requirement","ECSS-Q-ST-70_0490060","Whether the materials are already validated or remain to be validated, their selection shall take into account the following criteria:\n    1. continuity of supply;\n    2. reproducibility of characteristics.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.2.2a","Requirement","ECSS-Q-ST-70_0490061","Pure tin finish with more than 97 % purity shall not be used.\n    NOTE This is due to the possibility of whisker growth and transformation to grey tin powder at low temperatures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.2.2b","Requirement","ECSS-Q-ST-70_0490062","The incoming inspection of each component batch shall include the verification of the termination composition (to avoid assembly of pure tin finish).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.3a","Requirement","ECSS-Q-ST-70_0490063","The supplier shall establish and maintain a declared materials list in conformance with Annex A.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.4.2a","Requirement","ECSS-Q-ST-70_0490064","The supplier shall analyse all the materials contained in his preliminary lists with respect to criticality and in correlation with the risk analysis performed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.4.2b","Requirement","ECSS-Q-ST-70_0490065","Any material not meeting the project requirements shall be subject to a RFD to be submitted to the next customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.4.2c","Requirement","ECSS-Q-ST-70_0490066","Any critical material shall be subject to a RFA to be submitted to the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.4.2d","Requirement","ECSS-Q-ST-70_0490067","For any material not meeting the project requirements the supplier shall submit a RFA in conformance with Annex D.\n    NOTE Any material when specifically required, marking inks can be excluded.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.1a","Requirement","ECSS-Q-ST-70_0490068","Depending on the results of the criticality analysis, the supplier shall perform an evaluation phase before the validation phase for all critical materials with unknown characteristics (new materials) or with major changes in the use or in the configuration",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.1b","Permission","ECSS-Q-ST-70_0490195","In case of an extension of an existing application, the evaluation indicated in 5.5.1a need not be performed if so agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.1c","Requirement","ECSS-Q-ST-70_0490070","Guarantied characteristics of materials and material supplier inspection methods, together with associated documents, shall be available for review at the supplier’s premises before the start of evaluation or qualification phases.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.2a","Requirement","ECSS-Q-ST-70_0490071","The evaluation shall consider the following as a minimum:\n    1. the limits of use;\n    2. the materials physical, chemical or functional characteristics along with their values and tolerances;\n    3. behavioural tendencies and degradation processes depending on environmental parameters (including sensitivity to pollution);\n    4. acceptance criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.2b","Requirement","ECSS-Q-ST-70_0490072","When evaluation is performed, an evaluation programme (available at PDR, according to Figure 4-1) shall be drawn up, implemented and an evaluation report (available before CDR, according to Figure 4-1 and Table 4-1) shall be drawn up.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.3a","Requirement","ECSS-Q-ST-70_0490073","For all critical materials, a validation programme (available at PDR) shall be drawn up by the supplier and then implemented to check or confirm that the materials satisfy the mission requirements with appropriate margins as necessary to obtain validation status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.3b","Requirement","ECSS-Q-ST-70_0490074","Validation status shall depend on the results obtained (validation report) and the review of corresponding documentation (available at CDR).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.4a","Requirement","ECSS-Q-ST-70_0490075","The material shall not receive an approval identification in the declared material list for the project unless the requirements in 5.5.2 and 5.5.3 are satisfied.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.4b","Requirement","ECSS-Q-ST-70_0490076","If approval is not granted, the supplier in charge of the item shall either:\n    1. select another material, or\n    2. propose a modified evaluation programme and resubmit for approval, or\n    3. if actions 5.5.4b.1 and 5.5.4b.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.5.5a","Requirement","ECSS-Q-ST-70_0490077","For materials not conforming to project requirements, whether at the end of criticality analysis or of evaluation and validation tests, the supplier shall submit a request for deviation in conformance with ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1a","Requirement","ECSS-Q-ST-70_0490078","All materials shall be procured to an internationally or nationally recognized specification or an in-house fully configured procurement specification which defines the materials properties, the materials requirements, the test methods, the acceptance criteria for the specific applications, source inspection (if any) and material supplier inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1b","Requirement","ECSS-Q-ST-70_0490079","Where material suppliers do not accept specifications and procurement is by means of a datasheet the supplier shall introduce internal, in-house receipt inspection to ensure that the validation status of the material is maintained during the subsequent procurements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1c","Requirement","ECSS-Q-ST-70_0490080","Materials with long lead times or long procurement delays (versus the project schedule) shall be identified before the formal subsystem PDR. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1d","Requirement","ECSS-Q-ST-70_0490081","Procurement shall be thoroughly planned, documented and implemented in a timely manner to obtain reliable product assurance provision at CDR. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1e","Requirement","ECSS-Q-ST-70_0490082","Back-up plans shall be prepared and initiated whenever there is evidence of delays or technical problems.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.1f","Requirement","ECSS-Q-ST-70_0490083","The material requirements shall be explicitly accepted by the material supplier or manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.2a","Requirement","ECSS-Q-ST-70_0490084","All materials shall be submitted to an incoming inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.6.2b","Requirement","ECSS-Q-ST-70_0490085","An incoming inspection procedure shall define the inspections and tests to be carried out, particularly for materials that are known to be variable in their final properties.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.1a","Requirement","ECSS-Q-ST-70_0490086","The supplier shall verify that all critical materials are validated before being used in the manufacture of qualification or flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.1b","Requirement","ECSS-Q-ST-70_0490087","Any modification, change of condition or configuration of application shall lead to a re-evaluation in conformance with the process shown in Figure 4-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.2a","Requirement","ECSS-Q-ST-70_0490088","The supplier shall apply the traceability rules defined in ECSS-Q-ST-20 to all materials.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.2b","Recommendation","ECSS-Q-ST-70_0490196","Materials should be identified by a unique reference number, code or a lot number to provide traceability should there be an incident or nonconformance, or a need for a technical investigation following failure or damage, to reconstruct the materials history, either individually (individual traceability) or by the manufacturing lot of which it was a part (lot traceability).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.3a","Requirement","ECSS-Q-ST-70_0490090","The supplier shall define provisions for packaging, storage and removal from storage for materials.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.3b","Requirement","ECSS-Q-ST-70_0490091","Measurements and inspections used to guarantee the material integrity and monitoring during storage and removal from storage shall be identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.4a","Requirement","ECSS-Q-ST-70_0490092","The supplier shall ensure that all materials which have limited-life characteristics have their date of manufacture (when available, otherwise date of delivery) and shelf-life expiry date accurately identified and clearly marked on each lot or batch.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.4b","Permission","ECSS-Q-ST-70_0490197","Materials which have exceeded their shelf-life expiry date may be re-certified only after the physical and chemical characteristics are inspected and the parameters, subject to deterioration, are evaluated for continued acceptability according to the accept and reject criteria in conformance with ECSS-Q-ST-70-22.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.5a","Requirement","ECSS-Q-ST-70_0490094","Materials with limited-life after implementation (such as propellant) shall be identified and controlled in conformance with ECSS-Q-ST-10-04.\n    NOTE Storage and mission life are criteria for the assessment and control of those materials.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.6a","Requirement","ECSS-Q-ST-70_0490095","Nonconformances and alerts shall be managed in conformance with ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","5.7.7a","Requirement","ECSS-Q-ST-70_0490096","Material safety data sheet or equivalent shall be available for all materials.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.1a","Requirement","ECSS-Q-ST-70_0490097","The supplier shall verify that all materials and processes used in the manufacture of parts satisfy the mission technical requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.2a","Requirement","ECSS-Q-ST-70_0490098","Parts shall be chosen from those successfully used for an identical application in other space programmes similar with respect to environment constraints and lifetime whenever those parts exist.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.2b","Requirement","ECSS-Q-ST-70_0490099","Type reduction actions shall be implemented at all levels of the programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.2c","Requirement","ECSS-Q-ST-70_0490100","Whether the parts are already qualified or remain to be qualified, their selection shall take into account the following criteria:\n    1. durability of supply;\n    2. reproducibility of characteristics.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.3a","Requirement","ECSS-Q-ST-70_0490101","The supplier shall establish and maintain a declared mechanical parts list in conformance with Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.4.2a","Requirement","ECSS-Q-ST-70_0490102","The supplier shall analyse all the parts contained in their preliminary lists with respect to criticality and in correlation with the risk analyses performed in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.4.2b","Requirement","ECSS-Q-ST-70_0490103","Critical parts shall be identified in the DMPL and included in the critical items list.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.4.2c","Requirement","ECSS-Q-ST-70_0490104","Any critical part shall be the subject of a RFA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.1a","Requirement","ECSS-Q-ST-70_0490105","Depending on the results of the criticality analysis, the supplier shall perform an evaluation phase before the validation phase for all critical parts with unknown characteristics or with major changes in the use or in the configuration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.1b","Permission","ECSS-Q-ST-70_0490198","In case of an extension of an existing application, the evaluation indicated in 6.5.1a need not be performed if so agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.1c","Requirement","ECSS-Q-ST-70_0490107","Guarantied characteristics of materials and material supplier inspection methods, together with associated documents, shall be available for review at the suppliers premises before the start of evaluation or qualification phases.\n    NOTE Refer to Table 4-1 for an explanation of the steps involved.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.2a","Requirement","ECSS-Q-ST-70_0490108","The evaluation shall consider the following, as a minimum, for each critical part:\n    1. the limits of use,\n    2. the part’s physical or functional characteristics, along with its values and tolerances,\n    3. behavioural tendencies and degradation processes depending on environment parameters (including sensitivity to pollution), and\n    4. acceptance criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.2b","Requirement","ECSS-Q-ST-70_0490109","When an evaluation is performed an evaluation programme (available at PDR) shall be drawn up, implemented, and an evaluation report (available before CDR) shall be drawn up.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.2c","Requirement","ECSS-Q-ST-70_0490110","The behaviour of the parameters to be monitored which were also recorded during the evaluation programme tests, shall serve as a reference for the analysis of qualification test results.\n    NOTE Example of such behaviour is variation and change over time.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.3a","Requirement","ECSS-Q-ST-70_0490111","For each critical part a qualification programme shall be drawn up by the supplier (of the equipment using the critical part) and then implemented to check or confirm whether the parts satisfy mission requirements with appropriate margins.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.3b","Requirement","ECSS-Q-ST-70_0490112","Qualification status shall depend on the results obtained (qualification report) and the reviews of corresponding documentation (available at CDR).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.4a","Requirement","ECSS-Q-ST-70_0490113","The mechanical parts shall not receive an approval identification in the declared mechanical parts list for the project unless the requirements in 6.5.2 and 6.5.3 are satisfied.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.4b","Requirement","ECSS-Q-ST-70_0490114","If approval is not granted, the supplier in charge of the item shall either:\n    1. select another mechanical part, or\n    2. propose a modified evaluation programme and resubmit for approval, or\n    3. if actions 6.5.4b.1 and 6.5.4b.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.5.5a","Requirement","ECSS-Q-ST-70_0490115","For parts not conforming to project requirements, whether at the end of criticality analysis or of evaluation and qualification tests, the supplier shall submit a request for deviation in conformance with ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.1a","Requirement","ECSS-Q-ST-70_0490116","Mechanical parts with long lead times or procurement delays (versus the project schedule) shall be identified before the subsystem PDR.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.1b","Requirement","ECSS-Q-ST-70_0490117","Procurement shall be planned, documented and implemented in a timely manner to obtain reliable product assurance provision at CDR.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.1c","Requirement","ECSS-Q-ST-70_0490118","Back-up plans shall be prepared and initiated whenever there is evidence of possible delays or technical problems.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.2a","Requirement","ECSS-Q-ST-70_0490119","Each part shall be covered by a procurement specification or a standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.2b","Requirement","ECSS-Q-ST-70_0490120","The procurement specifications shall define the part characteristics, requirements, tests methods, acceptance criteria, lot acceptance testing, source inspection (if any) and material supplier inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.2c","Requirement","ECSS-Q-ST-70_0490121","The procurement specifications shall be explicitly accepted by the part supplier or manufacturer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.3a","Requirement","ECSS-Q-ST-70_0490122","For complex parts related to a specific project development, each supplier shall define the nature and frequency of their own source inspection points. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.3b","Requirement","ECSS-Q-ST-70_0490123","Source inspection shall be carried out by the customer on the premises of the supplier (part manufacturer) in conformance with ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.4a","Requirement","ECSS-Q-ST-70_0490124","Each part or batch of parts shall be submitted to an incoming inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.6.4b","Requirement","ECSS-Q-ST-70_0490125","An incoming inspection procedure shall be established defining the inspections and tests to be carried out.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.1a","Requirement","ECSS-Q-ST-70_0490126","The supplier shall ensure that all critical parts are qualified before being used in the manufacture of qualification or flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.1b","Requirement","ECSS-Q-ST-70_0490127","Any modification, change in condition or configuration of application shall lead to a re-evaluation in conformance with the process shown in Figure 4-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.2a","Requirement","ECSS-Q-ST-70_0490128","The supplier shall apply the traceability rules defined in ECSS-Q-ST-20 to his parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.2b","Recommendation","ECSS-Q-ST-70_0490199","Parts should be identified by a unique reference number or code and a lot number to provide traceability - where there is an incident or nonconformance, or for the purposes of technical investigations following failure or damage - to reconstruct the parts history, either individually (individual traceability) or by the manufacturing lot it was part of (lot traceability).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.3a","Requirement","ECSS-Q-ST-70_0490130","The supplier shall define provisions for packaging, storage and removal from storage for parts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.3b","Requirement","ECSS-Q-ST-70_0490131","Measurements and inspections used to guarantee the part integrity and monitoring during storage and removal from storage shall be identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.4a","Requirement","ECSS-Q-ST-70_0490132","Limited-life parts after implementation or subject to wear out shall be identified and controlled, taking into account storage and mission life.\n    NOTE Examples of such parts are mechanisms, pyro initiators and O-rings.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.4b","Requirement","ECSS-Q-ST-70_0490133","Limited-life parts shall be assessed as candidates to the critical items list in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","6.7.5a","Requirement","ECSS-Q-ST-70_0490134","Management of nonconformances and alerts shall be in conformance with ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.1a","Requirement","ECSS-Q-ST-70_0490135","Each process to be used in the manufacturing or assembly of a product shall be identified by a specification or procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.1b","Requirement","ECSS-Q-ST-70_0490136","Reference shall be made to accept and reject criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.2a","Requirement","ECSS-Q-ST-70_0490137","The supplier shall verify that the materials and the mechanical parts used during the implementation of processes satisfy the requirements of this Standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.3a","Requirement","ECSS-Q-ST-70_0490138","Processes shall be chosen from those already verified according to the following order of preference and priority:\n    1. those covered by space agencies or other governmental organization certification for identical conditions of use;\n    2. those for which satisfactory evaluation and verification results are obtained on samples representative of the application with a sufficient margin as regards conditions of use;\n    3. those already successfully used by the same supplier for other space programmes in the same conditions of use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.3b","Requirement","ECSS-Q-ST-70_0490139","Whether the processes are already verified or remain to be verified, their selection shall take into account the following criteria:\n    1. reliability;\n    2. inspectability;\n    3. re-workability of the process item;\n    4. reproducibility.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.4a","Requirement","ECSS-Q-ST-70_0490140","The supplier shall establish and maintain a declared processes list in conformance with Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2a","Requirement","ECSS-Q-ST-70_0490141","The supplier shall analyse all the processes contained in their preliminary lists with respect to criticality and in correlation with the risk analyses performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2b","Requirement","ECSS-Q-ST-70_0490142","Critical processes shall be identified in the DPL and included in the list of critical items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2c","Requirement","ECSS-Q-ST-70_0490143","Any critical process shall be the subject of an RFA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2d","Requirement","ECSS-Q-ST-70_0490144","Special processes shall be identified and controlled.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2e","Requirement","ECSS-Q-ST-70_0490145","Process control shall be ensured by means of procedures or personnel certification or inline process control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.5.2f","Permission","ECSS-Q-ST-70_0490200","Whenever feasible a statistical process may be carried out.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.1a","Requirement","ECSS-Q-ST-70_0490147","Depending on the results of the criticality analysis, the supplier shall perform an evaluation phase before the validation phase for all critical processes which are new or with major changes in the use or in the configuration. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.1b","Permission","ECSS-Q-ST-70_0490201","In case of an extension of an existing application, the evaluation indicated in 7.6.1a need not be performed if so agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.1c","Requirement","ECSS-Q-ST-70_0490149","For confidential processes, the supplier shall prove that the process has been verified.\n    NOTE 1 For example, by presenting a verification certificate from space agencies or other governmental organization responsible to check the applicability of this verification.\n    NOTE 2 Refer to Table 4-1 for an explanation of the steps involved.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.2a","Requirement","ECSS-Q-ST-70_0490150","The evaluation shall consider the following as a minimum for each critical process:\n    1. the limits of use,\n    2. the values, determined by test samples or technology samples, of relevant parameters and their tolerances, and\n    3. acceptance criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.2b","Requirement","ECSS-Q-ST-70_0490151","When an evaluation is performed, the supplier shall provide \n    1. an evaluation plan at PDR and\n    2. an evaluation report before CDR.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.3a","Requirement","ECSS-Q-ST-70_0490152","For each critical process, the supplier shall implement a verification programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.3b","Requirement","ECSS-Q-ST-70_0490153","The verification programme shall be defined in conformance with existing ECSS or national agency standards of verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.3c","Requirement","ECSS-Q-ST-70_0490154","The supplier shall ensure that the processes satisfy the mission requirements and that the parameters needed for the product design are defined so as to obtain verification status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.3d","Requirement","ECSS-Q-ST-70_0490155","Verification status shall depend on the results obtained (verification report) and the review of corresponding documentation (available at CDR).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.4a","Requirement","ECSS-Q-ST-70_0490156","The processes shall not receive an approval identification in the declared processes list unless requirements in 7.6.2 and 7.6.3 are satisfied. If approval is not granted, the supplier in charge of the item shall either\n    1. select other processes, or\n    2. propose a modified evaluation programme and resubmit for approval, or\n    3. if actions 7.6.4a.1 and 7.6.4a.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.6.5a","Requirement","ECSS-Q-ST-70_0490157","For processes not conforming to project requirements, whether at the end of criticality analysis or of evaluation and verification tests, the supplier shall submit a request for deviation in conformance with ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.1a","Requirement","ECSS-Q-ST-70_0490158","The supplier shall confirm that all critical processes have been verified before being used in the manufacture of qualification or flight products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.1b","Requirement","ECSS-Q-ST-70_0490159","Any modification, change of condition or configuration of application shall lead to a re-evaluation in conformance with the process shown in Figure 4-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.2a","Requirement","ECSS-Q-ST-70_0490160","When a process needs to be re-verified, a request for approval (RFA) shall be established and a re-verification programme shall be implemented.\n    NOTE Any prolonged stoppage in manufacturing, any major change of the facilities or procedures or any transfer of production to another entity can invalidate partially or completely the initial verification of a process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.3a","Requirement","ECSS-Q-ST-70_0490161","Before implementation of a process, the supplier shall ensure that personnel are trained and that environment, means and documentation are adequate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.3b","Requirement","ECSS-Q-ST-70_0490162","This verification shall ensure that: \n    1. manufacturing and quality control tools associated with the process are adequate, calibrated and properly maintained are used under appropriate environmental and cleanliness conditions, see clause 4.4,\n    2. personnel are properly trained and certified, and\n    3. the processes specifications, manufacturing and inspection procedures and workmanship standards including clear definition of manufacturing operations and clear acceptance criteria exist.\n        NOTE 1 Photographically documented if possible for visual acceptance criteria at the appropriate work and inspection stations.\n        NOTE 2 For planning of manufacturing, assembly and integration operation and inspection see ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.4a","Requirement","ECSS-Q-ST-70_0490163","Traceability of processes shall be ensured in conformance with ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.5a","Requirement","ECSS-Q-ST-70_0490164","Nonconformances and alerts shall be processed in conformance with ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.6a","Requirement","ECSS-Q-ST-70_0490165","MIPs shall be defined in conformance with ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","7.7.7a","Requirement","ECSS-Q-ST-70_0490166","The supplier shall define provisions for packaging, storage, and removal from storage for products or semi-finished products before and after implementation of processes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","A.2.1<1>a","Requirement","ECSS-Q-ST-70_0490167","The DML shall contain the following statements:\n    1. “Materials are classified into 20 groups depending on their type or their main use, see Table A-1”.                                         \n    2. “Primers are classified in the group of their associated component.”\n    3. “Where no project requirement exists for a separate DMPL, mechanical parts are entered on the DML as a separate group with the corresponding numbers.”",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","A.2.1<1>b","Requirement","ECSS-Q-ST-70_0490168","If new groups are created, for a given project, these shall have numbers over 21.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","A.2.1<2>a","Requirement","ECSS-Q-ST-70_0490169","The DML shall include the information stated in Figure A-1, where the header information identifies the list as the declared materials list and includes the issue number and date of issue, as follows:\n    1. Item number (applicable to equipment manufacturer level only)\n        (a) This consists of the material group identifier and the user code. It takes the form of:\n<group number>.<identifier within the group>.<running number>.<user code>\n            NOTE For example: 11.5.1.KOF.\n        (b) Characteristics of the item number are:\n              - The user, identified by an agreed user code for the project.\n              - One only per material type.\n              - Does not change during the life of the materials list (sub-items are permitted when deemed necessary).\n    2. Commercial identification or standardized designation\n        (a) Enter the correct and standard designation, such as the trade name plus number.\n        (b) If no trade name exists, enter the manufacturer’s name plus number.\n        (c) For metal alloys, the Aluminium Association (AA) system is recommended for aluminium alloys, and the American Iron and Steel Institute (AISI) system for steel. For other metals or alloys, the main constituent is entered first except in the case of a traditional name.\n            NOTE For example: brass or bronze.\n        (d) For each material, as designated in A.2.1<2>a2(a) to(c), use a unique item number. If several lines are used for different applications or processing, add sub-item numbers.\n    3. Chemical nature and product type\n        (a) For metallic materials, add the condition as procured if applicable.\n            NOTE Example of such conditions are rolled and heat treatment.\n        (b) Where a semi-finished product is procured, give the relevant state. \n            NOTE Example of such state are form, plate and sheet.\n        (c) Give the thickness of the material, that can be an important parameter.\n            NOTE Examples of chemical nature are: epoxy resin, polyurethane adhesive, Ti6Al4V.\n    4. Procurement information\n        (a) Manufacturer or distributor: name of the manufacturer and name of the distributor if different.\n        (b) Procurement specification: reference of the procurement specification with issue, revision and date. It may be replaced by a national or international specification or standard, if this exists, and identifies the source of procurement, if relevant. Indication of issue or date is not applicable when datasheets are used\n    5. Processing parameters\nList here a summary of the process parameters applied by the user of the process.\n        NOTE E.g. mixture proportions, cure temperature, special cleaning agent, surface treatment, thermal treatment and temperature, and reference to specification number.\n    6. Use and location\n        (a) Use codes able to define the location of the material with respect to the:\n            • subsystem;\n            • particular piece of equipment (box or item);\n            • use of the equipment, e.g. a structural element, thermal control, electrical insulation.\n            NOTE If the CI number is not included in the list header, then a suitable abbreviation of the relevant subsystem is included.\n        (b) Include any restrictions that apply to the use of a particular material in the corresponding comment column.\n    7. Environmental code\nThe environmental code is defined using Table A-2.\n    8. Size code\nThe size code is indicated by an alphanumeric combination, such as A5, V2 or M3, as in Table A-3.\n    9. Validation references, justification for approval and prime comments and prime approval\n        (a) Make reference to relevant test data that demonstrates the acceptability of the material under the environmental conditions and the application relevant to the particular project concerned. Specifically, in column 9.1, corrosion (CORR), stress corrosion (SCC), flammability (FLAM), offgassing (OFFG) and outgassing (OUTG) data or report-references are entered.\n        (b) Use standard abbreviations to summarize the acceptance status of a material for a particular property.\n        (c) Use the justification for approval (column 9.2) and prime approval (column 9.3) columns for any additional information to obtain customer approval.\n        (d) Standard abbreviations are used to summarize the acceptability or otherwise of a material for a specific property. These are defined for the project.\n        (e) Select the supplier approval status code from Table A-4.\n    10. Customer approval status code and comments\n        (a) Select this code from Table A-4.\n        (b) Include additional comments where appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","A.2.2a","Requirement","ECSS-Q-ST-70_0490170","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","A.2.2b","Requirement","ECSS-Q-ST-70_0490171","The change record shall include a brief description of the updates which contributed to each issue or revision.\n    NOTE This DRD recommends the format and define the content within the framework of a project or a programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.1<1>a","Requirement","ECSS-Q-ST-70_0490172","The DMPL shall contain the following statements:\n“Mechanical parts are classified into 11 groups depending on their type or their main use” (see Table B-1).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.1<1>b","Requirement","ECSS-Q-ST-70_0490173","If, for a given project it is considered necessary to create new groups, these shall have numbers over 61.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.1<1>c","Recommendation","ECSS-Q-ST-70_0490202","Items that appear in the EEE parts list should not be repeated here.\n    NOTE For example, heaters, some valves, thermostats, relays, transformer coils and solenoids.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.1<2>a","Requirement","ECSS-Q-ST-70_0490175","The DMPL shall include the information in Figure B-1, where the header information identifies the list as the declared mechanical parts list and includes the issue number and date of issue, as follows:\n    1. Item number (applicable at equipment supplier level only)\n        (a) This consists of the mechanical part identifier and the user code. It takes the form of:\n<group number>.<identifier within the group>.<running number>.<user code>\n            NOTE For example: 7.2.1.ACSA.\n        (b) Characteristics of the item number are:\n             - Identify the subcontractor by an agreed user code for the project.\n             - One only per mechanical part type.\n             - Does not change during the life of the mechanical parts list.\n    2. Commercial identification\n        (a) Enter the correct and standard designation, such as trade name plus number. \n        (b) If no trade name exists then enter the manufacturers’ name and number.\n    3. Type of part\nDescribe the material and surface treatment (if applicable).\n    4. Procurement information\n        (a) Manufacturer or distributor: name of the manufacturer and name of the distributor if different.\n        (b) Procurement specification: reference of the procurement specification with issue, revision and date. It may be replaced by a national or international specification or standard if this exists and identifies the source of procurement if relevant.\n    5. Elementary function, main characteristics\n        (a) Enter the function of the mechanical part.\n        (b) Enter the main characteristics of the mechanical part.\n            NOTE For example, number of revolutions per minute for a ball bearing.\n    6. Use and location\nUse codes able to define the location of the mechanical part with respect to the:\n        (a) subsystem;\n        (b) particular piece of equipment (box or item);\n        (c) use of the equipment.\n    7. Environmental code\nThe environmental code is defined using Table B-2.\n    8. Criticality\nEnter “C” for critical or “N” for non-critical. If a mechanical part is considered critical, describe the reason for the criticality and methods of control.\n    9. Supplier reference, prime comments and prime approval status \n        (a) Use the supplier reference, prime comments and approval columns to enter any additional information that can be necessary in order to obtain customer approval.\n        (b) This information comprises reference and issue of the RFA or approval, mechanical parts justification file, evaluation reports and deviation requests.\n        (c) Make reference to the relevant test data that demonstrates acceptability of the mechanical part under the environment conditions and the application relevant to the particular project concerned. \n        (d) Use standard abbreviations, defined by the customer, to summarize the acceptance status of a mechanical part for a particular property.\n        (e) In order to justify the use of a material for flammability resistance, list here the material thickness and height of oxygen share.\n        (f) Select the prime approval status code from Table B-3.\n    10. The customer approval status code and comments\n        (a) Select this code from Table B-3.   \n        (b) Include additional comments where appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.2a","Requirement","ECSS-Q-ST-70_0490176","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","B.2.2b","Requirement","ECSS-Q-ST-70_0490177","This record shall include a brief description of the updates which contributed to each issue or revision.\n    NOTE This DRD recommends the format and defines the content within the framework of a project or a programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","C.2.1<1>a","Requirement","ECSS-Q-ST-70_0490178","The DPL shall contain the following statements:\nProcesses are classified into 17 groups depending on their type or their main use, see Table C-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","C.2.1<1>b","Requirement","ECSS-Q-ST-70_0490179","If, for a given project it is considered necessary to create new groups, these shall have numbers over 17.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","C.2.1<2>a","Requirement","ECSS-Q-ST-70_0490180","The DPL shall include the information in Figure C-1, where the header information identifies the list as the declared processes list and includes the issue number and date of issue, as follows\n    1. Item number (applicable to equipment supplier level only)\n        (a) This consists of the process identifier and the user code. It takes the form of \n<group number>.<identifier within the group>.<running number>.<user code>\n            NOTE For example: 1.2.1.SSEX\n        (b) Characteristics of the item number are:\n             - Identify the subcontractor by an agreed user code for the project.\n             - One only per process type.\n             - Does not change during the life of the process list.\n    2. Process identification\nIndicate the correct and standard identification of the process, e.g. the process name or title: bonding, coating or soldering.\n    3. Specification\n        (a) Identify the name or abbreviation of the process executor.\n        (b) Make a reference to the associated procedure, together with the issue, revision and date.\n            NOTE For example, national, international, EN, ISO, ECSS or company in-house.\n    4. Process description\nEnter here a short description of the process.\n    5. Use and location\nUse codes able to define the location of the process with respect to the:\n        (a) subsystem,\n        (b) particular piece of equipment (box or item),\n        (c) use of the equipment.\n            NOTE For example, a structural element, thermal control, electrical insulation).\n    6. This column number is not used.\n    7. Associated item numbers\nEnter the associated material list (DML) or mechanical parts list (DMPL) with the process.\n    8. Criticality\n        (a) Enter “C” for critical or “N” for non-critical.\n        (b) If a process is considered to be critical, Enter the references to the relevant RFA.\n    9. Supplier reference, prime comments and approval\n        (a) Use the supplier reference and approval columns to enter any additional information that can be necessary to obtain customer approval.\n        (b) Select the supplier approval status code from Table C-2.\n    10. The customer approval status code and comments\n        (a) Select this code from Table C-2.\n        (b) Include additional comments where appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","C.2.2a","Requirement","ECSS-Q-ST-70_0490181","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","C.2.2b","Requirement","ECSS-Q-ST-70_0490182","This record shall include a brief description of the updates which contributed to each issue or revision.\n    NOTE This DRD recommends the format and define the content within the framework of a project or a programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","D.2.1a","Recommendation","ECSS-Q-ST-70_0490203","The RFA should contain the information in Figure D-1 (pages 1 and 2), as follows:\n    1. The header information, identifying the document as a request for approval together with the project logo and project name, RFA reference, issue revision and date.\n    2. Originator\nOriginator’s name and reference.\n    3. Location\nSubsystem and equipment codes.\n    4. Item description\nBrief description of the item.\n    5. PMP information\nThe DML, DMPL or DPL item number and list reference.\n    6. Item status, including the following information:\n        (a) manufacturers’ name and qualification reference;\n        (b) suppliers’ name and qualification status;\n        (c) product or material specification;\n        (d) procurement specification;\n        (e) process or handling specification;\n        (f) other related process or handling specifications;\n        (g) verification or qualification specification;\n        (h) report on verification or qualification.\n    7. Reason for RFA\nEnter the reason for the RFA.\n    8. Application and location details\nEnter here the details of the application and exact location of the item.\nGive the reference in the CIL.\n    9. Evaluation and validation programme\nReference and details of main tests.\n    10. Subcontractor supplier approval for the first issue of the RFA.\n    11. Customer initial decision, to be entered on first issue of the RFA providing:\n        (a) the decision concerning the proposed material,\n        (b) the requirement to perform tests (deviation request as necessary), and\n        (c) the decision concerning the proposed test programme.\n    12. Customer’s and final customer’s (if applicable) signature\n    13. Justification results obtained with reference to the supplier’s validation report and conclusion.\n    14. Subcontractor supplier approval on RFA final issue.\n    15. Final approval status of the RFA by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C","D.2.2a","Requirement","ECSS-Q-ST-70_0490184","The RFA shall be completed by the supplier (parts 1 to 10, 13 and 14) and the customer (parts 11 12 and 15).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.1a","Requirement","ECSS-Q-ST-10_0360001","The supplier shall identify the personnel responsible for implementing and performing PA management and other PA disciplines.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.1b","Requirement","ECSS-Q-ST-10_0360002","The supplier shall assign a project PA manager reporting to the project manager and having unimpeded access to higher management.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.1c","Requirement","ECSS-Q-ST-10_0360003","The appointed project PA manager, irrespective of other responsibilities, shall have organizational authority to establish and implement a product assurance programme in accordance with the project product assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.1d","Requirement","ECSS-Q-ST-10_0360004","The project PA Manager shall act as the focal point of contact within the project concerning Product Assurance matters.\n    NOTE The project PA manager is referred to as “PA manager” in the rest of this document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.2a","Requirement","ECSS-Q-ST-10_0360005","The supplier shall define and document the responsibility, the authority and the interrelation of personnel who manage, perform and verify work affecting product assurance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.2b","Requirement","ECSS-Q-ST-10_0360006","The supplier shall define and document the responsibilities and the interfaces of the PA functions, either external or internal, involved in a project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.2c","Requirement","ECSS-Q-ST-10_0360007","When the supplier's PA organization delegates product assurance tasks to another organization it shall be done in a documented and controlled way monitored by the PA organization.\n    NOTE The supplier PA organization retains the responsibility towards the Customer",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.3a","Requirement","ECSS-Q-ST-10_0360008","The supplier shall identify the PA resources needed to implement the PA programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.3b","Requirement","ECSS-Q-ST-10_0360009","The supplier shall provide resources capable to perform the PA tasks identified in the PA programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.1.3c","Requirement","ECSS-Q-ST-10_0360010","Reviews and audits of the product assurance programme, of processes or of product shall be carried out by personnel not directly involved in the work being performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.2a","Requirement","ECSS-Q-ST-10_0360011","The PA manager shall interface with project management, ensuring that the contractual provision and schedule planning for the definition and phasing of PA activities are met.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.2b","Requirement","ECSS-Q-ST-10_0360012","The PA manager shall interface with risk management, configuration management, engineering, procurement and AIV for the definition and execution of tasks in which PA activities are involved.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.2c","Requirement","ECSS-Q-ST-10_0360013","The PA manager shall interface with the customer regarding all Product Assurance matters.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.2d","Requirement","ECSS-Q-ST-10_0360014","The PA manager shall interface with lower-tier suppliers regarding all Product Assurance matters.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.3a","Requirement","ECSS-Q-ST-10_0360015","The supplier shall prepare, maintain and implement a plan of the PA activities in accordance with the customer PA requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.3b","Requirement","ECSS-Q-ST-10_0360016","The Product Assurance plan shall be prepared in conformance with DRD in Annex A.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.1.3c","Requirement","ECSS-Q-ST-10_0360017","The Product Assurance plan shall be submitted to the customer for approval.\n    NOTE 1 The Product Assurance plan can refer to Clauses of the Company Quality Manual and to in-house procedures.\n    NOTE 2 Information on the schedule for delivery of PA management documents is given in Annex C",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1a","Requirement","ECSS-Q-ST-10_0360018","The PA manager shall ensure that PA disciplines are organized at the beginning of the project according to customer contractual requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1b","Requirement","ECSS-Q-ST-10_0360019","The PA manager shall ensure that the inputs used by the PA disciplines are consistent and complete, and available in line with the project schedule.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1c","Requirement","ECSS-Q-ST-10_0360020","The PA manager shall ensure that the PA disciplines perform the tasks described in the PA Plan in line with the project schedule.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1d","Requirement","ECSS-Q-ST-10_0360021","The PA manager shall ensure that the outputs produced by the PA disciplines are consistent and complete, and delivered in line with the project schedule.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1e","Requirement","ECSS-Q-ST-10_0360022","The PA manager shall ensure the application of processes defined in applicable project plans and documents. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1f","Requirement","ECSS-Q-ST-10_0360023","The PA manager shall control the quality of his supplier’s products by:\n    1. issuing product assurance requirements applicable to the supplier \n    2. ensuring the implementation of the PA requirements by the supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1g","Requirement","ECSS-Q-ST-10_0360024","The PA manager shall ensure that PA contributions to verification are defined and provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1h","Requirement","ECSS-Q-ST-10_0360025","The PA manager shall ensure that a qualification programme is defined, approved and maintained by the relevant organization.\n    NOTE Requirement for the qualification programme are addressed in ECSS-Q-ST-20, ECSS-Q-ST-60, ECSS-Q-ST-70, ECSS-E-ST-10-02 and ECSS-E-ST-10-03.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1i","Requirement","ECSS-Q-ST-10_0360026","The PA manager shall ensure that the qualification programme is implemented and the qualification results are recorded, evaluated and documented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1j","Requirement","ECSS-Q-ST-10_0360027","The PA manager shall ensure that a Qualification Status List of the programme items is maintained in conformance with Annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1k","Requirement","ECSS-Q-ST-10_0360028","The PA manager shall review and approve the achieved qualification status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.1l","Requirement","ECSS-Q-ST-10_0360029","The PA manager shall approve the product acceptance during the Acceptance or Delivery Review.\n    NOTE The PA manager approval is based on the outputs of the Acceptance or Delivery Review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.2a","Requirement","ECSS-Q-ST-10_0360030","The supplier shall report on the status and progress of the product assurance program implementation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.2b","Requirement","ECSS-Q-ST-10_0360031","The PA report shall include at least the following items for the reporting period:\n    • Progress and accomplishment of each major product assurance task including resolved and new problems, future planning of major activities and events\n    • Status of PA reviews, Audits and MIPs, Waiver requests, Non conformances (minor and major), Critical items (including mitigation action plan status), Qualification status, EEE component status, Material and processes status, Alerts status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.2c","Permission","ECSS-Q-ST-10_0360066","The PA progress report may be part of the project progress report. \n    NOTE The general contents of the project progress report are detailed in ECSS-M-ST-10 Annex E.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.3a","Requirement","ECSS-Q-ST-10_0360033","The supplier shall perform audits on his own performance to verify the implementation and effectiveness of the provisions defined in the PA plan.\n    NOTE 1 Audits can be performed by sampling on various projects or by periodic audits of the supplier quality system.\n    NOTE 2 The general contents of project audits are detailed in ECSS-M-ST-10 clause 5.2.3.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.3b","Requirement","ECSS-Q-ST-10_0360034","The supplier shall establish and maintain an audit plan for procurement activities on the project, designating the lower tier suppliers to be audited, the current status and the schedule for auditing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.3c","Requirement","ECSS-Q-ST-10_0360035","In addition to the planned audits, extra audits shall be performed when necessary to overcome failure, consistent poor quality, or other problems. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.3d","Requirement","ECSS-Q-ST-10_0360036","The supplier shall plan and perform audits using established and maintained procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.4a","Requirement","ECSS-Q-ST-10_0360037","The supplier shall establish a critical items control programme in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.4b","Requirement","ECSS-Q-ST-10_0360038","The PA manager shall identify and evaluate critical items in support of the overall project risk management activities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.4c","Requirement","ECSS-Q-ST-10_0360039","The PA manager shall ensure that a critical item control programme is implemented to eliminate or mitigate associated risks.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.5a","Requirement","ECSS-Q-ST-10_0360040","The PA manager shall ensure that the applicable issues of all documents and data are available at all locations where activities required for the implementation of the PA programme are performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.5b","Requirement","ECSS-Q-ST-10_0360041","The PA manager shall ensure that invalid or obsolete documents and data are removed from all points of issue or use, or assured against unintended use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.5c","Requirement","ECSS-Q-ST-10_0360042","The PA manager shall ensure that obsolete documents and data retained for legal or knowledge preservation purposes are identified as such.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.5d","Requirement","ECSS-Q-ST-10_0360043","The PA manager shall identify the project documents requiring approval including those requiring approval by PA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.6a","Requirement","ECSS-Q-ST-10_0360044","The supplier shall establish and maintain quality records to provide objective evidence of complete and successful performance of all PA discipline tasks and to demonstrate compliance with requirements.\n    NOTE Requirements for the storage, retrieval and archiving of quality records are addressed in ECSS-M-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.7a","Requirement","ECSS-Q-ST-10_0360045","The PA manager shall verify during Configuration Control Boards the suitability for release of drawings, plans, specifications, procedures and changes thereto.\n    NOTE The operation of Configuration Control Boards is detailed in ECSS-M-ST-40",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.7b","Requirement","ECSS-Q-ST-10_0360046","The PA manager shall ensure that:\n    1. the as designed status is defined and released prior to manufacturing;\n    2. the as-built documentation is properly defined, identified and maintained in order to reflect approved modifications; and\n    3. items delivered comply with the as-built documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.8a","Requirement","ECSS-Q-ST-10_0360047","The supplier shall establish and maintain a nonconformance control system in conformance with ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.9a","Requirement","ECSS-Q-ST-10_0360048","The supplier shall notify its customer of preliminary information on failures or problems that can result in an alert.\n    NOTE 1 The above is applicable to failure or problems detected by the supplier or by one of his lower tier suppliers.\n    NOTE 2 The above is only applicable to failures or problems meeting all of the following criteria:\n        · The item with the observed failure or problem has multiple applications, which can have implications for more than one project, thus requiring prompt action.\n        · The failure or problem has occurred in the application of an item within the specified design and usage limitations. \n        · Failures or problems due to usage within reasonably expected limits of performance, but where these limits were not specified precisely.\n        · A preliminary investigation has provided evidence of the root cause of the failure or problem.\n        · Failure or problems are confirmed not to be of a random nature.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.9b","Requirement","ECSS-Q-ST-10_0360049","The supplier shall investigate in cooperation with the originator of the failure or problem to define the immediate measures to be taken, to identify the causes, and to recommend corrective actions for similar items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.9c","Requirement","ECSS-Q-ST-10_0360050","The PA manager shall ensure:\n    1. the assessment of any failure having the potential to lead to an alert by the customer,\n    2. the investigation, until disposition of the items subject of the potential alert, and\n    3. the assessment of incoming alerts for the definition, implementation and follow-up of necessary actions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","5.2.9d","Requirement","ECSS-Q-ST-10_0360051","The supplier shall participate in the alert system organized by the customer or other sources, by:\n    1. assessment of the impact of incoming alerts to project work, and definition, implementation and follow-up of necessary corrective actions at any contractual level.\n    2. distribution of incoming alerts to the possible affected users within the project.\n        NOTE The alert system is set up for the prompt interchange of information on failures or problems which can affect more than one user, or can recur in other projects or circumstances, if no preventive actions are taken.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<1>a","Requirement","ECSS-Q-ST-10_0360052","The PAP shall introduce the purpose, objective and the reason prompting its preparation.\n    NOTE For example: programme or project reference and phase.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<2>a","Requirement","ECSS-Q-ST-10_0360053","The PAP shall list the applicable and reference documents in support of the generation of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<3.1>a","Requirement","ECSS-Q-ST-10_0360054","The PAP shall describe the organization (including responsibilities and authorities), the activities, processes and procedures to be applied by the supplier to fulfil the applicable product assurance planning requirements defined in clause 5.1 of ECSS-Q-ST-10C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<3.2>a","Requirement","ECSS-Q-ST-10_0360055","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable product assurance implementation requirements defined in clause 5.2 of ECSS-Q-ST-10C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<4>a","Requirement","ECSS-Q-ST-10_0360056","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable quality assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<5>a","Requirement","ECSS-Q-ST-10_0360057","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable dependability requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<6>a","Requirement","ECSS-Q-ST-10_0360058","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable safety requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<7>a","Requirement","ECSS-Q-ST-10_0360059","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable EEE Component requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<8>a","Requirement","ECSS-Q-ST-10_0360060","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable Material and Processes requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<9>a","Requirement","ECSS-Q-ST-10_0360061","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable Software product assurance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.1<10>a","Requirement","ECSS-Q-ST-10_0360062","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil all other applicable PA requirements not covered in the clause A.2.1<3> to clause A.2.1<9> (e.g. Security, Planetary Protection, Off-The-Shelf, Customer Furnished equipment).\n    NOTE The order of the sections is not mandatory.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.2a","Permission","ECSS-Q-ST-10_0360067","The response to this DRD may be combined with the response to the project management plan, as defined in ECSS-M-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","A.2.2b","Permission","ECSS-Q-ST-10_0360068","The response to this DRD may be performed by reference to separate discipline plans addressing some of the above clauses of this DRD.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","B.2.1a","Requirement","ECSS-Q-ST-10_0360065","The QSL shall include or refer to the following information:\n    1. Equipment designation:\n        (a) Identification of hardware by name, \n        (b) Configuration Item number and model.\n    2. Next higher assembly level :\n        (a) Identification of next higher assembly.\n    3. Manufacturer's name :\n        (a) Identification of Item Supplier.\n    4. Reference of requirements documents\n        (a) Reference numbers of applicable requirement specifications.\n    5. Design heritage:\n        (a) Specify if the design is “New”, otherwise identification of the project in which the design was used.\n        (b) Summary of current qualification status:\n            • Basis for qualification (qualification test results, heritage, and qualification on other projects) programme on which the qualification test was conducted;\n            • Project on which the test was conducted.\n    6. Proposed category A, B, C, or D (related to Design heritage):\n        NOTE Qualification approach as defined in the ECSS-E-ST-10-02.\n    7. Reference of Qualification plan document:\n        (a) Current qualification status/screening and applicability of qualification test versus requirements.\n        (b) Reference numbers of Qualification Plan(s).\n        (c) Identification of developments models (EM, EQM, QM, PFM) to be manufactured and tested for the project.\n    8. Reports:\n        (a) Reference to Verification Control Document and/or reference to Analyses, Test and Inspection Reports;\n        (b) Qualification Authority: Organization in charge of the item qualification (if any).\n    9. The qualification status:\n        • QUALIFIED,\n        • TO BE QUALIFIED,\n        • QUALIFICATION IN PROGRESS\n    10. Open Actions / Due dates/Remarks:\n        (a) For an open action: summary of missing qualification actions and planned dates for the closure of such actions.\n        (b) List of major NCRs and associated waivers to the qualification items",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10C","B.2.2a","Permission","ECSS-Q-ST-10_0360069","The form may be a table which contains the here above information of B.2.1 or reference to separate document.\n    NOTE An example of such a table is shown in Figure B-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.1a","Requirement","ECSS-Q-ST-30_0410001","The dependability assurance shall be implemented by means of a systematic process for specifying requirements for dependability and demonstrating that these requirements are achieved. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.1b","Requirement","ECSS-Q-ST-30_0410002","The dependability assurance process shall be in conformance with the dependability assurance programme plan for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.2a","Requirement","ECSS-Q-ST-30_0410003","The supplier shall coordinate, implement and integrate the dependability programme management with the PA programme management.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3a","Requirement","ECSS-Q-ST-30_0410004","The supplier shall develop, maintain and implement a dependability plan for all project phases in conformance with the DRD in Annex C.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3b","Requirement","ECSS-Q-ST-30_0410005","The plan shall address the applicable requirements of this document.\n    ","NOTE The plan can be included in the PA programme plan.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3c","Requirement","ECSS-Q-ST-30_0410006","The extent that dependability assurance is applied shall take account of the severity (as defined in Table 5-1) of the consequences of failures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3d","Requirement","ECSS-Q-ST-30_0410007","The establishment and implementation of the dependability programme plan shall be considered in conjunction with the safety aspects of the programme. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3e","Requirement","ECSS-Q-ST-30_0410008","The Supplier shall ensure that any potential conflict between dependability and safety requirements are managed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.3f","Requirement","ECSS-Q-ST-30_0410009","Responsibilities for carrying out all dependability tasks within each phase of the lifecycle shall be defined.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.4a","Requirement","ECSS-Q-ST-30_0410010","As part of the risk management process implemented on the project, the Dependability engineer shall be responsible for identifying and reporting dependability associated risks .\n    ","NOTE ECSS-M-ST-80 describes the risk management process.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.4b","Requirement","ECSS-Q-ST-30_0410011","Dependability risk analysis reduction and control shall include the following steps:\n    1. identification and classification of undesirable events according to the severity of their consequences;\n    2. analysis of failure scenarios, determination of related failure modes, failure origins or causes;\n    3. classification of the criticality of the functions and associated products according to the severity of relevant failure consequences;\n    4. definition of actions and recommendations for detailed risk assessment, risk elimination, or risk reduction and control to an acceptable level;\n    5. status of risk reduction and risk acceptance;\n    6. implementation of risk reduction;\n    7. verification of risk reduction and assessment of residual risks.\n        ","NOTE The process of risk identification and assessment implies both qualitative and quantitative approaches.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.4c","Requirement","ECSS-Q-ST-30_0410012","Risk reduction measures that are proposed for dependability shall be assessed at system level in order to select the optimum solution to reduce the system level risk.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.5a","Requirement","ECSS-Q-ST-30_0410013","Dependability critical items shall be identified by dependability analyses performed to support the risk reduction and control process performed on the project. \n    ","NOTE The criteria for identifying dependability critical items are given in clause 6.5.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.5b","Requirement","ECSS-Q-ST-30_0410014","Dependability critical items, as part of the Critical Items List, shall be subject to risk assessment and critical items control in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.5c","Requirement","ECSS-Q-ST-30_0410015","The control measures shall include:\n    1. a review of all design, manufacturing and test documentation related to critical functions, critical items and procedures;\n    2. dependability representation on relevant Review Boards to ensure that the disposition takes account of their criticality level.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.5d","Requirement","ECSS-Q-ST-30_0410016","The dependability aspects shall be considered during the entire verification process for dependability critical items until closeout.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.6a","Requirement","ECSS-Q-ST-30_0410017","The supplier shall ensure that all dependability data for a design review are presented to the customer in accordance with the project review schedule. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.6b","Requirement","ECSS-Q-ST-30_0410018","All dependability data submitted shall indicate the design baseline and shall be coherent with all other supporting technical documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.6c","Requirement","ECSS-Q-ST-30_0410019","All design changes shall be assessed for their impact on dependability and a reassessment of the dependability shall be performed",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.7a","Requirement","ECSS-Q-ST-30_0410020","Dependability lessons learnt shall be collected during the project life cycle including operational and disposal phases.\n    ","NOTE Dependability lessons learnt consider:\n        · the impact of newly imposed requirements;\n        · assessment of all malfunctions, anomalies, deviations and waivers;\n        · effectiveness of strategies of the project;\n        · new dependability tools and methods that have been developed or demonstrated;\n        · effective versus ineffective verifications that have been performed.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.8a","Requirement","ECSS-Q-ST-30_0410021","The supplier shall report dependability progress to the customer as part of product assurance activities in conformance with ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","4.9a","Requirement","ECSS-Q-ST-30_0410022","The supplier shall maintain all data used for the dependability programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.1a","Requirement","ECSS-Q-ST-30_0410023","Dependability shall be integrated as part of the design process. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.1b","Requirement","ECSS-Q-ST-30_0410024","The dependability characteristics shall be traded off with other system attributes such as mass, size, cost and performance during the optimization of the design in all phases of the project. \n    ","NOTE Dependability is an inherent characteristic of a system or product.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.1c","Requirement","ECSS-Q-ST-30_0410025","Manufacture, assembly, integration, test and operations shall not degrade dependability attributes introduced into the design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.2a","Requirement","ECSS-Q-ST-30_0410026","The dependability requirement specification shall be part of the overall project requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.2b","Requirement","ECSS-Q-ST-30_0410027","Dependability requirements shall be apportioned, in a top-down process, to establish dependability requirements for lower level elements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.2c","Requirement","ECSS-Q-ST-30_0410028","Dependability requirements shall be applied during the preparation and review of design and test specifications. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.2d","Requirement","ECSS-Q-ST-30_0410029","The dependability requirements shall be included into the technical specifications. \n    ","NOTE The technical specifications typically include:\n        · functional, operational and environmental requirements,\n        · test requirements including stress levels, test parameters, and accept or reject criteria,\n        · design performance margins, derating factors, quantitative dependability requirements, and qualitative dependability requirements (identification and classification of undesirable events), under specified environmental conditions,\n        · the identification of human factors and how they can influence dependability during the project lifecycle,\n        · the identification of external, internal and installation factors that can influence dependability during the project lifecycle, \n        · the degree of tolerance to hardware failures or software malfunctions, \n        · the detection, isolation, diagnosis, and recovery of the system from failures and its restoration to an acceptable state,\n        · the requirement for the prevention of failures crossing interfaces with unacceptable consequences,\n        · definition of the maintenance concept,\n        · maintenance tasks and requirements for special skills, \n        · requirements for preventive maintenance, special tools, and special test equipment,\n        · requirements for process and technology margin demonstration and qualification,\n        · requirement on sampling strategy in serial production and for periodical demonstration of qualification preservation.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.1a","Requirement","ECSS-Q-ST-30_0410030","The identification of critical areas of design and the assessment of the severity of failure consequences shall be interpreted by the level at which the analysis is made. \n    ","NOTE The Space System level can be broken down into Space Segment and Ground Segment where separate requirements can be provided. The Space Segment and Ground Segment can be further broken down, dependant on particular contractual requirements, into lower levels elements (e.g. subsystem, equipment…). ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.1b","Requirement","ECSS-Q-ST-30_0410031","The success criteria (sometimes referred to as “mission success criteria”) shall be defined at each level to be analysed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.2a","Requirement","ECSS-Q-ST-30_0410032","A severity classification (either severity name or level) shall be assigned in accordance with Table 5-1 to each identified failure mode analysed according to the failure effect (consequence). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.2b","Requirement","ECSS-Q-ST-30_0410033","Severity categories shall be assigned without consideration of existing compensating provisions to provide a qualitative measure of the worst potential consequences resulting from item failure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.2c","Requirement","ECSS-Q-ST-30_0410034","For analyses lower than system level, the severity due to possible failure propagation shall be identified as level 1 for dependability. \n    ","NOTE For example, for analysis at subsystem, and equipment level",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.2d","Requirement","ECSS-Q-ST-30_0410035","The number identifying the severity category shall be followed by a suffix to indicate either redundancy (R) single point failures (SP) or safety hazards (SH).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.2e","Requirement","ECSS-Q-ST-30_0410036","An understanding to these criteria identified in table 1 shall be agreed between customer and supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.3a","Requirement","ECSS-Q-ST-30_0410037","Failure tolerance requirements shall be defined in the performance specifications.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.3b","Requirement","ECSS-Q-ST-30_0410038","The verification of the failure tolerance shall address all failure modes whose severity of consequence is classified as catastrophic, critical and major.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.4a","Requirement","ECSS-Q-ST-30_0410039","The supplier shall confirm that reliability is built into the design using fault tolerance and design margins. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.4b","Requirement","ECSS-Q-ST-30_0410040","The supplier shall analyse the failure characteristics of systems in order to identify areas of design weakness and propose corrective solutions. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.3.4c","Requirement","ECSS-Q-ST-30_0410041","In order to implement dependability aspects into the design, the following approaches shall apply:\n    1. functional design:\n        (a) the preferred use of software designs or methods that have performed successfully in similar applications\n        (b) the implementation of failure tolerance;\n        (c) the implementation of fault detection, isolation and recovery, allowing proper failure processing by dedicated flight and ground measures, and considering detection or reconfiguration times in relation with propagation times of events under worst case conditions;\n        (d) the implementation of monitoring of the parameters that are essential for mission performance, considering the failure modes of the system in relation to the actual capability of the detection devices, and considering the acceptable environmental conditions to be maintained on the product.\n    2. physical design:\n        (a) the application of proven design rules;\n        (b) the selective use of designs that have performed successfully in the same intended mission environment;\n        (c) the selection of parts having a quality level in accordance with project specification;\n        (d) the use of EEE parts derating and stress margins for mechanical parts;\n        (e) the use of design techniques for optimising redundancy (while keeping system design complexity as low as possible);\n        (f) the assurance that built-in equipment can be inspected and tested;\n        (g) the provision of accessibility to equipment.\n            ","NOTE Functional design is intended to imply non-physical design which includes software. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.4a","Requirement","ECSS-Q-ST-30_0410042","During the preliminary design phase, the contractor shall classify functions, operations and products in accordance with their criticality level.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.4b","Requirement","ECSS-Q-ST-30_0410043","Classification shall be approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.4c","Requirement","ECSS-Q-ST-30_0410044","The criticality of functions (hardware and/or software) and operations shall be directly related to the severity of the consequences resulting from failure of the function as defined in Table 5-1.\n    ","NOTE For example, a function whose failure induces a catastrophic consequence is required to be classified with the highest criticality level.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.4d","Requirement","ECSS-Q-ST-30_0410045","The criticality of a product (hardware and software) shall be identified at the highest criticality of the functions associated to that product.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.4e","Requirement","ECSS-Q-ST-30_0410046","The classification shall be used to focus efforts on the most critical areas during the project phases.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.5a","Requirement","ECSS-Q-ST-30_0410047","The supplier shall ensure that dependability aspects are covered in all development, qualification and acceptance test planning and reviews, including the preparation of test specifications and procedures and the evaluation of test results. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.5b","Requirement","ECSS-Q-ST-30_0410048","The dependability discipline shall support:\n    1. definition of test characteristics and test objectives,\n    2. selection of measurement parameters, and\n    3. statistical evaluation of test results.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.6a","Requirement","ECSS-Q-ST-30_0410049","The supplier shall ensure that dependability cognizant and qualified staff:\n    1. contribute to definition of operations manual and procedures, \n    2. review operations manual and procedures for verification of consistency with dependability analyses.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.6b","Requirement","ECSS-Q-ST-30_0410050","Procedures for operations shall be analysed to identify and assess the risks associated with operations, sequences and situations that can affect dependability performance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.6c","Requirement","ECSS-Q-ST-30_0410051","The analyses mentioned in 5.6b shall take into account the technical and human environment, and verify that the procedures:\n    1. include dispositions to face abnormal situations and supply the necessary safeguard measures;\n    2. do not compromise equipment reliability;\n    3. are in accordance with established maintenance dispositions; \n    4. include dispositions to minimize failures due to human errors.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.7a","Requirement","ECSS-Q-ST-30_0410052","The supplier shall establish and maintain a system to track the dependability recommendations, in order to support the risk reduction process. \n    ","NOTE These recommendations are derived from the dependability analyses, and trade-off studies (typically during Phases A and B). The dependability recommendations can be tracked in combination with safety recommendations.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.7b","Requirement","ECSS-Q-ST-30_0410053","All recommendations from 5.7a shall be justified, documented and tracked.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.7c","Requirement","ECSS-Q-ST-30_0410054","Formal evidence of acceptance or rejection of the recommendation by the supplier’s management shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","5.7d","Requirement","ECSS-Q-ST-30_0410055","An accepted dependability recommendation shall be implemented into the relevant corresponding documentation .\n    ","NOTE Example of corresponding documentation are: design documents, and operation manuals.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.1a","Requirement","ECSS-Q-ST-30_0410056","The supplier shall identify undesirable events that lead to the loss or degradation of product performances, together with their classification into categories related to the severity of their failures consequences (see Table 5-1).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.1b","Requirement","ECSS-Q-ST-30_0410057","Preliminary identification and classification of undesirable events shall be determined from analysis of criteria for mission success, during conceptual and preliminary design phases. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.1c","Requirement","ECSS-Q-ST-30_0410058","All undesirable events, whose occurrence can jeopardize, compromise, or degrade the mission success shall be assessed at the highest product level (overall system including space and ground segments). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.1d","Requirement","ECSS-Q-ST-30_0410059","The undesirable events, at lower levels of the product tree, shall be the product failure effects which can induce the undesirable events identified for the highest product level. \n    ","NOTE For example, at space segment, ground segment, subsystem, and equipment level.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.1e","Requirement","ECSS-Q-ST-30_0410060","Identification and classification of undesirable events shall be finalised after assessment of failure scenarios (see clause 6.2).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.2a","Requirement","ECSS-Q-ST-30_0410061","The supplier shall analyse the possible scenarios leading to the occurrence of undesirable events, ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.2b","Requirement","ECSS-Q-ST-30_0410062","The supplier shall identify failure modes, failure origins and causes, detailed failure effects leading to undesirable events.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.3a","Requirement","ECSS-Q-ST-30_0410063","Dependability analyses shall be performed on all space projects throughout the project life cycle to support the tasks and requirements specified in clause 5.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.3b","Requirement","ECSS-Q-ST-30_0410064","Dependability analyses shall be performed initially to contribute to the definition of the conceptual design and the system requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.3c","Requirement","ECSS-Q-ST-30_0410065","The analyses shall be performed to support the conceptual, preliminary and detailed development and optimization of the design, including the testing phase that leads to design qualification. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.3d","Requirement","ECSS-Q-ST-30_0410066","Dependability analyses shall be implemented in order to:\n    1. ensure conformance to reliability, availability and maintainability requirements, and\n    2. identify all potential failure modes and technical risks with respect to functional requirements that can lead to non-compliance to the dependability requirements, \n    3. provide inputs to risk assessment and risk reduction and their control measures in line with the risk management process implemented on the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.3e","Requirement","ECSS-Q-ST-30_0410067","The results of dependability analyses shall be incorporated into the design justification file in order to support improvements to the design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.1a","Requirement","ECSS-Q-ST-30_0410068","Dependability analyses shall be conducted on all levels of the space system and be performed in respect of the level that is being assessed i.e. System, Subsystem and Equipment levels.\n    ","NOTE The main purpose of all dependability analyses is to improve the design by providing timely feedback to the designer, to reduce risks within the processes used to realize the products and to verify conformance to the specified dependability requirement.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.1b","Requirement","ECSS-Q-ST-30_0410069","The analyses identified in clauses 6.4.2 to 6.4.4 shall be:\n    1. conducted as required by the contract, \n    2. tailored to match the generic requirements on each project, \n    3. taking into account the hardware, software and human functions comprising the system. \n        ","NOTE As it is not possible to quantitatively assess the software functions, only a qualitative assessment can be made as the dependability of software is influenced by the software development process.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.1c","Requirement","ECSS-Q-ST-30_0410070","A set of analyses selected from clauses 6.4.2 to 6.4.4 shall be defined as part of the contract requirement.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.1a","Requirement","ECSS-Q-ST-30_0410071","Reliability prediction techniques shall be used with the following objectives:\n    1. to optimize the reliability of a design against competing constraints such as cost and mass, \n    2. to predict the in–service reliability of a product,\n    3. to provide failure probability data for purposes such as risk assessment. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.1b","Requirement","ECSS-Q-ST-30_0410072","The reliability data sources and methods used in reliability predictions shall be as specified by the customer. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.1c","Requirement","ECSS-Q-ST-30_0410073","If the reliability data sources and methods are not specified by the customer, the supplier shall justify the selected data sources and methods used, for customer approval. \n    ","NOTE ECSS-Q-HB-30-08 is a guideline for the selection of reliability data sources and their use.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.1d","Requirement","ECSS-Q-ST-30_0410074","Reliability models shall be prepared to support predictions and FMEA/FMECA. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2a","Requirement","ECSS-Q-ST-30_0410075","Failure Modes and Effects Analysis (FMEA) / Failure Modes, Effects and Criticality Analysis (FMECA) shall be performed on the functional and physical design (Functional FMECA and Product FMECA respectively) and, if required by the contract, the processes used to realize the final product (Process FMECA). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2b","Requirement","ECSS-Q-ST-30_0410076","All potential failure modes shall be identified and classified according to the severity (FMEA) or criticality (FMECA) of their consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2c","Requirement","ECSS-Q-ST-30_0410077","Measures shall be proposed in the analysis and introduced in the product design and in the control of processes to render all such consequences acceptable to the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2d","Requirement","ECSS-Q-ST-30_0410078","When any design or process changes are made, the FMEA/FMECA shall be updated and the effects of new failure modes introduced by the changes shall be assessed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2e","Requirement","ECSS-Q-ST-30_0410079","Provisions for failure detection and recovery actions shall be identified as part of the FMEA/FMECA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2f","Requirement","ECSS-Q-ST-30_0410080","The FMEA/FMECA shall be used to support the verification of the reliability modelling, the reliability and safety analyses, maintainability analysis, logistic support activity, test and maintenance planning, and the Failure Detection, Isolation and Recovery (FDIR) policy.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.2g","Requirement","ECSS-Q-ST-30_0410081","As part of the FMEA/FMECA, potential failure propagation shall be assessed.\n    ","NOTE For FMEA/FMECA refer to ECSS-Q-ST-30-02.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.3a","Requirement","ECSS-Q-ST-30_0410082","HSIA shall be performed to ensure that the software reacts in an acceptable way to hardware failure. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.3b","Requirement","ECSS-Q-ST-30_0410083","HSIA shall be performed at the level of the technical specification of the software. \n    ","NOTE HSIA can be included in the FMEA/FMECA (refer to ECSS-Q-ST-30-02).",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.4a","Requirement","ECSS-Q-ST-30_0410084","Contingency analysis shall be performed in conformance with Annex D in order to:\n    1. identify the failure, identify the cause, control the effect and indicate how recovery of the mission integrity can be achieved\n    2. identify the methods of recovery of the nominal or degraded functionalities, with respect to project dependability policy,\n        ","NOTE 1 For example, availability targets.\nNOTE 2 The contingency analysis is typically a system level task.\nNOTE 3 FMEA/FMECA is an input to contingency analysis.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.5a","Requirement","ECSS-Q-ST-30_0410085","A Fault Tree Analysis shall be performed to ensure that the design conforms to the failure tolerance requirements for combinations of failures. \n    ","NOTE 1 ECSS-Q-ST-40-12 is a guideline for FTA.\nNOTE 2 The system supplier performs FTA to identify possible event combinations leading to the undesirable end event (e.g. “loss of mission”). Subsystem supplier provides input to this activity by establishing FTA at subsystem level with respect to the top events:\n        · loss of function of the subsystem, and\n        · inadvertent activation of the subsystem function.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.6a","Requirement","ECSS-Q-ST-30_0410086","Common-cause analyses shall be performed on reliability and safety critical items in conformance with Annex I, to identify the root cause of failures that have a potential to negate failure tolerance levels (see clause 5.3.3). \n    ","NOTE 1 The analyses can be accomplished as part of FMEA/FMECA or FTA. \nNOTE 2 An example of check list of generic common-cause parameters is provided in Annex L                                                 ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.7a","Requirement","ECSS-Q-ST-30_0410087","Worst case analysis shall be performed on electrical equipment in conformance with Annex J, to demonstrate that it performs within specification despite variations in its constituent part parameters and the imposed environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.7b","Requirement","ECSS-Q-ST-30_0410088","The WCA report shall contain all baseline information (assumptions, methods and techniques) used for the preparation of the analysis, the results obtained and a comparison of the specified parameters as derived from the specification of the equipment or module.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.7c","Requirement","ECSS-Q-ST-30_0410089","If not specified in the project requirement, the supplier shall propose the component aging parameter drifts for customer approval.\n    ","NOTE 1 The document ECSS-Q-TM-30-12 is a source for component aging parameter drifts, but is to be complemented with others inputs as it does not cover exhaustively the EEE parts.\nNOTE 2 ECSS-Q-HB-30-01 describes the WCA methodology.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.8a","Requirement","ECSS-Q-ST-30_0410090","Part derating shall be implemented in conformance with ECSS-Q-ST-30-11 to assure that the stress levels applied to all EEE parts are within the limits. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.8b","Requirement","ECSS-Q-ST-30_0410091","Part stress analyses shall be performed at part level to verify that the derating rules have been implemented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.9a","Requirement","ECSS-Q-ST-30_0410092","Zonal analysis shall be performed in conformance with Annex G, in order to evaluate the consequences due to potential subsystem-to-subsystem interactions inherent in the system installation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.2.10a","Requirement","ECSS-Q-ST-30_0410093","FDIR analysis shall be performed at System level in conformance with Annex F, to ensure that the autonomy and failure tolerance requirements are fulfilled.\n    ","NOTE ECSS-E-ST-70-11 provides the description of FDIR process.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.3a","Requirement","ECSS-Q-ST-30_0410094","Maintainability requirements shall be apportioned to set maintainability requirements for lower level products to conform to the maintenance concept and maintainability requirements of the system.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.3b","Requirement","ECSS-Q-ST-30_0410095","Maintainability prediction shall be performed at system level in conformance with Annex H, and used as a design tool to assess and compare design alternatives with respect to specified maintainability quantitative requirements:\n    1. the time to diagnose (i.e. detect and isolate) item failures,\n    2. the time to remove and replace the defective item, \n    3. the time to return the system or subsystem to its nominal configuration and to perform the necessary checks, and\n    4. the item failure rates. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.3c","Requirement","ECSS-Q-ST-30_0410096","Preventive maintenance analysis shall be performed at system level to determine the maintenance plan. \n    ","NOTE Each preventive maintenance action is based on the results of the application of systematic decision logic approved by the customer.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.3d","Requirement","ECSS-Q-ST-30_0410097","The maintainability analysis shall identify maintainability critical items.\n    ","NOTE Maintainability critical items include:\n        · products that cannot be checked and tested after integration, \n        · limited-life products, \n        · products that do not meet, or cannot be validated as compliant to the maintainability requirements.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.4a","Requirement","ECSS-Q-ST-30_0410098","The supplier shall perform availability analysis or simulations in order to assess the availability of the system. \n    ","NOTE The results are used to:\n        · optimize the system concept with respect to design, operations and maintenance,\n        · verify conformance to availability requirements, \n        · provide inputs to estimate the overall cost of operating the system.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.4b","Requirement","ECSS-Q-ST-30_0410099","The supplier shall perform an analysis of outages in order to supply input data for availability analysis. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.4c","Requirement","ECSS-Q-ST-30_0410100","The availability analysis output shall include a list of all potential outages identified (as defined in the project), their causes, probabilities of occurrence and duration. \n    ","NOTE Instead of outage probabilities, failure rates associated with outages can be provided.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.4d","Requirement","ECSS-Q-ST-30_0410101","The means of outage detection and the recovery methods shall be identified in the analysis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.4.4e","Requirement","ECSS-Q-ST-30_0410102","The availability analysis shall be carried out at system level using the system reliability and maintainability models as well as the data from the outages. \n    ","NOTE For availability analysis, refer to ECSS-Q-ST-30-09.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5a","Requirement","ECSS-Q-ST-30_0410103","The Dependability critical items identified by the dependability analyses shall be documented in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5b","Requirement","ECSS-Q-ST-30_0410104","Items identified as single-point failure with at least a failure consequence severity classified as catastrophic, critical or major, shall be included in the dependability critical items list.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5c","Requirement","ECSS-Q-ST-30_0410105","Items that have a criticality number greater than or equal to 6 shall be included in the dependability critical items list in conformance with ECSS-Q-ST-30-02.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5d","Requirement","ECSS-Q-ST-30_0410106","All items that have failure consequences classified as catastrophic shall be included in the dependability critical items list.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5e","Requirement","ECSS-Q-ST-30_0410107","Products that cannot be checked and tested after integration, limited–life products, products that do not meet - or cannot be verified as meeting - applicable maintainability requirements, shall be included in the dependability critical items list.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","6.5f","Requirement","ECSS-Q-ST-30_0410108","The documentation for each dependability critical item shall include a justification for retention of that item and be subject to approval by the customer.\n    ","NOTE Further criteria for the classification of dependability critical items can be specified by the customer in line with the risk management policy defined on the project.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","7.1a","Requirement","ECSS-Q-ST-30_0410109","Reliability testing and demonstration shall be performed according to the project requirements in order to:\n    1. validate failure modes and effects,\n    2. check failure tolerance, failure detection and recovery,\n    3. obtain statistical failure data to support predictions and risk assessment,\n    4. consolidate reliability assessments,\n    5. validate the capability of the hardware to operate with software or to be operated by a human being in accordance with the specifications,\n    6. demonstrate the reliability of critical items, and\n    7. validate or justify data bases used for theoretical demonstrations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","7.2a","Requirement","ECSS-Q-ST-30_0410110","Availability testing and demonstration shall be performed according to the project requirements in order to validate or justify data bases used for theoretical demonstrations (duration of outages and probability of occurrence).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","7.3a","Requirement","ECSS-Q-ST-30_0410111","Maintainability demonstration shall be performed by performing the verification of the applicable maintainability requirements and by ensuring that preventive and corrective maintenance activities are successfully performed within the scope of the maintenance concept. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","7.3b","Requirement","ECSS-Q-ST-30_0410112","“The maintainability demonstration” shall verify the ability to:\n    1. detect, diagnose and isolate each faulty line replaceable unit or orbit replaceable unit;\n    2. remove and replace each line replaceable unit or orbit replaceable unit;\n    3. perform mission-essential repairs on units that are not intended to be replaced;\n    4. check that the product is fully functional after maintenance actions have been completed;\n    5. demonstrate that no safety hazard is introduced as a result of maintenance actions;\n    6. demonstrate that the maintenance operations can be performed within the applicable constraints, including the operations necessary to prepare a system during the launch campaign \n        ","NOTE 1 xample of such a constraints are time and volume or accessibility. \nNOTE 2 Example of such operations are “remove-before-flight” items or replacement of batteries. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","7.4a","Requirement","ECSS-Q-ST-30_0410113","Dependability data as specified in the contract, shall be collected for a period agreed with the customer from sources such as non-conformance and problem or failure reports, and maintenance reports. \n    ","NOTE Dependability data can be used for dependability performances monitoring through agreed or specified models. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","C.7a","Requirement","ECSS-Q-ST-30_0410114","The dependability plan shall include as a minimum:\n    • list of the applicable and reference documents,\n    • applicable dependability requirements,\n    • description of the dependability organisation and management,\n    • contractor / supplier management,\n    • details of the dependability tasks for each phase,\n    • dependability activities status reporting.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","D.7a","Requirement","ECSS-Q-ST-30_0410115","The contingency analysis document shall include:\n    • a description of the system,\n    • a description of the method to perform contingency analysis,\n    • details of the failure detection method,\n    • details of the diagnostics,\n    • details of the recovery actions or procedures,\n    • actions and recommendations for project team.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","E.7a","Requirement","ECSS-Q-ST-30_0410116","The reliability prediction document shall include:\n    • a clear identification of the design being analysed,\n    • reliability block diagrams,\n    • the methodology used with rationales,\n    • an analysis of the results,\n    • recommendations for project decision.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","F.7a","Requirement","ECSS-Q-ST-30_0410117","The FDIR analysis document shall include:\n• a description of the system\n• a description of the method to perform FDIR (e.g. FMEA/FMECA synthesis, FDIR reviews),\n• details of considered failures,\n• symptoms of failures (e.g. TM, observables),\n• detailed failure impact on the system,\n• the recovery actions (e.g. TC, automatic on board mechanism),\n• actions and recommendations for project team.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","G.7a","Requirement","ECSS-Q-ST-30_0410118","The zonal analysis document shall include:\n    • an identification of the perimeter under investigation, \n    • a detailed definition of the interface(s),\n    • the description of the potential interaction(s),\n    • the list of actions and recommendations for project decision.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","H.7a","Requirement","ECSS-Q-ST-30_0410119","The document shall contain, as a minimum:\n    • maintenance levels: for corrective and preventive actions,\n    • identification of FDIR policy,\n    • mathematical model description,\n    • the maintenance indicators (e.g. MTTR, maintenance time per year, maintenance frequency),\n    • the sparing recommendations (e.g. number of spares, weight and volume of up and downloading spares),\n    • identification of Maintainability Critical Items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","I.7a","Requirement","ECSS-Q-ST-30_0410120","The common-cause analysis document shall include:\n    • a description of the perimeter of the design being analysed,\n    • the list of the ‘common-cause’ parameters and their effects,\n    • actions and recommendations for project team.\n\t","NOTE See check lists parameters examples in Annex L.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-30C","J.7a","Requirement","ECSS-Q-ST-30_0410121","The WCA document shall include:\n    • assumptions applicable to the environmental condition,\n    • a list of the selected parts database with the worst case parameters,\n    • a description of the general methodology, \n    • an explanation of the numerical analysis technique, \n    • results and conclusion of the WCA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.1a","Requirement","ECSS-Q-ST-40_0440001","The supplier shall establish and maintain a safety programme to assure conformance with project safety policy and requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.1b","Requirement","ECSS-Q-ST-40_0440002","The safety programme shall establish a safety management system to implement provisions of this Standard - commensurate with the programme requirements and tailored by the customer \n    NOTE 1 For tailoring, refer to clause 1                                         \n    NOTE 2 The system safety programme requirements are subject to tailoring, without diminishing the intent to protect flight and ground personnel, the launch vehicle, associated payloads, ground support equipment, the general public, public and private property, the space system and associated segments and the environment from hazards associated with space systems.\n    NOTE 3 As support to tailoring, informative Annex F provides a guideline for determining the applicability of this standard depending on the type of project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.2a","Requirement","ECSS-Q-ST-40_0440003","The supplier shall establish and maintain a safety programme plan in conformance with the DRD in Annex B.\n    NOTE The plan can either be included as part of an overall project product assurance plan or as a separate safety programme plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.2b","Requirement","ECSS-Q-ST-40_0440004","The supplier shall cover, in his safety programme plan, the safety tasks for the project phases in conformance with 5.7.1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.3a","Requirement","ECSS-Q-ST-40_0440005","The supplier shall comply with all applicable national or international safety regulations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.3b","Requirement","ECSS-Q-ST-40_0440006","The launch site safety regulations and rules shall be applied.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.3c","Requirement","ECSS-Q-ST-40_0440007","The implementation of safety requirements shall not be compromised by other requirements.\n    NOTE For example: security requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.1a","Requirement","ECSS-Q-ST-40_0440008","Each supplier shall appoint a safety manager who has appropriate training or experience.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.1b","Requirement","ECSS-Q-ST-40_0440009","The safety manager shall have organisational authority and independence to:\n    1. establish and maintain a safety programme in accordance with the project safety requirements,\n    2. manage all safety assurance aspects of the design of the system (including software) and its operation in accordance with the Safety Plan,\n    3. coordinate the interfaces:\n        (a) with the relevant bodies involved in the project in accordance with the safety plan,\n        (b) with the safety launcher authority.\n            NOTE Depending on the project safety criticality, the safety manager can be combined with other functions (e.g. PA manager) when agreed with the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.2.1a","Requirement","ECSS-Q-ST-40_0440010","The safety manager shall:\n    1. have the right of access to safety-related data relevant to project safety in conformance with ECSS-M-ST-40, \n    2. have unimpeded access to any management level without organizational constraint on any aspect of project safety.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.2.2a","Requirement","ECSS-Q-ST-40_0440011","The safety manager or safety relevant authority shall have the authority to:\n    1. reject any project document, or to stop any project activity that does not conform to approved safety requirements or procedures,\n    2. interrupt hazardous operations when it becomes clear by the Safety Manager that the operation does not conform to the agreed measures defined in the corresponding hazard report and derived approved hazard procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.3a","Requirement","ECSS-Q-ST-40_0440012","The supplier shall perform safety audits or reviews to verify compliance to project safety policy and requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.3b","Requirement","ECSS-Q-ST-40_0440013","The safety audits shall be in accordance with ECSS-M-ST-10 and ECSS-Q-ST-10.\n    NOTE The safety audits can be part of the project audits.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.3c","Requirement","ECSS-Q-ST-40_0440014","The customer shall be informed of the audit schedule.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.4a","Requirement","ECSS-Q-ST-40_0440015","Documentation related to safety shall be approved by the safety manager upon his verification of completeness, compliance with stated safety requirements and formal closeout of open safety verification items (as defined and agreed during safety audits and reviews).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.5a","Requirement","ECSS-Q-ST-40_0440016","The safety manager (or a designated representative) shall have concluded the review of, and approved, any hazardous operation before it is executed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.6a","Requirement","ECSS-Q-ST-40_0440017","The safety manager or designated delegate shall be represented at configuration control boards (CCBs), nonconformance review boards (NRBs), test review board (TRBs), and at qualification, and acceptance reviews, where safety requirements and safety-critical functions are involved.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.6b","Requirement","ECSS-Q-ST-40_0440018","The safety function shall be further represented at all boards dealing with health matters where exposure or endurance limits are defined for flight and ground crews.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.4.7a","Requirement","ECSS-Q-ST-40_0440019","The safety approval authority shall:\n    1. review and disposes the safety data submittals,\n    2. approve the close-out of hazards,\n    3. decide on deviations and waivers, and finally\n    4. accept the statement of safety compliance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.5a","Requirement","ECSS-Q-ST-40_0440020","The safety risk identification, reduction and control shall be part of the project's risk management process as specified in ECSS-M-ST-80.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.5b","Requirement","ECSS-Q-ST-40_0440021","Safety risk identification, reduction and control shall be a continuous and iterative process throughout the project life cycle, encompassing\n    1. allocation of safety requirements;\n    2. hazard and safety risk identification;\n    3. evaluation (including categorisation) of consequence severity;\n    4. hazard and safety risk reduction and control;\n    5. close out and acceptance of residual risk.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.5c","Requirement","ECSS-Q-ST-40_0440022","For the identification of hazards and associated safety risks, consideration shall be given to past experience, studies, ground and flight tests, reviews, the industrial process as well as the operational use.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.6a","Requirement","ECSS-Q-ST-40_0440023","The safety critical items shall be part of the project's overall critical items control programme as specified in ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.1a","Requirement","ECSS-Q-ST-40_0440024","Safety analysis shall support the identification of sources of safety risk as well as the performance of preliminary trade-off analyses between alternative system concepts.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.1b","Requirement","ECSS-Q-ST-40_0440025","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Analyse safety requirements and lessons-learnt associated with similar previous missions;\n    2. Perform preliminary hazard analysis of the proposed system and operations concept to support concept trade-offs;\n    3. Perform comparative safety risk assessment of the concept options;\n    4. Identify the relevant project safety requirements;\n    5. Plan safety activities for the feasibility phase;\n    6. Support the mission definition review.\n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.2a","Requirement","ECSS-Q-ST-40_0440026","Safety analysis shall support trade-off analyses in arriving at the concept that has acceptable safety risk considering the project and mission constraints. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.2b","Requirement","ECSS-Q-ST-40_0440027","The design technology selected and the operational concept to be implemented shall be selected based on the analysis data for the safest system architecture to eliminate or reduce hazards to acceptable levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.2c","Requirement","ECSS-Q-ST-40_0440028","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Commence hazard analyses of the design and operations concepts in order to identify applicable system level hazards, hazardous conditions, and potential hazardous events and consequences; \n    2. Support concept trades by identifying safety critical aspects of the concept options;\n    3. Apply hazard elimination and minimization and make safety recommendations; \n    4. Perform comparative safety risk assessments of the concept options; \n    5. Identify system level safety critical functions;\n    6. Identify system level project specific safety requirements; \n    7. Plan safety activities for the project definition phase; \n    8. Support the preliminary requirements review. \n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.3a","Requirement","ECSS-Q-ST-40_0440029","The safety analysis shall support a continued and more detailed safety optimization of the system design and operations and the identification of technical safety requirements and their applicability.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.3b","Requirement","ECSS-Q-ST-40_0440030","The analysis shall also provide inputs to safety risk assessment in support of safety risk evaluation, the identification of risk contributors in the design and in the operational concept.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.3c","Requirement","ECSS-Q-ST-40_0440031","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Update hazard analysis in support of design and mission concept definition activities; identify additional project specific safety requirements; \n    2. Update safety critical functions identification, and define the failure tolerance requirements; \n    3. Identify emergency, warning, and caution situations;\n    4. Update the system safety risk assessment as part of the contribution provided by the safety domain to the risk management process;\n    5. Identify project safety requirements; \n    6. Ensure that project requirement documentation and activities comply with project safety requirements;\n    7. Support a system requirements review and preliminary design review; \n    8. Plan verification of safety requirements implementation; \n    9. Prepare the safety plan for the detailed definition, production and qualification phase. \n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.4a","Requirement","ECSS-Q-ST-40_0440032","Safety analysis shall support detailed design, production, qualification, testing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.4b","Requirement","ECSS-Q-ST-40_0440033","Safety analysis shall also support operational safety optimization, safety requirements implementation evaluation, risk reduction verification, and hazard and risk acceptance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.4c","Requirement","ECSS-Q-ST-40_0440034","Analysis of operations shall also support the identification of emergency and contingency response planning and training requirements, and the development of procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.4d","Requirement","ECSS-Q-ST-40_0440035","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Perform detailed system level hazard analysis; \n    2. Perform supporting safety analysis;\n    3. Update the project technical safety requirements to incorporate the results of safety analyses; \n    4. Ensure that the project implementation and verification programme covers identified hazard control verification activities; \n        NOTE For example: reviews, inspections, analyses and tests.\n    5. Update safety critical functions identification, failure tolerance requirements, and identify safety critical items; \n    6. Implement control programme for safety critical items; \n    7. Perform safety risk assessment in support of design improvement, project resource apportionment, control programme for safety critical items and project reviews; \n    8. Monitor verification of safety requirements implementation; \n    9. Verify and document hazard control implementation; \n    10. Check that all open verification items are recorded and agreed procedures are in place;\n    11. Support the critical design review, the qualification review and the acceptance review;\n    12. Perform project internal safety reviews and internal audits; \n    13. Identify, monitor and control project assembly, integration, testing and handling operations which are potentially hazardous to personnel or hardware; \n    14. Review and approve hazardous and safety critical operational procedures;\n    15. Perform accident-incident reporting and investigation; \n    16. Support customer safety reviews at defined programme milestones;\n    17. Prepare a project safety “lessons-learned” report; \n    18. Prepare operational phase safety plan. \n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.5a","Requirement","ECSS-Q-ST-40_0440036","Safety analysis shall evaluate design and operational changes for impact to safety, assuring that safety margins are maintained and that operations are conducted within accepted risk.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.5b","Requirement","ECSS-Q-ST-40_0440037","The analysis shall also support the evaluation of operational anomalies for impact to safety, and the continued evaluation of risk trends.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.5c","Requirement","ECSS-Q-ST-40_0440038","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Issue the operational phase safety plan;\n    2. Review operational procedures; \n    3. Approve safety critical operational procedures; \n    4. Identify and monitor hazardous operations; \n    5. Support the flight readiness review, operational readiness review, launch readiness review and flight qualification reviews;\n    6. Support ground and flight operations; \n    7. Perform safety critical items control; \n    8. Monitor and assess evolution of the system configuration and operations resulting from design fixes and updates;\n    9. Update hazard analyses and implement additional hazard controls as necessary; \n    10. Investigate safety related flight anomalies and trends; \n    11. Update safety risk assessment as necessary to support operational decisions;\n    12. Prepare disposal phase safety plan. \n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.6a","Requirement","ECSS-Q-ST-40_0440039","Safety analysis shall evaluate all disposal operations and associated hazards. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.6b","Requirement","ECSS-Q-ST-40_0440040","Disposal solutions shall be identified which meet the project's safety requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.1.6c","Requirement","ECSS-Q-ST-40_0440041","The following safety programme tasks shall apply for human spaceflight programmes and safety critical systems:\n    1. Perform hazard analysis with respect to the disposal operations;\n    2. Check that the disposal operation conforms to international safety regulations by performing the necessary safety analysis;\n    3. Review the procedures of the disposal operations;\n    4. Support the mission close-out review.\n        NOTE These tasks should also serve as a guideline for other space programmes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.2a","Requirement","ECSS-Q-ST-40_0440042","The supplier shall hold regular safety status and progress meetings with the customer and his lower tier suppliers as part of the project progress meetings as specified in ECSS-M-ST-10. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.2b","Requirement","ECSS-Q-ST-40_0440043","The relevant customer and supplier specialists shall attend the meetings.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.3a","Requirement","ECSS-Q-ST-40_0440044","The customer shall define, conduct and chair the safety reviews to ensure satisfactory implementation of safety programme and technical safety requirements. \n    NOTE A supplier is considered as a customer vis-à-vis its lower tier suppliers (as defined in ECSS-S-ST-00).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.3b","Requirement","ECSS-Q-ST-40_0440045","The supplier shall support safety reviews by the customer and the relevant safety approval authority, as specified in the relevant review plans. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.3c","Requirement","ECSS-Q-ST-40_0440046","Each supplier participating in a safety review shall prepare, and submit for review, the safety data package.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.7.3d","Requirement","ECSS-Q-ST-40_0440047","Safety reviews shall be performed, and the review objectives achieved, in conformance with clause 5.7.1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.8a","Requirement","ECSS-Q-ST-40_0440048","The supplier shall provide a statement of safety compliance to demonstrate that the space system elements conform to stated safety requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.8b","Requirement","ECSS-Q-ST-40_0440049","The supplier shall include in his statement of compliance a statement that open verifications are followed up in the safety verification tracking log (SVTL), as defined in clause 8.5.1, and do not affect further safe processing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.8c","Requirement","ECSS-Q-ST-40_0440050","The project shall provide to the safety approval authority all safety-related information for their acceptance of the statement of safety compliance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.1a","Requirement","ECSS-Q-ST-40_0440051","Safety training shall be part of the overall training in accordance with ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.1b","Requirement","ECSS-Q-ST-40_0440052","All safety related training of any personnel working - permanently or occasionally - with system elements that can have hazardous properties shall have three major aspects:\n    1. general awareness briefings on safety measures to be taken at a given location or working environment;\n    2. basic technical training in the required safety techniques and skills which is a prerequisite to fulfil the job function under consideration;\n        NOTE For example: inspection, test, maintenance or integration.\n    3. product specific training that focuses on the hazards related to the specific system element.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.2a","Requirement","ECSS-Q-ST-40_0440053","The supplier shall identify the need for product specific safety training and implement the corresponding safety training programme for all relevant parties. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.2b","Requirement","ECSS-Q-ST-40_0440054","The supplier shall inform the customer of any safety training identified by him as necessary for the flight operations crew or mission control personnel, together with a definition of the type of training required and its scope.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.2c","Requirement","ECSS-Q-ST-40_0440055","The supplier shall support the implementation of the customer's training programme for the flight operations crew or mission control personnel.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.3a","Requirement","ECSS-Q-ST-40_0440056","All personnel accessing the area where the product is processed shall participate previously in the general safety awareness briefing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.4a","Requirement","ECSS-Q-ST-40_0440057","The supplier shall provide basic technical training to all project engineering and safety personnel working with hazardous products.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.9.5a","Requirement","ECSS-Q-ST-40_0440058","The supplier shall maintain records of personnel having received safety training in accordance with ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10a","Requirement","ECSS-Q-ST-40_0440059","The supplier shall report to the customer all accidents and incidents occurred during project activities under the control of the supplier or his lower tier suppliers that affect the system element. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10b","Requirement","ECSS-Q-ST-40_0440060","The supplier shall support - at request - project related accident and incident investigations that occur outside of the supplier’s control or facility.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10c","Requirement","ECSS-Q-ST-40_0440061","The supplier shall coordinate the investigation activities in cooperation with other supplier functional departments and lower tier suppliers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10d","Requirement","ECSS-Q-ST-40_0440062","The accident or incident investigation report shall be formally closed by the supplier upon approval by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10e","Requirement","ECSS-Q-ST-40_0440063","If the conclusion of the assessment is that the accident-incident has had an effect on the project, i.e. the safety of the product or its operation, the organisations safety representative shall be informed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.10f","Requirement","ECSS-Q-ST-40_0440064","In case of 5.10e., the accident-incident report shall become part of the project's safety data and is documented in the safety data package.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.1a","Requirement","ECSS-Q-ST-40_0440065","The supplier shall maintain, as part of the project documentation, all safety-related data to support reviews and safety compliance demonstration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.1b","Requirement","ECSS-Q-ST-40_0440066","The customer shall be given access to this data on request during audits, safety reviews and meetings held at the supplier’s premises in accordance with ECSS-M-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2a","Requirement","ECSS-Q-ST-40_0440067","The supplier shall submit a safety data package (SDP) to support reviews.\n    NOTE This can be a stand-alone package or be integrated into the overall data package if the safety review is part of an overall project review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2b","Requirement","ECSS-Q-ST-40_0440068","The safety data package shall contain at least the following safety related documentation:\n    1. Safety analysis report (in accordance with Annex D);\n    2. Supporting analysis (if applicable);\n    3. Safety risk assessment (if applicable);\n    4. Hazardous ground operations list and procedures;\n    5. Safety verification tracking log (SVTL, in accordance with Annex C).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2c","Requirement","ECSS-Q-ST-40_0440069","The contents of the safety data packages for the planned safety reviews of a project or programme shall be specified by the Safety Approval Authority to assure they support the objectives of the safety reviews for which they are delivered (in conformance with clause 5.7.2). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2d","Requirement","ECSS-Q-ST-40_0440070","The supplier shall use the actual configuration baseline, as defined by ECSS-M-ST-40, as the design and operational baseline that is the subject of the safety data package.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2e","Requirement","ECSS-Q-ST-40_0440071","The supplier shall integrate safety data related to the various subsystems or equipment that makes up the system into the safety data package that is presented at the review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.2f","Requirement","ECSS-Q-ST-40_0440072","All safety data shall be traceable from the safety data package and available for review.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.1a","Requirement","ECSS-Q-ST-40_0440073","Safety requirements that cannot be met shall be identified as specified in ECSS-M-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.1b","Requirement","ECSS-Q-ST-40_0440074","A request for deviation or waiver shall be generated and tracked according to the requirements of ECSS-M-ST-40. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.2a","Requirement","ECSS-Q-ST-40_0440075","All RFD/RFW shall be assessed in order to identify those which impact safety. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.2b","Requirement","ECSS-Q-ST-40_0440076","The accumulated deviations and waivers that affect safety shall be assessed to ensure that the effects of individual deviations do not invalidate the rationale used for the acceptance of other deviations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.3a","Requirement","ECSS-Q-ST-40_0440077","Safety deviations and waivers shall be subject to safety approval authority acceptance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.3.4a","Requirement","ECSS-Q-ST-40_0440078","Deviations and waivers that affect project safety requirements or safety-critical functions which the supplier considers acceptable shall be subject of review and disposition by the customer and the safety approval authority.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.4a","Requirement","ECSS-Q-ST-40_0440079","Safety lessons learned shall be collected during the project and used during the project, as far as they are relevant.\n    NOTE Safety lessons learned should consider as a minimum:\n        a. the impact of newly imposed requirements;\n        b. assessment of all malfunctions, accidents, anomalies, deviations and waivers;\n        c. effectiveness of safety strategies of the project;\n        d. new safety tools and methods that have been developed or demonstrated;\n        e. effective versus ineffective verifications that have been performed;\n        f. changes proposed to safety policy, strategy or technical requirements with rationale.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.4b","Requirement","ECSS-Q-ST-40_0440080","The safety lessons learned information shall be made available to the customer and suppliers, particularly to project and safety managers as well as design and safety engineers upon request for use on other projects. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","5.11.5a","Requirement","ECSS-Q-ST-40_0440081","The safety critical items identified by the safety analysis shall be documented in accordance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.2a","Requirement","ECSS-Q-ST-40_0440082","Safety requirements shall be identified and traced from the system level into the design and then allocated to the lower levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.2b","Requirement","ECSS-Q-ST-40_0440083","When specified by the project, the identified safety requirements shall be justified in the design and presented in an appropriate document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.2a","Requirement","ECSS-Q-ST-40_0440084","Appropriate design features shall be selected to ensure inherent safety.\n    NOTE Such features are fail safe design solutions, damage control, containment and isolation of potential hazards. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.1a","Requirement","ECSS-Q-ST-40_0440085","The following sequence of activities shall be applied to identified hazards, hazardous conditions, and functions whose failures have hazardous consequences:\n    1. Hazard elimination\n    2. Hazard minimization\n    3. Hazard control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.2a","Requirement","ECSS-Q-ST-40_0440086","Hazards and hazardous conditions shall, consistent with the project constraints and mission objectives, be eliminated from the design and operational concepts by the selection of design technology, architecture and operational characteristics. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.3a","Requirement","ECSS-Q-ST-40_0440087","Where hazards and hazardous conditions are not eliminated, the severity of the associated hazardous events and consequences shall, consistent with the project constraints and mission objectives, be reduced to an accepted level through the change of the design architecture, technologies, and operational characteristics allowing the substitution of those hazards by other hazards with lower potential threat.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.1a","Requirement","ECSS-Q-ST-40_0440088","Hazards that have not been eliminated and have been subjected to hazard minimization (as defined in 6.3.3.3a) shall be controlled through preventative or mitigation measures, associated to hazard scenarios, which are introduced into the system design and operation to avoid the events or to interrupt their propagation to consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.1b","Requirement","ECSS-Q-ST-40_0440089","The following measures shall be applied in order of precedence:\n    1. Design selection\n    2. Automatic safety devices\n    3. Warning devices\n    4. Special procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.2a","Requirement","ECSS-Q-ST-40_0440090","Failure tolerance is the basic safety requirement that shall be used to control most hazards. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.2b","Requirement","ECSS-Q-ST-40_0440091","The design shall tolerate a minimum number of credible failures and/or operator errors determined by the hazard consequence.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.2c","Requirement","ECSS-Q-ST-40_0440092","The supplier shall establish the list of failures to be considered as \"non credible\" for customer approval as early as possible in development.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.3a","Requirement","ECSS-Q-ST-40_0440093","Hazard which cannot be controlled by compliance to failure tolerance shall be reduced to an accepted level by compliance with specific safety related properties and characteristics of the design. \n    NOTE Examples are: structures, pressures vessels, mechanisms, material compatibility, flammability.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.4a","Requirement","ECSS-Q-ST-40_0440094","Hazards that are not eliminated through design selection shall be reduced and made controllable through the use of automatic safety devices as part of the system, subsystem or equipment. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.4b","Requirement","ECSS-Q-ST-40_0440095","The safety devices, specified in 6.3.3.4.4a, shall not be dependant on human performance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.4c","Recommendation","ECSS-Q-ST-40_0440320","Use of software in automatic safety devices should be avoided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.4d","Requirement","ECSS-Q-ST-40_0440097","If software is used in automatic safety devices, justification shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.5a","Requirement","ECSS-Q-ST-40_0440098","When it is not practical to preclude the existence or occurrence of known hazards or to use automatic safety devices, devices shall be used for the timely detection of the condition and the generation of a warning signal.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.5b","Requirement","ECSS-Q-ST-40_0440099","This shall be coupled with emergency controls of corrective action for operators to safe or shut down the affected subsystem.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.6a","Requirement","ECSS-Q-ST-40_0440100","When it is not possible to reduce the magnitude of a hazard through the design, the use of safety devices or the use of warning devices, special procedures shall be developed to control the hazardous conditions for the enhancement of safety.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.6b","Requirement","ECSS-Q-ST-40_0440101","Special procedures shall be verified by test and appropriate training be provided for personnel.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.6c","Requirement","ECSS-Q-ST-40_0440102","Hazard detection shall be implemented if alternative means cannot be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.3.4.6d","Requirement","ECSS-Q-ST-40_0440103","To permit the use of real time monitoring, hazard detection and safing systems for hazard control, the availability of sufficient response time shall be verified and corresponding safing procedures be developed and verified and the personnel trained.\n    NOTE Special procedures are the least effective of the hazard control and risk reduction measures available. They can include emergency and contingency procedures, procedural constraints, or the application of a controlled maintenance programme. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.4a","Requirement","ECSS-Q-ST-40_0440104","The system design shall meet the safety requirements under the worst-case natural and induced environments defined for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.4b","Requirement","ECSS-Q-ST-40_0440105","Design and performance margins shall be established and applied for worst-case combinations of induced and natural environments and operating characteristics.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.5a","Requirement","ECSS-Q-ST-40_0440106","Loss, malfunctioning, and sudden restoration of external services shall be defined as an input to the development phase.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.5b","Requirement","ECSS-Q-ST-40_0440107","The system design shall be defined so that catastrophic or critical consequences are not induced by loss, malfunctioning, and sudden restoration of external services.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6a","Requirement","ECSS-Q-ST-40_0440108","Safety monitoring, display, alarm and safing capabilities shall be incorporated for manned space systems.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6b","Requirement","ECSS-Q-ST-40_0440109","These capabilities shall provide the information to allow the crew and system operators to take actions to protect personnel from the consequences of failures within safety-critical functions and the failure of hazard control measures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6c","Requirement","ECSS-Q-ST-40_0440110","The system design shall provide the capability for detecting failures that result in degradation of failure tolerance with respect to the hazard detection, signalling and safing function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6d","Requirement","ECSS-Q-ST-40_0440111","The performance of these functions shall be verifiable during flight and ground operational phases.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6e","Requirement","ECSS-Q-ST-40_0440112","The emergency, caution and warning function shall detect and notify the crew and system operators of emergency, warning and caution situations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6f","Requirement","ECSS-Q-ST-40_0440113","Safing functions and capabilities shall be included that provide for the containment or control of emergency, warning and caution situations. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6g","Requirement","ECSS-Q-ST-40_0440114","Provisions shall be included for the monitoring of safing function execution. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6h","Requirement","ECSS-Q-ST-40_0440115","Dedicated safing functions shall be provided for emergency situations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6i","Requirement","ECSS-Q-ST-40_0440116","Control of warning and caution situations shall be acceptable by system reconfiguration or by dedicated safing functions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6j","Requirement","ECSS-Q-ST-40_0440117","A single failure shall not cause loss of the emergency and warning function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6k","Requirement","ECSS-Q-ST-40_0440118","Where the operation of a safing system introduces a new hazard, inadvertent activation of the safing system shall be controlled in accordance with the failure tolerance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6l","Requirement","ECSS-Q-ST-40_0440119","A single failure shall not cause loss of the emergency and warning functions together with the monitored functions. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6m","Requirement","ECSS-Q-ST-40_0440120","Emergency, warning and caution data, out of limit annunciation and safing commands shall be given priority over other data processing and command functions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6n","Requirement","ECSS-Q-ST-40_0440121","When systems or elements are integrated into, or docked with the other systems or elements, the emergency, warning, caution, and safing function shall enable the areas of control responsibility to monitor and display the applicable parameters, and to control the related safing functions. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6o","Requirement","ECSS-Q-ST-40_0440122","Emergency, warning, and caution parameter status information shall be available and displayed at the launch control and mission control centres in “near real time” during the operational phases. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.6p","Requirement","ECSS-Q-ST-40_0440123","It shall be possible for the crew to ascertain and monitor in “real time” the status of emergency, warning and caution parameters of non-crewed systems or elements prior to docking with crewed systems.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.7a","Requirement","ECSS-Q-ST-40_0440124","The design and the operational characteristics of the space system shall be such that the generation of space debris is minimized consistent with the project constraints and mission objectives.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.8a","Requirement","ECSS-Q-ST-40_0440125","The space vehicle shall be designed and operated (post-mission disposal manoeuvres) such that, where applicable, the risk of a catastrophic event does not exceed the level of acceptable risk specified by the project and by the launch base safety authority.\n    NOTE Hardware of a space system that is returned from orbit presents a potential threat to the Earth's population due to the risk of debris entering the atmosphere in an uncontrolled manner.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.9a","Requirement","ECSS-Q-ST-40_0440126","Biological contamination (including organic-constituents) resulting from the introduction of extraterrestrial matter shall be avoided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.9b","Requirement","ECSS-Q-ST-40_0440127","The introduction of extraterrestrial matter shall not affect the environmental conditions on Earth.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.9c","Requirement","ECSS-Q-ST-40_0440128","Extraterrestrial matter shall be treated as hazardous substances until proven otherwise.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.9d","Requirement","ECSS-Q-ST-40_0440129","A containment function for hazardous substances of the spacecraft, which prevents release in case of accidents until recovery or arrival at a dedicated containment facility, shall be provided. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.9e","Requirement","ECSS-Q-ST-40_0440130","If containment cannot be verified, the hazardous substances (and any part of the space system that has potentially been exposed) shall not be returned to Earth (unless sterilized in space).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10a","Requirement","ECSS-Q-ST-40_0440131","A mission abort capability shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10b","Requirement","ECSS-Q-ST-40_0440132","Safing and safe heaven functions shall be provided. \n    NOTE These functions can be implemented through measures such as resource conservation, increased shielding (solar flares, meteoroids and radiation), vehicle or systems reconfiguration and trajectory changes. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10c","Requirement","ECSS-Q-ST-40_0440133","Escape and rescue functions shall be provided. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10d","Requirement","ECSS-Q-ST-40_0440134","The capability to reconfigure the system to restore the functional capability of safety critical functions in case of failures or accidents shall be provided. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10e","Requirement","ECSS-Q-ST-40_0440135","The capability to monitor, detect and assess hazards and effects of slow insidious events with hazardous consequences shall be detailed according to project constraints and mission objectives.\n    NOTE Such hazards include fatigue, corrosion, micro-organisms, aging, deterioration, contamination. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.10f","Requirement","ECSS-Q-ST-40_0440136","The space system shall provide an on-board medical facility and the capability for handling a permanently impaired or deceased crewmember.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.3.11a","Requirement","ECSS-Q-ST-40_0440137","System shall be designed such that any required access to system elements during flight or ground operations can be accomplished with an accepted level of risk to personnel. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1a","Requirement","ECSS-Q-ST-40_0440138","The severity of potential consequences of identified hazardous events shall be categorized as shown in Table 6-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1b","Requirement","ECSS-Q-ST-40_0440139","An understanding of the criteria defined in Table 6-1 shall be agreed between customer and supplier.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1c","Requirement","ECSS-Q-ST-40_0440140","Detrimental environmental effects, from the point of view of severe hazardous consequences to the global public, shall be included in the consequence severity evaluation.\n    NOTE 1 Table 6-1 is used both in ECSS-Q-ST-30 and ECSS-Q-ST-40.\n    NOTE 2 This impact can be immediate and personal. It also can be on a broader scale not limited to a single person only. The hazardous consequences can be short term or long term.\n    NOTE 3 In space flight, the environment concerned can be outer space, including the Moon and the planets, geostationary orbit (GEO), low Earth orbit (LEO) as well as the Earth’s atmosphere.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1d","Requirement","ECSS-Q-ST-40_0440141","The availability of the following shall not be used as rationale for the reduction of the severity: \n    1. design features which reduce the probability of a hazardous event occurring, but which do not affect its severity; \n    2. warning devices, crew safe haven, or crew escape capabilities. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1e","Requirement","ECSS-Q-ST-40_0440142","For international programmes, a coherent set of consequence severity shall be established for joint operational phases.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1f","Requirement","ECSS-Q-ST-40_0440143","These categories shall not violate the safety policy and principles as defined in clause 4.2.1 for the protection of human life or the principles of categorization in accordance with the definition of consequence severity categories in Table 6-1.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1g","Requirement","ECSS-Q-ST-40_0440144","The expert assessment on determining limits for exposures that do not create a hazard, those that create critical hazards and those that create catastrophic hazards shall be performed by the responsible authority, early in the design process.\n    NOTE Examples of responsible authority are medical boards or radiation protection committees.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.1h","Requirement","ECSS-Q-ST-40_0440145","The detailed safety requirements and measures shall be derived from allowed exposure levels.\n    NOTE For example: maximum allowable concentrations, maximum emission concentrations or radiation doses.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.1a","Requirement","ECSS-Q-ST-40_0440146","Failure tolerance shall be the basic safety requirement used to control hazards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.1b","Requirement","ECSS-Q-ST-40_0440147","No single system failure or single operator error shall have critical or catastrophic consequences. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.1c","Requirement","ECSS-Q-ST-40_0440148","No combination of two independent system failures or operator errors shall have catastrophic consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.1d","Requirement","ECSS-Q-ST-40_0440149","Safety inhibits shall be independent, verifiable, stable and stay in a safe position even in case of energy failure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.1e","Requirement","ECSS-Q-ST-40_0440150","Multiple failures, which result from common-cause or common-mode failure mechanisms, shall be analysed as single failures for determining failure tolerance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.2a","Requirement","ECSS-Q-ST-40_0440151","The system design shall:\n    1. include the capability for on-board redundancy management of safety-critical functions, \n    2. provide failure tolerance and redundancy status information to the flight and ground crews, including immediate crew notification in the case of failure detection, redundancy switch-over, or loss of operational redundancy,\n    3. include failure detection, failure isolation and switching of redundant items.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.2b","Requirement","ECSS-Q-ST-40_0440152","The capability shall be provided to the flight crew and mission control to override automatic safing and redundancy switch-over.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.2c","Requirement","ECSS-Q-ST-40_0440153","Alternate or redundant safety-critical functions shall be physically and functionally separated or protected in such a way that any event that causes the loss of one path does not result in the loss of alternative or redundant paths.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.2.3a","Requirement","ECSS-Q-ST-40_0440154","Hardware failures or software errors shall not cause additional failures with hazardous effects or propagate to cause the hazardous operation of interfacing hardware.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.1a","Requirement","ECSS-Q-ST-40_0440155","Technical requirements for areas of design for minimum risk shall be identified and approved by the relevant safety approval authorities\n    NOTE “Design for minimum risk” is a safety requirement used to control hazards by specifying safety-related properties and characteristics of the design.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.2a","Requirement","ECSS-Q-ST-40_0440156","Structural safety factors shall be defined and applied in accordance with ECSS-E-ST-32-10 or higher safety factor where applicable.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.2b","Requirement","ECSS-Q-ST-40_0440157","Safety margins shall be based on worst credible combinations of environmental conditions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.3a","Requirement","ECSS-Q-ST-40_0440158","For manned systems, where structural failure can have catastrophic or critical consequences, structures, pressure vessels, fasteners and load-bearing paths within mechanisms shall be designed in accordance with ECSS-E-ST-32-01.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.3b","Requirement","ECSS-Q-ST-40_0440159","For unmanned systems, only pressure vessels shall be designed in accordance with ECSS-E-ST-32-01, when required by launch site safety authority.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.4a","Requirement","ECSS-Q-ST-40_0440160","Materials shall be selected and controlled in accordance with ECSS-Q-ST-70.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.4b","Requirement","ECSS-Q-ST-40_0440161","Material selection shall assure that hazards associated with material characteristics are either eliminated or controlled.\n    NOTE Examples of these material properties to be characterized are: toxicity, flammability, resistance to stress corrosion, outgassing, offgassing, resistance to radiation, resistance to thermal cycling, arc tracking, thermal degradation, resistance to cleaning fluid and microbiological growth.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.3.4c","Requirement","ECSS-Q-ST-40_0440162","If requirement 6.4.3.4b. is not feasible, the system design shall include the necessary provisions to control hazardous events associated with material characteristics in accordance with the requirements of this Standard.\n    NOTE An example of provisions to be included by the system design is containment of hazardous substances. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.4a","Requirement","ECSS-Q-ST-40_0440163","When given, the probabilistic safety targets shall be used for\n    1. identifying and ranking major risk contributors,\n    2. making the acceptable risk decision for each identified hazard,\n    3. supporting the disposition making for those cases where nonconformance to the qualitative requirements is identified.\n        NOTE Probabilistic safety targets can be established by the customer for hazardous consequences at system level for each project or programme. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.4.4b","Requirement","ECSS-Q-ST-40_0440164","Probabilistic safety targets shall conform to the requirements given by launch safety authorities and national and international regulations.\n    NOTE Informative Annex E provides criteria for the establishing of probabilistic safety targets.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.1a","Requirement","ECSS-Q-ST-40_0440165","A safety critical function that, if lost or degraded, or through incorrect or inadvertent operation, can result in a catastrophic or critical hazardous consequence, shall be identified as a safety-critical function.\n    NOTE As an example, a series of operational events that can result in a hazard if they occur inadvertently or are operated out of order.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.1b","Requirement","ECSS-Q-ST-40_0440166","Identification shall be done without taking into account hazards controls to be or already implemented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.2a","Requirement","ECSS-Q-ST-40_0440167","Inadvertent operation of a safety-critical function shall be prevented by\n    1. two independent inhibits, if it induces critical consequences, or\n    2. three independent inhibits, if it induces catastrophic consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.3a","Requirement","ECSS-Q-ST-40_0440168","The system shall provide failure tolerance and redundancy status information of safety-critical functions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.3b","Requirement","ECSS-Q-ST-40_0440169","The system shall provide the status of at least two inhibits on functions that, if inadvertently operated, can lead to catastrophic consequences, including\n    1. notification in real time in case of failure detection,\n    2. announcement of any loss of operational redundancy, \n    3. notification of redundancy switch-over, or \n    4. changes of inhibit status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.4a","Requirement","ECSS-Q-ST-40_0440170","The design shall either provide the capability for the safe shutdown of safety-critical functions prior to in-flight maintenance operations or conform to the failure tolerance requirements during maintenance operations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.5a","Requirement","ECSS-Q-ST-40_0440171","Electronic, electrical, electromechanical (EEE) components used to support safety-critical functions in flight standard hardware shall be selected and procured in accordance with the applicable programme requirements of ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.1a","Requirement","ECSS-Q-ST-40_0440172","Safety aspects associated with the software function shall be an integral part of the overall system safety efforts and not be assessed in isolation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.1b","Requirement","ECSS-Q-ST-40_0440173","A software component shall be considered safety-critical if the loss or degradation of its function, or its incorrect or inadvertent operation, can result in catastrophic or critical consequences. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.2a","Requirement","ECSS-Q-ST-40_0440174","During the project life cycle, safety analysis shall be carried out to:\n    1. identify the criticality of software components in accordance with the severity of the consequences as defined in Table 6-1,\n    2. determine where and under what conditions the system can trigger hazardous events caused by the software,\n    3. define verification methods for hazard controls involving software,\n    4. provide verification evidence of hazard control implementation. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.3a","Requirement","ECSS-Q-ST-40_0440175","The criticality of a software component shall be evaluated taking into account the overall system design which can provide for, e.g. back-up or emergency procedures, hardware inhibits and certain time to effect.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.4a","Requirement","ECSS-Q-ST-40_0440176","A safety-critical software component shall be designed, implemented, verified and operated according to the engineering and product assurance requirements defined in ECSS-E-ST-40 and ECSS-Q-ST-80.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.4b","Requirement","ECSS-Q-ST-40_0440177","Safety-critical software shall be analysed for the identification and verification of adequate software controls and inhibits and validated accordingly. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.5.6.4c","Requirement","ECSS-Q-ST-40_0440178","The level of required software product assurance effort shall be determined in accordance with the criticality of the software component.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1a","Requirement","ECSS-Q-ST-40_0440179","Safety involvement in the operational phase shall be planned.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1b","Requirement","ECSS-Q-ST-40_0440180","Responsibilities, rules and contingency procedures shall be established prior to operation for hazardous “limit” conditions that can occur during ground and in-flight operations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1c","Requirement","ECSS-Q-ST-40_0440181","Operating ranges and performance limits for safe operation shall be established and specified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1d","Requirement","ECSS-Q-ST-40_0440182","The design shall not require continuous active control by personnel in order to stay within the established operating ranges and performance limits.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1e","Requirement","ECSS-Q-ST-40_0440183","Man-machine interfaces shall be designed and the personnel tasks shall be scoped to reduce the potential for hazardous events resulting from human error to an accepted level.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.1f","Requirement","ECSS-Q-ST-40_0440184","Limits for crew exposure to natural and system-induced environments shall be established and maintained by design features or operational constraints that cover nominal, contingency, and emergency operational modes, in order to preclude crew injury or inability to perform safety-critical functions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.1a","Requirement","ECSS-Q-ST-40_0440185","Hazards to the humans, public and private property and the environment, resulting from launcher system operation or malfunction shall be precluded by compliance with the regulations of the launch safety authority.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.2a","Requirement","ECSS-Q-ST-40_0440186","Normal or abort operations shall not result in contamination of the Earth’s environment that endangers human health, crops or natural resources or that exceed limits set by national or international regulations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.3a","Requirement","ECSS-Q-ST-40_0440187","Flight rules shall be prepared for each mission that outline pre-planned decisions in case of off-nominal situations and consistent with safety requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.4a","Requirement","ECSS-Q-ST-40_0440188","Hazardous commanding control shall ensure that all hazardous commands are identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.4b","Requirement","ECSS-Q-ST-40_0440189","Hazardous commanding control shall ensure that failure modes, associated with flight and ground operation - including hardware, software and procedures - used in commanding from control centres or other ground equipment, are included in the safety assessment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.4c","Requirement","ECSS-Q-ST-40_0440190","Hazardous commanding control shall ensure that the system design provides protection to avoid the erroneous acceptance of commands that can result in catastrophic or critical consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.4d","Requirement","ECSS-Q-ST-40_0440191",".Hazardous commanding control shall ensure that commands, which can result in catastrophic or critical hazardous consequences, are not performed until they are authorized and verified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.5a","Requirement","ECSS-Q-ST-40_0440192","Mission operation change control shall ensure that all changes, which are desired or become necessary during mission, are reviewed for safety impact.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.5b","Requirement","ECSS-Q-ST-40_0440193","Mission operation change control shall ensure that the responsible safety approval authority approves all operational change requests with safety impact.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.6a","Requirement","ECSS-Q-ST-40_0440194","Safety status parameters shall be identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.6b","Requirement","ECSS-Q-ST-40_0440195","Safety status parameters shall be monitored.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.6c","Requirement","ECSS-Q-ST-40_0440196","Deviation from specified limits shall be managed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.7a","Requirement","ECSS-Q-ST-40_0440197","In the case of a deviation from the planned launch trajectory during ascent, launch vehicle stages shall be remotely destroyed or have their propulsion engines shut off to prevent stages or debris from falling outside pre-defined safe areas.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.7b","Requirement","ECSS-Q-ST-40_0440198","The launch vehicle and spent stage trajectories shall be monitored to determine vehicle, stage or debris impact points.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.2.7c","Requirement","ECSS-Q-ST-40_0440199","Residual propellants contained in spent or aborted suborbital stages shall be safely dispersed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.1a","Requirement","ECSS-Q-ST-40_0440200","Safety requirements of the clause shall be applied during the following ground operations:\n    1. development, qualification or acceptance testing;\n    2. assembly, integration or test operations;\n    3. launch site operations;\n    4. servicing or turn-around operations; and\n    5. transportation or handling operations,",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.2a","Requirement","ECSS-Q-ST-40_0440201","The supplier shall establish procedures to perform safety readiness reviews and inspections prior to the performance of any applicable operation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.3a","Requirement","ECSS-Q-ST-40_0440202","To verify conformance to safety requirements, readiness reviews and inspections shall include safety review and assessment of facilities, equipment (incl. GSE), test articles, operating, test and contingency procedures, access controls, and personnel capabilities to comply with the safety requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.4a","Requirement","ECSS-Q-ST-40_0440203","Hazardous operations shall be monitored for conforming to safety requirements and procedures, and for the possible development of unforeseen hazardous situations. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.4b","Requirement","ECSS-Q-ST-40_0440204","Where necessary, contingency and emergency plans or procedures shall be established and verified prior to the commencement of the operation. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.4c","Requirement","ECSS-Q-ST-40_0440205","The safety manager or safety relevant authority shall have the authority to stop any operation that does not conform to safety requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.5a","Requirement","ECSS-Q-ST-40_0440206","Launch, landing, turn-around and mission operations shall be subject to hazard analysis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.5b","Requirement","ECSS-Q-ST-40_0440207","For ground operations, the analysis shall address the:\n    1. potential hazardous consequences of human error and procedural deficiencies;\n    2. adequacy and maintenance of operational margins;\n    3. potential for human exposure to hazards and hazardous effects;\n    4. requirements for operator and flight crew training;\n    5. adequacy of information and data provided by the flight hardware, ground support equipment (GSE), or test equipment, as appropriate, to support the performance of the operations in accordance with all applicable safety requirements (including all safety regulations).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.6a","Requirement","ECSS-Q-ST-40_0440208","All Ground support equipment (GSE) shall be subjected to hazard analysis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.6b","Requirement","ECSS-Q-ST-40_0440209","All GSE shall conform to the ‘Essential Health & Safety Requirements’ of all applicable EU ‘New Approach directives’. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.6c","Requirement","ECSS-Q-ST-40_0440210","Conformance to 6.6.3.6b. shall be shown by the addition of the ‘CE’ mark to the product and the issuing of a ‘Declaration of Conformity’.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","6.6.3.6d","Requirement","ECSS-Q-ST-40_0440211","Conformance to any other product related directives shall be demonstrated.\n    NOTE Further guidance is given in Annex G.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.2a","Requirement","ECSS-Q-ST-40_0440212","Safety analysis shall be performed in a systematic manner as a basis for all applicable phases and to ensure that hazards are identified, eliminated or minimized and controlled and safety risks are assessed and reduced.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.2b","Requirement","ECSS-Q-ST-40_0440213","Safety analyses shall be initiated early in the design process and provide concurrent support to project engineering in the selection of the least hazardous design and operational options that are compatible with the project mission and programme constraints and conform to the requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.2c","Requirement","ECSS-Q-ST-40_0440214","The results of safety analyses shall also be used to support project management in the assessment of the overall risks, verification of risk reduction, ranking of risk sources, support to project resource allocation, monitoring of risk trends, and residual risk acceptance. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.2d","Requirement","ECSS-Q-ST-40_0440215","Analysis shall always be made with reference to a defined configuration baseline as defined by ECSS-M-ST-40.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.1a","Requirement","ECSS-Q-ST-40_0440216","The supplier shall respond to and comply with the applicable safety requirements for the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.2a","Requirement","ECSS-Q-ST-40_0440217","The supplier shall identify additional safety requirements, where applicable, through the use of lessons learned from previous projects and the safety analyses performed during the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.3a","Requirement","ECSS-Q-ST-40_0440218","The supplier shall define the safety requirements for the various functions of the system.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.4a","Requirement","ECSS-Q-ST-40_0440219","The supplier shall define the safety requirements associated with the various subsystems and lower levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.5a","Requirement","ECSS-Q-ST-40_0440220","The supplier shall justify to the customer the proposed allocation of safety requirements at the latest at the end of the detailed definition phase.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.3.6a","Requirement","ECSS-Q-ST-40_0440221","The supplier shall ensure that the function and subsystem safety requirements are included in the relevant functional and subsystem specification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.4a","Requirement","ECSS-Q-ST-40_0440222","Safety analysis shall be refined and updated in an iterative manner as the design process proceeds, to ensure that hazards and hazardous events are assessed, and that the relevant detailed design and operational requirements, hazard controls, and verification activities are defined and implemented.\n    NOTE Refer to 5.7 for detailed safety programme tasks in the different project phases",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.1a","Requirement","ECSS-Q-ST-40_0440223","The safety analysis report shall be established in conformance with the DRD in Annex D in order to gather results of safety analyses, which use deterministic and probabilistic methods which are described in the clauses 7.5.2 to 7.5.4.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2a","Requirement","ECSS-Q-ST-40_0440224","Hazard analysis shall be performed in a systematic manner, beginning in the concept phase and continuing through the operational phase, including end-of-life and disposal.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2b","Requirement","ECSS-Q-ST-40_0440225","Hazard analysis shall support the hazard reduction process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2c","Requirement","ECSS-Q-ST-40_0440226","Hazard analysis shall identify and evaluate:\n    1. hazards associated with system design, its operation (both on ground and in flight) and the operation environment; \n    2. the hazardous effects resulting from the physical and functional propagation of initiator events;\n    3. the hazardous events resulting from the failure of system functions and functional components;\n    4. time critical situations. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2d","Requirement","ECSS-Q-ST-40_0440227","The following potential initiator events shall be considered:\n    1. hardware failure (random or time dependent);\n    2. latent software error;\n    3. operator error;\n    4. design inadequacies, including:\n        (a) inadequate margins;\n        (b) unintended operating modes caused by sneak-circuits;\n        (c) material inadequacies and incompatibilities;\n        (d) hardware-software interactions;\n    5. natural and induced environmental effects;\n    6. procedural deficiencies.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2e","Requirement","ECSS-Q-ST-40_0440228","Hazard analysis includes a systematic analysis of the “system” operations and operating procedures that shall be performed in the detailed design and operational stages of a project. \n    NOTE This analysis evaluates the capability of the system to be operated safely, to determine the safest operating modes, and to evaluate the acceptability of the operating procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.2f","Requirement","ECSS-Q-ST-40_0440229","The systematic analysis of system operation and operating procedures shall be repeated as the design and operational detail evolves, including the system’s operational modes and man-machine interfaces.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.3a","Requirement","ECSS-Q-ST-40_0440230","Safety risk assessment shall \n    1. comprise the identification, classification and ranking of safety risks and their contributors,\n    2. be based on deterministic hazard analysis by combining the consequence severity and the likelihood of occurrence of the consequence,\n    3. be used to facilitate effective and efficient safety risk reduction and control, \n    4. support project risk management as defined in ECSS-M-ST-80, \n    5. assess compliance with probabilistic safety targets.\n        NOTE 1 The estimation of event likelihoods is based on the use of different sources of data i.e.: \n            · previous experience on the particular system (i.e. measured or observed directly relevant test or experience data), \n            · data from other systems or projects (i.e. extrapolation from generic data, similarity data, or physical models), and \n            · expert judgment (i.e. direct estimation of likelihoods by domain specialists).\n        NOTE 2 The determination of likelihood is not a mean to downgrade the severity of function (see 6.4.1d)                                                     ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.3b","Requirement","ECSS-Q-ST-40_0440231","Safety risk assessment shall be started early in the design process and performed in progressive steps during the implementation of the safety programme. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.1a","Requirement","ECSS-Q-ST-40_0440232","Following supporting assessment and analysis methods shall be used as necessary (tailored by project) to support hazards analysis and safety risk assessment.\n    NOTE 1 Example of tailoring by project is when the supporting assessment and analysis methods are not applicable in e.g. unmanned missions.\n    NOTE 2 Assessments and analyses from ECSS-Q-ST-30 can be used to support safety assessment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.1b","Requirement","ECSS-Q-ST-40_0440233","Supporting analyses shall be agreed with all relevant parties.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.2a","Requirement","ECSS-Q-ST-40_0440234","Warning time analysis shall be performed during the concept definition phase and the design and development phase in order to evaluate time-critical situations identified in the hazard analysis and to support the implementation of hazardous-situation detection and warning devices or contingency procedures. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.2b","Requirement","ECSS-Q-ST-40_0440235","The analysis shall determine the\n    1. time interval during which the event is detected and the response action taken; \n    2. detection capability of the proposed design with respect to detection sensitivity and detection time; \n    3. resultant time available for response;\n    4. adequacy of the proposed design or contingency procedures, including emergency evacuation, rescue, system reconfiguration, redundancy switching, and maintenance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.2c","Requirement","ECSS-Q-ST-40_0440236","The detection times shall be determined from the\n    1. occurrence of the initiating event to the time when a hazardous consequence occurs (propagation time); \n    2. occurrence of the initiating event to the time of earliest detection or annunciation; and \n    3. time taken for corrective action to be implemented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.3a","Requirement","ECSS-Q-ST-40_0440237","Caution and warning analysis shall be performed during the concept definition phase and the design and development phase of human space flight programmes in order to identify\n    1. emergency, warning, and caution parameters;\n    2. the required safing functions and capabilities;\n    3. limit sensing requirements;\n    4. the applicability of the individual “caution and warning” functions to the different mission phases. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.3b","Requirement","ECSS-Q-ST-40_0440238","The caution and warning analysis shall utilize the results of the warning time and hazards analyses as appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.1a","Requirement","ECSS-Q-ST-40_0440239","Multiple failures, which result from common-cause or common-mode failure mechanisms, shall be analysed as single failures for determining failure tolerance. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.2a","Requirement","ECSS-Q-ST-40_0440240","The supplier shall identify the requirement for and the scope of dedicated common-cause and common-mode analyses by means of the review of the results of the other safety analyses, such as FTA and hazard analysis, and of the characteristic of the system and of its environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.3a","Requirement","ECSS-Q-ST-40_0440241","The supplier shall identify potential common-cause failures by assessment of the effects of common-causes. \n    NOTE For example: radiation, thermal environment and fires.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.3b","Requirement","ECSS-Q-ST-40_0440242","The common-cause failure analysis shall be performed in coordination with the FTA and the hazard analysis.\n    NOTE The analysis of common-cause failures can require that use be made of the result of dedicated engineering analyses, e.g. thermal analyses, meteorite or debris impact analysis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.4a","Requirement","ECSS-Q-ST-40_0440243","Common-mode failures shall be analysed by means of the use of check-lists (to be established by the supplier) that list potential common-modes for system components during the manufacturing, integration, test, operation and maintenance phases. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.4b","Requirement","ECSS-Q-ST-40_0440244","The common-mode analysis shall be coordinated with the FMEA/FMECA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.4.5a","Requirement","ECSS-Q-ST-40_0440245","Results of common-cause and common-mode analysis shall be integrated with the results of the system level safety analyses (fault tree analysis, hazard analysis).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.5a","Requirement","ECSS-Q-ST-40_0440246","The fault tree analysis shall be used to establish the systematic link between the system-level hazard and the contributing hazardous events and subsystem, equipment or piece part failure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.5b","Requirement","ECSS-Q-ST-40_0440247","A fault tree analysis, or its equivalent, shall be performed to verify the failure tolerance requirements.\n    NOTE Refer to ECSS-Q-ST-40-12 “Fault tree analysis - Adoption notice ECSS/IEC 61025” for further instructions on fault tree analyses.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.6a","Requirement","ECSS-Q-ST-40_0440248","Whenever safety analyses identify operator errors as a cause of catastrophic or critical hazards, a dedicated analysis shall be carried out.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.6b","Requirement","ECSS-Q-ST-40_0440249","The human error analysis shall be used to support the safety analysis for the identification of human operator error modes and their effects and for the definition of adequate countermeasures to prevent or control human operator errors.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.6c","Requirement","ECSS-Q-ST-40_0440250","The human error analysis shall be developed from the early phases of the project onwards in order to define recommendations for the hardware and software design, procedure development and training preparation programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.7a","Requirement","ECSS-Q-ST-40_0440251","The results of failure modes and effects analysis (FMEA) or failure modes, effects and criticality analysis (FMECA) shall be used to support the hazard analysis in the evaluation of the effects of failures. FMEA/FMECA and hazard analysis are complementary analyses.\n    NOTE Refer to ECSS-Q-ST-30-02 for further instructions on FMEA/FMECA.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.8a","Requirement","ECSS-Q-ST-40_0440252","Zonal analysis shall be performed where redundancy is used to reduce the probability of losing a function or of inadvertently actuating a safety-critical function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","7.5.4.8b","Requirement","ECSS-Q-ST-40_0440253","The objectives of the zonal analysis shall ensure that equipment installation meets the adequate safety requirements regarding:\n    1. basic installation rules and space practices;\n    2. interaction between subsystems;\n    3. implication of operator errors;\n    4. effects of external events.\n        NOTE Zonal analysis is the systematic inspection of the topology of a system, the evaluation of potential component-to-component interactions with and without failure, and the assessment of the severity of potential hazards inherent in the system installation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.1a","Requirement","ECSS-Q-ST-40_0440254","A system shall be in place that tracks all hazards and related risks, to relate all verifications of the corresponding hazard uniquely to unambiguous causes and controls.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.1b","Requirement","ECSS-Q-ST-40_0440255","For common techniques for verification of design features used to control hazards, the requirements of ECSS-E-ST-10 shall apply. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.1c","Requirement","ECSS-Q-ST-40_0440256","To successfully complete the safety process, positive feedback shall be provided on completion results for all verification items associated with a given hazard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.1a","Requirement","ECSS-Q-ST-40_0440257","The supplier shall establish a hazard reporting system for tracking the status of all identified hazards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.1b","Requirement","ECSS-Q-ST-40_0440258","The system shall be applied for all hazards with potentially catastrophic or critical consequences.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.1c","Requirement","ECSS-Q-ST-40_0440259","The supplier shall report, and provide evidence, that\n    1. controls are defined and agreed;\n    2. verification methods are defined and agreed; \n    3. verification is completed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.1d","Requirement","ECSS-Q-ST-40_0440260","If verification cannot be completed, the supplier shall establish a Safety Verification Tracking Log (SVTL) (refer to clause 8.5.1a.).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.2a","Requirement","ECSS-Q-ST-40_0440261","Status of hazard control and risk reduction activities shall be reviewed at safety progress meetings and project safety reviews for compliance with decisions taken and achievement of intended results.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.2.3a","Requirement","ECSS-Q-ST-40_0440262","All hazard documentation shall be formally issued for each safety review and major project review, as specified in clause 5.11). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.1a","Requirement","ECSS-Q-ST-40_0440263","Verification engineering shall select the verification methods consistent:\n    1. with the verification requirements documented in the hazard report,\n    2. with the launch base safety rules.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.1b","Requirement","ECSS-Q-ST-40_0440264","Verification planning shall commence in an integrated manner upon selection of the control method.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.2a","Requirement","ECSS-Q-ST-40_0440265","Safety verification methods shall include alternatively or in combination review of design, analysis, inspection and test.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.2b","Requirement","ECSS-Q-ST-40_0440266","For all safety verifications traceability shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.3a","Requirement","ECSS-Q-ST-40_0440267","All relevant technical safety and engineering analyses performed or updated with analysis in respect to the as-built configuration shall be used for verification. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.3b","Requirement","ECSS-Q-ST-40_0440268","When similarity analysis is provided, for tracking purposes it shall contain a copy of (or a unique reference to) the referenced previous verification, verification procedure and requirement valid at the time of the first verification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.1a","Requirement","ECSS-Q-ST-40_0440269","Inspections which are considered as necessary in order to meet safety requirements of the system shall be identified and included in user manuals and procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2a","Requirement","ECSS-Q-ST-40_0440270","All preflight safety inspections shall be assessed for inclusion in the MIP list. \n    NOTE If preflight safety inspections are included on the MIP list, closeout is feasible by MIP reporting or individual reporting as appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2b","Requirement","ECSS-Q-ST-40_0440271","Launch preparation inspections shall be entered into the launch base procedure. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2c","Requirement","ECSS-Q-ST-40_0440272","The closeout shall be given by the approved launch authority procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2d","Requirement","ECSS-Q-ST-40_0440273","Late access procedures shall be the subject of training and be performed by qualified personnel. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2e","Requirement","ECSS-Q-ST-40_0440274","Training for flight crew and mission operation teams shall be performed, including specific safety briefing, training and mission simulation. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.2f","Requirement","ECSS-Q-ST-40_0440275","Close-out shall be by safety-approved procedure, documented training session and simulations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.4.3a","Requirement","ECSS-Q-ST-40_0440276","Inflight inspections shall be entered into flight procedures and operation manuals.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.5a","Requirement","ECSS-Q-ST-40_0440277","The supplier shall select, and propose to the safety approval authority, the safety verification methods to be used in conformance to the applicable safety requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.3.5b","Requirement","ECSS-Q-ST-40_0440278","The results of safety verification shall be submitted for approval to the relevant safety approval authority.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.1a","Requirement","ECSS-Q-ST-40_0440279","Safety-critical functions shall be verified by testing which include application of the operating procedures, the “man-in-the-loop”, and the verification of the effectiveness of applicable failure tolerance requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.1b","Requirement","ECSS-Q-ST-40_0440280","The tests shall include the demonstration of nominal, contingency and emergency operational modes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.2a","Requirement","ECSS-Q-ST-40_0440281","The safety-critical characteristics of all safety-critical functions shall be qualified by test.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.2b","Requirement","ECSS-Q-ST-40_0440282","Safety-critical function qualification testing shall include the determination of performance margins considering worst case combinations of induced and natural environments and operating conditions. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.2c","Requirement","ECSS-Q-ST-40_0440283","Qualification “by similarity” shall not be applied except after customer approval on a case-by-case basis. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.3a","Requirement","ECSS-Q-ST-40_0440284","Induced failure tests shall be performed when required by safety analysis for evaluating failure effects, and for demonstrating failure tolerance conformance in safety-critical functions. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.4a","Requirement","ECSS-Q-ST-40_0440285","Verification of unique safety required design or operational characteristics shall form part of the development, qualification or acceptance testing programmes as appropriate. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.5a","Requirement","ECSS-Q-ST-40_0440286","Where full-scale testing is not performed, equivalent safety verification method based on technically representative hardware or models shall be justified, approved and performed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.4.5b","Requirement","ECSS-Q-ST-40_0440287","For the verification of hazard controls in catastrophic hazards where non-flight equipment replaces part of the flight equipment to test a flight function the verification shall be performed independently by a third party which was not involved in the design and qualification of the flight model (FM).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.5.1a","Requirement","ECSS-Q-ST-40_0440288","A safety verification tracking log (SVTL) shall be established, in conformance with the DRD in Annex C, to collect all the open verification items of the different hazard reports from the safety analysis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.5.1b","Requirement","ECSS-Q-ST-40_0440289","In time for acceptance by the customer, and in preparation of transfer to the next stage of system integration, the safety manager shall verify that: \n    1. hazard close-outs performed so far by the responsible engineer are still valid; \n    2. the verifications reflect the as-built or as-modified status of the hardware;\n    3. all open verifications at this time are acceptable for transfer to the next stage of system integration; \n    4. all open verifications are entered into the verification tracking log (SVTL);\n    5. the verification tracking log is maintained to reflect the current status.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.5.1c","Requirement","ECSS-Q-ST-40_0440290","If the safety verification constrains any ground operations, the safety manager shall give notification to the safety review panel.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.5.2a","Requirement","ECSS-Q-ST-40_0440291","The safety manager shall assure that each hazard considered for closure has the approval by the safety approval authority, verifying that\n    1. hazards not eliminated are controlled in accordance with the applicable requirements and associated verification activities are successfully completed, or, when applicable,\n    2. deviations from, or waivers of requirements, are granted by the safety approval authority.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","8.6a","Requirement","ECSS-Q-ST-40_0440292","All ground equipment that falls into the scope of an applicable ‘New Approach directive’ shall be ‘CE’ marked and supplied with a supporting ‘Declaration of Conformity’ and User Manual detailing all safety warnings.\"\n    NOTE Additional information is provided in Informative Annex G. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.1<1>a","Requirement","ECSS-Q-ST-40_0440293","The safety programme plan shall include a description of the project safety organization, responsibilities, and its working relationship and interfaces with product assurance disciplines (reliability, maintainability, software product assurance, parts, materials and processes and quality assurance according to ECSS-Q-ST-10, -20, -30, -60, -70 and -80), with configuration management according to ECSS-M-ST-40, system engineering according to ECSS-E-ST-10, design and other project functions and departments of organizations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.1<1>b","Requirement","ECSS-Q-ST-40_0440294","The safety programme plan shall describe how the provisions of ECSS-Q-ST-40 are implemented:\n    1. Safety programme and organization;\n    2. Safety engineering;\n    3. Safety analysis requirements and techniques;\n    4. Safety verification;\n    5. Operational safety.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.1<2>a","Requirement","ECSS-Q-ST-40_0440295","The plan shall show how the project safety organization implements concurrent safety and project engineering activities in continuous support of the project design and development process.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.1<3>a","Requirement","ECSS-Q-ST-40_0440296","The plan shall describe how safety-related activities and requirements are defined for and controlled at suppliers’ and lower tier suppliers’ premises.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.1<4>a","Requirement","ECSS-Q-ST-40_0440297","The plan shall make provisions for assuring conformance to safety requirements and regulations that are applicable to any other facilities and service that are utilized during the course of the project. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","B.2.2a","Permission","ECSS-Q-ST-40_0440321","The safety programme plan may be incorporated within the Product Assurance Plan when agreed between the relevant parties.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<1>a","Requirement","ECSS-Q-ST-40_0440299","The SVTL shall identify the following general information:\n    1. name of the project for which it has been established;\n    2. project documentation identification number;\n    3. applicability for flight or ground safety verifications;\n    4. indication of the specific page number followed by the total number of pages;\n    5. name of the equipment, payload or experiment for which the SVTL has been established;\n    6. mission or flight to which the equipment, payload or experiment has been manifested;\n    7. dates of issue and update.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<2>a","Requirement","ECSS-Q-ST-40_0440300","For each verification item to be tracked a unique identifier shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<2>b","Requirement","ECSS-Q-ST-40_0440301","The SVTL shall use the designations assigned by the safety manager.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<3>a","Requirement","ECSS-Q-ST-40_0440302","The identification number of the hazard report containing the verification item shall be indicated.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<4>a","Requirement","ECSS-Q-ST-40_0440303","The verification method or the verification means shall be transferred from the hazard report including the procedures by number and title.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<5>a","Requirement","ECSS-Q-ST-40_0440304","The input of “yes” or “no” shall indicate whether this safety verification constrains any ground operations.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<5>b","Requirement","ECSS-Q-ST-40_0440305","If “yes” for flight tracking log: an attachment shall be provided that identifies which ground operation is constrained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<5>c","Requirement","ECSS-Q-ST-40_0440306","If “yes” for ground tracking log: the ground operation constrained by this verification shall be indicated specifically in the user manual and included as a step in a procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<6>a","Requirement","ECSS-Q-ST-40_0440307","The input of \"yes\" or \"no\" shall indicate whether the verification has to be performed independently (in accordance with 8.4.5b). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<7>a","Requirement","ECSS-Q-ST-40_0440308","The planned date for the completion of the verification shall be indicated.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<8>a","Requirement","ECSS-Q-ST-40_0440309","The SVTL log shall indicate the title and serial number of the tests, review of designs, inspections and analyses by which this verification is formally closed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","C.2.1<8>b","Permission","ECSS-Q-ST-40_0440322","Any appropriate information or remarks may be added.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<1>a","Requirement","ECSS-Q-ST-40_0440311","Title - The title of the safety analysis report shall identify the applicable project. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<1>b","Requirement","ECSS-Q-ST-40_0440312","Title page - A title page shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<1>c","Requirement","ECSS-Q-ST-40_0440313","Contents - A contents list shall be provided. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<1>d","Requirement","ECSS-Q-ST-40_0440314","Foreword - A foreword shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<1>e","Requirement","ECSS-Q-ST-40_0440315","Introduction - An introduction shall be provided.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<2>a","Requirement","ECSS-Q-ST-40_0440316","The safety analysis report shall identify the following general information:\n    1. the project documentation identification number, the title of the safety analysis report, date of release and release authority;\n    2. the project phase;\n    3. identification of which organizational entity prepared the document;\n    4. information regarding the approval of the document;\n    5. a statement of effectivity identifying which other documents have been cancelled and replaced in whole or in part.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<2>b","Requirement","ECSS-Q-ST-40_0440317","The safety analysis report shall contain the following analysis specific information:\n    1. objective of safety analysis;\n    2. applicable requirements relevant to the safety analysis;\n    3. description of system design & operation from a safety point of view;\n    4. description of safety analysis process and methods;\n    5. detailed results of safety analysis documented in form of a set of hazard reports (see D.2.1<2>c.);\n    6. list of safety critical functions;\n    7. safety critical item list;\n    8. safety input to risk management;\n    9. support analyses used (e.g. FTA, FMEA/FMECA);\n    10. overall conclusions from safety assessment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-40C","D.2.1<2>c","Requirement","ECSS-Q-ST-40_0440318","Each hazard report shall contain as a minimum the following data:\n    1. title;\n    2. types of hazards and description of their manifestation in the system design and operational configuration and environment;\n    3. identified hazard scenario with description of causes (associated with the hazard manifestation), hazardous events (physical and functional propagation) and consequences; \n    4. consequence severity category;\n    5. propagation time from cause to consequence;\n    6. likelihood of hazard scenario and magnitude of safety risk (optional);\n    7. applicable safety requirements;\n    8. hazard reduction measures (implementation of safety requirements, hazard elimination or minimization and control);\n    9. verification measures;\n    10. safety risk trend after hazard reduction (optional); \n    11. status (safety verification actions open or closed, non-conformances and waivers);\n    12. approval;\n    13. acceptance of safety risk (optional).\n        NOTE Example of formats that can be used for “Hazard and safety risk register”, and “Ranked hazard and safety risk log” are given in the annexes of ECSS-Q-ST-40-02. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70-26C","5.1.1.2a","Requirement","ECSS-Q-ST-70-26_0130001","The supplier shall provide cleaning services for production facilities of high reliability crimping.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.2b","Requirement","ECSS-Q-ST-70-26_0130002","The areas, in which crimping is carried out, shall be maintained in an orderly fashion.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.2c","Requirement","ECSS-Q-ST-70-26_0130003","Loose material that can cause contamination of the crimped connection shall be removed. \n    NOTE For example: Dirt, dust, oils and clipped wires.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.2d","Requirement","ECSS-Q-ST-70-26_0130004","Furniture shall be kept to a minimum in the work areas and be arranged to allow easy and thorough cleaning of the floor.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.2e","Requirement","ECSS-Q-ST-70-26_0130005","Working surfaces shall be covered with an easily cleaned hard top or have a replaceable surface of clean, non-corrosive silicone-free paper.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.3a","Requirement","ECSS-Q-ST-70-26_0130006","The crimping area shall have a controlled environment, which limits entry of contamination. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.3b","Requirement","ECSS-Q-ST-70-26_0130007","The area shall be continuously controlled as follows:\n    1. room temperature:(22 ± 3) °C;\n    2. relative humidity: (55 ± 10) %.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.3c","Requirement","ECSS-Q-ST-70-26_0130008","The workstations shall not be exposed to draughts.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.3d","Requirement","ECSS-Q-ST-70-26_0130009","Fresh air shall be supplied to the room through a filtering system with positive pressure difference with regard to adjacent rooms.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.3e","Requirement","ECSS-Q-ST-70-26_0130010","The exhaust air shall be suitably restricted.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.4a","Requirement","ECSS-Q-ST-70-26_0130011","The supplier shall ensure adequate illumination conditions of the crimp workstations.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.4b","Requirement","ECSS-Q-ST-70-26_0130012","The light intensity shall be 1 080 lux on the work surface. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.1.4c","Requirement","ECSS-Q-ST-70-26_0130013","90 % of the work area shall be shadowless and without severe reflections.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1a","Requirement","ECSS-Q-ST-70-26_0130014","The supplier shall provide the tooling necessary for continued high quality crimping.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1b","Requirement","ECSS-Q-ST-70-26_0130015","Tools used shall employ an integral mechanism, which controls the crimping operation in conformance to MIL-DTL-22520G.\n    NOTE The mechanism ensures that, once the operation is started, the tool cannot be opened until the crimping cycle is complete.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1c","Requirement","ECSS-Q-ST-70-26_0130016","Tools shall be marked to show the size and type of termination for which it is calibrated.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1d","Requirement","ECSS-Q-ST-70-26_0130017","Tool calibration shall be verified once each shift in conformance with the clause 5.5.5 requirements.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1e","Requirement","ECSS-Q-ST-70-26_0130018","Proper operation of the integral ratcheting mechanism or the positive stops on pneumatic tools shall be verified as defined in clause 5.5.6.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1f","Requirement","ECSS-Q-ST-70-26_0130019","Before starting a crimping process on a new terminal size and wire type, tools used for crimping of the previous wire type shall be returned to the tool facility.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1g","Requirement","ECSS-Q-ST-70-26_0130020","If the tool settings seals are broken, the tool shall be returned immediately for recalibration.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.1h","Requirement","ECSS-Q-ST-70-26_0130021","Tools used in the crimping operation shall be clean; excess lubricants shall be removed before crimping starts.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.2a","Requirement","ECSS-Q-ST-70-26_0130022","The supplier shall provide the tooling necessary to avoid damage to the conductor.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.2b","Requirement","ECSS-Q-ST-70-26_0130023","The selection of thermal or precision cutting devices, manual or automatic power-driven, shall provide protection of the conductor strands. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.2c","Requirement","ECSS-Q-ST-70-26_0130024","Wire stretching by use of mechanical strippers shall be avoided.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.2d","Requirement","ECSS-Q-ST-70-26_0130025","The conductor shall not be twisted, ringed, nicked, cut or scored by stripping operation.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.2e","Requirement","ECSS-Q-ST-70-26_0130026","Both thermal and mechanical stripping tools shall be calibrated periodically on sample evaluation during a production run.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.3a","Requirement","ECSS-Q-ST-70-26_0130027","The supplier shall provide the tooling necessary for precision wire trimming and cutting.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.3b","Requirement","ECSS-Q-ST-70-26_0130028","The cutter used for trimming conductor wire shall shear sharply and consistently produce a clean, flat, smooth-cut surface along the entire cutting edge. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.3c","Requirement","ECSS-Q-ST-70-26_0130029","Twisting action during cutting operation shall be avoided. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.3d","Requirement","ECSS-Q-ST-70-26_0130030","Smooth, long-nose pliers or tweezers shall be used for attaching or removing conductor wire.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.3e","Requirement","ECSS-Q-ST-70-26_0130031","The cutting edges of pliers shall be regularly checked for damage and maintained in a sharp condition.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.1.2.4a","Requirement","ECSS-Q-ST-70-26_0130032","The supplier shall provide the equipment specified in Table 5-1 necessary for verification activities specified in clauses 5.4.2 and 5.4.3. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1a","Requirement","ECSS-Q-ST-70-26_0130033","The supplier shall visually examine wire, terminal and connector contacts for cleanliness, absence of oil films and freedom from tarnish or corrosion before assembly.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1b","Requirement","ECSS-Q-ST-70-26_0130034","The supplier shall perform cleaning of the work pieces in conformance with ECSS-Q-ST-70-08. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1c","Requirement","ECSS-Q-ST-70-26_0130035","Further cleaning or other treatment shall not be carried out.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1d","Requirement","ECSS-Q-ST-70-26_0130036","The supplier shall handle work pieces with clean lint free gloves or finger cots.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1e","Requirement","ECSS-Q-ST-70-26_0130037","Before a crimping activity, tools at the operator’s station shall be verified to conform to those selected in accordance with the applicable PID.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1f","Requirement","ECSS-Q-ST-70-26_0130038","All conductor strands shall be inserted cleanly into the barrel without any buckling. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1g","Requirement","ECSS-Q-ST-70-26_0130039","Strands shall not be left outside or cut back to reduce the conductor diameter to fit an undersized barrel. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1h","Requirement","ECSS-Q-ST-70-26_0130040","The supplier shall use tools specified in MIL-DTL-22520.\n    NOTE Examples of crimping parameters are given in Table A-2 and Table A-3",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1i","Requirement","ECSS-Q-ST-70-26_0130041","The supplier shall take provisions to avoid degradation of the silver plated wire caused by tarnish during storage. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.1j","Requirement","ECSS-Q-ST-70-26_0130042","In cases when the same wire is joined later by soldering, the solder fluxes prescribed in ECSS-Q-ST-70-08 shall be used to avoid degradation.\n    NOTE For shift performance inspection requirements see clause 5.5.5.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2a","Requirement","ECSS-Q-ST-70-26_0130043","The supplier shall use silver plated copper multi stranded wire and braided shield cable in crimp type connectors. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2b","Requirement","ECSS-Q-ST-70-26_0130044","Exceptional cases when nickel- or tin-plated wires are used shall be approved by the customer through a request for approval (RFA), in conformance with ECSS-Q-ST-70, clause 5.1.4.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2c","Requirement","ECSS-Q-ST-70-26_0130045","The supplier shall use high strength copper alloy wire for 24 AWG, 26 AWG and 28 AWG crimped joints.\n    NOTE Soft or annealed copper wire are not acceptable for crimped joints of 24 AWG, 26 AWG and 28 AWG size. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2d","Requirement","ECSS-Q-ST-70-26_0130046","The supplier shall use space-qualified components having gold plated terminals in conformance with ECSS-Q-ST-60.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2e","Requirement","ECSS-Q-ST-70-26_0130047","Specific terminals such as ferrules, splices and lugs shall be purchased to MIL or SAE-AS-7928 specifications. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2f","Requirement","ECSS-Q-ST-70-26_0130048","When gold plating is not available the finish shall be in conformance with ECSS-Q-ST-70-71.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.2g","Requirement","ECSS-Q-ST-70-26_0130049","Cadmium, chromate-coated cadmium and non-fused tin-plating shall not be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.3a","Requirement","ECSS-Q-ST-70-26_0130050","The supplier shall perform a review of all the materials, tools and techniques planned to be used to ensure conformance to requirements of this standard and as a means of identifying potential problems.\n    NOTE Type of wire includes number of strands, plating metal, type and thickness of insulation.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.3b","Requirement","ECSS-Q-ST-70-26_0130051","Dies, setting of controls for the length of strip in automatic stripping machines and the selection of specific locators or positioners, shall be selected to meet process requirements.\n    NOTE The requirement is valid for power driven and manual crimping processes as well as for size and tolerance for crimping tools",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.3c","Requirement","ECSS-Q-ST-70-26_0130052","The results of the review shall be documented in a PID in conformance with DRD of ECSS-Q-ST-70-38.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4a","Requirement","ECSS-Q-ST-70-26_0130053","The supplier shall give preference to the selection of single wire interconnections.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4b","Requirement","ECSS-Q-ST-70-26_0130054","The supplier shall not use strands of wire doubled backed to increase the conductor diameter.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4c","Requirement","ECSS-Q-ST-70-26_0130055","The supplier shall use additional stranded wires to increase the cross-sectional area up to a selected barrel size; \n    NOTE The requirement is applied for cases where the insulation is prepared as normal and transparent “shrink-fit insulation” to cover the loose end of the wire to prevent any risk of a short circuit.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4d","Requirement","ECSS-Q-ST-70-26_0130056","For 28 AWG up to 16 AWG wire sizes, the maximum insulation clearance shall be equal to the outside diameter (over the insulation) of the wire being used. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4e","Requirement","ECSS-Q-ST-70-26_0130057","The gaps for larger size wires shall not exceed 2 mm.\n    NOTE No minimum gap is specified except that the conductor wire shall be visible to permit inspection.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.4f","Requirement","ECSS-Q-ST-70-26_0130058","Where the terminal or contact is supplied with insulation support, the wire insulation shall enter the support to the extent that no bare wire is exposed. \n    NOTE An example of a typical connector barrel and single wire crimping is shown Figure 5-1.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5a","Requirement","ECSS-Q-ST-70-26_0130059","Requirements of this clause shall be applied when single wire crimping cannot be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5b","Requirement","ECSS-Q-ST-70-26_0130060","The maximum number of wires in one crimp barrel shall be two.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5c","Requirement","ECSS-Q-ST-70-26_0130061","The sum of the two nominal conductor sections shall be compatible with the crimp barrel used \n    NOTE 2 ´ 24 AWG is approximately equal to 1 ´ 20 AWG.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5d","Requirement","ECSS-Q-ST-70-26_0130062","Both conductors shall be of the same material and support the same plating finish.\n    NOTE 1 For example: Both are silver and not a combination of silver and nickel\n    NOTE 2 Before introduction into the barrel wires or conductors can be twisted to obtain a “single” conductor.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5e","Requirement","ECSS-Q-ST-70-26_0130063","Axial strength measurements shall be performed on the two associated wires and the axial strength shall be 75 % of the sum of the two wires axial strength requirements.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.5f","Requirement","ECSS-Q-ST-70-26_0130064","For separate conductors introduced into the barrel the following shall apply: \n    1. the actual strength measurement is performed on one of the wires (the smaller, if two different sizes are used);\n    2. the axial strength requirement is as quoted in Table 5-3 for the actual size of wire pulled, assuming a barrel size equal to that wire’s gauge.\n        NOTE Examples of crimping parameters are given in Table A-1 and an example of a typical connector barrel and multi-wire crimping is shown in Figure 5-2.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.6a","Requirement","ECSS-Q-ST-70-26_0130065","The shielded wires on coaxial cables shall be braided.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.6b","Requirement","ECSS-Q-ST-70-26_0130066","Axial strength measurements shall be performed only on the shield after removal of the core dielectric.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.6c","Requirement","ECSS-Q-ST-70-26_0130067","Following crimping, the assembly shall be protected by shrink tubing.\n    NOTE Examples of crimping parameters are given in Table A-3 and an example of a typical ferrule shield crimping is shown in Figure 5-3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7a","Requirement","ECSS-Q-ST-70-26_0130068","Tools specified by the manufacturer of the terminals shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7b","Requirement","ECSS-Q-ST-70-26_0130069","The maximum number of wires shall be ten.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7c","Requirement","ECSS-Q-ST-70-26_0130070","Seven wires maximum shall be on the same side.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7d","Requirement","ECSS-Q-ST-70-26_0130071","All conductors shall be of the same material and within a size range of 4 wire gauges on the same side.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7e","Requirement","ECSS-Q-ST-70-26_0130072","All conductors shall be positioned parallel in the terminal before crimping.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7f","Requirement","ECSS-Q-ST-70-26_0130073","Axial strength measurements shall be performed on \n    1. all of the grouped wires for groups with equal wire sizes\n    2. on the smallest wire for groups with different wire sizes.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7g","Requirement","ECSS-Q-ST-70-26_0130074","In the case where opposed wires are tested a specifically designed test fixture shall be used. \n    NOTE A typical test fixture is shown in Figure A-6.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.2.7h","Requirement","ECSS-Q-ST-70-26_0130075","Following crimping, the assembly shall be protected by shrink tubing.\n    NOTE Examples of typical lug and splice wire crimping are shown in Figure 5-4.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.1a","Requirement","ECSS-Q-ST-70-26_0130076","Requirement of this clause shall be applied to crimp configurations that are not specified in clauses 5.2.4 to 5.2.7",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.1b","Requirement","ECSS-Q-ST-70-26_0130077","The supplier shall document the data of successful process qualification in the PID format to ensure continued high quality of production performance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.1c","Requirement","ECSS-Q-ST-70-26_0130078","An approved PID and additional relevant data from a previous project shall be presented to substantiate a RFA.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.2a","Requirement","ECSS-Q-ST-70-26_0130079","The supplier shall perform tensile strength and voltage drop tests on samples prepared at a number of tool settings, in conformance with the methods defined in clause 5.4 and in conformance with the following process:\n    1. Ten samples prepared at the point specified by the crimping tool manufacturer as a starting point for calibrating tools and pulled (in conformance with Table A-1, Table A-2 and Table A-3).\n    2. The tool indenter opening is then adjusted in convenient increments above and below this point, and ten samples pulled at each increment. \n    3. Voltage drop tests are then performed on five samples for each tool setting.\n    4. A plot is made with increments being close enough together to obtain a smooth curve.\n    5. The minimum in voltage drop and maximum in tensile strength is then determined and evaluated as per Table 5-2 and Table 5-3.\n    6. The design value or operating point should lie approximately in the middle of the flat top portion of the tensile-strength plot, as per Figure 5-5",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.2b","Requirement","ECSS-Q-ST-70-26_0130080","The supplier shall validate satisfactory results achieved from the final tool setting at the operating point in conformance with the methods defined in clause 5.4 and according to the following process: \n    1. Tensile strength tests are performed on five samples corresponding to the operating point.\n    2. Voltage drop tests are performed on five samples corresponding to the operating point.\n    3. Metallographic tests are performed on a minimum of three of these samples corresponding to the operating point.\n    4. Not tested samples are retained for reference.\n        NOTE This approach is conducted from the variation of the main parameter involved to the relevant terminal crimping.\n            a. Connector barrel crimping: selector setting;\n            b. Ferrule crimping: die selection;\n            c. Lug and splice crimping: total cross-section of stranded wires.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.2c","Requirement","ECSS-Q-ST-70-26_0130081","Test data shall be recorded for PID justification.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.3.3a","Requirement","ECSS-Q-ST-70-26_0130082","The supplier shall seal and mark calibrated tools in conformance with clause 5.5.6.3 requirements.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.1a","Requirement","ECSS-Q-ST-70-26_0130083","The supplier shall submit samples to the tests detailed below. \n    NOTE The number of samples is dependent on the specific process requirement (in conformance with clauses 5.3.2 , 5.5.5 and 5.5.6.2 requirements). ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.1b","Requirement","ECSS-Q-ST-70-26_0130084","Test samples shall meet the requirements of clause 5.5.4.1. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.1c","Requirement","ECSS-Q-ST-70-26_0130085","Records of all results shall be tabulated in conformance with 5.5.7. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.2a","Requirement","ECSS-Q-ST-70-26_0130086","The supplier shall measure the voltage drop from a point on the positioning shoulder of the contact to another point 14 mm distant on the attached wire (in conformance with the Table 5-2). ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.2b","Requirement","ECSS-Q-ST-70-26_0130087","In cases of two or more wires being crimped in the same contact, lug or splice, the voltage drop measurement shall be performed on each wire. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.2c","Requirement","ECSS-Q-ST-70-26_0130088","The voltage drop of the contact crimp joint shall not exceed the value specified in Table 5-2 for each wire tested.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.1a","Requirement","ECSS-Q-ST-70-26_0130089","The supplier shall use a tensile testing device with characteristics in conformance with Table 5-1. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.1b","Requirement","ECSS-Q-ST-70-26_0130090","The connections shall be loaded until failure occurs. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.1c","Requirement","ECSS-Q-ST-70-26_0130091","The value at failure shall be recorded, together with the information as to whether the failure was “pull-out”, “broke in crimp” or “break in wire”. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.1d","Requirement","ECSS-Q-ST-70-26_0130092","The required ultimate axial strengths for compacted and dispersive crimped joints shall be as shown in Table 5-3 and in clauses 5.4.3.2 and 5.4.3.3.\n    NOTE 1 The insulation may be stripped approximately 2 cm on test specimens to promote visual inspection of the mode of failure in the tensile test.\n    NOTE 2 The required ultimate axial strength values for crimped copper alloy wire are calculated based on the requirement of a minimum wire strength of 343 N/mm\n    NOTE 3 A typical test fixture for testing lug and splice crimps is shown in Figure A-6",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.2a","Requirement","ECSS-Q-ST-70-26_0130093","The required axial strength shall be 75 % of the wire strength.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.2b","Requirement","ECSS-Q-ST-70-26_0130094","Axial strength for copper and copper-alloy wires having either silver-, tin- or nickel-plated finishes shall be as specified in Table 5-3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.3.3a","Requirement","ECSS-Q-ST-70-26_0130095","The required axial strength shall be:\n    1. 70 % of the shield strength,\n    2. 70 % of one of the smallest gauge wires within the connection if pulled individually, or\n    3. 70 % of the sum of all the wires axial strength requirements if all wires are pulled together.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4a","Requirement","ECSS-Q-ST-70-26_0130096","The supplier shall employ a certified laboratory to perform the metallographic tests described below.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4b","Requirement","ECSS-Q-ST-70-26_0130097","The customer shall approve the certification status of the laboratory.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4c","Requirement","ECSS-Q-ST-70-26_0130098","The joint to be sectioned shall be mounted in a low exotherm resin capable of being moulded without the application of external pressure. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4d","Requirement","ECSS-Q-ST-70-26_0130099","The joint shall be oriented that the wire is perpendicular to the polishing surface. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4e","Requirement","ECSS-Q-ST-70-26_0130100","The specimen shall be ground with the aid of appropriate grades of silicon carbide papers, in order to expose the mid-section of the joint. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4f","Requirement","ECSS-Q-ST-70-26_0130101","This section shall then be polished with successively finer grades of diamond paste down to 1 µm. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4g","Requirement","ECSS-Q-ST-70-26_0130102","To aid microscopic examination, the polished section shall be very lightly etched with an accepted chemical reagent specific to the composition of the materials being crimped.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4h","Requirement","ECSS-Q-ST-70-26_0130103","The section shall be examined in both as-polished and etched states using a metallographic microscope at a magnification up to ´400.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.4.4i","Requirement","ECSS-Q-ST-70-26_0130104","The following acceptance criteria shall be met:\n    1. Each micro section is free from contamination;\n    2. The crimp barrel is evenly deformed;\n    3. Voids occupy less than 10 % of the cross sectioned area of the wire volume;\n    4. The wires and barrel appear as a gas-tight joint and conform to the workmanship sample prepared during qualification;\n    5. All wires are deformed from their circular cross section;\n    6. There are no indentations or fracturing of the deformed receptacle barrel or its plated finish.\n        NOTE 1 For ferrule shield crimping the requirements of 5.4.4i.3. and 5. are not applicable.\n        NOTE 2 For wire barrel contact size 20 - 18 the requirement 5.4.4i.3. is not applicable due to localized voiding at the crimp corners.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.1a","Requirement","ECSS-Q-ST-70-26_0130105","The supplier shall install a Quality Assurance (QA) function in conformance with the requirements as defined in ECSS-Q-ST-20. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.1b","Requirement","ECSS-Q-ST-70-26_0130106","The quality control process shall be as specified in Figure 5-7.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.1a","Requirement","ECSS-Q-ST-70-26_0130107","The supplier shall employ trained and competent personnel for all crimping operations. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.1b","Requirement","ECSS-Q-ST-70-26_0130108","The supplier shall develop, maintain and implement a training programme, in conformance with ECSS-Q-ST-20. \n    NOTE The aim of the training programme is to provide for excellence of workmanship and personnel skills, careful and safe operations, and improvement of the quality of crimped joints.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.2a","Requirement","ECSS-Q-ST-70-26_0130109","Trained personnel, performing crimping operations, shall be certified according to a customer approved process ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.2b","Requirement","ECSS-Q-ST-70-26_0130110","The certification of personnel shall be based upon objective evidence of crimp quality, resulting from test and inspection of the crimped joints. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.2c","Requirement","ECSS-Q-ST-70-26_0130111","Operators or inspectors shall be re-certified in cases of repeatedly unacceptable quality levels and changes in crimping techniques, parameters or required skills.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.2d","Requirement","ECSS-Q-ST-70-26_0130112","The supplier shall perform training and certification at a school authorized by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.2.3a","Requirement","ECSS-Q-ST-70-26_0130113","The supplier shall maintain records of the training and certification status of crimping operators and inspection personnel.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.3a","Requirement","ECSS-Q-ST-70-26_0130114","The supplier shall prepare standards consisting of satisfactory work samples (in conformance with the Figure 5-8 and Figure 5-9)",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.3b","Requirement","ECSS-Q-ST-70-26_0130115","The supplier shall have readily available visual aids, which clearly illustrate the quality characteristics of all crimped connections utilized. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.3c","Requirement","ECSS-Q-ST-70-26_0130116","Defects such as those listed in clause 5.5.4.2 and shown in Figure 5-8 shall be included as examples.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.3d","Requirement","ECSS-Q-ST-70-26_0130117","The operator shall discard production crimps which in his judgement are defective.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.3e","Requirement","ECSS-Q-ST-70-26_0130118","Defective test samples shall not be discarded.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.1a","Requirement","ECSS-Q-ST-70-26_0130119","The operator shall examine the wire for nicks, rings, broken strands, untwisted lay or not-removed insulation in the area of the crimp before the stripped wire is inserted into the contact or terminal barrel. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.1b","Requirement","ECSS-Q-ST-70-26_0130120","Damaged wires where the base material is exposed shall not be used. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.1c","Requirement","ECSS-Q-ST-70-26_0130121","Contacts and terminal barrels that show evidence of the presence of tarnish, corrosion or physical damage, including bent contacts, shall not be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.1d","Requirement","ECSS-Q-ST-70-26_0130122","Inspection shall verify that wire size and type, the contact and terminal are as specified in the drawing or control document.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.2a","Requirement","ECSS-Q-ST-70-26_0130123","The QA inspector shall carry out inspection with the aid of a binocular microscope having an initial linear magnification of ´7. \n    NOTE Further examination of surface characteristics can be performed at higher magnifications. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.2b","Requirement","ECSS-Q-ST-70-26_0130124","The inspector shall not physically disturb parts and conductor leads to aid inspection. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.2c","Requirement","ECSS-Q-ST-70-26_0130125","The following acceptance criteria shall be met; \n    1. Insulation is not damaged by the crimping tool or the terminal;\n    2. The conductor is visible in the inspection hole when an inspection hole is provided;\n    3. The crimp barrel has no unintentional sharp edges, peeled metal, burrs, cracked platings or cuts after crimping;\n    4. All functional parts, including all retention clips or locking devices, are operational after the crimp has been made;\n    5. No tarnished or corroded contacts are present;\n    6. No misplaced crimps, as determined by marks found on areas not designed to take crimping, are present;\n    7. No undercrimps or overcrimps are present;\n        NOTE An undercrimp is detected by a loose conductor and an overcrimp by broken strands or deformed wire at end of terminal.\n    8. If undercrimps or overcrimps are detected this is cause to stop \n        · operations at that station, \n        · reject all production crimps made since the last verification or pull test, \n        · investigate tool, wire and terminals for the cause of failure.\n    9. No bent contacts are present.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.4.2d","Requirement","ECSS-Q-ST-70-26_0130126","Failure to meet the acceptance criteria of 5.5.4.2c shall be cause for rejection.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5a","Requirement","ECSS-Q-ST-70-26_0130127","Each operator shall prepare four samples at the beginning of a shift or before a series of crimping operations.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5b","Requirement","ECSS-Q-ST-70-26_0130128","At the end of the operation four further samples shall be crimped. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5c","Requirement","ECSS-Q-ST-70-26_0130129","Alternatively the supplier shall keep a logbook for each tool. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5d","Requirement","ECSS-Q-ST-70-26_0130130","The logbook shall show the quantity of parts crimped since each calibration and since each go/no-go operation. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5e","Requirement","ECSS-Q-ST-70-26_0130131","Four samples shall be crimped after each 100 crimping operations have been performed.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5f","Requirement","ECSS-Q-ST-70-26_0130132","A tool shall be changed whenever a wire size or contact size is changed. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5g","Requirement","ECSS-Q-ST-70-26_0130133","The operator shall prepare four samples at the start of the operation after such a change.\n    NOTE This can be omitted if samples have already been prepared by the tool during the shift.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5h","Requirement","ECSS-Q-ST-70-26_0130134","In each case, the operator shall submit three samples to the tensile strength test detailed in clause 5.4.3. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5i","Requirement","ECSS-Q-ST-70-26_0130135","The fourth sample shall be retained for reference and traceability purposes (in conformance with clause 5.5.6.2 requirements).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.5j","Requirement","ECSS-Q-ST-70-26_0130136","The supplier shall perform an analysis of shift performance test results, in comparison with initial tool calibration results, to determine any drift in tool performance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.1a","Requirement","ECSS-Q-ST-70-26_0130137","The QA organization of the supplier shall ensure that each crimping tool and piece of measuring equipment is calibrated as indicated in the subsequent sub clauses. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.1b","Requirement","ECSS-Q-ST-70-26_0130138","The QA organization of the supplier shall record any suspected and actual equipment failure as a project nonconformance report \n    NOTE Based on past nonconformance reports previous results can be examined to ascertain whether or not re-inspection or retesting is required. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.1c","Requirement","ECSS-Q-ST-70-26_0130139","The QA organization of the supplier shall notify the customer of the nonconformance details.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.1d","Requirement","ECSS-Q-ST-70-26_0130140","The supplier’s calibration procedure shall include the requirements specified in this clause for tool calibration.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.2a","Requirement","ECSS-Q-ST-70-26_0130141","The QA organization of the supplier shall ensure that crimping tools, both manual and powered, are calibrated when initially set up for each specific wire size, connection size and type prior to first use. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.2b","Requirement","ECSS-Q-ST-70-26_0130142","Calibration shall be verified in conformance with the following check-list:\n    1. cleanliness control of the active part of the tool (e.g. indenters);\n    2. set up with the aid of the “go/no-go” gauge in conformance with specified conditions;\n    3. tests in conformance with the clause 5.4 requirements on not less than four samples.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.2c","Requirement","ECSS-Q-ST-70-26_0130143","After satisfactory calibration the tool status shall be documented in a “tool calibration sheet” to ensure tool traceability.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.2d","Requirement","ECSS-Q-ST-70-26_0130144","This traceability shall be established by periodic analysis of the corresponding data from the shift performance inspection and tests (in conformance with clause 5.5.5 requirements), \n    NOTE The frequency of analysis is defined in relation to production activity such as six months or 2 500 crimping operations.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.2e","Requirement","ECSS-Q-ST-70-26_0130145","A significant drift in test results shall result in tool rejection.\n    NOTE Such a tool is generally labelled \"out-of-calibration tool\" (in conformance with clause 5.5.6.4 requirements).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.3a","Requirement","ECSS-Q-ST-70-26_0130146","The supplier shall provide sealing for calibrated crimping tools to ensure against unauthorized alteration of adjustment settings. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.3b","Requirement","ECSS-Q-ST-70-26_0130147","A wire and lead seal method shall be used if the tool has provisions for it; ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.3c","Requirement","ECSS-Q-ST-70-26_0130148","Alternatively, the tool shall be sealed by a non-reusable decal seal, which, if the calibrated setting is altered, is visibly damaged. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.3d","Requirement","ECSS-Q-ST-70-26_0130149","Seals shall be placed on all external adjustment points of the tool.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.4a","Requirement","ECSS-Q-ST-70-26_0130150","Tools that are out of calibration shall be returned to the tool facility for readjustment and calibration. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.6.4b","Requirement","ECSS-Q-ST-70-26_0130151","Tools that are worn or damaged shall be identified as rejected and removed from the fabrication area.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.7a","Requirement","ECSS-Q-ST-70-26_0130152","The supplier shall maintain traceability throughout the process from incoming inspection to final test, including details of test equipment, tools and personnel employed in performing the task.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.7b","Requirement","ECSS-Q-ST-70-26_0130153","Quality records and logbooks shall be retained for at least ten years ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.7c","Requirement","ECSS-Q-ST-70-26_0130154","Quality records and logbooks shall contain the following information:\n    1. the as-built and test configuration list (waiver and deviation summary);\n    2. non conformance reports and corrective actions;\n    3. copy of the visual inspection and shift performance test results with reference to the relevant procedure, personnel and tools used;\n    4. records of the training, testing and certification status of crimping operators (in conformance with clause 5.5.3 requirements) and ECSS-Q-ST-70-08.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.8a","Requirement","ECSS-Q-ST-70-26_0130155","The QA organization of the supplier shall disposition any nonconformance which is observed in respect of the process in conformance with the quality assurance requirements, in conformance with ECSS-Q-ST-20-09. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.5.8b","Requirement","ECSS-Q-ST-70-26_0130156","Failure of a crimping tool to pass any requirement specified in clause 5.1.2.1 shall require rejection of all crimps made by that tool since it was last tested successfully for acceptance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.6a","Requirement","ECSS-Q-ST-70-26_0130157","The supplier shall produce documentation for: \n    1. Process identification, PID and RFA,\n    2. Inspection,\n    3. Traceability,\n    4. Testing, both procedures and records,\n    5. Logbooks, and\n    6. Calibration.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-26C","5.6b","Requirement","ECSS-Q-ST-70-26_0130158","The format of the documents shall be in accordance with the deliverables item list defined in the business agreement.\n    NOTE No specific DRD requirements emerge from this Standard.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-80C","5.1.1a","Requirement","ECSS-Q-ST-80_0720001","The supplier shall ensure that an organizational structure is defined for software development, and that individuals have defined tasks and responsibilities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.2.1a","Requirement","ECSS-Q-ST-80_0720002","The responsibility, the authority and the interrelation of personnel who manage, perform and verify work affecting software quality shall be defined and documented.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.2.2a","Requirement","ECSS-Q-ST-80_0720003","The responsibilities and the interfaces of each organisation, either external or internal, involved in a project shall be defined and documented.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.2.3a","Requirement","ECSS-Q-ST-80_0720004","The delegation of software product assurance tasks by a supplier to a lower level supplier shall be done in a documented and controlled way, with the supplier retaining the responsibility towards the customer.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.3.1a","Requirement","ECSS-Q-ST-80_0720005","The supplier shall provide adequate resources to perform the required software product assurance tasks.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.3.2a","Requirement","ECSS-Q-ST-80_0720006","Reviews and audits of processes and of products shall be carried out by personnel not directly involved in the work being performed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.4.1a","Requirement","ECSS-Q-ST-80_0720007","The supplier shall identify the personnel responsible for software product assurance for the project (SW PA manager/engineer).\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.4.2a","Requirement","ECSS-Q-ST-80_0720008","The software product assurance manager/engineer shall\n    1. report to the project manager (through the project product assurance manager, if any);\n    2. have organisational authority and independence to propose and maintain a software product assurance programme in accordance with the project software product assurance requirements;\n    3. have unimpeded access to higher management as necessary to fulfil his/her duties.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.5.1a","Requirement","ECSS-Q-ST-80_0720009","The supplier shall review the project requirements to establish and make timely provision for acquiring or developing the resources and skills for the management and technical staff.\n","EXPECTED OUTPUT: Training plan [MGT, -; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.5.2a","Requirement","ECSS-Q-ST-80_0720010","The supplier shall maintain training records.\n","EXPECTED OUTPUT: Records of training and experience [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.5.3a","Requirement","ECSS-Q-ST-80_0720011","The supplier shall ensure that the right composition and categories of appropriately trained personnel are available for the planned activities and tasks in a timely manner.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.1.5.4a","Requirement","ECSS-Q-ST-80_0720012","The supplier shall determine the training subjects based on the specific tools, techniques, methodologies and computer resources to be used in the development and management of the software product. \n    NOTE Personnel can undergo training to acquire skills and knowledge relevant to the specific field with which the software is to deal.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.1a","Requirement","ECSS-Q-ST-80_0720013","The supplier shall develop a software product assurance plan in response to the software product assurance requirements in conformance with DRD in annex B.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.1b","Requirement","ECSS-Q-ST-80_0720014","The software product assurance plan shall be either a standalone document or a section of the supplier overall product assurance plan.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.2a","Requirement","ECSS-Q-ST-80_0720015","Any internal manuals, standards or procedures referred to by the software product assurance plan shall become an integral part of the supplier’s software product assurance programme.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.3a","Requirement","ECSS-Q-ST-80_0720016","The software product assurance plan shall be revisited and updated as needed at each milestone to ensure that the activities to be undertaken in the following phase are fully defined.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.4a","Requirement","ECSS-Q-ST-80_0720017","Before acceptance review, the supplier shall either supplement the software product assurance plan to specify the quality measures related to the operations and maintenance processes, or issue a specific software product assurance plan. \n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.5a","Requirement","ECSS-Q-ST-80_0720018","The supplier shall provide with the software product assurance plan a compliance matrix documenting conformance with the individual software product assurance requirements applicable for the project or business agreement.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.1.5b","Requirement","ECSS-Q-ST-80_0720019","For each software product assurance requirement, the compliance matrix shall provide a reference to the document where the expected output of that requirement is located.\n    NOTE For compliance with the required DRDs a general statement of compliance is acceptable.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.2.1a","Requirement","ECSS-Q-ST-80_0720020","The supplier shall report on a regular basis on the status of the software product assurance programme implementation, if appropriate as part of the overall product assurance reporting of the project.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.2.2a","Requirement","ECSS-Q-ST-80_0720021","The software product assurance report shall include:\n    1. an assessment of the current quality of the product and processes, based on measured properties, with reference to the metrication as defined in the software product assurance plan;\n    2. verifications undertaken;\n    3. problems detected;\n    4. problems resolved. \n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.2.3a","Requirement","ECSS-Q-ST-80_0720022","The supplier shall deliver at each milestone review a software product assurance milestone report, covering the software product assurance activities performed during the past project phases.\n","EXPECTED OUTPUT: Software product assurance milestone report [PAF, SPAMR; SRR, PDR, CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.3a","Requirement","ECSS-Q-ST-80_0720023","For software audits, ECSS-Q-ST-10 clause 5.2.3 shall apply.\n","EXPECTED OUTPUT: Audit plan and schedule [PAF, -; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.4a","Requirement","ECSS-Q-ST-80_0720024","For software alerts, ECSS-Q-ST-10 clause 5.2.9 shall apply.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Preliminary alert information [PAF, -; -];\n          b.Alert information [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.5.1a","Requirement","ECSS-Q-ST-80_0720025","The supplier shall define and implement procedures for the logging, analysis and correction of all software problems encountered during software development.\n","EXPECTED OUTPUT: Software problem reporting procedures [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.5.2a","Requirement","ECSS-Q-ST-80_0720026","The software problem report shall contain the following information:\n    1. identification of the software item;\n    2. description of the problem;\n    3. recommended solution;\n    4. final disposition;\n    5. modifications implemented (e.g. documents, code, and tools);\n    6. tests re-executed.\n","EXPECTED OUTPUT: Software problem reporting procedures [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.5.3a","Requirement","ECSS-Q-ST-80_0720027","The procedures for software problems shall define the interface with the nonconformance system (i.e. the circumstances under which a problem qualifies as a nonconformance).\n","EXPECTED OUTPUT: Software problem reporting procedures [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.5.4a","Requirement","ECSS-Q-ST-80_0720028","The supplier shall ensure the correct application of problem reporting procedures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.6.1a","Requirement","ECSS-Q-ST-80_0720029","For software nonconformance handling, ECSS-Q-ST-10-09 shall apply \n","EXPECTED OUTPUT: The following outputs are expected:\n          a.NCR SW procedure as part of the Software product assurance plan [PAF, SPAP; SRR];\n          b.Nonconformance reports [DJF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.6.1b","Requirement","ECSS-Q-ST-80_0720030","When dealing with software nonconformance, the NRB shall include, at least, a representative from the software product assurance and the software engineering organizations.\n","EXPECTED OUTPUT: Identification of SW experts in NRB [MGT, -; SRR]",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.6.2a","Requirement","ECSS-Q-ST-80_0720031","The software product assurance plan shall specify the point in the software life cycle from which the nonconformance procedures apply.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.7.1a","Requirement","ECSS-Q-ST-80_0720032","Quality models shall be used to specify the software quality requirements.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.2.7.2a","Requirement","ECSS-Q-ST-80_0720033","The following characteristics shall be used to specify the quality model:\n    1. functionality;\n    2. reliability;\n    3. maintainability;\n    4. reusability;\n    5. suitability for safety;\n    6. security;\n    7. usability;\n    8. efficiency;\n    9. portability;\n    10. software development effectiveness.\n        NOTE 1 Quality models are the basis for the identification of process metrics (see clause 6.2.5) and product metrics (see clause 7.1.4).\n        NOTE 2 quality models are also addressed by ISO/IEC 9126 or ECSS-Q-HB-80-04.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.3.1a","Requirement","ECSS-Q-ST-80_0720034","Risk management for software shall be performed by cross-reference to the project risk policy, as specified in ECSS-M-ST-80.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.3.2.1a","Requirement","ECSS-Q-ST-80_0720035","For critical item control, ECSS-Q-ST-10-04 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.3.2.2a","Requirement","ECSS-Q-ST-80_0720036","The supplier shall identify the characteristics of the software items that qualify them for inclusion in the Critical Item List.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.1.1a","Requirement","ECSS-Q-ST-80_0720037","For supplier selection ECSS-Q-ST-20 clause 5.4.1 shall apply.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Results of pre-award audits and assessments [PAF, -; -];\n          b.Records of procurement sources [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.1.2a","Requirement","ECSS-Q-ST-80_0720038","For the selection of suppliers of existing software, including software contained in OTS equipments and units, the expected output of clauses 6.2.7.2 to 6.2.7.6 shall be made available.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.2.1a","Requirement","ECSS-Q-ST-80_0720039","The supplier shall establish software product assurance requirements for the next level suppliers, tailored to their role in the project, including a requirement to produce a software product assurance plan.\n","EXPECTED OUTPUT: Software product assurance requirements for suppliers [PAF, -; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.2.2a","Requirement","ECSS-Q-ST-80_0720040","The supplier shall provide the software product assurance requirements applicable to the next level suppliers for customer’s acceptance.\n","EXPECTED OUTPUT: Software product assurance requirements for suppliers [PAF, -; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.3.1a","Requirement","ECSS-Q-ST-80_0720041","The supplier shall monitor the next lower level suppliers’ conformance to the product assurance requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.3.2a","Requirement","ECSS-Q-ST-80_0720042","The monitoring process shall include the review and approval of the next lower level suppliers’ product assurance plans, the continuous verification of processes and products, and the monitoring of the final validation of the product.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.3.3a","Requirement","ECSS-Q-ST-80_0720043","The supplier shall ensure that software development processes are defined and applied by the next lower level suppliers in conformance with the software product assurance requirements for suppliers.\n","EXPECTED OUTPUT: Next level suppliers’ software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.3.4a","Requirement","ECSS-Q-ST-80_0720044","The supplier shall provide the next lower level suppliers’ software product assurance plan for customer’s acceptance.\n","EXPECTED OUTPUT: Next level suppliers’ software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.4.4a","Requirement","ECSS-Q-ST-80_0720045","The supplier shall provide the lower level suppliers with the relevant results of the safety and dependability analyses performed at higher and his level (ref. clauses 6.2.2.1 and 6.2.2.2), including:\n    1. the criticality classification of the software products to be developed;\n    2. information about the failures that can be caused at higher level by the software products to be developed.\n","EXPECTED OUTPUT: Safety and dependability analyses results for lower level suppliers [RB, -; SRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.1a","Requirement","ECSS-Q-ST-80_0720046","For procurement documents, ECSS-Q-ST-20 clause 5.4.2 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.2a","Requirement","ECSS-Q-ST-80_0720047","The choice of procured software shall be described and submitted for customer review.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.3a","Requirement","ECSS-Q-ST-80_0720048","For each of the software items the following data shall be provided:\n    1. ordering criteria\n        NOTE For example: versions, options and extensions.\n    2. receiving inspection criteria;\n    3. back-up solutions if the product becomes unavailable;\n    4. contractual arrangements with the supplier for the development, maintenance and upgrades to new releases.\n","EXPECTED OUTPUT: Procurement data [MGT, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.4a","Requirement","ECSS-Q-ST-80_0720049","All the procured software shall be identified and registered by configuration management.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.5a","Requirement","ECSS-Q-ST-80_0720050","The supplier shall subject the procured software to a planned receiving inspection, in accordance with ECSS-Q-ST-20 clause 5.4.4, and the receiving inspection criteria as required by clause 5.5.3.\n","EXPECTED OUTPUT: Receiving inspection report [PAF, -; PDR, CDR, QR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.5.6a","Requirement","ECSS-Q-ST-80_0720051","Exportability constraints shall be identified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.1.1a","Requirement","ECSS-Q-ST-80_0720052","Methods and tools to be used for all the activities of the development cycle, (including requirements analysis, software specification, modelling, design, coding, validation, testing, configuration management, verification and product assurance) shall be identified by the supplier and agreed by the customer.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.1.2a","Requirement","ECSS-Q-ST-80_0720053","The choice of development methods and tools shall be justified by demonstrating through testing or documented assessment that:\n    1. the development team has appropriate experience or training to apply them,\n    2. the tools and methods are appropriate for the functional and operational characteristics of the product, and\n    3. the tools are available (in an appropriate hardware environment) throughout the development and maintenance lifetime of the product.\n","EXPECTED OUTPUT: Software product assurance milestone report [PAF, SPAMR; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.1.3a","Requirement","ECSS-Q-ST-80_0720054","The correct use of methods and tools shall be verified and reported. \n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.2.1a","Requirement","ECSS-Q-ST-80_0720055","The software development environment shall be selected according to the following criteria:\n    1. availability;\n    2. compatibility;\n    3. performance;\n    4. maintenance;\n    5. durability and technical consistency with the operational equipment;\n    6. the assessment of the product with respect to requirements, including the criticality category;\n    7. the available support documentation;\n    8. the acceptance and warranty conditions;\n    9. the conditions of installation, preparation, training and use;\n    10. the maintenance conditions, including the possibilities of evolutions;\n    11. copyright and intellectual property rights constraints;\n    12. dependence on one specific supplier.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.2.2a","Requirement","ECSS-Q-ST-80_0720056","The suitability of the software development environment shall be justified.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.6.2.3a","Requirement","ECSS-Q-ST-80_0720057","The availability of the software development environment to developers and other users shall be verified before the start of each development phase.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.1a","Requirement","ECSS-Q-ST-80_0720058","The supplier shall monitor and control the effectiveness of the processes used during the development of the software, including the relevant processes corresponding to the services called from other organizational entities outside the project team.\n    NOTE The process assessment and improvement performed at organization level can be used to provide evidence of compliance for the project.\n","EXPECTED OUTPUT: Software process assessment records: Overall assessments and improvement programme plan [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.2.1a","Requirement","ECSS-Q-ST-80_0720059","The process assessment model and method to be used when performing any software process assessment shall be documented. \n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software process assessment record: assessment model [PAF, -; -];\n          b.Software process assessment record: assessment method [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.2.2a","Requirement","ECSS-Q-ST-80_0720060","Assessments performed and process assessment models used shall be in conformance with ISO/IEC 15504 (Part 2).\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software process assessment record: evidence of conformance of the process assessment model [PAF, -; -];\n          b.Software process assessment record: assessment method [PAF, -; -]. \n    NOTE 1 The model and method documented in ECSS-Q-HB-80-02 are conformant to ISO/IEC 15504 (Part 2).\n    NOTE 2 Currently the CMMI model is not fully conformant to ISO/IEC 15504, however it can be used, provided that the SCAMPI A method is applied.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.2.3a","Requirement","ECSS-Q-ST-80_0720061","The process assessment model, the method, the assessment scope, the results and the assessors shall be verified as complying with the project requirements.\n    NOTE 1 Examples of assessment scopes are: organizational unit evaluated, and processes evaluated.\n    NOTE 2 ECSS-Q-HB-80-02 provides space specific process reference model and their indicators.\n","EXPECTED OUTPUT: Software process assessment record: Software process assessment recognition evidence [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.2.4a","Requirement","ECSS-Q-ST-80_0720062","Assessments, carried out in accordance with ECSS-Q-HB-80-02, shall be performed by a competent assessor, whereas the other assessment team members can be either competent assessor or provisional assessor.\n    NOTE 1 For other assessment schemes conformant to ISO/IEC 15504 (Part 2), assessors certified under INTRSA are competent assessors.\n    NOTE 2 When using CMMI/SCAMPI A, SEI authorized lead appraisers are competent assessors.\n","EXPECTED OUTPUT: Software process assessment record: competent assessor justification [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.3.1a","Requirement","ECSS-Q-ST-80_0720063","The results of the assessment shall be used as feedback to improve as necessary the performed processes, to recommend changes in the direction of the project, and to determine technology advancement needs.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.3.1b","Requirement","ECSS-Q-ST-80_0720064","The suppliers shall ensure that the results of previous assessments are used in its project activity \n","EXPECTED OUTPUT: Software process assessment records: improvement plan [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.3.2a","Requirement","ECSS-Q-ST-80_0720065","The process improvement shall be conducted according to a documented process improvement process.\n    NOTE 1 For the definition of the process improvement process, see ECSS-Q-HB-80-02.\n    NOTE 2 For CMMI, the process improvement is described in the OPF (Organizational Process Focus) process area.\n","EXPECTED OUTPUT: Software process assessment records: improvement process [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","5.7.3.3a","Requirement","ECSS-Q-ST-80_0720066","Evidence of the improvement in performed processes or in project documentation shall be provided.\n    NOTE See ECSS-Q-HB-80-02.\n","EXPECTED OUTPUT: Software process assessment records: evidence of improvements [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.1a","Requirement","ECSS-Q-ST-80_0720067","The software development life cycle shall be defined or referenced in the software product assurance plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.1b","Requirement","ECSS-Q-ST-80_0720068","The following characteristics of the software life cycle shall be defined:\n    1. phases;\n    2. input and output of each phase;\n    3. status of completion of phase output;\n    4. milestones;\n    5. dependencies;\n    6. responsibilities;\n    7. role of the customer at each milestone review, in conformance with ECSS-M-ST-10 and ECSS-M-ST-10-01.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.2a","Requirement","ECSS-Q-ST-80_0720069","In the definition of the life cycle and associated milestones and documents, the quality objectives shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.3a","Requirement","ECSS-Q-ST-80_0720070","The software life cycle shall be reviewed against the contractual software engineering and product assurance requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.4a","Requirement","ECSS-Q-ST-80_0720071","The software life cycle shall be reviewed for suitability and for the availability of resources to implement it by all functions involved in its application.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.1.5a","Requirement","ECSS-Q-ST-80_0720072","A milestone (SW TRR as defined in ECSS-E-ST-40 clause 5.3.5.1) shall be scheduled immediately before the software validation process starts, to check that:\n    1. the software status is compatible with the commencement of validation activities;\n    2. the necessary resources, software product assurance plans, test and validation documentation, simulators or other technical means are available and ready for use.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.1a","Requirement","ECSS-Q-ST-80_0720073","The following activities shall be covered either in software-specific plans or in project general plans:\n    1. development;\n    2. specification, design and customer documents to be produced;\n    3. configuration and documentation management;\n    4. verification, testing and validation activities;\n    5. maintenance.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.2a","Requirement","ECSS-Q-ST-80_0720074","All plans shall be finalized before the start of the related activities.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.3a","Requirement","ECSS-Q-ST-80_0720075","All plans shall be updated for each milestone to reflect any changes during development.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.4a","Requirement","ECSS-Q-ST-80_0720076","The software product assurance plan shall identify all plans to be produced and used, the relationship between them and the time-scales for their preparation and update.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.5a","Requirement","ECSS-Q-ST-80_0720077","Each plan shall be reviewed against the relevant contractual requirements. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.6a","Requirement","ECSS-Q-ST-80_0720078","Procedures and project standards shall address all types of software products included in the project.\n","EXPECTED OUTPUT: Procedures and standards [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.7a","Requirement","ECSS-Q-ST-80_0720079","All procedures and project standards shall be finalized before starting the related activities.\n","EXPECTED OUTPUT: Procedures and standards [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.8a","Requirement","ECSS-Q-ST-80_0720080","Each procedure or standard shall be reviewed against the relevant plans and contractual requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.1.9a","Requirement","ECSS-Q-ST-80_0720081","Before any activity is started, each procedure or standard for that activity shall be reviewed by all functions involved in its application, for suitability and for the availability of resources to implement it.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.1a","Requirement","ECSS-Q-ST-80_0720082","For the system-level analyses leading to the criticality classification of software products based on the severity of failures consequences, ECSS-Q-ST-40 Table 6-1, and ECSS-Q-ST-30 Table 5-1, shall apply.\n","EXPECTED OUTPUT: Criticality classification of software products [PAF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.2a","Requirement","ECSS-Q-ST-80_0720083","The supplier shall perform a software dependability and safety analysis of the software products, in accordance with the requirements of ECSS-Q-ST-30 and ECSS-Q-ST-40 and using the results of system-level safety and dependability analyses, in order to determine the criticality of the individual software components.\n","EXPECTED OUTPUT: Software dependability and safety analysis report [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.3a","Requirement","ECSS-Q-ST-80_0720084","The supplier shall identify the methods and techniques for the software dependability and safety analysis to be performed at technical specification and design level.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.3b","Requirement","ECSS-Q-ST-80_0720085","Methods and techniques for software dependability and safety analysis shall be agreed between the supplier and customer.\n    NOTE ECSS-Q-HB-80-03 provides indication on methods and techniques that can be applied such as: \n        · software failure modes, effects and criticality analysis (for the performing of this analysis, see also ECSS-Q-ST-30-02);\n        · software fault tree analysis;\n        · software common cause failure analysis.\n","EXPECTED OUTPUT: Criticality classification of software components [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.4a","Requirement","ECSS-Q-ST-80_0720086","Based on the results of the software criticality analysis, the supplier shall apply engineering measures to reduce the number of critical software components and mitigate the risks associated with the critical software (ref. clause 6.2.3).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.5a","Requirement","ECSS-Q-ST-80_0720087","The supplier shall report on the status of the implementation and verification of the SW dependability and safety analysis recommendations.\n","EXPECTED OUTPUT: Software dependability and safety analysis report [PAF, -; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.6a","Requirement","ECSS-Q-ST-80_0720088","The supplier shall update the software dependability and safety analysis at each software development milestone, to confirm the criticality category of software components.\n","EXPECTED OUTPUT: Software dependability and safety analysis report [PAF, -; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.7a","Requirement","ECSS-Q-ST-80_0720089","The supplier shall provide the results of the software dependability and safety analysis for integration into the system-level dependability and safety analyses, addressing in particular:\n    1. additional failure modes identified at software design level;\n    2. recommendations for system-level activities.\n        NOTE For example: introduction of hardware inhibits, and modifications of the system architecture.\n","EXPECTED OUTPUT: Software dependability and safety analysis report [PAF, -; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.8a","Requirement","ECSS-Q-ST-80_0720090","As part of the software requirements analysis activities (ref. clause 6.3.2), the supplier shall contribute to the Hardware-Software Interaction Analysis (HSIA) by identifying, for each hardware failure included in the HSIA, the requirements that specify the software behaviour in the event of that hardware failure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.2.9a","Requirement","ECSS-Q-ST-80_0720091","During the verification and validation of the software requirements resulting from the Hardware-Software Interaction Analysis, the supplier shall verify that the software reacts correctly to hardware failures, and no undesired software malfunctions occur that may lead to system failures.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.1a","Requirement","ECSS-Q-ST-80_0720092","The supplier shall define and implement measures to avoid propagation of failures between software components of different criticality.\n    NOTE This can be achieved by design measures such as separate hardware platforms, isolation of software processes or prohibition of shared memory (segregation and partitioning). ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.1b","Requirement","ECSS-Q-ST-80_0720093","Software components whose malfunction may cause failures of higher criticality components shall be classified in accordance with the consequences of those failures.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software product assurance plan [PAF, SPAP; PDR, CDR];\n          b.Software dependability and safety analysis report [PAF, -; PDR, CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.2a","Requirement","ECSS-Q-ST-80_0720094","The supplier shall define, justify and apply measures to assure the dependability and safety of critical software.\n    NOTE These measures can include:\n        · use of software design or methods that have performed successfully in a similar application;\n        · insertion of features for failure isolation and handling (ref. ECSS-Q-HB-80-03, software failure modes, effects and criticality analysis);\n        · defensive programming techniques, such as input verification and consistency checks;\n        · use of a “safe subset” of programming language;\n        · use of formal design language for formal proof;\n        · 100 % code branch coverage at unit testing level;\n        · full inspection of source code;\n        · witnessed or independent testing;\n        · gathering and analysis of failure statistics;\n        · removing deactivated code or showing through a combination of analysis and testing that the means by which such code can be inadvertently executed are prevented, isolated, or eliminated.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.3a","Requirement","ECSS-Q-ST-80_0720095","The application of the chosen measures to handle the critical software shall be verified.\n","EXPECTED OUTPUT: Software product assurance milestone report [PAF, SPAMR; PDR, CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.4a","Requirement","ECSS-Q-ST-80_0720096","Critical software shall be subject to regression testing after:\n    1. any change of functionality of the underlying platform hardware;\n        NOTE For example: instruction set of a processor.\n    2. any change of the tools that affect directly or indirectly the generation of the executable code.\n        NOTE In case of minor changes in tools that affect the generation of the executable code, a binary comparison of the executable code generated by the different tools can be used to verify that no modifications are introduced.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.5a","Requirement","ECSS-Q-ST-80_0720097","The need for additional verification and validation of critical software shall be analysed after:\n    1. any change of functionality or performance of the underlying platform hardware;\n    2. any change in the environment in which the software or the platform hardware operate.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.6a","Requirement","ECSS-Q-ST-80_0720098","Identified unreachable code shall be removed and the need for re-verification and re-validation shall be analysed. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.7a","Requirement","ECSS-Q-ST-80_0720099","Unit and integration testing shall be (re-)executed on non-instrumented code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.3.8a","Requirement","ECSS-Q-ST-80_0720100","Validation testing shall be (re-)executed on non-instrumented code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.1a","Requirement","ECSS-Q-ST-80_0720101","ECSS-M-ST-40 shall be applied for software configuration management, complemented by the following requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.2a","Requirement","ECSS-Q-ST-80_0720102","The software configuration management system shall allow any reference version to be re-generated from backups.\n","EXPECTED OUTPUT: Software configuration management plan [MGT, SCMP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.3a","Requirement","ECSS-Q-ST-80_0720103","The software configuration file and the software release document shall be provided with each software delivery.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software configuration file [DDF, SCF; -];\n          b.Software release document [DDF, SRelD; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.4a","Requirement","ECSS-Q-ST-80_0720104","The software configuration file shall be available and up to date for each project milestone.\n","EXPECTED OUTPUT: Software configuration file [DDF, SCF; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.5a","Requirement","ECSS-Q-ST-80_0720105","Any components of the code generation tool that are customizable by the user shall be put under configuration control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.5b","Requirement","ECSS-Q-ST-80_0720106","The change control procedures defined for the project shall address the specific aspects of these components.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software configuration file [DDF, SCF; CDR, QR, AR, ORR];\n          b.Software configuration management plan [MGT, SCMP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.6a","Requirement","ECSS-Q-ST-80_0720107","The supplier shall ensure that all authorized changes are implemented in accordance with the software configuration management plan.\n","EXPECTED OUTPUT: Authorized changes - Software configuration file [DDF, SCF; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.7a","Requirement","ECSS-Q-ST-80_0720108","The following documents shall be controlled (see ECSS-Q-ST-10 clause 5.2.5):\n    1. procedural documents describing the quality system to be applied during the software life cycle;\n    2. planning documents describing the planning and progress of the activities;\n    3. documents describing a particular software product, including:\n        (a) development phase inputs,\n        (b) development phase outputs,\n        (c) verification and validation plans and results,\n        (d) test case specifications, test procedures and test reports,\n        (e) traceability matrices,\n        (f) documentation for the software and system operators and users, and\n        (g) maintenance documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.8a","Requirement","ECSS-Q-ST-80_0720109","The supplier shall identify a method and tool to protect the supplied software against corruption.\n    NOTE For example: source, executable and data.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software product assurance plan [PAF, SPAP; SRR, PDR]; \n          b.Software configuration file [DDF, SCF; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.9a","Requirement","ECSS-Q-ST-80_0720110","The supplier shall define a checksum-type key calculation for the delivered operational software.\n    NOTE For example: executable binary, database. \n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.10a","Requirement","ECSS-Q-ST-80_0720111","The checksum value shall be provided in the software configuration file with each software delivery.\n","EXPECTED OUTPUT: Software configuration file [DDF, SCF; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.4.11a","Requirement","ECSS-Q-ST-80_0720112","The media through which the software is delivered to the customer shall be marked by the supplier indicating the following information as a minimum:\n    1. the software name;\n    2. the version number;\n    3. the reference to the software configuration file.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software product assurance plan [PAF, SPAP; SRR, PDR];\n          b.Labels [DDF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.5.1a","Requirement","ECSS-Q-ST-80_0720113","Metrics shall be used to manage the development and to assess the quality of the development processes. \n    NOTE Process metrics are based on quality models (see clause 5.2.7).\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.5.2a","Requirement","ECSS-Q-ST-80_0720114","Process metrics shall be collected, stored and analysed on a regular basis by applying quality models and procedures. \n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.5.3a","Requirement","ECSS-Q-ST-80_0720115","The following basic process metrics shall be used within the supplier’s organization: \n    1. duration: how phases and tasks are being completed versus the planned schedule;\n    2. effort: how much effort is consumed by the various phases and tasks compared to the plan.\n","EXPECTED OUTPUT: Internal metrics report.",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.5.4a","Requirement","ECSS-Q-ST-80_0720116","Process metrics shall be used within the supplier’s organization and reported to the customer, including:\n    1. number of problems detected during verification;\n    2. number of problems detected during integration and validation testing and use. \n        NOTE See also software problem reporting described in clause 5.2.5.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.5.5a","Requirement","ECSS-Q-ST-80_0720117","Metrics reports shall be included in the software product assurance reports.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.1a","Requirement","ECSS-Q-ST-80_0720118","Activities for the verification of the quality requirements shall be specified in the definition of the verification plan. \n    NOTE Verification includes various techniques such as review, inspection, testing, walk-through, cross-reading, desk-checking, model simulation, and many types of analysis such as traceability analysis, formal proof or fault tree analysis. \n","EXPECTED OUTPUT: Software verification plan [DJF, SVerP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.2a","Requirement","ECSS-Q-ST-80_0720119","The outputs of each development activity shall be verified for conformance against pre-defined criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.2b","Requirement","ECSS-Q-ST-80_0720120","Only outputs which have been subjected to planned verifications shall be used as inputs for subsequent activities.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.3a","Requirement","ECSS-Q-ST-80_0720121","A summary of the assurance activities concerning the verification process and their findings shall be included in software product assurance reports.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.4a","Requirement","ECSS-Q-ST-80_0720122","The completion of actions related to software problem reports generated during verification shall be verified and recorded.\n","EXPECTED OUTPUT: Software problem reports [DJF, -; SRR, PDR, CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.5a","Requirement","ECSS-Q-ST-80_0720123","Software containing deactivated code shall be verified specifically to ensure that the deactivated code cannot be activated or that its accidental activation cannot harm the operation of the system.\n","EXPECTED OUTPUT: Software verification report [DJF, SVR; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.6a","Requirement","ECSS-Q-ST-80_0720124","Software containing configurable code shall be verified specifically to ensure that any unintended configuration cannot be activated at run time or included during code generation.\n","EXPECTED OUTPUT: Software verification report [DJF, SVR; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.7a","Requirement","ECSS-Q-ST-80_0720125","The supplier shall ensure that:\n    1. the planned verification activities are adequate to confirm that the products of each phase are conformant to the applicable requirements;\n    2. the verification activities are performed according to the plan. \n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.8a","Requirement","ECSS-Q-ST-80_0720126","Reviews and inspections shall be carried out according to defined criteria, and according to the defined level of independence of the reviewer from the author of the reviewed item. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.9a","Requirement","ECSS-Q-ST-80_0720127","Each review and inspection shall be based on a written plan or procedure.\n    NOTE For projects reviews, ECSS-E-ST-40 clause 5.3.3.3, bullet b and Annex P are applicable.\n","EXPECTED OUTPUT: Review and inspection plans or procedures [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.10a","Requirement","ECSS-Q-ST-80_0720128","The review or inspection plans or procedures shall specify: \n    1. the reviewed or inspected items;\n    2. the person in charge;\n    3. the participants;\n    4. the means of review or inspection (e.g. tools or check list);\n    5. the nature of the report.\n","EXPECTED OUTPUT: Review and inspection plans or procedures [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.11a","Requirement","ECSS-Q-ST-80_0720129","Review and inspection reports shall:\n    1. refer to the corresponding review/inspection procedure or plan; \n    2. identify the reviewed item, the author, the reviewer, the review criteria and the findings of the review.\n","EXPECTED OUTPUT: Review and inspection reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.12a","Requirement","ECSS-Q-ST-80_0720130","Traceability matrices (as defined in ECSS-E-ST-40 clause 5.8) shall be verified at each milestone.\n","EXPECTED OUTPUT: Software product assurance milestone report [PAF, SPAMR; SRR, PDR, CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.13a","Requirement","ECSS-Q-ST-80_0720131","Independent software verification shall be performed by a third party.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.6.13b","Requirement","ECSS-Q-ST-80_0720132","Independent software verification shall be a combination of reviews, inspections, analyses, simulations, testing and auditing.\n    NOTE This requirement is applicable where the risks associated with the project justify the costs involved. The customer can consider a less rigorous level of independence, e.g. an independent team in the same organization.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.ISVV plan [DJF, -; SRR, PDR];\n          b.ISVV report [DJF, -; PDR, CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.2a","Requirement","ECSS-Q-ST-80_0720133","Analyses of the advantages to be obtained with the selection of existing software (ref. 3.2.11) instead of new development shall be carried out.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software reuse approach, including approach to delta qualification [PAF, SPAP; SRR, PDR];\n          b.Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.3a","Requirement","ECSS-Q-ST-80_0720134","The existing software shall be assessed with regards to the applicable functional, performance and quality requirements.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software reuse approach, including approach to delta qualification [PAF, SPAP; SRR, PDR];\n          b.Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.4a","Requirement","ECSS-Q-ST-80_0720135","The quality level of the existing software shall be analysed with respect to the project requirements, according to the criticality of the system function implemented, taking into account the following aspects:\n    1. software requirements documentation;\n    2. software architectural and detailed design documentation;\n    3. forward and backward traceability between system requirements, software requirements, design and code;\n    4. unit tests documentation and coverage;\n    5. integration tests documentation and coverage;\n    6. validation documentation and coverage;\n    7. verification reports;\n    8. performance;\n        NOTE For example: memory occupation, CPU load.\n    9. operational performances;\n    10. residual nonconformances and waivers;\n    11. user operational documentation;\n        NOTE For example: user manual.\n    12. code quality (adherence to coding standards, metrics).\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software reuse approach, including approach to delta qualification [PAF, SPAP; SRR, PDR];\n          b.Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.5a","Requirement","ECSS-Q-ST-80_0720136","The results of the reused software analysis shall be recorded in the software reuse file, together with an assessment of the possible level of reuse and a description of the assumptions and the methods applied when estimating the level of reuse.\n    NOTE Results of the reused software analysis, such as detailed reference to requirement and design documents, test reports and coverage results.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software reuse approach, including approach to delta qualification [PAF, SPAP; SRR, PDR];\n          b.Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.6a","Requirement","ECSS-Q-ST-80_0720137","The analysis of the suitability of existing software for reuse shall be complemented by an assessment of the following aspects:\n    1. the acceptance and warranty conditions;\n    2. the available support documentation; \n    3. the conditions of installation, preparation, training and use; \n    4. the identification and registration by configuration management; \n    5. maintenance responsibility and conditions, including the possibilities of changes; \n    6. the durability and validity of methods and tools used in the initial development, that are envisaged to be used again; \n    7. the copyright and intellectual property rights constraints (modification rights); \n    8. the licensing conditions;\n    9. exportability constraints.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.7a","Requirement","ECSS-Q-ST-80_0720138","Corrective actions shall be identified, documented in the reuse file and applied to the reused software not meeting the applicable requirements related to the aspects as specified in clauses 6.2.7.2 to 6.2.7.6.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.8a","Requirement","ECSS-Q-ST-80_0720139","Reverse engineering techniques shall be applied to generate missing documentation and to reach the required verification and validation coverage.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.8b","Requirement","ECSS-Q-ST-80_0720140","For software products whose life cycle data from previous development are not available and reverse engineering techniques are not fully applicable, the following methods shall be applied:\n    1. generation of validation and verification documents based on the available user documentation (e.g. user manual) and execution of tests in order to achieve the required level of test coverage;\n    2. use of the product service history to provide evidence of the product’s suitability for the current application, including information about:\n        (a) relevance of the product service history for the new operational environment;\n        (b) configuration management and change control of the software product;\n        (c) effectiveness of problem reporting;\n        (d) actual error rates and maintenance records;\n        (e) impact of modifications.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.9a","Requirement","ECSS-Q-ST-80_0720141","The software reuse file shall be updated at project milestones to reflect the results of the identified corrective actions for reused software not meeting the project requirements.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.10a","Requirement","ECSS-Q-ST-80_0720142","All the reused software shall be kept under configuration control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.7.11a","Requirement","ECSS-Q-ST-80_0720143","The detailed configuration status of the reused software baseline shall be provided to the customer in the reuse file for acceptance.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; SRR, PDR, CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.1a","Requirement","ECSS-Q-ST-80_0720144","For the selection of tools for automatic code generation, the supplier shall evaluate the following aspects:\n    1. evolution of the tools in relation to the tools that use the generated code as an input;\n        NOTE For example: compilers or code management systems.\n    2. customization of the tools to comply with project standards; \n    3. portability requirements for the generated code; \n    4. collection of the required design and code metrics; \n    5. verification of software components containing generated code; \n    6. configuration control of the tools including the parameters for customisation;\n    7. compliance with open standards.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.2a","Requirement","ECSS-Q-ST-80_0720145","The requirements on testing applicable to the automatically generated code shall ensure the achievement of the same objectives as those for manually generated code.\n","EXPECTED OUTPUT: Validation and testing documentation [DJF, SValP; PDR], [DJF, SVS; CDR, QR, AR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.3a","Requirement","ECSS-Q-ST-80_0720146","The required level of verification and validation of the automatic generation tool shall be at least the same as the one required for the generated code, if the tool is used to skip verification or testing activities on the target code.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.4a","Requirement","ECSS-Q-ST-80_0720147","Modelling standards for automatic code generation tools shall be defined and applied.\n","EXPECTED OUTPUT: Modelling standards [PAF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.5a","Requirement","ECSS-Q-ST-80_0720148","Adherence to modelling standards shall be verified.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.6a","Requirement","ECSS-Q-ST-80_0720149","Clause 6.3.4 shall apply to automatically generated code, unless the supplier demonstrates that the automatically generated code does not need to be manually modified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.2.8.7a","Requirement","ECSS-Q-ST-80_0720150","The verification and validation documentation shall address separately the activities to be performed for manually and automatically generated code.\n","EXPECTED OUTPUT: Validation and testing documentation [DJF, SValP; PDR], [DJF, SVS; CDR, QR, AR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.1.1a","Requirement","ECSS-Q-ST-80_0720151","For the definition of the software related system requirements to be specified in the requirements baseline, ECSS-E-ST-40 clause 5.2 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.1.2a","Requirement","ECSS-Q-ST-80_0720152","The requirements baseline shall be subject to documentation control and configuration management as part of the development documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.1.3a","Requirement","ECSS-Q-ST-80_0720153","For the definition of the requirements baseline, all results from the safety and dependability analyses (including results from the HSIA ECSS-Q-ST-30 clause 6.4.2.3) shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.2.1a","Requirement","ECSS-Q-ST-80_0720154","The requirements baseline shall be analyzed to fully and unambiguously define the software requirements in the technical specification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.2.2a","Requirement","ECSS-Q-ST-80_0720155","The technical specification shall be subject to documentation control and configuration management as part of the development documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.2.3a","Requirement","ECSS-Q-ST-80_0720156","For the definition of the technical specification, all results from the safety and dependability analyses (including results from the HSIA ECSS-Q-ST-30 clause 6.4.2.3) shall be used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.2.4a","Requirement","ECSS-Q-ST-80_0720157","In addition to the functional requirements, the technical specification shall include all non-functional requirements necessary to satisfy the requirements baseline, including, as a minimum, the following:\n    1. performance,\n    2. safety,\n    3. reliability,\n    4. robustness,\n    5. quality,\n    6. maintainability,\n    7. configuration management,\n    8. security,\n    9. privacy,\n    10. metrication, and\n    11. verification and validation.\n        NOTE Performance requirements include requirements on numerical accuracy.\n","EXPECTED OUTPUT: Software requirements specification [TS, SRS; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.2.5a","Requirement","ECSS-Q-ST-80_0720158","Prior to the technical specification elaboration, customer and supplier shall agree on the following principles and rules as a minimum:\n    1. assignment of persons (on both sides) responsible for establishing the technical specification;\n    2. methods for agreeing on requirements and approving changes;\n    3. efforts to prevent misunderstandings such as definition of terms, explanations of background of requirements;\n    4. recording and reviewing discussion results on both sides.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.1a","Requirement","ECSS-Q-ST-80_0720159","The design definition file shall be subject to documentation control and configuration management. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.2a","Requirement","ECSS-Q-ST-80_0720160","Mandatory and advisory design standards shall be defined and applied.\n","EXPECTED OUTPUT: Design standards [PAF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.3a","Requirement","ECSS-Q-ST-80_0720161","For software in which numerical accuracy is relevant to mission success specific rules on design and code shall be defined to ensure that the specified level of accuracy is obtained.\n    NOTE For example: for an attitude and orbit control subsystem, scientific data generation components.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.4a","Requirement","ECSS-Q-ST-80_0720162","Adherence to design standards shall be verified.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.5a","Requirement","ECSS-Q-ST-80_0720163","The supplier shall define means, criteria and tools to ensure that the complexity and modularity of the design meet the quality requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.5b","Requirement","ECSS-Q-ST-80_0720164","The design evaluation shall be performed in parallel with the design process, in order to provide feedback to the software design team.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.6a","Requirement","ECSS-Q-ST-80_0720165","Synthesis of the results obtained in the software complexity and modularity evaluation and corrective actions implemented shall be described in the software product assurance reports.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.3.7a","Requirement","ECSS-Q-ST-80_0720166","The supplier shall review the design documentation to ensure that it contains the appropriate level of information for maintenance activities.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software product assurance plan [PAF, SPAP; PDR];\n          b.Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.1a","Requirement","ECSS-Q-ST-80_0720167","Coding standards (including consistent naming conventions and adequate commentary rules) shall be specified and observed.\n","EXPECTED OUTPUT: Coding standards [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.2a","Requirement","ECSS-Q-ST-80_0720168","The standards shall be consistent with the product quality requirements.\n    NOTE Coding standards depend on the software quality objectives (see clause 5.2.7).\n","EXPECTED OUTPUT: Coding standards [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.3a","Requirement","ECSS-Q-ST-80_0720169","The tools to be used in implementing and checking conformance with coding standards shall be identified in the product assurance plan before coding activities start.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.4a","Requirement","ECSS-Q-ST-80_0720170","Coding standards shall be reviewed with the customer to ensure that they reflect product quality requirements.\n","EXPECTED OUTPUT: Coding standards and description of tools [PAF, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.5a","Requirement","ECSS-Q-ST-80_0720171","Use of low-level programming languages shall be justified.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.6a","Requirement","ECSS-Q-ST-80_0720172","The supplier shall define measurements, criteria and tools to ensure that the software code meets the quality requirements.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.6b","Requirement","ECSS-Q-ST-80_0720173","The code evaluation shall be performed in parallel with the coding process, in order to provide feedback to the software programmers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.7a","Requirement","ECSS-Q-ST-80_0720174","Synthesis of the code analysis results and corrective actions implemented shall be described in the software product assurance reports.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.4.8a","Requirement","ECSS-Q-ST-80_0720175","The code shall be put under configuration control immediately after successful unit testing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.1a","Requirement","ECSS-Q-ST-80_0720176","Testing shall be performed in accordance with a strategy for each testing level (i.e. unit, integration, validation against the technical specification, validation against the requirements baseline, acceptance), which includes:\n    1. the types of tests to be performed;\n        NOTE For example: functional, boundary, performance, and usability tests.\n    2. the tests to be performed in accordance with the plans and procedures;\n    3. the means and organizations to perform assurance function for testing and validation.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.2a","Requirement","ECSS-Q-ST-80_0720177","Based on the criticality of the software, test coverage goals for each testing level shall be agreed between the customer and the supplier and their achievement monitored by metrics: \n    1. for unit level testing;\n    2. for integration level testing;\n    3. for validation against the technical specification and validation against the requirements baseline.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.3a","Requirement","ECSS-Q-ST-80_0720178","The supplier shall ensure through internal review that the test procedures and data are adequate, feasible and traceable and that they satisfy the requirements.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.4a","Requirement","ECSS-Q-ST-80_0720179","Test readiness reviews shall be held before the commencement of test activities, as defined in the software development plan.\n","EXPECTED OUTPUT: Test readiness review reports [DJF, -; TRR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.5a","Requirement","ECSS-Q-ST-80_0720180","Test coverage shall be checked with respect to the stated goals.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.5b","Requirement","ECSS-Q-ST-80_0720181","Feedback from the results of test coverage evaluation shall be continuously provided to the software developers.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.6a","Requirement","ECSS-Q-ST-80_0720182","The supplier shall ensure that nonconformances and software problem reports detected during testing are properly documented and reported to those concerned.\n","EXPECTED OUTPUT: Nonconformance reports and software problem reports [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.7a","Requirement","ECSS-Q-ST-80_0720183","The test coverage of configurable code shall be checked to ensure that the stated requirements are met in each tested configuration.\n","EXPECTED OUTPUT: Statement of compliance with test plans and procedures [PAF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.8a","Requirement","ECSS-Q-ST-80_0720184","The completion of actions related to software problem reports generated during testing and validation shall be verified and recorded.\n","EXPECTED OUTPUT: Software problem reports [DJF, -; SRR, PDR, CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.9a","Requirement","ECSS-Q-ST-80_0720185","Provisions shall be made to allow witnessing of tests by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.10a","Requirement","ECSS-Q-ST-80_0720186","Provisions shall be made to allow witnessing of tests by supplier personnel independent of the development.\n    NOTE For example: specialist software product assurance personnel.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.11a","Requirement","ECSS-Q-ST-80_0720187","The supplier shall ensure that:\n    1. tests are conducted in accordance with approved test procedures and data, \n    2. the configuration under test is correct, \n    3. the tests are properly documented, and \n    4. the test reports are up to date and valid. \n","EXPECTED OUTPUT: Statement of compliance with test plans and procedures [PAF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.12a","Requirement","ECSS-Q-ST-80_0720188","The supplier shall ensure that tests are repeatable by verifying the storage and recording of tested software, support software, test environment, supporting documents and problems found.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.13a","Requirement","ECSS-Q-ST-80_0720189","The supplier shall confirm in writing that the tests are successfully completed.\n","EXPECTED OUTPUT: Testing and validation reports [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.14a","Requirement","ECSS-Q-ST-80_0720190","Review boards looking to engineering and product assurance aspects shall be convened after the completion of test phases, as defined in the software development plan.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.15a","Requirement","ECSS-Q-ST-80_0720191","Areas affected by any modification shall be identified and re-tested (regression testing).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.16a","Requirement","ECSS-Q-ST-80_0720192","In case of re-testing, all test related documentation (test procedures, data and reports) shall be updated accordingly.\n","EXPECTED OUTPUT: Updated test documentation [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.17a","Requirement","ECSS-Q-ST-80_0720193","The need for regression testing and additional verification of the software shall be analysed after any change of the platform hardware.\n","EXPECTED OUTPUT: Updated test documentation [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.18a","Requirement","ECSS-Q-ST-80_0720194","The need for regression testing and additional verification of the software shall be analysed after a change or update of any tool used to generate it.\n    NOTE For example: source code or object code.\n","EXPECTED OUTPUT: Updated test documentation [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.19a","Requirement","ECSS-Q-ST-80_0720195","Validation shall be carried out by staff who have not taken part in the design or coding of the software being validated.\n    NOTE This can be achieved at the level of the whole software product, or on a component by component basis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.20a","Requirement","ECSS-Q-ST-80_0720196","Validation of the flight software against the requirement baseline on the flight equipment model shall be performed on a software version without any patch. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.21a","Requirement","ECSS-Q-ST-80_0720197","The supplier shall review the test documentation to ensure that it is up to date and organized to facilitate its reuse for maintenance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.22a","Requirement","ECSS-Q-ST-80_0720198","Tests shall be organized as activities in their own right in terms of planning, resources and team composition. \n","EXPECTED OUTPUT: Test and validation documentation [DJF, SValP; PDR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.23a","Requirement","ECSS-Q-ST-80_0720199","The necessary resources for testing shall be identified early in the life cycle, taking into account the operating and maintenance requirements. \n","EXPECTED OUTPUT: Test and validation documentation [DJF, SValP; PDR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.24a","Requirement","ECSS-Q-ST-80_0720200","Test tool development or acquisition (hardware and software) shall be planned for in the overall project plan.\n","EXPECTED OUTPUT: Test and validation documentation [DJF, SValP; PDR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.25a","Requirement","ECSS-Q-ST-80_0720201","The supplier shall establish and review the test procedures and data before starting testing activities and also document the constraints of the tests concerning physical, performance, functional, controllability and observability limitations.\n","EXPECTED OUTPUT: Test and validation documentation [DJF, SValP; PDR], [DJF, SVS; CDR, QR, AR], [DJF, SUITP; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.26a","Requirement","ECSS-Q-ST-80_0720202","Before offering the product for delivery and customer acceptance, the supplier shall validate its operation as a complete product, under conditions similar to the application environment as specified in the requirements baseline.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.27a","Requirement","ECSS-Q-ST-80_0720203","When testing under the operational environment is performed, the following concerns shall be addressed:\n    1. the features to be tested in the operational environment;\n    2. the specific responsibilities of the supplier and customer for carrying out and evaluating the test;\n    3. restoration of the previous operational environment (after test).\n","EXPECTED OUTPUT: Test and validation documentation [DJF, -; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.28a","Requirement","ECSS-Q-ST-80_0720204","Independent software validation shall be performed by a third party.\n    NOTE This requirement is applicable where the risks associated with the project justify the costs involved. The customer can consider a less rigorous level of independence, e.g. an independent team in the same organization.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.ISVV plan [DJF, -; SRR, PDR];\n          b.ISVV report [DJF, -; PDR, CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.29a","Requirement","ECSS-Q-ST-80_0720205","The validation shall include testing in the different configurations possible or in a representative set of them when it is evident that the number of possible configurations is too high to allow validation in all of them.\n","EXPECTED OUTPUT: Test and validation documentation [DJF, SValP; PDR], [DJF, SVS; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.30a","Requirement","ECSS-Q-ST-80_0720206","Software containing deactivated code shall be validated specifically to ensure that the deactivated code cannot be activated or that its accidental activation cannot harm the operation of the system.\n","EXPECTED OUTPUT: Testing and validation reports [DJF, -; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.31a","Requirement","ECSS-Q-ST-80_0720207","Software containing configurable code shall be validated specifically to ensure that unintended configuration cannot be activated at run time or included during code generation.\n","EXPECTED OUTPUT: Testing and validation reports [DJF, -; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.5.32a","Requirement","ECSS-Q-ST-80_0720208","Activities for the validation of the quality requirements shall be specified in the definition of the validation specification. \n","EXPECTED OUTPUT: Software validation specification [DJF, SVS; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.1a","Requirement","ECSS-Q-ST-80_0720209","The roles, responsibilities and obligations of the supplier and customer during installation shall be established.\n","EXPECTED OUTPUT: Installation procedure [DDF, SCF; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.2a","Requirement","ECSS-Q-ST-80_0720210","The installation shall be performed in accordance with the installation procedure.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.3a","Requirement","ECSS-Q-ST-80_0720211","The customer shall establish an acceptance test plan specifying the intended acceptance tests including specific tests suited to the target environment (see ECSS-E-ST-40 clause 5.7.3.1).\n    NOTE 1 The acceptance tests can be partly made up of tests used during previous test activities.\n    NOTE 2 The acceptance test plan takes into account the requirement for operational demonstration, either as part of acceptance or after acceptance.\n","EXPECTED OUTPUT: Acceptance test plan [DJF, -; QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.4a","Requirement","ECSS-Q-ST-80_0720212","The customer shall ensure that the acceptance tests are performed in accordance with the approved acceptance test plan (see ECSS-E-ST-40 clause 5.7.3.2).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.5a","Requirement","ECSS-Q-ST-80_0720213","Before the software is presented for customer acceptance, the supplier shall ensure that:\n    1. the delivered software complies with the contractual requirements (including any specified content of the software acceptance data package);\n    2. the source and object code supplied correspond to each other;\n    3. all agreed changes are implemented;\n    4. all nonconformances are either resolved or declared.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.6a","Requirement","ECSS-Q-ST-80_0720214","The customer shall verify that the executable code was regenerated from configuration managed source code components and installed in accordance with predefined procedures on the target environment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.7a","Requirement","ECSS-Q-ST-80_0720215","Any discovered problems shall be documented in nonconformance reports.\n","EXPECTED OUTPUT: Nonconformance reports [DJF, -; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.8a","Requirement","ECSS-Q-ST-80_0720216","On completion of the acceptance tests, a report shall be drawn up and be signed by the supplier’s representatives, the customer’s representatives, the software quality engineers of both parties and the representative of the organization charged with the maintenance of the software product.\n","EXPECTED OUTPUT: Acceptance test report [DJF, -; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.6.9a","Requirement","ECSS-Q-ST-80_0720217","The customer shall certify conformance to the procedures and state the conclusion concerning the test result for the software product under test (accepted, conditionally accepted, rejected).\n","EXPECTED OUTPUT: Acceptance test report [DJF, -; AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.7.1a","Requirement","ECSS-Q-ST-80_0720218","During operations, the quality of the mission products related to software shall be agreed with the customer and users.\n    NOTE Quality of mission products can include parameters such as: error-free data, availability of data and permissible outages; permissible information degradation.\n","EXPECTED OUTPUT: Software operation support plan [OP, -; ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.7.2a","Requirement","ECSS-Q-ST-80_0720219","During the demonstration that the software conforms to the operational requirements, the following shall be covered as a minimum:\n    1. availability and maintainability of the host system (including reboot after maintenance interventions);\n    2. safety features;\n    3. human-computer interface;\n    4. operating procedures;\n    5. ability to meet the mission product quality requirements.\n","EXPECTED OUTPUT: Validation of the operational requirements [PAF, -; ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.7.3a","Requirement","ECSS-Q-ST-80_0720220","The product assurance plan for system operations shall include consideration of software.\n","EXPECTED OUTPUT: Input to product assurance plan for systems operation [PAF, -; ORR]",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.1a","Requirement","ECSS-Q-ST-80_0720221","The organization responsible for maintenance shall be identified to allow a smooth transition into the operations and maintenance.\n    NOTE An organization, with representatives from both supplier and customer, can be set up to support the maintenance activities. Attention is drawn to the importance of the flexibility of this organization to cope with the unexpected occurrence of problems and the identification of facilities and resources to be used for the maintenance activities.\n","EXPECTED OUTPUT: Maintenance plan [MF, -; QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.2a","Requirement","ECSS-Q-ST-80_0720222","The maintenance organization shall specify the assurance, verification and validation activities applicable to maintenance interventions.\n","EXPECTED OUTPUT: Maintenance plan [MF, -; QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.3a","Requirement","ECSS-Q-ST-80_0720223","The maintenance plans shall be verified against specified requirements for maintenance of the software product.\n    NOTE The maintenance plans and procedures can address corrective, improving, adaptive and preventive maintenance, differentiating between “routine” and “emergency” maintenance activities.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.4a","Requirement","ECSS-Q-ST-80_0720224","The maintenance plans and procedures shall include the following as a minimum:\n    1. scope of maintenance;\n    2. identification of the first version of the software product for which maintenance is to be done;\n    3. support organization;\n    4. maintenance life cycle;\n    5. maintenance activities;\n    6. quality measures to be applied during the maintenance;\n    7. maintenance records and reports.\n","EXPECTED OUTPUT: Maintenance plan [MF, -; QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.5a","Requirement","ECSS-Q-ST-80_0720225","Rules for the submission of maintenance reports shall be established and agreed as part of the maintenance plan.\n","EXPECTED OUTPUT: Maintenance plan [MF, -; QR, AR, ORR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.6a","Requirement","ECSS-Q-ST-80_0720226","All maintenance activities shall be logged in predefined formats and retained. \n","EXPECTED OUTPUT: Maintenance records [MF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","6.3.8.7a","Requirement","ECSS-Q-ST-80_0720227","Maintenance records shall be established for each software product, including, as a minimum, the following information,:\n    1. list of requests for assistance or problem reports that have been received and the current status of each;\n    2. organization responsible for responding to requests for assistance or implementing the appropriate corrective actions;\n    3. priorities assigned to the corrective actions;\n    4. results of the corrective actions;\n    5. statistical data on failure occurrences and maintenance activities.\n        NOTE The record of the maintenance activities can be utilized for evaluation and enhancement of the software product and for improvement of the quality system itself.\n","EXPECTED OUTPUT: Maintenance records [MF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.1a","Requirement","ECSS-Q-ST-80_0720228","The software quality requirements (including safety and dependability requirements) shall be derived from the requirements defined at system level.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.2a","Requirement","ECSS-Q-ST-80_0720229","Quality requirements shall be expressed in quantitative terms or constraints.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.3a","Requirement","ECSS-Q-ST-80_0720230","The supplier shall define assurance activities to ensure that the product meets the quality requirements as specified in the technical specification.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.4a","Requirement","ECSS-Q-ST-80_0720231","In order to verify the implementation of the product quality requirements, the supplier shall define a metrication programme based on the identified quality model (see clause 5.2.7), specifying:\n    1. the metrics to be collected and stored;\n    2. the means to collect metrics (measurements);\n    3. the target values, with reference to the product quality requirements;\n    4. the analyses to be performed on the collected metrics, including the ones to derive:\n        (a) descriptive statistics;\n            NOTE For example: the number of units at each level of complexity.\n        (b) trend analysis (such as trends in software problems).\n    5. how the results of the analyses performed on the collected metrics are fed back to the development team and used to identify corrective actions;\n    6. the schedule of metrics collection, storing, analysis and reporting, with reference to the whole software life cycle.\n        NOTE Guidance for software metrication programme implementation can be found in ECSS-Q-HB-80-04. \n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.5a","Requirement","ECSS-Q-ST-80_0720232","The following basic products metrics shall be used:\n    1. size (code);\n    2. complexity (design, code);\n    3. fault density and failure intensity;\n    4. test coverage;\n    5. number of failures.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.6a","Requirement","ECSS-Q-ST-80_0720233","The results of metrics collection and analysis shall be included in the software product assurance reports, in order to provide the customer with an insight into the level of quality obtained.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.7a","Requirement","ECSS-Q-ST-80_0720234","Numerical accuracy shall be estimated and verified.\n","EXPECTED OUTPUT: Numerical accuracy analysis [DJF, SVR; PDR, CDR, QR]. ",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.1.8a","Requirement","ECSS-Q-ST-80_0720235","The supplier shall define the organization and means implemented to collect and analyse data required for the study of software maturity.\n    NOTE For example: failures, corrections, duration of runs.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.1.1a","Requirement","ECSS-Q-ST-80_0720236","The software quality requirements shall be documented in the requirements baseline and technical specification.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.1.2a","Requirement","ECSS-Q-ST-80_0720237","The software requirements shall be: \n    1. correct;\n    2. unambiguous;\n    3. complete;\n    4. consistent;\n    5. verifiable;\n    6. traceable.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.1.3a","Requirement","ECSS-Q-ST-80_0720238","For each requirement the method for verification and validation shall be specified.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.2.1a","Requirement","ECSS-Q-ST-80_0720239","The software design shall meet the non-functional requirements as documented in the technical specification.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.2.2a","Requirement","ECSS-Q-ST-80_0720240","The software shall be designed to facilitate testing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.2.3a","Requirement","ECSS-Q-ST-80_0720241","Software with a long planned lifetime shall be designed with minimum dependency on the operating system and the hardware, in order to aid portability.\n    NOTE This requirement is applicable to situations where the software lifetime can lead to the obsolescence and non-availability of the original operating system and/or hardware, thereby jeopardizing the maintainability the software.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Software product assurance plan [PAF, SPAP; SRR, PDR];\n          b.Justification of design choices [DDF, SDD; PDR, CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.1a","Requirement","ECSS-Q-ST-80_0720242","Detailed test and validation documentation (data, procedures and expected results) defined in the ECSS-E-ST-40 DJF shall be consistent with the defined test and validation strategy (see clause 6.3.5 and ECSS-E-ST-40 clauses 5.5.3, 5.5.4, 5.6 and 5.8).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.2a","Requirement","ECSS-Q-ST-80_0720243","The test documentation shall cover the test environment, tools and test software, personnel required and associated training requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.3a","Requirement","ECSS-Q-ST-80_0720244","The criteria for completion of each test and any contingency steps shall be specified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.4a","Requirement","ECSS-Q-ST-80_0720245","Test procedures, data and expected results shall be specified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.5a","Requirement","ECSS-Q-ST-80_0720246","The hardware and software configuration shall be identified and documented as part of the test documentation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.2.3.6a","Requirement","ECSS-Q-ST-80_0720247","For any requirements not covered by testing a verification report shall be drawn up documenting or referring to the verification activities performed.\n","EXPECTED OUTPUT: Software verification report [DJF, SVR; CDR, QR, AR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.1a","Requirement","ECSS-Q-ST-80_0720248","For the development of software intended for reuse, ECSS-E-ST-40 clauses 5.2.4.7 and 5.4.3.6 shall apply.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.2a","Requirement","ECSS-Q-ST-80_0720249","The information related to the components developed for reuse shall be separated from the others in the technical specification, design justification file, design definition file and product assurance file. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.3a","Requirement","ECSS-Q-ST-80_0720250","The information related to components developed for reuse in the technical specification, the design justification file, the design definition file and the product assurance file shall be self-contained.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.4a","Requirement","ECSS-Q-ST-80_0720251","The technical specification of components developed for reuse shall include requirements for maintainability, portability and verification of those components.\n","EXPECTED OUTPUT: Technical specification for reusable components [TS, -; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.5a","Requirement","ECSS-Q-ST-80_0720252","The configuration management system shall include provisions for handling specific aspects of software developed for reuse, such as:\n    • longer lifetime of the components developed for reuse compared to the other components of the project;\n    • evolution or change of the development environment for the next project that intends to use the components;\n    • transfer of the configuration and documentation management information to the next project reusing the software.\n","EXPECTED OUTPUT: Software configuration management plan [MGT, SCMP; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.6a","Requirement","ECSS-Q-ST-80_0720253","Where the components developed for reuse are developed to be reusable on different platforms, the testing of the software shall be performed on all those platforms. \n","EXPECTED OUTPUT: Verification and validation documentation for reusable components [DJF, -; CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.3.7a","Requirement","ECSS-Q-ST-80_0720254","The supplier shall provide a certificate of conformance that the tests have been successfully completed on all the relevant platforms.\n    NOTE In case not all platforms are available, the certificate of conformance states the limitations of the validation performed.\n","EXPECTED OUTPUT: Verification and validation documentation for reusable components [DJF, -; CDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.4.1a","Requirement","ECSS-Q-ST-80_0720255","The subcontracting and procurement of hardware shall be carried out according to the requirements of ECSS-Q-ST-20 clause 7.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Justification of selection of operational ground equipment [DJF, -; SRR, PDR];\n          b.Receiving inspection reports [PAF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.4.2a","Requirement","ECSS-Q-ST-80_0720256","The procurement of support services to be used in operational phases shall be justified as covering service level agreements, quality of services and escalation procedures, as needed for system exploitation and maintenance.\n","EXPECTED OUTPUT: Justification of selection of operational support services [DJF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.4.3a","Requirement","ECSS-Q-ST-80_0720257","The choice of procured hardware and services shall address the constraints associated with both the development and the actual use of the software.\n","EXPECTED OUTPUT: Justification of selection of operational ground equipment [DJF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.4.4a","Requirement","ECSS-Q-ST-80_0720258","The ground computer equipment and supporting services for implementing the final system shall be selected according to the project requirements regarding:\n    1. performance;\n    2. maintenance;\n    3. durability and technical consistency with the operational equipment;\n    4. the assessment of the product with respect to requirements, including the criticality category;\n    5. the available support documentation;\n    6. the acceptance and warranty conditions;\n    7. the conditions of installation, preparation, training and use;\n    8. the maintenance conditions, including the possibilities of evolutions;\n    9. copyright constraints;\n    10. availability;\n    11. compatibility;\n    12. site operational constraints.\n","EXPECTED OUTPUT: Justification of selection of operational ground equipment [DJF, -; SRR, PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.4.5a","Requirement","ECSS-Q-ST-80_0720259","Taking account of the provider’s maintenance and product policy, it shall be ensured that the hardware and support services can be maintained throughout the specified life of the software product within the operational constraints.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.5.1a","Requirement","ECSS-Q-ST-80_0720260","The supplier shall establish procedures for firmware device programming and duplication of firmware devices.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.5.2a","Requirement","ECSS-Q-ST-80_0720261","The firmware device shall be indelibly marked to allow the identification (by reference) of the hardware component and of the software component.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","7.5.3a","Requirement","ECSS-Q-ST-80_0720262","The supplier shall ensure that the firmware programming equipment is calibrated.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<1>a","Requirement","ECSS-Q-ST-80_0720263","The SPAP shall contain a description of the purpose, objective, content and the reason prompting its preparation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<2>a","Requirement","ECSS-Q-ST-80_0720264","The SPAP shall list the applicable and reference documents to support the generation of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<3>a","Requirement","ECSS-Q-ST-80_0720265","The SPAP shall include any additional terms, definition or abbreviated terms used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<4>a","Requirement","ECSS-Q-ST-80_0720266","The SPAP shall include or refer to a description of the system and software products being developed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.1>a","Requirement","ECSS-Q-ST-80_0720267","The SPAP shall describe the organization of software product assurance activities, including responsibility, authority and the interrelation of personnel who manage, perform and verify work affecting software quality.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.1>b","Requirement","ECSS-Q-ST-80_0720268","The following topics shall be included:\n    1. organizational structure;\n    2. interfaces of each organisation, either external or internal, involved in the project; \n    3. relationship to the system level product assurance and safety;\n    4. independence of the software product assurance function;\n    5. delegation of software product assurance tasks to a lower level supplier, if any.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.2>a","Requirement","ECSS-Q-ST-80_0720269","The SPAP shall describe the responsibilities of the software product assurance function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.3>a","Requirement","ECSS-Q-ST-80_0720270","The SPAP shall describe the resources to be used to perform the software product assurance function.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.3>b","Requirement","ECSS-Q-ST-80_0720271","The description in B.2.1<5.3>a shall include human resources and skills, hardware and software tools.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.4>a","Requirement","ECSS-Q-ST-80_0720272","The SPAP shall describe the reporting to be performed by software product assurance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.5>a","Requirement","ECSS-Q-ST-80_0720273","The SPAP shall describe the quality models applicable to the project and how they are used to specify the quality requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.6>a","Requirement","ECSS-Q-ST-80_0720274","The SPAP shall describe the contribution of the software product assurance function to the project risk management.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.7>a","Requirement","ECSS-Q-ST-80_0720275","The SPAP shall describe the contribution of the software product assurance function to the next level suppliers selection and control.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.8>a","Requirement","ECSS-Q-ST-80_0720276","The SPAP shall describe the methods and tools used for all the activities of the development cycle, and their level of maturity.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.9>a","Requirement","ECSS-Q-ST-80_0720277","1.The SPAP shall state the scope and objectives of process assessment.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.9>b","Requirement","ECSS-Q-ST-80_0720278","2.The SPAP shall describe the methods and tools to be used for process assessment and improvement.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<5.10>a","Requirement","ECSS-Q-ST-80_0720279","The SPAP shall specify the quality measures related to the operations and maintenance processes (alternatively, a separate SPAP is produced).",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.1>a","Requirement","ECSS-Q-ST-80_0720280","The SPAP shall refer to the software development cycle description in the software development plan. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.1>b","Requirement","ECSS-Q-ST-80_0720281","If not covered in the software development plan, the life cycle shall be described.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.1>c","Requirement","ECSS-Q-ST-80_0720282","The life cycle shall include a milestone immediately before the starting of the software validation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.2>a","Requirement","ECSS-Q-ST-80_0720283","The SPAP shall describe all plans to be produced and used in the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.2>b","Requirement","ECSS-Q-ST-80_0720284","The relationship between the project plans and a timely planning for their preparation and update shall be described.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.3>a","Requirement","ECSS-Q-ST-80_0720285","The SPAP shall contain a description and justification of the measures to be applied for the handling of critical software, including the analyses to be performed and the standards applicable for critical software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.4>a","Requirement","ECSS-Q-ST-80_0720286","The SPAP shall describe the contribution of the software product assurance function to the proper implementation of documentation and configuration management.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.4>b","Requirement","ECSS-Q-ST-80_0720287","The nonconformance control system shall be described or referenced. The point in the software life cycle from which the nonconformance procedures apply shall be specified.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.4>c","Requirement","ECSS-Q-ST-80_0720288","The SPAP shall identify method and tool to protect the supplied software, a checksum-type key calculation for the delivered operational software, and a labelling method for the delivered media.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.5>a","Requirement","ECSS-Q-ST-80_0720289","The SPAP shall describe the process metrics derived from the defined quality models, the means to collect, store and analyze them, and the way they are used to manage the development processes.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.6>a","Requirement","ECSS-Q-ST-80_0720290","The SPAP shall describe the approach for the reuse of existing software, including delta qualification. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.7>a","Requirement","ECSS-Q-ST-80_0720291","The following processes and activities shall be covered, taking into account the project scope and life cycle:\n    1. software requirements analysis;\n    2. software architectural design and design of software items;\n    3. coding;\n    4. testing and validation (including regression testing);\n    5. verification;\n    6. software delivery and acceptance;\n    7. operations and maintenance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.8>a","Requirement","ECSS-Q-ST-80_0720292","The SPAP shall describe or list by reference all procedures and standards applicable to the development of the software in the project.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.8>b","Requirement","ECSS-Q-ST-80_0720293","The software product assurance measures to ensure adherence to the project procedures and standards shall be described. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<6.8>c","Requirement","ECSS-Q-ST-80_0720294","The standards and procedures to be described or listed in accordance with B.2.1<6.8>a shall be as a minimum those covering the following aspects:\n    1. project management;\n    2. risk management;\n    3. configuration and documentation management;\n    4. verification and validation;\n    5. requirements engineering;\n    6. design;\n    7. coding;\n    8. metrication;\n    9. nonconformance control;\n    10. audits;\n    11. alerts;\n    12. procurement;\n    13. reuse of existing software;\n    14. use of methods and tools;\n    15. numerical accuracy;\n    16. delivery, installation and acceptance;\n    17. operations;\n    18. maintenance;\n    19. device programming and marking.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<7>a","Requirement","ECSS-Q-ST-80_0720295","The SPAP shall describe the approach taken to ensure the quality of the software product. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<7>b","Requirement","ECSS-Q-ST-80_0720296","The description of the approach specified in B.2.1<7>a shall include the:\n    1. specification of the product metrics, their target values and the means to collect them;\n    2. definition of a timely metrication programme;\n    3. analyses to be performed on the collected metrics;\n    4. way the results are fed back to the development team;\n    5. documentation quality requirements;\n    6. assurance activities meant to ensure that the product meets the quality requirements.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<8>a","Requirement","ECSS-Q-ST-80_0720297","The SPAP shall include the compliance matrix to the applicable software product assurance requirements (e.g. ECSS-Q-ST-80 clauses, as tailored by a product assurance requirements document), or provide a reference to it.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","B.2.1<8>b","Requirement","ECSS-Q-ST-80_0720298","For each software product assurance requirement, the following information shall be provided:\n    1. requirement identifier;\n    2. compliance (C = compliant, NC = non–compliant, NA = not applicable);\n    3. reference to the project documentation covering the requirement (e.g. section of the software product assurance plan);\n    4. remarks.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<1>a","Requirement","ECSS-Q-ST-80_0720299","The SPAMR shall contain a description of the purpose, objective, content and the reason prompting its preparation.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<2>a","Requirement","ECSS-Q-ST-80_0720300","The SPAMR shall list the applicable and reference documents to support the generation of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<3>a","Requirement","ECSS-Q-ST-80_0720301","The SPAMR shall include any additional terms, definition or abbreviated terms used.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<4>a","Requirement","ECSS-Q-ST-80_0720302","The SPAMR shall contain reporting on verification activities performed by the product assurance function, including:\n    1. reviews;\n    2. inspections;\n    3. walk-throughs;\n    4. review of traceability matrices;\n    5. documents reviewed.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<4>b","Requirement","ECSS-Q-ST-80_0720303","The SPAMR shall contain reporting on the verification of the measures applied for the handling of critical software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<5>a","Requirement","ECSS-Q-ST-80_0720304","The SPAMR shall include or reference a justification of the suitability of the methods and tools applied in all the activities of the development cycle, including requirements analysis, software specification, design, coding, validation, testing, configuration management, verification and product assurance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<5>b","Requirement","ECSS-Q-ST-80_0720305","The SPAMR shall include reporting on the correct use of methods and tools.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<6>a","Requirement","ECSS-Q-ST-80_0720306","The SPAMR shall include reporting on the adherence of software products to the applicable modelling, design and coding standards, including:\n    1. reporting on the application of measures meant to ensure that the design complexity and modularity meet the quality requirements;\n    2. reporting on design documentation w.r.t. suitability for maintenance.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<7>a","Requirement","ECSS-Q-ST-80_0720307","The SPAMR shall include reporting on the collected product and process metrics, the relevant analyses performed, the corrective actions undertaken and the status of these actions.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<7>b","Requirement","ECSS-Q-ST-80_0720308","The results of the software maturity analysis shall also be reported.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<8>a","Requirement","ECSS-Q-ST-80_0720309","The SPAMR shall include reporting on adequacy of the testing and validation documentation (including feasibility, traceability repeatability), and on the achieved test coverage w.r.t. stated goals.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<9>a","Requirement","ECSS-Q-ST-80_0720310","The SPAMR shall include reporting on the status of software problem reports and nonconformances relevant to software.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-80C","C.2.1<10>a","Requirement","ECSS-Q-ST-80_0720311","Whenever relevant and up-to-date information has been already delivered as part of the regular PA progress reporting, a representative summary shall be provided, together with a detailed reference to the progress report(s) containing that information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-10-09C","5.1a","Requirement","ECSS-Q-ST-10-09_0350001","The supplier’s project PA representative shall perform an immediate preliminary assessment of the nonconformance to establish its extent and cause when it is detected.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1b","Requirement","ECSS-Q-ST-10-09_0350002","Based on the preliminary assessment the supplier’s project PA representative shall take the following actions without delay:\n    1. Provisions for the safety of the personnel and of the equipment.\n    2. Prevention of unauthorized use of the nonconforming items, by marking and, unless otherwise determined by the PA representative, segregation until their disposition.\n    3. Prevention of the recurrence of the nonconformances on similar or identical items under processing or testing at that time.\n        NOTE This can lead to the suspension of manufacturing or testing.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1c","Requirement","ECSS-Q-ST-10-09_0350003","The supplier shall apply the following actions to the segregation of nonconforming articles:\n    1. Establish a clearly marked holding area for nonconforming items pending NRB disposition.\n    2. Limit the access to this area to NRB members or personnel authorized by the NRB.\n    3. Make provisions to prevent unauthorized removal of any item.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1d","Requirement","ECSS-Q-ST-10-09_0350004","For items whose segregation in the holding area is not practicable the supplier shall perform the following actions:\n    1. Mark the item as “not to be used”.\n    2. Make sure that the item can not be used by unauthorized personnel.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1e","Requirement","ECSS-Q-ST-10-09_0350005","The supplier shall complete the nonconformance report in conformance with Annex A, and submit it to the internal NRB. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1f","Requirement","ECSS-Q-ST-10-09_0350006","The supplier shall describe the nonconformance clear, unambiguous and sufficiently detailed that it can be understood by personnel not involved in its detection.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.1g","Requirement","ECSS-Q-ST-10-09_0350007","The supplier shall ensure traceability between the NCR and the quality and manufacturing records related to the nonconforming item.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.1a","Requirement","ECSS-Q-ST-10-09_0350008","The NRB shall be the sole technical authority for the treatment of nonconformances occurring in the frame of a business agreement.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.1b","Requirement","ECSS-Q-ST-10-09_0350009","All NRB members shall make dispositions and decisions by consensus.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.1c","Requirement","ECSS-Q-ST-10-09_0350010","The NRB chairman shall involve higher management levels in case of conflict.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.1a","Requirement","ECSS-Q-ST-10-09_0350011","The supplier shall nominate and authorize the internal NRBs core members for the business agreement.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.1b","Requirement","ECSS-Q-ST-10-09_0350012","The responsibilities and authorities of each member shall be assigned.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.1c","Requirement","ECSS-Q-ST-10-09_0350013","The internal NRB shall include, at least, core members from the following areas:\n    1. Project PA (chairman),\n    2. Engineering.\n        NOTE Additional members, or experts, depending on the NCR subject can be nominated by the chairman.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.1d","Requirement","ECSS-Q-ST-10-09_0350014","Immediately after the reporting of a nonconformance, the chairman shall convene an internal NRB.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.2a","Requirement","ECSS-Q-ST-10-09_0350015","The internal NRB shall classify nonconformances as major or minor, based on the severity of their consequences. \n    NOTE Classification of nonconformances is not based on their consequences on cost and schedule.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.2b","Requirement","ECSS-Q-ST-10-09_0350016","In case of several different minor nonconformances on the same item, the internal NRB shall evaluate whether the nonconformances remain minor or reclassified as “major”.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.2c","Requirement","ECSS-Q-ST-10-09_0350017","In case of doubt, the internal NRB shall classify nonconformances as major.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3a","Requirement","ECSS-Q-ST-10-09_0350018","The internal NRB shall investigate the cause(s) of the nonconformance.\n    NOTE If necessary, a separate group of experts can be assigned for the investigation.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3b","Requirement","ECSS-Q-ST-10-09_0350019","The supplier shall carry out physical operation of an irreversible nature on the nonconforming item only with prior approval by the customer.\n    NOTE Non-destructive testing can be used, if the techniques involved have previously been approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3c","Requirement","ECSS-Q-ST-10-09_0350020","The internal NRB shall analyse whether human error or poor workmanship are the primary or secondary cause for the nonconformance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3d","Requirement","ECSS-Q-ST-10-09_0350021","In case that human error or poor workmanship are the primary or secondary cause for the nonconformance, the supplier shall review all related documents and the competence level of personnel in order to prevent recurrence.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3e","Requirement","ECSS-Q-ST-10-09_0350022","The internal NRB shall investigate the consequences of the nonconformance.\n    NOTE This can be supported, where appropriate, by dependability experts or by documentation such as FMECA, CIL, or DJF.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.2.3f","Requirement","ECSS-Q-ST-10-09_0350023","The internal NRB shall document the results of the investigation in the nonconformance report.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.2.3.4a","Requirement","ECSS-Q-ST-10-09_0350039","The customer NRB shall dispose major nonconformances according to the following criteria:\n    1. Return to supplier\n    2. Use “as-is”\n    3. Rework\n    4. Repair\n    5. Scrap",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.3c","Requirement","ECSS-Q-ST-10-09_0350046","A NRB dispositioned “use as-is” need not any physical action on the nonconforming item to make it usable, however corrective and preventive actions shall be performed.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","5.5.3e","Recommendation","ECSS-Q-ST-10-09_0350146","The supplier should show the trends separately for hardware, EEE parts and software.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","A.2.1<1>a","Requirement","ECSS-Q-ST-10-09_0350092","The NCR shall identify the supplier of the nonconforming item.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","A.2.1<20>a","Requirement","ECSS-Q-ST-10-09_0350113","The NCR shall contain the date and reference to written notification.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","A.2.1<23>a","Requirement","ECSS-Q-ST-10-09_0350116","The NCR shall provide the document identification number of the failure analysis report.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-10-09C","B.2.1<8>a","Requirement","ECSS-Q-ST-10-09_0350141","The NCR status shall refer to a RFW, if a related RFW exists.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","6.3c","Requirement","ECSS-Q-ST-70-10_0590020","Minor nonconformances (m) shall be:\n    1. processed through an internal NRB of the PCB manufacturer to determine the causes and consequences;\n    2. reported in the qualification test report in conformance with Annex B;\n    3. assessed by the qualification authority;",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","6.4f","Requirement","ECSS-Q-ST-70-10_0590027","If the PCBs are used for manned space programmes the customer shall assure the PCB base material is tested for the following items:\n    1. Flammability in conformance with ECSS-Q-ST-70-21.\n    2. Offgassing (toxicity) and odour according to ECSS-Q-ST-70-29.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","6.5.14a","Requirement","ECSS-Q-ST-70-10_0590048","The following measurements shall be performed on test pattern X:\n    1. Evaluation of continuity of conductors after exposing the pattern to bending cycles.\n    2. Evaluation of adhesion between conductors and insulating material after exposing the pattern to bending cycles.\n        NOTE See example in Figure 6-15.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.2.2c","Requirement","ECSS-Q-ST-70-10_0590069","The nonconformance criteria shall be as follows:\n1.\tIdentification impossible\tM\n2.\tMarking not conforming to supplier’s specification\tM\n3.\tDefects not affecting identifications\tm\n",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.2.7a","Requirement","ECSS-Q-ST-70-10_0590096","The PCBs number 1-2 shall be used for the tests.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.2.8.4h","Requirement","ECSS-Q-ST-70-10_0590117","The nonconformance criteria shall be as follows:\n    1. Evidence of breakdown, flashover or sparking \t\t\t\t\t\t\tM",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.2.8.5c","Requirement","ECSS-Q-ST-70-10_0590120","The measurement shall be performed using a method ensuring an error no greater than 5 % (four wire method).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.3.3.1e","Requirement","ECSS-Q-ST-70-10_0590145","The rate of traction shall be kept constant at 50 mm/min.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.3.3.3g","Requirement","ECSS-Q-ST-70-10_0590166","For the test the alternating movement shall be continued until an electrical discontinuity appears or until 500 cycles are completed without defect.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.3.4.1b","Requirement","ECSS-Q-ST-70-10_0590173","The test shall be carried out on SnPb finished boards before reflow of test board.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.3.4.3.2l","Requirement","ECSS-Q-ST-70-10_0590194","The nonconformance criteria for the etch undercut on external and internal layers for Au plating with or without Ni finish (see Figure 7-11) shall be as follows:\n    1. If undercut (d) > 30 μm \t\t\t\t\t\t\t\t\tM",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.3.5.2b","Requirement","ECSS-Q-ST-70-10_0590215","The test shall be carried out in an insulation area in conformance with Figure 7-16.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.4.2.2c","Requirement","ECSS-Q-ST-70-10_0590240","Depending on the time passed after the first thermal shock (during the solder bath float test), the board shall be conditioned for 1 h to 6 h at (140 ± 2) °C.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.5d","Requirement","ECSS-Q-ST-70-10_0590261","The temperature range ΔT shall be 200 °C with the highest temperature not exceeding the glass transition temperature of the substrate.\n    NOTE The lower temperature can be (-70 ± 15) °C.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.6.2a","Requirement","ECSS-Q-ST-70-10_0590268","The test shall be carried out in conformance with test Ca of IEC 60068-2-3 (1969-01).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","7.6.3r","Requirement","ECSS-Q-ST-70-10_0590289","The nonconformance criteria shall be as follows:\n    1. Poor wettability of conductors, terminal pads and plated-through holes: see Figure 7-7 for terminal pads and plated-through holes M\n    2. Microsectioning (if necessary): broken metallization \t\t\t\t\tM\n    3. Evidence of corrosion \t\t\t\t\t\t\t\tM",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","8.11e","Requirement","ECSS-Q-ST-70-10_0590310","The PCBs shall be cleaned and dried before packaging according to ECSS-Q-ST-70-11 clause 5.4.2.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","9.1d","Requirement","ECSS-Q-ST-70-10_0590317","The limits for the mechanical characteristics shall be as follows:\n1.\tWarp and twist: \n£ 1,1 % for board thickness ³ 1,6 mm, \n£ 1,5 % for board thickness < 1,6 mm;\n2.\tConductor adhesion/peel strength:\n(a)\tOn epoxy: ³ 16 N/cm;\n(b)\tOn polyimide: ³ 12 N/cm;\n3.\tPull strength:\n(a)\tFor terminal pads 4 mm Æ on epoxy: ³ 140 N;\n(b)\tFor terminal pads 4 mm Æ on polyimide: ³ 80 N;\n(c)\tFor terminal pads 2 mm Æ on epoxy: ³ 35 N;\n(d)\tFor terminal pads 2 mm Æ on polyimide: ³ 20 N.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-10C","9.6c","Requirement","ECSS-Q-ST-70-10_0590338","The limits for the electrolytic coatings shall be as follows:\n1.\tElectrolytic copper plating:\n(a)\tMinimum purity: 99,5 %;\n(b)\tThickness of surface pattern: ³ 25 mm;\n(c)\tThickness of plated­through holes: ³ 25 mm;\n(d)\tThickness of via holes: ³ 20 mm;\n(e)\tThickness of buried via holes: ³ 18 mm;\n(f)\tThickness of blind via holes: ³ 18 mm;\n2.\tTin lead plating after reflow:\n(a)\tTin content of alloy: (63 ± 8) %;\n(b)\tThickness on surface: ³ 8 mm in highest part;\n(c)\tThickness in plated­through holes: ³ 8 mm highest part (minimum half height of hole wall);\n(d)\tOn corner angle: ³ 2 mm;\n3.\tElectrolytic gold plating:\n(a)\tMinimum purity: 99,8 % \n(b)\tNot containing more than 0,2 % silver;\n(c)\tThickness on nickel: (4 ± 3) mm;\n(d)\tThickness on copper: (5 ± 2) mm;\n4.\tElectrolytic nickel plating:\n(a)\tThickness: 2 mm to 10 mm;\nNOTE \tIt is optional under gold.\n\n\t\t\t5.\tResin fill in buried vias: see 7.3.4.3.3h;\n\t\t\t6.\tInsulation between layers: 70 mm minimum.\n",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","5.1.2c","Requirement","ECSS-Q-ST-70-11_0600005","The supplier shall include the manufacturing tolerances given by the PCB manufacturer when designing the PCB layout. \n    NOTE The tolerances and requirements for the various finished PCBs are specified in clause 7.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","5.2.3.3a","Requirement","ECSS-Q-ST-70-11_0600030","The electrolytic nickel plating over copper shall have a thickness from 2 mm to 10 mm.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","5.2.4.1a","Requirement","ECSS-Q-ST-70-11_0600038","The PCB manufacturer shall use copper - invar - copper or copper - molybdenum - copper in conformance with IPC-CF-152B.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","5.4.2f","Requirement","ECSS-Q-ST-70-11_0600059","Desiccant or dry nitrogen filling shall be used in the packaging.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","6.2.2f","Requirement","ECSS-Q-ST-70-11_0600080","The nonconformance criteria for the routing shall be as follows:\n1.\tIncomplete routing of board, such that dimensional or \nmechanical requirements are not met\tM\n2.\tArbitrary cutting defects that remain acceptable \nwithin the dimensional requirements................................................................................m",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","6.3.2a","Requirement","ECSS-Q-ST-70-11_0600103","The test shall be carried out on a microsection.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","6.3.2h","Requirement","ECSS-Q-ST-70-11_0600110","The nonconformance criteria for the thickness of tin­lead alloy in holes shall be as follows:\n1.\tIn highest part of half of the hole wall height (see Figure 6-7 number 3): thickness < 8 mm\tM\n2.\tOn angle of hole corner (see Figure 6-7 number 4): 1 mm < thickness < 2 mm\tm\n3.\tOn angle of hole corner (see Figure 6-7 number 4): thickness < 1 mm.................................M",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","7.2c","Requirement","ECSS-Q-ST-70-11_0600131","The limits for the electrolytic coatings shall be as follows:\n1.\tElectrolytic copper plating:\n(a)\tMinimum purity: 99,5 %;\n(b)\tThickness of surface pattern for soldering pads: ³ 25 mm (total thickness of basic plus electrolytic copper ³ 40 mm);\n(c)\tThickness of plated­through holes: ³ 25 mm;\n(d)\tThickness of via hole: ³ 20 mm;\n2.\tTin lead plating after reflow:\n(a)\tTin content of alloy: (63 ± 8) %;\n(b)\tThickness on surface: ³ 8 mm in highest part;\n(c)\tThickness in plated­through holes: ³ 8 mm in highest part (minimum half height of hole wall);\n(d)\tOn corner angle: ³ 2 mm;\n3.\tElectrolytic gold plating:\n(a)\tMinimum purity: 99,8 % \n(b)\tNot containing more than 0,2 % silver;\n(c)\tThickness on nickel: 1 mm to 7 mm;\n4.\tElectrolytic nickel plating:\nNOTE \tOptional under gold.\n(a)\tThickness: 2 mm to 10 mm;",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-11C","A.2.2a","Permission","ECSS-Q-ST-70-11_0600167","The example PCB CoC document in Figure A-1 may be used.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","6.6.5a","Requirement","ECSS-Q-ST-70-38_0210026","ECSS-Q-ST-70-08 shall apply for \"Insulation strippers\".",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","6.8.3b","Requirement","ECSS-Q-ST-70-38_0210047","The placement equipment used shall be of a type that:\n    1. prevents device or board damages\n    2. indexes devices with respect to the circuit\n    3. aligns the device leads or castellations with the board terminal areas.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","6.8.7d","Requirement","ECSS-Q-ST-70-38_0210054","The sensitivity shall be demonstrated by means of actual 0,03 mm diameter solder balls, stuck to adhesive tape, attached to the multilayer board assembly being inspected.\n    NOTE For guidelines, see C.4.3 and E.1 for X-ray inspection.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","7.7a","Requirement","ECSS-Q-ST-70-38_0210075","ECSS-Q-ST-70-08 shall apply for \"Wires\".",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","7.9.3a","Requirement","ECSS-Q-ST-70-38_0210096","Moisture sensitive components shall be stored and handled in conformance with the component manufacturer’s recommendations. See also clause 8.5b.\n    NOTE Many types of plastic encapsulated components, particularly some plastic BGAs, are moisture sensitive.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","7.10a","Requirement","ECSS-Q-ST-70-38_0210103","Adhesives shall be dispensable, non-stringing, and shall have a reproducible dot profile after application. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","9.4a","Requirement","ECSS-Q-ST-70-38_0210124","ECSS-Q-ST-70-08 shall apply for \"Lead attachment to through holes\".",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","9.7.9c","Requirement","ECSS-Q-ST-70-38_0210149","Staking compounds shall be mixed and cured in accordance with the manufacturer’s procedures. ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","11.5.6a","Requirement","ECSS-Q-ST-70-38_0210170","Solder joints formed to round, flattened, ribbon, “L” and gull-wing shaped leads shall meet the dimensional and solder fillet requirements of Table 11-5 and Figure 11-5.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","14.1a","Requirement","ECSS-Q-ST-70-38_0210191","The supplier shall establish a verification programme to be approved by the Approval authority.\n    NOTE Annex A presents an example of such a programme ",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","14.1h","Requirement","ECSS-Q-ST-70-38_0210198","The configuration shall be submitted to a verification test programme as specified in clause 14.3.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","14.6b","Requirement","ECSS-Q-ST-70-38_0210219","The total number of temperature cycles shall be 500, except for area array devices with conformal coating when clause 14.9.2 is applicable.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","14.10g","Requirement","ECSS-Q-ST-70-38_0210240","After removing the area array device during the dye penetrant test the dye penetrant shall not cover more than 25 % of the ruptured solder joint area. \n    NOTE 1 See C.4.5 for an example of dye penetrant test.\n    NOTE 2 For details see also Figure 16-41 to Figure 16-43 in clause 16.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-38C","15.2a","Requirement","ECSS-Q-ST-70-38_0210247","ECSS-Q-ST-70-08 shall apply for \"Data\".",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-20C Rev.1","5.2.1a","Requirement","ECSS-Q-ST-20_0380007","The supplier shall implement Critical-items control in conformance with ECSS-Q-ST-10-04.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.2.6k","Requirement","ECSS-Q-ST-20_0380032","The supplier shall assess and document the validity of previous inspection and test results when inspection, measuring or test equipment is found to be out of calibration.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.3.1.2a","Requirement","ECSS-Q-ST-20_0380052","The supplier shall ensure that the product is designed such that its performances and characteristics can be reproduced over different models and serial production. ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.3.2.4.4a","Requirement","ECSS-Q-ST-20_0380072","The supplier shall report the qualification status in conformance with the “Qualification status list” DRD as defined in ECSS-Q-ST-10.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.4.1.3b","Requirement","ECSS-Q-ST-20_0380079","The supplier shall submit to the customer, upon request, the list of procurement sources, including all the information in the records 5.4.1.3a, for information.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.5.1f","Requirement","ECSS-Q-ST-20_0380100","Only “first off” shop travellers shall be reviewed unless subsequent travellers incorporate a significant change of inspection requirements or order of events.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.5.6.2a","Requirement","ECSS-Q-ST-20_0380125","The supplier shall ensure that computer-aided techniques and data for processing and machining are validated prior to use and controlled during their use in manufacturing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.5.7.2a","Requirement","ECSS-Q-ST-20_0380128","Contamination-sensitive items shall be cleaned, controlled and maintained to the required cleanliness levels.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.6.2a","Requirement","ECSS-Q-ST-20_0380155","The supplier shall ensure that computer-aided testing techniques and data are validated prior to use and controlled during their use in testing.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.7.1b","Requirement","ECSS-Q-ST-20_0380172","The supplier shall ensure that the preparation of the items for delivery and the physical delivery itself are performed in such a way that degradation is prevented.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","5.8.1.1.1c","Requirement","ECSS-Q-ST-20_0380236","<< deleted, requirement moved to 5.8.1c >>",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","A.2.1<1>a","Requirement","ECSS-Q-ST-20_0380205","The Quality Assurance Plan shall introduce the purpose, objective and the reason prompting its preparation ",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-20C Rev.1","A.2.1<8>a","Requirement","ECSS-Q-ST-20_0380212","The Quality Assurance Plan shall describe the activities to be applied to fulfil the applicable Quality assurance requirements for acceptance and delivery defined in ECSS-Q-ST-20 clause 5.7.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","4.1.3f","Requirement","ECSS-Q-ST-70_0490197","The MMPP manager shall organize Materials, Mechanical Parts and Processes Control Board (MPCB) at all suppliers with the task to review and approve the Materials, Mechanical Parts and Processes as specified in the Clauses 5, 6, and 7.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","4.2.4d","Requirement","ECSS-Q-ST-70_0490023","The following documentation shall be delivered to the customer upon request:\n1.\tRFA with reference and issue in conformance with DRD in Annex D;\n2.\tevaluation reports;\n3.\tdeviation requests.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","4.3b","Requirement","ECSS-Q-ST-70_0490026","Mechanical parts, and materials and processes shall satisfy both ground environment and flight requirements and constraints.\nNOTE \tExamples are:\n·\tGround environment constraints: manufacture, tests, storage, maintenance, transport and integration\n·\tFlight constraints: launch and orbit.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","5.1.5a","Requirement","ECSS-Q-ST-70_0490040","Spacecraft and associated equipment shall be manufactured from materials and by processes that do not cause hazard to personnel or hardware, either on the ground or in space.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","5.1.14a","Requirement","ECSS-Q-ST-70_0490055","The effect of impacts by micrometeoroids and debris on materials shall be reviewed and assessed on a case by case basis.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","5.2.1f","Requirement","ECSS-Q-ST-70_0490234","The supplier shall be responsible for storing and maintain all materials data in an internal database.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","5.5.2a","Requirement","ECSS-Q-ST-70_0490071","The evaluation specified in 5.5.1a shall assess as a minimum the following:\n1.\tthe limits of use;\n2.\tthe materials physical, chemical or functional characteristics along with their values and tolerances;\n3.\tbehavioural tendencies and degradation processes depending on environmental parameters including sensitivity to pollution;\n4.\tacceptance criteria.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","5.5.5a","Requirement","ECSS-Q-ST-70_0490077","For materials not conforming to project requirements, whether at the end of criticality analysis or of evaluation and validation tests, the supplier shall submit a request for deviation in conformance with requirements from the clause 5.2.3.5 of ECSS-Q-ST-10-09.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","6.2a","Requirement","ECSS-Q-ST-70_0490098","Mechanical parts shall be chosen from used for an identical application in other space programmes similar with respect to environment constraints and lifetime.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","6.6.2b","Requirement","ECSS-Q-ST-70_0490120","The procurement specifications shall define the part characteristics, requirements, tests methods, acceptance criteria, lot acceptance testing, source inspection and material supplier inspection.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","6.6.3b","Requirement","ECSS-Q-ST-70_0490123","Source inspection shall be carried out by the customer on the premises of the supplier, mechanical part manufacturer, in conformance with requirements from the clauses 5.4.3 and 5.4.4 of ECSS-Q-ST-20.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","7.3g","Requirement","ECSS-Q-ST-70_0490256","Operators performing special processes shall be certified in conformance with the requirements of the relevant standard.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","7.6.4a","Requirement","ECSS-Q-ST-70_0490156","A processes shall not receive an approval identification in the declared processes list unless requirements from clauses 7.6.2 and 7.6.3 are satisfied.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","B.2.1<2>a","Requirement","ECSS-Q-ST-70_0490175","The DMPL shall include the information in Figure B-1, where the header information identifies the list as the declared mechanical parts  list and includes the issue number and date of issue, as follows:\n1.\tItem number (applicable at equipment supplier level only)\n(a)\tThis consists of the mechanical part identifier and the user code. It takes the form of:\n<group number>.<identifier within the group>.<running number>.<user code>\nNOTE \tFor example: 7.2.1.ACSA.\n(b)\tCharacteristics of the item number are:\n-\tIdentify the subcontractor by an agreed user code for the project.\n-\tOne only per mechanical part type. \n-\tDoes not change during the life of the mechanical parts list.\n2.\tCommercial identification\n(a)\tEnter the correct and standard designation, such as trade name plus number. \n(b)\tIf no trade name exists then enter the manufacturers’ name and number.\n3.\tType of part\nDescribe the material and surface treatment (if applicable).\n4.\tProcurement information\n(a)\tManufacturer or distributor: name of the manufacturer and name of the distributor if different.\n(b)\tProcurement specification: provide reference to one of the following:\n-\tthe procurement specification with issue, revision and date\n-\ta national or international specification or standard, if this exists, and identifies the source of procurement (if relevant), with issue, revision and date.\n5.\tElementary function, main characteristics\n(a)\tEnter the function of the mechanical part.\n(b)\tEnter the main characteristics of the mechanical part.\nNOTE \tFor example, number of revolutions per minute for a ball bearing.\n6.\tUse and location\nUse codes able to define the location of the mechanical part with respect to the:\n(a)\tsubsystem;\n(b)\tparticular piece of equipment (box or item);\n(c)\tuse of the equipment.\n7.\tEnvironmental code\nThe environmental code is defined using Table B-2.\n8.\tCriticality\nEnter “C” for critical or “N” for non­critical. If a mechanical part is considered critical, describe the reason for the criticality and methods of control.\n9.\tSupplier reference, prime comments and prime approval status \n(a)\tUse the supplier reference, prime comments and approval columns to enter all additional information that are necessary in order to obtain customer approval.\n(b)\tThis information comprises reference and issue of the RFA or approval, mechanical parts justification file, evaluation reports and deviation requests.\n(c)\tMake reference to the relevant test data that demonstrates acceptability of the mechanical part under the environment conditions and the application relevant to the particular project concerned.\n(d)\tUse standard abbreviations, defined by the customer, to summarize the acceptance status of a mechanical part for a particular property.\n(e)\tIn order to justify the use of a material for flammability resistance, list here the material thickness and height of oxygen share.\n(f)\tSelect the prime approval status code from Table B-3.\n10.\tThe customer approval status code and comments\n(a)\tSelect this code from Table B-3. \n(b)      Include additional comments where appropriate.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70C Rev.1","C.2.2a","Requirement","ECSS-Q-ST-70_0490181","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"superseded","Product Assurance","Level 1"]
["ECSS-Q-ST-70-05C","5.1.5.2b","Requirement","ECSS-Q-ST-70-05_0540018","The sample holder shall be aligned so that the infrared beam is positioned in the centre of the IR transparent window.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-05C","5.3d","Requirement","ECSS-Q-ST-70-05_0540039","For contact or immersion tests, the surface area shall correspond to the contact surface of the sample.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-05C","5.4.3.3e","Requirement","ECSS-Q-ST-70-05_0540064","The detection limit of the analysis shall be specified and reported in Mass/specific area.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-05C","5.4.3.4a","Requirement","ECSS-Q-ST-70-05_0540067","Contamination levels shall be expressed in terms of the contribution of the following four main group equivalents: hydrocarbons, esters, methyl silicones, and phenyl silicones.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-05C","5.5.2c","Requirement","ECSS-Q-ST-70-05_0540088","The customer shall issue the certificate of conformance after a successful audit or renew it every three years after a successful audit.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-31C","4.2.2.1f","Requirement","ECSS-Q-ST-70-31_0660017","Limited-life materials shall be labelled with their relative shelf-lives and dates of manufacture or date of delivery if date of manufacture is not known.\n    ","NOTE See ECSS-Q-ST-70-22, clause 4.1.3.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-31C","4.2.5d","Requirement","ECSS-Q-ST-70-31_0660038","A spray gun shall be cleaned with an adequate solvent before and after spraying.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-31C","4.3.1.2a","Requirement","ECSS-Q-ST-70-31_0660045","Surfaces shall be cleaned according to an agreed procedure between the supplier and the customer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-31C","4.3.4.1a","Requirement","ECSS-Q-ST-70-31_0660066","The paint shall be thoroughly homogenised in its original container by stirring or shaking, as defined in the manufacturer’s or other paint specific application procedure.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-31C","4.3.4.3b","Requirement","ECSS-Q-ST-70-31_0660081","The temperature, humidity and pressure conditions used for the final curing shall be as defined in manufacture or other paint specific application procedure.\n    ","NOTE For temperature sensitive equipment, it is possible to reduce the temperature, provided that the cure time is increased.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.2d","Requirement","ECSS-Q-ST-70-71_1260006","Black anodising shall not be used on 2000 and 7000 series of Aluminium Alloys.\n","NOTE\tThe black anodizing of metals is covered by ECSS-Q-ST-70-03.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.3b","Requirement","ECSS-Q-ST-70-71_1260009","Copper coatings shall not be used on external surfaces exposed to atomic oxygen in the low Earth orbit.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.8g","Requirement","ECSS-Q-ST-70-71_1260030","Design shall include the effect of the brazing process on the strength of the parent metal.\n","NOTE\tBase metal is the example of the parent metal.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.11g","Requirement","ECSS-Q-ST-70-71_1260055","When acceptability of the mismatch of thermal expansion coefficients between substrates and coatings is verified by test, the test procedure shall conform to the requirements of clause 5 of ECSS-Q-ST-70-04.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.13a","Requirement","ECSS-Q-ST-70-71_1260075","The surfaces on which paints or inks are applied shall be clean and dry prior to their application.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.14d","Requirement","ECSS-Q-ST-70-71_1260082","When oils and greases are directly exposed to space environment, the supplier shall demonstrate that the selected grade complies with the mission requirements.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.17a","Requirement","ECSS-Q-ST-70-71_1260103","Designs using rubber and elastomeric materials shall be assessed for: \n1.\t“set” under stress, \n2.\teffects of cyclic stress, \n3.\tenvironmental resistance, and\n4.\tchemical resistance.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.2.18i","Requirement","ECSS-Q-ST-70-71_1260123","PTFE shall not be used in creep resistance applications.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.1b","Requirement","ECSS-Q-ST-70-71_1260148","Process conditions and environments shall be specified and controlled during all stages of adhesive bonding.\n","NOTE\tAdhesive bonding stages include preparation, application, curing or drying, inspection or testing and storage.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.1e","Requirement","ECSS-Q-ST-70-71_1260151","Prepared surfaces shall be stored in controlled environment within a specified maximum duration demonstrated during the verification phase.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.6k","Requirement","ECSS-Q-ST-70-71_1260176","The weld repair process and inspection shall be performed only under nonconformance review board approval.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.9.3a","Requirement","ECSS-Q-ST-70-71_1260197","Chemical conversion layers shall be continuous when used as the final surface finish of a part.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.13a","Requirement","ECSS-Q-ST-70-71_1260218","Heat treatment of metals and alloys shall conform to national or international specifications for aerospace applications approved by the customer.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-70-71C","4.3.14e","Requirement","ECSS-Q-ST-70-71_1260225","Stamping resulting in stress-raisers shall not be performed.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-60-14C","4.1.4a","Requirement","ECSS-Q-ST-60-14_0470004","Rules for cleanliness efficiency shall be implemented.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-60-14C","6.1.2d","Requirement","ECSS-Q-ST-60-14_0470025","For all type of tantalum capacitors (solid and non-solid), the following specific tests shall be performed before the parametrical measurement: \n    1. Apply 9 discharges and 8 charges with a cycle time of 2 seconds and under nominal voltage. \n    2. Perform a burn-in tests (96 hours, rated voltage, 85°C).\n    3. Monitor the current during both charge and discharge tests to detect short circuit.\n        ","NOTE See (4) in Table 6-1.",{"$nulls":3},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-60-14C","6.5c","Requirement","ECSS-Q-ST-60-14_0470050","Discarded batches shall be processed internally by the relevant reject system of the supplier.",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-Q-ST-60-14C","A.2.1c","Requirement","ECSS-Q-ST-60-14_0470053","The relifing report shall include a conclusion (accepted / rejected).",{"$nulls":4},"superseded","Product Assurance","Level 2"]
["ECSS-E-ST-20-07C","4.2.11.2b","Requirement","ECSS-E-ST-20-07_0080024","An equipment bonding stud connected to the unit housing shall be provided as a ground reference at equipment level.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.2.2a","Requirement","ECSS-E-ST-20-07_0080045","The enclosures shall be large such that the EUT arrangement requirements of 5.2.6 and antenna positioning requirements described in the individual test procedures are satisfied.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.4c","Requirement","ECSS-E-ST-20-07_0080066","The LISN's shall be located at the power source end of the exposed length of power leads specified in 5.2.6.6.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.5.1a","Requirement","ECSS-E-ST-20-07_0080073","Clause 4.2.7 shall apply for tests involving high electromagnetic power or high voltage test equipment.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.6.6.3a","Requirement","ECSS-E-ST-20-07_0080094","Two metres of input power leads (including neutrals and returns) shall be routed parallel to the front edge of the setup in the same manner as the interconnecting leads.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.9.1d","Requirement","ECSS-E-ST-20-07_0080119","If receiver bandwidths larger that those in Table 5-2 are used, no bandwidth correction factors shall be applied to test data due to the use of larger bandwidths.\n    NOTE Larger bandwidths can result in higher measured emission levels.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.10.4a","Requirement","ECSS-E-ST-20-07_0080140","The susceptibility criteria defined in the EMI test procedure shall be repeated in the test report, or the “as run” EMI test procedure shall be an annex to the EMI test report.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.2.10.4d","Requirement","ECSS-E-ST-20-07_0080143","Information shall be displayed after application of correction factors, including transducers, attenuators, and cable loss.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.4.2.2a","Requirement","ECSS-E-ST-20-07_0080168","The test equipment shall be as follows:\n    1. Measurement receiver,\n    2. Current probe,\n    3. Signal generator with amplifier,\n    4. DC-current supply,\n    5. Data recording device,\n    6. Oscilloscope,\n    7. Coaxial “T” connector and coaxial to bifilar transition,\n    8. 1 W and 10 W power metal film resistors with inductance lower than 100 nH,\n    9. LISN defined in 5.2.4.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.4.6.3c","Requirement","ECSS-E-ST-20-07_0080189","To test the EUT antenna positioning, the test setup boundary of the EUT and associated cabling for use in positioning of antennas shall be determined. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.4.9.2a","Requirement","ECSS-E-ST-20-07_0080208","The test equipment shall be as follows:\n    1. Spike generator with following characteristics:\n        (a) Pulse width of 10 µs and 0,15 µs,\n        (b) Pulse repetition rate capability up to 10 pulses per second,\n        (c) Voltage output as required, positive then negative,\n        (d) Output control,\n        (e) Adequate transformer current capacity commensurate with line being tested,\n        (f) Output impedance 5 W or less for 0,15 µs and 1 W or less for 10µs transient,\n        (g) External synchronization and triggering capability.\n    2. Oscilloscope with 10 MHz bandwidth or greater.\n    3. Differential high-voltage probe.\n    4. Isolation transformer.\n    5. 5 W resistor power metal film resistor with inductance lower 100 nH and peak power capability.\n    6. LISN defined in 5.2.4, with added inductor for a total inductance not less than 20 µH for parallel injection.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-07C","5.4.11.3a","Requirement","ECSS-E-ST-20-07_0080218","A basic test setup shall be maintained for the EUT as shown and specified in 5.2.6. and Figure 5-3.\n    NOTE The LISN can be used.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","4.3.2c","Requirement","ECSS-E-ST-20-08_0090008","Instrumentation whose calibration period runs out during the planned test time shall not be used. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.3.2.7a","Requirement","ECSS-E-ST-20-08_0090033","PVA materials shall be capable of tolerating a defined level of degradation resulting from an ATOX environment, without degradation in the nominal performance of the PVA, in conformance with the solar array specification.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.3.3.11.1a","Requirement","ECSS-E-ST-20-08_0090054","The adherence of SCAs to the substrate shall be measured using representative process samples. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.3.3.12a","Requirement","ECSS-E-ST-20-08_0090057","The thickness boundaries, including manufacturing and repair tolerances, shall be defined by means of analysis or test.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.1.2c","Requirement","ECSS-E-ST-20-08_0090082","Qualification margins shall not exceed component and material specifications unless agreed between supplier and customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.1.3.3k","Requirement","ECSS-E-ST-20-08_0090103","Dedicated electrical test points shall be included in the electrical design of the qualification coupon such that the capacitance of single strings can be measured.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.1.4.5a","Requirement","ECSS-E-ST-20-08_0090124","On completion the test, the following conditions shall be met:\n    1. there is electrical continuity (no open circuit), and\n    2. the power output of the test coupon and the insulation is within the limits stated in the SCD-PVA for the specified temperatures.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.2.4b","Requirement","ECSS-E-ST-20-08_0090131","All results of the acceptance test shall be reported in the data documentation package (DDP).\n    NOTE For the DDP, see clause 5.7 and Annex G.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.3.2.7c","Requirement","ECSS-E-ST-20-08_0090152","After coverglass or solar cell repair,, the maximum total projected area of additional bubbles shall not exceed 0,2 % of cell area, discounting:\n    1. bubbles less than 0,02 mm2 in the projected area, and\n    2. bubbles, discolorations and voids located at less than 2 mm from the interconnector edges.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.3.2.19c","Requirement","ECSS-E-ST-20-08_0090177","For mounted components (temperature sensor, resistors and diodes), the following shall be performed:\n    1. Verify the status of the following items: \n        (a) fixation on the substrate;\n        (b) body aspect and absence of cracks;\n        (c) connections;\n        (d) shrinkage tube.\n    2. Ensure that conformal coating of the components,:\n        (a) consist of a uniform layer of the specified adhesive, and \n        (b) encapsulate the components.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.3.3.8b","Requirement","ECSS-E-ST-20-08_0090198","The thermal sensor resistance shall be the value stated in the SCD PVA.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.3.4.2a","Requirement","ECSS-E-ST-20-08_0090201","The electrical power performance at the string level shall be measured at a reference temperature of 25 °C at the interface connector.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.5.3.8c","Requirement","ECSS-E-ST-20-08_0090226","The reflectance shall not change during testing more than as stated in the SCD-PVA. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","5.7a","Requirement","ECSS-E-ST-20-08_0090247","The supplier shall provide a data documentation package (DDP) in conformance with Annex G for the qualification approval records for each coupon.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.1.2c","Requirement","ECSS-E-ST-20-08_0090254","Any deviation from the required in-process, acceptance and qualification test shall be justified in the documentation package.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.1e","Requirement","ECSS-E-ST-20-08_0090275","The supplier shall provide details of the outcome of the qualification programme to the customer. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.3.1.5b","Permission","ECSS-E-ST-20-08_0091074","Chips and nicks may be present on coverglasses if the bare surface of the solar cell is 100 % covered.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.3.4a","Requirement","ECSS-E-ST-20-08_0090321","Temperature coefficient measurement at SCA level need not be performed if already performed during qualification at bare cell level.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.3.8.2f","Requirement","ECSS-E-ST-20-08_0090342","High-purity water in conformance with ASTM D1193-99, Type I, shall be used.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.3.9.2a","Requirement","ECSS-E-ST-20-08_0090345","All SCAs of subgroup D shall be subjected to a coating adherence test on the coverglass SCA face.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.4.3.15.2b","Requirement","ECSS-E-ST-20-08_0090370","For photons with a wavelength between 200 nm to 400 nm, the integrated intensity at the end of test shall be as follows: \n    1. equal to (1000 - 1500) Sun-hours or 1 % of the mission life, whichever is the longer period;\n    2. have a UV irradiation acceleration factor of less than 10 Suns.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","6.6a","Requirement","ECSS-E-ST-20-08_0090391","The supplier shall provide a data documentation package in conformance with Annex G for the qualification approval records and for each SCA delivery lot.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.1.1.2b","Requirement","ECSS-E-ST-20-08_0090398","The SCD-BSC shall be prepared by the supplier in conformance with Annex C and provided to the customer for reviewing and agreement.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.3.2.2.2b","Requirement","ECSS-E-ST-20-08_0090419","The specified test voltage (Vtest) shall be defined in the SCD-BSC.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.4.2.2e","Requirement","ECSS-E-ST-20-08_0090440","Facilities shall be available to safely store the qualification lot including failed samples for a minimum of 6 years (equivalent to five years in storage and one year in orbit).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.1.5.4d","Requirement","ECSS-E-ST-20-08_0090465","The maximum area of worm shaped bulges shall be 3 % of total cell contact area.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.6.3a","Requirement","ECSS-E-ST-20-08_0090486","For single junction solar cells, the coverglass gain-loss stated in the SCD-BSC shall be determined by using n-Amyl alcohol in order to simulate the optical properties of the adhesive. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.7.1.2e","Requirement","ECSS-E-ST-20-08_0090496","In the case of solar cells with Aluminium content window layers, this test shall be extended to simulate on-ground expected duration, and humidity and temperature conditions.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.11.2a","Requirement","ECSS-E-ST-20-08_0090515","The surface finish in the interconnector weld area shall be checked with a micro surface-roughness tester.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.16.2a","Requirement","ECSS-E-ST-20-08_0090536","For solar cells without a protection diode or with a protection diode electrically isolated from the cell, the process shall be as follows:\n    1. Measure the reverse I/V characteristics of the bare solar cell under illumination of 1 S.C. (AM0) with a limiting power supply (to avoid destructive breakdown).\n    2. Ensure that the parameters of reverse I/V characteristics measurement are as stated in the SCD-BSC concerning temperature, hold time, current limitation, maximum reverse bias (voltage).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","7.5.19.3a","Requirement","ECSS-E-ST-20-08_0090543","The deflection of the bare cell shall be lower than the deflection value stated on the SCD-BSC. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.3.3b","Requirement","ECSS-E-ST-20-08_0090564","The orientation method along with associated dimensional tolerances shall be stated in the SCD-CVG.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.7.1.1a","Requirement","ECSS-E-ST-20-08_0090585","All the coverglasses shall be visually inspected with the naked eye to verify the requirements for defects on coverglasses in conformance with clause 8.7.1.2.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.7.4.5b","Requirement","ECSS-E-ST-20-08_0090610","The perpendicularity shall be as stated in the SCD-CVG.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.7.11.1.2f","Requirement","ECSS-E-ST-20-08_0090631","Water condensation on the surface of the coverglasses shall be prevented.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.7.11.2.2f","Requirement","ECSS-E-ST-20-08_0090638","Water condensation on the surface of the cells shall be prevented.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","8.7.16c","Requirement","ECSS-E-ST-20-08_0090659","The coverglasses shall show no degradation in the measured optical performance.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.2.2.1a","Requirement","ECSS-E-ST-20-08_0090680","Delivered integral protection diodes shall be processed and inspected in conformance with the requirements of the process identification document (PID) defined in clause 7.2, and ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.3.2b","Requirement","ECSS-E-ST-20-08_0090687","The supplier shall do the following:\n    1. maintain configuration control of all documents;\n    2. keep the issues of the documents effective at the date of acceptance by the customer;\n    3. provide the PID to the customer for review;\n    4. submit to the customer for review and approval any modifications or changes to documents in the PID ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.5.2e","Requirement","ECSS-E-ST-20-08_0090708","The integral protection diodes shall be equipped with front interconnectors as step 7 in Table 7-2.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.6.2.5.1a","Requirement","ECSS-E-ST-20-08_0090729","The protection diode contact area shall be free of digs, scratches, and probe prints, unless metallization is still present.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.6.9.2a","Requirement","ECSS-E-ST-20-08_0090754","The surface finish in the interconnector weld area shall be checked with a micro surface-roughness tester.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.6.15.2a","Requirement","ECSS-E-ST-20-08_0090775","The test under illumination shall be performed at 1 S.C. (AM0).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.6.16.2b","Requirement","ECSS-E-ST-20-08_0090782","The diodes shall be in flight like configuration which means connected to the adjacent cell.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","9.7.2a","Requirement","ECSS-E-ST-20-08_0090803","A component shall be considered to have failed if it exhibits one or more of the failure modes specified in clause 9.7.1. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","10.1.3a","Requirement","ECSS-E-ST-20-08_0090824","For the regular time interval of data acquisition of a particular test the irradiance, shall be stable to the degree specified for one of the corresponding class of solar simulator in Table 10-4.\n    NOTE See requirement 10.2.6.1c for solar simulator verification.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","10.2.2.1b","Requirement","ECSS-E-ST-20-08_0090831","For multi-junctions, three sets of component solar cells representing a spectral response range similar when compared in conformance with requirement 10.2.2.1d to the cells to be tested, shall be calibrated for their AM0 equivalent short-circuit current using a multi-source solar simulator, conforming to clause 10.1, using the accepted primary standards.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","10.2.6.1b","Requirement","ECSS-E-ST-20-08_0090852","For multi-junction solar cells, the irradiance in the test plane shall be adjusted to AM0 equivalent conditions for each component cell with a maximum allowable deviation of 1 % in the calibrated short-circuit current of each SWS component cell.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","11.2.2.4b","Recommendation","ECSS-E-ST-20-08_0091101","The voltage determined in requirement 11.2.2.4a should be used to calculate the capacitance according to the expression and conditions specified in clause 11.2.1.2.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","A.2.1<8.3>e","Requirement","ECSS-E-ST-20-08_0090898","For blocking diode test, in conformance with clause 5.5.3.3.6, the SCD-PVA shall state:\n    1. The IFORWARD in A, and the VREVERSE in V, of the blocking diode.\n    2. The values for VFORWARD, in V, and IREVERSE, in A, to be obtained from the test.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","B.2.1<6.4>a","Requirement","ECSS-E-ST-20-08_0090919","In conformance with clause 6.4.3.5, the SCD-SCA shall include for multi-junction GaAs solar cells, the number of narrow band interference filters and their wavelength.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","B.2.1<6.11>a","Requirement","ECSS-E-ST-20-08_0090926","In conformance with clause 6.4.3.13, the SCD-SCA shall describe:\n    1. The method to perform the surface conductivity test that shall be between the contact dots or an alternative one to be specified here n the SCD-SCA.\n    2. The minimum value, in W, and the maximum variation after any test, in W, of the cover conductivity before and after qualification tests of SCA of subgroup D (in conformance with Table 6-1).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","C.2.1<6.10>a","Requirement","ECSS-E-ST-20-08_0090947","In conformance with clause 7.5.6.3, the SCD-BSC shall include:\n    1. the agent used to simulate the properties of the adhesive;\n    2. the coverglass used for the test;\n    3. for the test conditions, the temperature, in °C;\n    4. for the pass-fail criteria, the maximum ISC, in %. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","D.2.1<4>a","Requirement","ECSS-E-ST-20-08_0090968","In conformance with requirement 8.3.1.2., the SCD-CVG shall include the justification for any deviation in the in-process, acceptance and qualification tests.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","D.2.1<7.5>a","Requirement","ECSS-E-ST-20-08_0090975","In conformance with clause 8.7.11.2, the SCD-CVG shall state the chemical contents (type and percentage (%) in the mist) of the humid environment when there are specific requirements on the contents of the environment.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","E.2.1<4>a","Requirement","ECSS-E-ST-20-08_0090996","In conformance with requirement 9.2.1.2.2d, the SCD-EPD shall include the justification for any deviation in the in-process, acceptance and qualification tests.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-08C","G.3.1h","Requirement","ECSS-E-ST-20-08_0091028","The DDP for SCA, BSC, CVG and protection diode shall consist of acceptance and qualification test reports.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","4.2.1.2.1c","Requirement","ECSS-E-ST-50-05_0900015","The devices on spacecraft used to switch-off emissions shall have a reliability which is commensurate with the mission lifetime. \n    NOTE The 2 200 MHz - 2 290 MHz band is one of the most densely occupied bands allocated to the space science services with an average occupation density in excess of 25 MHz assigned per each 1 MHz allocated. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","5.3a","Requirement","ECSS-E-ST-50-05_0900036","Earth-space and space-Earth links shall be circularly polarized. \n    NOTE For a right-hand circularly-polarized wave, the sense of polarization determined by the electric field vector rotates with time in a right-hand or clockwise direction when observed in any fixed plane, normal to the direction of propagation, whilst looking in the direction of propagation.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","5.5.1.3a","Recommendation","ECSS-E-ST-50-05_0900273","Unwanted emissions falling into the frequency bands of Space Research (deep space) should be kept to power flux spectral density values less than those given in Table 5-9 at the deep space antenna sites.\n    NOTE From Recommendation ITU-R SA.1157-1 and SFCG Recommendation 14-1R1. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.1.3b","Requirement","ECSS-E-ST-50-05_0900064","For all data signals producing a square wave baseband PCM waveform, the symbol asymmetry measured at 50 % of the peak-to-peak amplitude point shall not exceed 1 % with the symbol asymmetry defined as follows:\n \nwhere long and short symbol refers to the duration of the long and short symbols",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.1.4.2.3c","Requirement","ECSS-E-ST-50-05_0900085","At each transition in the PCM waveform, the subcarrier shall be reversed in phase.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.1.6a","Requirement","ECSS-E-ST-50-05_0900092","The peak modulation index shall be between the minima and the maxima stated in Table 6-3. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.2.1c","Requirement","ECSS-E-ST-50-05_0900113","Data signals shall be PCM. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.2.3.4d","Requirement","ECSS-E-ST-50-05_0900138","Modulation shall be such that for each channel, the suppression of the signal from the other channel is more than 21 dB.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","6.2.5c","Requirement","ECSS-E-ST-50-05_0900159","The telemetry symbol rate short-term variation shall be less than ±1 × 10-6, over any time period less than or equal to 100 times the symbol duration.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","7.2.1f","Requirement","ECSS-E-ST-50-05_0900184","The lock status of the transponder shall be transmitted in the spacecraft telemetry data for operational use by the Earth station. \n    NOTE A standard location of the transponder lock status telemetry is specified in the Command Link Control (CLCW) as described in clause 6.3 of ECSS-E-ST-50-04.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","7.2.1m","Requirement","ECSS-E-ST-50-05_0900191","Subcarrier (when present) and bit clock acquisition shall be achieved using the preamble transmitted before all uplink messages.\n    NOTE The idle sequence as specified in clause 9.2.3 of ECSS-E-ST-50-04 is transmitted at all times (except during acquisition) to limit the power spectral density from the Earth transmitters. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","8.3.2d","Recommendation","ECSS-E-ST-50-05_0900289","From the design value, the adverse and the favourable tolerances, the mean value mn and the variance (sn2), based on a particular probability density function identified in Table 8-1 for each parameter should be calculated according to the equations given in Figure 8-1 for each of the distributions represented.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","9.2.5d","Requirement","ECSS-E-ST-50-05_0900237","A roll-off factor of 0,35 or 0,5 shall be used.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 1","9.2.6.2a","Recommendation","ECSS-E-ST-50-05_0900299","This type of channel filtering should be used for linear amplifier conditions, or with amplifier linearization, when the symbol rate to central frequency ratio is low. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-08C","4.2.7e","Requirement","ECSS-E-ST-32-08_0220014","A sensitivity analysis shall be performed for all composite materials used in high stability structural applications.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-08C","4.5.1a","Requirement","ECSS-E-ST-32-08_0220039","The determination of A-basis and B-basis design allowables shall include all factors relating to the processing and environmental effects, including:\n    1. Form. \n        NOTE E.g. bar, sheet and plate.\n    2. Size, thickness range.\n    3. Manufacturing process.\n        NOTE E.g. extrusion, rolling and forging.\n    4. Grain direction.\n        NOTE E.g. longitudinal, longitudinal transverse and short transverse.\n    5. Temper condition\n        NOTE E.g. heat treatment and cold working.\n    6. Test direction.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-08C","4.6.4c","Requirement","ECSS-E-ST-32-08_0220060","The validation of the composite material shall be performed by measuring properties on test pieces having the hardware lay-up configuration at ambient under nominal conditions and under worst case conditions expected during the life. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10C","5.2.1e","Requirement","ECSS-E-ST-10_0790008","The system engineering organisation shall ensure that each requirement for the lower level elements has a justification reflected in the requirement justification file in conformance with Annex O.\n    NOTE This applies also to a standard as a whole. Tailoring of a standard in a list of applicable standards, or of a requirement in an applicable standard, is possible where each tailoring measure is duly justified.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.2.3.1d","Requirement","ECSS-E-ST-10_0790015","In systems where the supply chain consists of at least 3 layers (including the customer), the system engineering organisation of the highest level supplier shall define at the beginning of a project, a set of requirements specifications covering aspects common to more than one lower level product. \n    NOTE 1 These “common” technical specifications have been historically called support specifications (e.g. GDIR “General Design and Interface Requirements”, environmental, test, EMC requirements specifications) and are separated from other requirements specifications addressing product specific characteristics and functionalities.\n    NOTE 2 Requirements for equipment level products (or below) can be issued in self contained specifications.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.3.1h","Requirement","ECSS-E-ST-10_0790036","The system engineering organisation shall analyse the performances of the system, including end-to-end evaluation, documenting the results of the analysis in the Design Justification File in conformance with Annex K.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.4.1.2a","Requirement","ECSS-E-ST-10_0790061","The system engineering organisation shall define and maintain all technical budgets of the system in conformance with Annex I in terms of target, current status and their trends.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.4.1.3a","Requirement","ECSS-E-ST-10_0790064","The system engineering organisation shall define the design methods, tools and related models to be used during the product life cycle and document them in the SEP.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.5.2f","Requirement","ECSS-E-ST-10_0790085","The system engineering organisation shall ensure that the verification covers the complete product including hardware, software, man in the loop, operations and representative mission scenarios (including pre-launch, launch and early orbit, in-orbit, post-landing, or other mission scenario).\n    NOTE 1 The testing performed during and at the end of the integration of a system is defined as System Functional Test (SFT).\n    NOTE 2 For system composed of different segments (e.g. space segment, ground segment), the testing performed to ensure operability and functionality of the complete system is defined as System Validation Test (SVT).",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","5.6.9b","Requirement","ECSS-E-ST-10_0790110","The system engineering organization shall provide a technical assessment on any nonconformance to the status of the product.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","6.7c","Requirement","ECSS-E-ST-10_0790131","The system engineering organization shall support QR and AR and ensure implementation of the QR and AR actions.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","B.2.1<1>a","Requirement","ECSS-E-ST-10_0790138","The MDD shall contain a description of the purpose, objective, content and the reason prompting its preparation (e.g. logic, organization, process or procedure).",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","D.2.1<4.1>b","Requirement","ECSS-E-ST-10_0790159","The SEP shall list the external means and facilities (e.g. equipment, software, and premises) made available by the customer or by any other entity external to the organization that is responsible of this SEP, and, for each identified mean or facility, identify the applicable interface requirements (e.g. interface control documentation) as well as the authority in charge of it.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","D.2.1<5.1.2>j","Requirement","ECSS-E-ST-10_0790180","The SEP shall define the process and control to be put in place to meet requirements for ground and in-orbit logistics and maintenance, addressing, amongst others, technical activities, related engineering standards, methods and analyses to be performed to ensure that the development of space systems (i.e. manned and unmanned) properly takes into account and integrates the supportability and support aspects for the whole life cycle.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","E.2.1<4.3>b","Requirement","ECSS-E-ST-10_0790197","The TP shall define the model philosophy for each technology or technological element, based on an assessment on the maturity status and on the criticality of the technology with respect to functions' requirements.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","F.2.1<4>b","Requirement","ECSS-E-ST-10_0790209","For each technology or technological element, the following information shall be listed:\n    1. index of technology readiness and maturity as defined in proposed table in definition 3.2.12 “technology readiness level”;\n    2. proof of company's maturity concerning the knowledge and mastership of the technology, including a description of the necessary technology acquisition activities;\n    3. identification of potential risks, e.g. technology availability, programmatic and financial aspects.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","G.2.1<6>b","Requirement","ECSS-E-ST-10_0790230","The DDF shall contain or refer to the system or product technical budget, the latter conforming to Annex I.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","K.2.1<2>a","Requirement","ECSS-E-ST-10_0790255","The DJF shall list the applicable and reference documents in support to its generation.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","K.2.1<8.2.3>a","Requirement","ECSS-E-ST-10_0790276","The DJF shall contain all evidence (e.g. analyses, test results, and model descriptions and correlations) regarding the suitability and validation of all models used for the analysis of the system.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","K.2.1<10.2>a","Requirement","ECSS-E-ST-10_0790283","The DJF shall present the justification of constraints induced by the system or product design definition on the implementation of the operations e.g. operational allowable envelopes, restrictions on operating modes, and exclusion zones.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","L.2.1<10>b","Requirement","ECSS-E-ST-10_0790304","The trade-off report shall present the identified technical and programmatic risks induced by the choice of the recommended solution, and any additional activity necessary to be performed for risk mitigation.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","O.2.1<4>a","Requirement","ECSS-E-ST-10_0790325","The RJF shall present and justify the life profile situations for the concept presented in the technical requirements specification.\n    NOTE For justification, reference can be made to the system concept report of the considered project where relevant.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","P.2.1<4.9.2>a","Requirement","ECSS-E-ST-10_0790350","The PUM shall include:\n    1. Baseline event timelines for all nominal and contingency modes and phases.\n    2. Related constraints.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","P.2.1<4.9.3>b","Requirement","ECSS-E-ST-10_0790353","The PUM shall describe the allowable mode transitions and the operations procedure corresponding to each such transition.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-10C","P.2.1<5.8>a","Requirement","ECSS-E-ST-10_0790374","The PUM shall describe:\n    1. product constituent modes;\n    2. nominal operational procedures;\n    3. contingency procedures.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-31-02C","5.1.2d","Requirement","ECSS-E-ST-31-02_1190008","Abbreviated terms used in requirements shall be defined in a dedicated section of the specification.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.3.1a","Requirement","ECSS-E-ST-31-02_1190027","The qualification stage shall be completed before launch.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.4a","Requirement","ECSS-E-ST-31-02_1190034","The scope of the qualification process shall be adapted to the qualification heritage of the product.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.5.3.3.2b","Requirement","ECSS-E-ST-31-02_1190057","Qualification by similarity shall not be performed on a product that has been previously qualified by similarity.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.6.3.2.1a","Requirement","ECSS-E-ST-31-02_1190080","The test tolerances specified in Table 5-2 shall be applied to the nominal test values specified.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.6.9.1a","Requirement","ECSS-E-ST-31-02_1190106","Thermal performance test results, obtained under 1-g conditions, shall be correlated to predict 0-g (on-orbit) performance.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.6.9.1d","Requirement","ECSS-E-ST-31-02_1190109","When establishing the maximum heat transport capability, the vapour temperature shall be varied in increments within the specified operational temperature range such that a performance over temperature curve is generated.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.6.10.2a","Requirement","ECSS-E-ST-31-02_1190135","The test levels and duration for the sinusoidal vibration test, for generic equipment qualification, independent of the launcher or space element, shall be as specified in Table 5-5.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","5.7b","Requirement","ECSS-E-ST-31-02_1190157","The procedures specified in 5.7a shall be compatible with the safety requirements and personnel control requirements at the facility where the operations are conducted.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","B.2.1<1>b","Requirement","ECSS-E-ST-31-02_1190178","Open issues, assumptions and constraints relevant to this document shall be stated and described.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","B.2.1<7>b","Requirement","ECSS-E-ST-31-02_1190185","The allocation of the requirements to the specific verification tasks shall be given.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","D.2.1<4>a","Requirement","ECSS-E-ST-31-02_1190204","The IRPT shall describe the product configuration data of the inspected item.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","F.2.1<4>a","Requirement","ECSS-E-ST-31-02_1190225","The TPRO shall provide a mapping matrix to the TSPE giving traceability towards the test requirement.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","G.2.1<6>b","Requirement","ECSS-E-ST-31-02_1190249","Open issues shall be clearly stated and described.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-31-02C","H.2.1<1>b","Requirement","ECSS-E-ST-31-02_1190252","Open issues, assumptions and constraints relevant to this document shall be stated and described.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.2.5.2a","Requirement","ECSS-E-ST-33-01_0820018","During the design of the mechanism, all single point failure modes shall be identified.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.5.2.4c","Requirement","ECSS-E-ST-33-01_0820039","ECSS-Q-ST-70-71 clause “Stress corrosion resistance” shall apply.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.3.1c","Requirement","ECSS-E-ST-33-01_0820060","It shall be verified that the degradation of the lubricant in the on-ground and in-orbit environments does not lead to a mechanism performance degradation below the limits specified in the SMS.\n    NOTE Examples of such degradation are friction, wear and lubricant performance variability.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.3.4.2b","Requirement","ECSS-E-ST-33-01_0820081","The calculation specified in requirement 4.7.3.4.2a shall be made available to the customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.3.4.3a","Requirement","ECSS-E-ST-33-01_0820089","Mechanical cables under friction used on moving parts or assemblies shall be lubricated in conformance with 4.7.3.1, 4.7.3.2 and 4.7.3.3.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.5.2.5e","Requirement","ECSS-E-ST-33-01_0820110","The margin of safety (MOS) shall employ the factors of safety (FOS) identified in clause 4.7.5.2.6.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.5.4.2a","Requirement","ECSS-E-ST-33-01_0820135","Unless monitored at spacecraft system level, the design of mechanisms shall include means to monitor the execution of its main functions. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.5.4.3b","Requirement","ECSS-E-ST-33-01_0820138","Unless agreed by the customer, locking or latching mechanisms shall provide an indication of whether the latch or lock is open or closed.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.5.4.6c","Recommendation","ECSS-E-ST-33-01_0820408","Ball bearings should be shielded.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.7.1.1a","Requirement","ECSS-E-ST-33-01_0820184","Mechanisms shall be designed to meet all the requirements regarding electrical interfaces and performances.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.7.5c","Requirement","ECSS-E-ST-33-01_0820205","Connector types and configurations shall be selected to preclude damage or inadvertent operation resulting from mis-mating.\n    NOTE For example, for the number of pins.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.7.7.7d","Requirement","ECSS-E-ST-33-01_0820212","The relative position of cables within the harness shall not change during motion.\n    NOTE The four previous requirements are introduced in order to achieve reproducible resistive torques or forces of moving cable harness.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.1b","Requirement","ECSS-E-ST-33-01_0820233","A verification matrix shall be established by the supplier and provided to the customer for agreement.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.2.12a","Requirement","ECSS-E-ST-33-01_0820258","The mechanism operation shall be verified by analysis to comply with the specified requirements for induced loads. \n    NOTE For example, micro-vibrations. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.3.1d","Requirement","ECSS-E-ST-33-01_0820279","The tests shall verify that the mechanism conforms to the functional dimensioning requirements specified in clause 4.7.5.3.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.3.1g","Requirement","ECSS-E-ST-33-01_0820282","The mechanism shall be subjected to a structural verification.\n    NOTE For structural requirements, see ECSS-E-ST-32.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.3.3.10a","Requirement","ECSS-E-ST-33-01_0820307","The mathematical model used to analyse the dynamic behaviour of the control system shall be correlated with measurements performed on representative hardware agreed by the customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","4.8.3.4.2d","Recommendation","ECSS-E-ST-33-01_0820420","After acceptance testing, refurbishment should not be performed. \n    NOTE This is for the test levels experienced to be at a level, which is not detrimental to the health of the hardware.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","A.2.1<4>c","Requirement","ECSS-E-ST-33-01_0820349","The SMS shall include the stray light and emission requirements.\n    NOTE These requirements are used to select the materials and coatings (see 4.5.2.7).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","A.2.1<6>f","Requirement","ECSS-E-ST-33-01_0820356","The SMS shall include the specified maximum positions of the mechanism.\n    NOTE These maximum positions are provided to design end stops in accordance with 4.7.5.4.4a.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C","C.2.1<3>b","Requirement","ECSS-E-ST-33-01_0820377","For each of the analyses of C.2.1<3>a, the results shall be summarized in a table and compared to the requirements.\n    NOTE Each specific analysis can be provided in a separate document or grouped together.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.2.2.1c","Requirement","ECSS-E-ST-10-02_0740009","Verification of software shall include testing in the target hardware environment.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.2.3a","Requirement","ECSS-E-ST-10-02_0740030","Verification shall be accomplished through the selected verification levels.\n    NOTE Usual levels are defined in 4.2.3.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.2.4.1a","Requirement","ECSS-E-ST-10-02_0740033","Verification shall be accomplished through the selection of the appropriate stages on the basis of project specificity from the following:\n    1. qualification,\n    2. acceptance,\n    3. pre-launch,\n    4. in-orbit (including commissioning),\n    5. post-landing.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.2.6.2a","Requirement","ECSS-E-ST-10-02_0740058","All ground support equipment (GSE) shall be verified under expected environmental conditions and operational constraints.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.2.8.3a","Requirement","ECSS-E-ST-10-02_0740079","The supplier shall provide the AITP for the reviews as agreed with the customer \n    NOTE Guidelines are provided in Annex G.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.3.2.5d","Requirement","ECSS-E-ST-10-02_0740104","The supplier shall provide a Verification report (VRPT) for the reviews as agreed with the customer \n    NOTE Guidelines are provided in Annex G.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","5.3.2.6c","Requirement","ECSS-E-ST-10-02_0740107","The Test procedures shall be in conformance with the DRD in Annex D of ECSS-E-ST-10-03.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","A.2.1<1>b","Requirement","ECSS-E-ST-10-02_0740128","Open issues, assumptions and constraints relevant to this document shall be stated and described.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","B.2.1<6>a","Requirement","ECSS-E-ST-10-02_0740153","The VCD shall collect in the form of a matrix, for each requirement, the following verification information:\n    1. Requirement identifier,\n    2. Requirement text\n    3. traceability between requirement,\n    4. Levels and stages of verification,\n    5. methods, \n    6. link to the relevant section of the verification plan and any planning document, \n        NOTE For example, test specification.\n    7. References to any documentation that demonstrates compliance to the requirements,\n        NOTE For example, report, analysis, waivers, RFD, NCR, NRB, customer closeout records. \n    8. Status of Compliance (yes, no, partial),\n    9. Close-out status (open / closed),\n    10. Reasons of the close-out status,",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","E.2.1<1>b","Requirement","ECSS-E-ST-10-02_0740174","Open issues, assumptions and constraints relevant to this document shall be stated and described.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-02C","E.2.1<4>a","Requirement","ECSS-E-ST-10-02_0740177","The IRPT shall describe the product configuration data of the inspected item.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.2.2e","Requirement","ECSS-E-ST-33-11_0280013","The safety characteristics of items at any level of assembly shall be specified at the specified level of reliability and confidence (see 4.2.2c). ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.3a","Requirement","ECSS-E-ST-33-11_0280036","The use of explosive functions including those for flight termination and range safety during all phases of the mission shall be specified.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.5.2.2c","Requirement","ECSS-E-ST-33-11_0280061","The pre-arm function shall remain in its switched state after operation until the fire function has reverted to its initial state.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.5.2.3b","Requirement","ECSS-E-ST-33-11_0280064","The select function shall select the explosive devices.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.7.2d","Requirement","ECSS-E-ST-33-11_0280085","Each interface shall sustain without degradation in both coupled and separated states\n    1. the assembly and dismantling duty-cycle, and\n    2. the operational and environmental conditions of the application.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.8.2.4b","Requirement","ECSS-E-ST-33-11_0280110","The explosive system shall provide shielding to the same levels noted above when exposed to externally generated electromagnetic fields. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.8.2.11b","Requirement","ECSS-E-ST-33-11_0280131","When exposed to RF conditions, the explosive system shall not be degraded.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.8.2.12c","Requirement","ECSS-E-ST-33-11_0280134","The explosive system shall not generate magnetic fields exceeding the “Electromagnetic interference safety margins” defined in ECSS-E-ST-20.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.9f","Requirement","ECSS-E-ST-33-11_0280159","The nature and condition of age-sensitive materials shall be identified and documented in the DMPL.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.10.3d","Recommendation","ECSS-E-ST-33-11_0280421","Double layer cable shielding should be used.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.10.11.1c","Requirement","ECSS-E-ST-33-11_0280205","It shall not be possible to arm the safe and arm device in case an initiator has been activated with the safe and arm device in safe position.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.10.11.1f","Requirement","ECSS-E-ST-33-11_0280208","Remote operation and status indication shall be provided.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.11.1.1a","Requirement","ECSS-E-ST-33-11_0280229","Clauses from 4.11.1.2 until 4.11.6 shall apply to explosive components, which cannot be fully tested before flight. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.11.3.1a","Requirement","ECSS-E-ST-33-11_0280254","The configuration of the connector shall be used only for initiators.\n    NOTE This is the integral (upper) part of the initiator.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.11.4.6a","Requirement","ECSS-E-ST-33-11_0280275","The properties of distribution boxes given in Table 4-14 shall be quantified and conform to the figures where shown.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.11.6b","Requirement","ECSS-E-ST-33-11_0280282","Under the conditions in column E of Table 4-16, the properties in column A, expressed in the units specified in column B, shall be between the values in column C (maximum) and column D (minimum).",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.12.6c","Requirement","ECSS-E-ST-33-11_0280303","The type of valve NO or NC shall be marked on the device.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.14.2d","Requirement","ECSS-E-ST-33-11_0280324","It shall be demonstrated by inspection of all fired components that the internal dimensions, surfaces and material properties have not been degraded beyond specified limits. \n    NOTE Erosion, corrosion and burning due to the functioning can cause failure or leakage.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.14.4.3b","Requirement","ECSS-E-ST-33-11_0280349","Acceptance tests shall be in conformance with Table 4-26.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.15.2a","Requirement","ECSS-E-ST-33-11_0280352","Devices containing explosives shall be transported in conformance with ST/SG/AC.10/1 Rev.14. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-11C","4.15.4h","Requirement","ECSS-E-ST-33-11_0280373","Site safety regulations, provisions and procedures shall be checked for adequacy for explosive activities.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","6.3.1b","Requirement","ECSS-E-ST-20-06_0070008","Ground shall be carried across an articulating joint or hinge using a ground strap.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","6.3.3.6c","Requirement","ECSS-E-ST-20-06_0070029","For a dielectric material, adjacent to a more conductive material and both exposed to vacuum, hereby constituting a triple point, the resistivity of the dielectric shall be such that the dielectric does not charge at any location to more than 1 kV negative or to more than 100 V positive with respect to the adjacent conductor. \n    NOTE 1 Normally, for a slab geometry, this is fulfilled through the requirement that the resistivity r is such that \n\t \n\tor\n\t \n\twhere t is the material thickness and d is the minimum distance at the surface of the dielectric to the adjacent grounded conductor.\n\tor\n\t \n\twhere ρ is surface resistivity in Ω/square.\n\n    NOTE 2 The first equation in NOTE 1 is when the main conduction path is through the thickness of the material, e.g., to an underlying conductor while the second and third equations are when the main conduction path is parallel to the surface, e.g. to an adjacent conductor.\n\tFor a VMAX of 100 V and J of 10 nA cm-2,   W m2.\t\n\tFor example, a 100 µm thickness dielectric must have a resistivity of less than 1010 W.m if on top of a conductor and a resistivity of less than 106 W.m if on top of a very resistive material and grounded every 1 cm.\n\tFor a scientific mission where, say VMAX=10V,   W m2 usually implies that all surface materials must be good conductors. \n    NOTE 3 No margin is included in the values in NOTE 2.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","6.6.1c","Requirement","ECSS-E-ST-20-06_0070036","The tests shall either:\n    - reproduce the physical process of concern, i.e. charging, in a worst-case environment, or \n    - yield electrostatic material properties enabling the materials response to such an environment to be assessed.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","6.7c","Requirement","ECSS-E-ST-20-06_0070057","The floating potential of the particle detector entrance and of neighbouring surfaces shall be analysed.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","7.2.3.1e","Requirement","ECSS-E-ST-20-06_0070078","The test duration shall be such as to allow at least 10 discharges in each area.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","9.2.2a","Requirement","ECSS-E-ST-20-06_0070103","All metallic components shall be supplied with a grounding path.\n    NOTE This requirement includes structural elements, spot shielding, transformer cores, metal packaging of components, unused tracks on PCBs etc. Also included are cables used for testing on the ground but unused in orbit and cables that become temporarily isolated through the operation of a relay, e.g. antenna feeds when in redundant mode. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","9.2.3a","Requirement","ECSS-E-ST-20-06_0070106","Unless it is demonstrated that the material, in the situation in which it is used, is capable to sustain a higher bulk field without ESD, electric fields within dielectric materials shall be kept to below a maximum electric field, Emax= 107 V/m.\n    NOTE 1 The objective is to minimize the occurrence of discharges due to internal dielectric charging.\n    NOTE 2 The default value does not contain a safety margin. It is usual for a project specification to define an additional margin, depending on the mission and the approach to risk. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","10.2.7b","Requirement","ECSS-E-ST-20-06_0070131","Effects of electrostatic sticking from static electricity or environmentally induced charging shall be analysed. \n    NOTE Other requirements for the design of a tether system lie outside of the scope of this standard, e.g.\n        · mechanical strength,\n        · outgassing,\n        · meteoroid/debris impact,\n        · radiation degradation,\n        · atomic Oxygen,\n        · thermal expansion, and\n        · twisting stresses",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20-06C","11.3.2a","Requirement","ECSS-E-ST-20-06_0070155","Computer models shall include the geometry of the spacecraft and its operative environment including thruster, power supply, grounding scheme and surfaces surrounding the thrusters and its plume. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","4.1.4.1c","Requirement","ECSS-E-ST-60-20_0920011","The unit of all inputs shall be indicated.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","4.1.6.1d","Requirement","ECSS-E-ST-60-20_0920018","The supplier shall document whether the star sensor initialization uses either:\n    • Internal initialization, or\n    NOTE The information to initialize the sensor is provided by the attitude determination function of the star sensor.\n    • Direct initialization.\n    NOTE The information to initialize the sensor is supplied by an external source e.g. AOCS.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","4.4f","Requirement","ECSS-E-ST-60-20_0920039","If the star sensor has the capability of autonomous attitude determination, the supplier shall deliver the on-board star pattern catalogue.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","5.4m","Requirement","ECSS-E-ST-60-20_0920060","No aided tracking shall be considered.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","5.5.6.1b","Requirement","ECSS-E-ST-60-20_0920085","The ‘temporal’ interpretation shall be used, and the performance shall be specified under the related performance general conditions.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","5.5.6.3b","Requirement","ECSS-E-ST-60-20_0920088","Error source contributors 5.5.6.2a.1, 5.5.6.2a.2, 5.5.6.2a.3, 5.5.6.2a.4 shall be validated against on ground test data at (BOL) for finite scenarios. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","5.9.4a","Requirement","ECSS-E-ST-60-20_0920113","Probability of Correct Attitude Determination:\n    1. The correct attitude threshold shall be specified.\n        NOTE E.g. “The correct attitude threshold shall be 0,1 degree around X an Y axis and 0,3 degree around Z axis”\n    2. The probability of correct attitude determination shall be estimated considering all possible initial pointing directions within a defined region within the celestial sphere.\n    3. The probability of correct attitude determination shall be estimated under the conditions given in 5.4 and 5.9.2.\n    4. The probability of correct attitude determination shall be verified using the method specified in 5.9.3.\n        NOTE E.g. “An example of requirement specification is the following: the probability of correct attitude determination within 10 s shall be greater than 99,99 % for random initial pointings within the entire celestial sphere, for rates around any axis of up to 100 arcsec/s at EOL and for accelerations up to 10 arcsec/s².” ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 1","5.12d","Requirement","ECSS-E-ST-60-20_0920134","The functional mathematical model shall be established with customer approved methods.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.2.4.1.2a","Requirement","ECSS-E-ST-33-01_0820004","Marking shall be applied on non-functional surfaces.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.2.4.4b","Requirement","ECSS-E-ST-33-01_0820011","If the design is not maintenance free, the maintenance requirements shall be documented in the SMS, justified, agreed by the customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.4.2d","Requirement","ECSS-E-ST-33-01_0820032","The movement of each part shall ensure that there is no mechanical interference with any other part of the mechanism, the spacecraft, the payload or the launcher.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.5.3d","Requirement","ECSS-E-ST-33-01_0820053","Mechanisms moving with limited oscillatory travel shall be identified.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.3.3.3c","Requirement","ECSS-E-ST-33-01_0820078","The integrity of the anti­creep barrier shall be verifiable by indicators.","NOTE \tFor example, UV­detectable.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.3.4.2b","Requirement","ECSS-E-ST-33-01_0820081","The calculation specified in requirement 4.7.3.4.2a shall be made available to the customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.5.2.3b","Requirement","ECSS-E-ST-33-01_0820397","For cases where a statistical distribution of the loads cannot be demonstrated, the limit loads shall be defined based on the worst-case conditions.","NOTE \tExamples of cases where a statistical distribution of the loads cannot be demonstrated are mechanisms operating loads.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.5.3.1e","Requirement","ECSS-E-ST-33-01_0820122","The minimum actuation force (Fmin) shall be derived by the equation:\n \nwhere:\n-\tI is the resistive inertial force applied to a mechanism subjected to acceleration in an inertial frame of reference (e.g. spinning spacecraft, payload or other).\n-\tFD is the inertial resistance force caused by the worst-case acceleration function specified by the customer at the mechanism level.\n-\tFL is the deliverable output force, when specified by the customer.","NOTE \t1\tMargins against any dynamic coupling between the mechanism and its payload are not covered by the above formulae, and they are addressed on a case by case basis when appropriate.\nNOTE \t2\tThe inertial resistance torque (TD) or force (FD)apply to mechanisms which have a specified acceleration requirement or for which an indirect acceleration requirement can be deduced from speed, time or other (dynamic) requirements.\nNOTE \t3\tWhen a function of the mechanism is to deliver output torques (TL) or forces (FL) for further actuation at higher level, the output torque or force is derived by the customer according to the torque or force requirements specified in 4.7.5.3.1d and 4.7.5.3.1e., taking into account the specified uncertainty factors on the individual resistive contributors and applying a motorization factor of two as presented as : \n \n \nwhere all resistive contributors in the two equations above are related to the customer specific actuation application.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.5.4.3b","Requirement","ECSS-E-ST-33-01_0820138","Unless agreed by the customer, locking or latching mechanisms shall provide an indication of whether the latch or lock is open or closed.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.5.4.3i","Requirement","ECSS-E-ST-33-01_0820145","Shock loads for latches and locks shall be derived by analysis or test, and specified in the mechanism requirements specification.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.5.4.6d","Requirement","ECSS-E-ST-33-01_0820409","For the evaluation of the peak hertzian contact stress, a minimum factor of 1,45 shall be applied to the design limit load.","NOTE \tThe design limit load is derived in compliance with requirements of clause 4.2 of ECSS-E-ST-32-10.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.7.1.1d","Requirement","ECSS-E-ST-33-01_0820187","Fault propagation shall be prevented.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.7.5d","Requirement","ECSS-E-ST-33-01_0820206","Electrical connectors shall be redundant.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.7.7.7a","Requirement","ECSS-E-ST-33-01_0820209","Routing shall be designed to be reproducible.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.2.1a","Requirement","ECSS-E-ST-33-01_0820234","The mechanisms parts, components and assembly analytical verification shall include the analysis specified in 4.8.2.2 to 4.8.2.19.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.2.10a","Requirement","ECSS-E-ST-33-01_0820255","An analytical verification of the conformity of dimensioning and sizing of gears shall be performed.","NOTE \tFor gear dimensioning and sizing see ISO 6336.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.3.1a","Requirement","ECSS-E-ST-33-01_0820276","The tests to be performed to verify that the mechanism fulfils the requirements for use as space hardware shall be:\n1.\tdefined in a test plan, and\n2.\tagreed by the customer. ","NOTE \tThe aim of testing can be either characterization, development, qualification or acceptance. \n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.3.1h","Requirement","ECSS-E-ST-33-01_0820283","Non-linearities shall be measured in order to characterize the dynamic behaviour of the mechanism.","NOTE \tExamples of non-linearities are hysteresis and backlash.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.3.3.9a","Requirement","ECSS-E-ST-33-01_0820303","Electrical wires and connectors shall be tested to verify their insulation from the structure and from each other by not less than 100 MW with a DC voltage of 500 V applied for a duration of 1 minute or until a steady state resistance value is measured.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.8.3.4.2b","Requirement","ECSS-E-ST-33-01_0820326","The acceptance test sequence shall be agreed by the customer.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","4.9.2a","Requirement","ECSS-E-ST-33-01_0820332","Manufacturing drawings shall be established in conformance with ISO 128.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","A.2.1<4>a","Requirement","ECSS-E-ST-33-01_0820347","The SMS shall include the specific climatic protection and environmental requirements.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","C.2.1<1>b","Requirement","ECSS-E-ST-33-01_0820372","The MAV shall list:\n1.\tall the applicable documents regarding requirements related to design and performance; \n2.\tthe design definition file reference of the mechanism being analysed;\n3.\tthe list of documents providing inputs to analyses presented in this document; \n4.\tany other applicable and reference documents to support the generation of the document.","NOTE 1 \tto item 3: For example, thermal analysis, structural analysis, and test reports.\nNOTE 2\tto item 3: Subsystems and parts data to be included.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","D.2.1<11>b","Requirement","ECSS-E-ST-33-01_0820393","For each operational mode  the following topics shall be described:\n1.\toperational configuration;\n2.\tspecific precautions including limitations in terms of operation;\n3.\toperation sequence;\n4.\ttelemetry requirements and health monitoring;\n5.\trecovery contingencies.","NOTE \tExamples of such operational modes are release, calibration, deployment, pointing, and scanning.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.1","G.2.1<3>b","Requirement","ECSS-E-ST-33-01_0820445","The MSVR shall contain the analysis of test data and the relevant assessment.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-10C Rev. 1","4.1.2b","Requirement","ECSS-E-ST-32-10_0110002","The factors in clauses 4.1.4, 4.1.5 and 4.3 shall be applied for both the design and test phases as defined in Figure 4-1.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-10C Rev. 1","4.3.2.1d","Requirement","ECSS-E-ST-32-10_0110023","For expendable launch vehicles, FOSU and FOSY associated with thermal induced loads shall be 1,0.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","5.2.3.10a","Requirement","ECSS-E-ST-50-12_0910024","The jacket colour of the differential signal pairs shall be white.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","5.2.4.15a","Requirement","ECSS-E-ST-50-12_0910045","The skew between the parts of the differential signal in one differential signal pair shall be 0,1 ns/m maximum.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","5.2.5.2a","Requirement","ECSS-E-ST-50-12_0910048","The minimum bend radius of complete cable shall be 45 mm.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","5.4.2a","Recommendation","ECSS-E-ST-50-12_0910360","The maximum length of the cable assembly should be 10 m to ensure that the end to end skew and jitter introduced by the cable assembly does not exceed the maximum budget for the cable. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","6.4a","Requirement","ECSS-E-ST-50-12_0910094","SpaceWire shall use low voltage differential signalling (LVDS) for the Data and Strobe signals.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","6.6.5a","Requirement","ECSS-E-ST-50-12_0910101","After a reset or disconnect (see clause 8.9.2.1) the SpaceWire link transmitter shall initially commence operating at a data signalling rate of (10±1) Mb/s. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","7.7c","Requirement","ECSS-E-ST-50-12_0910122","TICK_OUT shall be asserted whenever the link interface is in the Run state and the receiver receives a valid Time-Code.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.3n","Requirement","ECSS-E-ST-50-12_0910143","The outstanding counter shall contain a maximum count of 56, corresponding to seven FCTs.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.5.2.5f","Requirement","ECSS-E-ST-50-12_0910168","In the Started state the sending from the transmitter of at least one NULL shall be requested before moving to the Connecting state. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.5.3.7.2b","Requirement","ECSS-E-ST-50-12_0910189","The disconnect detection mechanism shall be activated after leaving the ErrorReset state as soon as the first edge is detected on the D or S line.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.5.3.7.4a","Requirement","ECSS-E-ST-50-12_0910192","The Escape error shall be detected by the receiver in the link interface.\n    ","NOTE The escape error event occurs if an ESC character is followed by any control character other than an FCT (ESC followed by FCT is a NULL, see clause 7.3). ESC followed by a data character is a Time-Code (clause 7.3).",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.9.2.4a","Requirement","ECSS-E-ST-50-12_0910217","A credit error shall be identified when in the Run state, a normal character is received when the host system is not expecting any N-Chars.\n    ","NOTE A credit error can be caused if an error occurs undetected by the parity bit (e.g. two bits in error) which results in one or more spurious FCTs. ",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.12.2f","Requirement","ECSS-E-ST-50-12_0910238","Time-Codes shall not be sent out until a link interface is in the Run state \n    ","NOTE For the Run state, see clause 8.5.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","8.12.2m","Requirement","ECSS-E-ST-50-12_0910245","After reset or disconnect-reconnect (state machine in ErrorReset state) the time-counter shall be set to zero and any control-flag outputs shall be set to zero.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","10.2.3d","Requirement","ECSS-E-ST-50-12_0910266","The routing switch addresses shall be assigned as shown in Table 10-1.\n    ","NOTE 1 A leading data character with a value of 0 results in the packet being routed to the routing switch configuration logic.\nNOTE 2 A leading data character with a value of 6 results in the packet being routed to output port 6.\nNOTE 3 A leading data character with a value of 49 results in the packet being routed to the output port that is referred to in location 49 of the routing table within the routing switch.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","10.2.5b","Requirement","ECSS-E-ST-50-12_0910287","When the assigned output port becomes free the input port selected through arbitration shall transfer one packet to the output port.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","10.5.4.4a","Requirement","ECSS-E-ST-50-12_0910312","A routing switch receiving an empty packet shall discard it by deleting the second EOP or EEP.\n    ","NOTE An EOP or EEP received immediately after an EOP or EEP represents an empty packet which does not have a destination address.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-50-12C","12.2.9c","Requirement","ECSS-E-ST-50-12_0910333","If figures for the above parameters are also provided, the conditions applying for the figure measurements shall be clearly stated \n    ","NOTE 1 E.g. temperature, operating voltage.\nNOTE 2 If a SpaceWire routing switch unit supports system time distribution as defined in clause 8.12 then the following conformance statement may be used:\n“This product supports SpaceWire system time distribution according to ECSS-E-ST-50-12.”",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-10C Rev.2","4.1.4.2b","Requirement","ECSS-E-ST-32-10_0110006","KM value shall be justified.","NOTE \tJustification can be performed based on relevant historical practice (e.g. typical values of 1,2 are used for satellites at the beginning of new development and 1,0 for internal pressure loads for pressurized hardware), analytical or experimental means.\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-32-10C Rev.2","4.3.2.3a","Requirement","ECSS-E-ST-32-10_0110025","The factor of safety for global and local buckling shall be selected from Table 4-5.","NOTE \tThe factor of safety does not cover the knock down factors commonly used in buckling analyses - see Buckling handbook (ECSS-E-HB-32-24).\n",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-04C","6.2.2d","Requirement","ECSS-E-ST-10-04_0760020","The ap values of Table 6-4 shall be used together with the relevant (low, moderate or high) long term averaged values of F10.7, S10.7 and M10.7 given in Table 6-3.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-04C","7.2.1.1c","Requirement","ECSS-E-ST-10-04_0760027","For altitudes below 120 km, NRLMSISE-00 shall be used for calculating the total air density.\nNOTE \tThis recommendation follows the advice of the CIRA Working Group, sponsored by COSPAR and URSI.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-04C","9.2.1.2.1b","Requirement","ECSS-E-ST-10-04_0760058","For conservative analysis, the upper case model shall be used.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-04C","9.2.2.2b","Requirement","ECSS-E-ST-10-04_0760070","For mission durations shorter than 1 year, the fluences for one year shall be used [RN.15].\nNOTE \tFor mission durations shorter than 1 year, this results in a conservative fluence estimate.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-10-04C","10.2.3a","Requirement","ECSS-E-ST-10-04_0760095","The MASTER-2005 flux model [RN.26] shall be used together with the following input parameters: \n1.\tMASTER-2005’s latest reference epoch of May 2005 for mission periods after May 2005.\n2.\tThe size interval given in terms of diameter.\n3.\tAll sources included. \nNOTE \tAccess points for the ESA Master model and its patches are defined in Annex J. Model characteristics, uncertainties, some general aspects and other space debris flux models are discussed in Annex J as well. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-20C","4.1.2e","Requirement","ECSS-E-ST-20_0020005","An undetermined status at the interfaces of a powered unit shall not cause damage to an un-powered interface. \n    NOTE 1 Undetermined status includes: non-nominal operating modes, permanent and non permanent failure modes, powered and un-powered interfaces.\n    NOTE 2 In case verification by analysis is not conclusive a complementary verification by test is necessary.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","4.1.3f","Requirement","ECSS-E-ST-20_0020012","The functionality shall be provided to repeat the transmission of all the executable commands without degradation of the function or a change of its status.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","4.2.1m","Requirement","ECSS-E-ST-20_0020033","Override of critical on-board autonomous functions shall be implemented only if a safety interlock is implemented which prevents the activation of the override feature on both main and redundant functions. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","4.2.3f","Requirement","ECSS-E-ST-20_0020054","If the equipment has several connectors, visibility and clearance around each of them shall be such as to enable mating or de-mating without disturbing others already in place or necessitating custom-made tooling. \n    NOTE A usual practice is the insertion of a breakout box for trouble shooting.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","4.2.3m","Requirement","ECSS-E-ST-20_0020061","The following shall be performed for any connector the loss of which can lead to the loss of the mission:\n    1. Document the connector in the single point failure list\n    2. Verify its integrity up to the highest spacecraft integration level",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","4.2.6c","Requirement","ECSS-E-ST-20_0020082","When components operating in a single event are used, 4 times the quantity to be used for flight units shall be procured as one lot: 25 % for the lot acceptance test, 25 % for flight use, 25 % for spares and 25 % for a confirmation test near to the launch date. \n    NOTE Example of such components are fuses.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.4d","Requirement","ECSS-E-ST-20_0020103","The solar array interface voltage shall be defined at the solar array harness connector interface.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.5.3g","Requirement","ECSS-E-ST-20_0020128","For recently developed solar cells and produced in large scale, the string current calculation shall include as a random parameter the increase of solar cell performance.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.6.2n","Requirement","ECSS-E-ST-20_0020149","The battery mechanical design shall ensure that cell stress and fatigue limits are not exceeded",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.6.3g","Requirement","ECSS-E-ST-20_0020156","The battery supplier shall inform the customer of any change in design, materials or process from cells which have experienced life testing or flight.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.7.2h","Requirement","ECSS-E-ST-20_0020177","A fully regulated bus shall keep its nominal value in steady state within ± 0,5 % of the bus voltage at the main regulation point. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.7.4a","Requirement","ECSS-E-ST-20_0020198","For fuse protected busses the delay before non-essential loads disconnection in the event of a bus undervoltage of more than 10% below the minimum value shall be at least 50 ms.\n    NOTE Rationale for the requirement:\nThe bus overload can be due to a failure of a load. Disconnecting prematurely or attempting to disconnect prematurely this load can damage the relay in the presence of a high fusing current. Fuses blow within 20 ms (see requirement 5.8.1i), thus leaving 50 ms allows the fuse clearance which can restore the bus to its nominal value without performing a non-essential load shedding.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.7.5b","Requirement","ECSS-E-ST-20_0020205","The phase margin of converters and regulators not belonging to the spacecraft power system shall be at least 50° and the gain margin 10 dB for worst case end-of-life conditions with representative loading. \n    NOTE Rationale for this requirement:\nThe condition expressed in requirements 5.7.5a and 5.7.5b assumes that the converter has a monotonic decreasing transfer function for which the sufficient condition of the Nyquist criterion can be applied. It indirectly encourages the designer to make designs for which the verification of the stability is simple. A higher quality is used for converters driving the bus quality, and in particular 60° is selected to minimize the “overshoot” in the response.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.8.1k","Requirement","ECSS-E-ST-20_0020226","The stability of current limiters shall be ensured for the actual loads characteristics, verified by analysis under worst case conditions, and tested under a set of cases agreed with the customer. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","5.11.2c","Requirement","ECSS-E-ST-20_0020251","FMECA shall be performed and based on the failure modes previously defined at component level.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","6.3.4.3c","Requirement","ECSS-E-ST-20_0020273","Provision shall be made such that an unintended action does not result.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","7.2.1.2.2a","Requirement","ECSS-E-ST-20_0020294","The following engineering process shall be applied:\n    1. Perform an analysis of the mission requirements for RF signal transmission and reception for all systems and payload for all phases of the mission.\n    2. Perform electrical, mechanical and thermal computer assessments to identify feasibility and performance margin for the whole antenna farm\n    3. Establish performance budgets, including losses, simulation/measurement error and technology maturity margins for the whole antenna farm.\n    4. Establish prediction, measurement and operational error/accuracy budgets for the whole antenna farm.\n        NOTE E.g. Pointing, excitation, phase centre.\n    5. Establish a plan for the maintenance and periodical review of the budgets established in requirement 7.2.1.2.2a.3 and 7.2.1.2.2a.4 during all project phases.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","7.2.2.2.2c","Requirement","ECSS-E-ST-20_0020301","Deformations of reflector antennas, which parts are physically attached to different portions of the spacecraft platform, shall be quantified and their impact on antenna performance assessed.\n    NOTE For large reflector antennas that use hold-down and release, deployment mechanisms as well as pointing devices, ECSS-E-ST-33-11 can be applied.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","7.2.2.3.4c","Requirement","ECSS-E-ST-20_0020322","In all RF BFN structures having a central conductor (ideally insulated), the thermal power generated by Joule effect on the conductor itself shall be quantified and its impact on antenna performances assessed. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","7.2.3.1c","Requirement","ECSS-E-ST-20_0020343","For antenna ports the applicable pressure range and gas properties shall be specified. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","7.3.3.1a","Requirement","ECSS-E-ST-20_0020350","All the components and equipments of the RF chain shall be free of any risk of Gas discharge (Corona) at the maximum specified operating RF power over the full pressure range during: \n    1. the depressurization of the RF components and equipments at launch environmental conditions,\n    2. the pressurization due to out-gassing of the spacecraft in orbit,\n    3. ground testing at ambient pressure, and \n    4. the pressurization of the spacecraft during planetary re-entry phases at the mission environmental conditions. ",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-20C","B.2.1c","Requirement","ECSS-E-ST-20_0020371","The EMEVP shall include any additional definition, abbreviation or symbol used.",{"$nulls":4},"superseded","Engineering","Level 1"]
["ECSS-E-ST-35-06C Rev.1","4.2.2.1b","Requirement","ECSS-E-ST-35-06_0200017","Tank internal structures shall allow for draining and cleaning.","NOTE Examples of such structures are diaphragms, bladders, baffles, and surface tension screens.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.2.3a","Requirement","ECSS-E-ST-35-06_0200038","The system shall allow for ground draining of simulation fluids and of propellants.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.3.4f","Requirement","ECSS-E-ST-35-06_0200059","Component interiors shall be protected by internally plugging the tubing stud in case of acid pickling.\n    ","NOTE For example, valves.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.3.4m","Requirement","ECSS-E-ST-35-06_0200066","Abrasion and surface damage of a seal during integration shall be avoided.\n    ","NOTE E.g. by using application compatible lubricants, masking of sharp edges.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.3.5m","Requirement","ECSS-E-ST-35-06_0200082","Purging or flushing of thrusters shall take the thrusters characteristics into account.\n    ","NOTE 1 Monopropellant thrusters with catalytic beds have limitations regarding flushing liquids, gas flow rates and pressure differentials.\nNOTE 2 Actuation of a flow control valve with gas flow is subject to limitations to avoid overheating of the valve.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.4.4f","Requirement","ECSS-E-ST-35-06_0200113","Helium shall be equivalent to ISO 14951-4:2000.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","4.4.4i","Recommendation","ECSS-E-ST-35-06_0200390","Cleaning and test liquids should be selected from Annex D.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","5.1i","Requirement","ECSS-E-ST-35-06_0200137","Temporary installed hardware shall:\n    1. be compatible with the cleaning process\n    2. be pre-cleaned\n    3. not compromise the hardware to be cleaned\n    4. be marked as temporarily installed",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","5.3.3.1a","Requirement","ECSS-E-ST-35-06_0200162","Acid cleaners shall be used to remove contamination not removable by other solutions.\n    ","NOTE Acid cleaners include nitric acid, chromic acid inhibited hydrochloric acid, inhibited sulphuric acid, inhibited phosphoric acid, mixed acid de-oxidisers and alcoholic phosphoric acid.",{"$nulls":3},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","5.5.1d","Requirement","ECSS-E-ST-35-06_0200183","The temperature used during drying shall not exceed the component or system allowable temperature ranges.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","5.5.4a","Requirement","ECSS-E-ST-35-06_0200204","Flow rates and pressures during dry purging and verification shall not exceed the specified operational limits of components, subsystems or systems.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","5.5.5.3c","Requirement","ECSS-E-ST-35-06_0200211","During the procedure qualification, the thermocouple shall be attached, e.g. by clamping, to the largest part placed in the oven. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","6.2.1a","Requirement","ECSS-E-ST-35-06_0200232","Items cleaned in a controlled environment, except those processed to level visually clean (VC) or level visually clean and inspected with the aid of an ultraviolet (UV) light, shall be tested for conformance to the applicable cleanliness level by the test liquid-flush procedure given in 6.2.2 to 6.2.4.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","6.2.6.3c","Requirement","ECSS-E-ST-35-06_0200257","All items shall meet the dryness requirements of clause 4.4.3.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","6.3.1b","Requirement","ECSS-E-ST-35-06_0200260","The pressurant gas shall be either: \n    - nitrogen in conformance with ISO 14951-3, Grade A, filtered to remove particulates greater than 2 mm , or \n    - helium in conformance with ISO 14951-4, Type 1, Grade A, filtered to remove particulates greater than 2 mm.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","6.4.4b","Requirement","ECSS-E-ST-35-06_0200281","The selected sample shall be representative for the hardware under test.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","8.1f","Requirement","ECSS-E-ST-35-06_0200306","The bags shall be completely sealed to ensure the storage environment is inert. ",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","11.1.2a","Requirement","ECSS-E-ST-35-06_0200327","The liquid flush test shall be performed for particle population and NVR remaining on critical surfaces of items cleaned in a controlled environment.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","A.2.1<4>a","Requirement","ECSS-E-ST-35-06_0200348","The CRA shall present a description of the related propulsion component, subsystem or system and present the cleanliness critical function(s) and performance.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.1","A.2.1<5>e","Requirement","ECSS-E-ST-35-06_0200355","The results of the CRA shall be summarized in defining the required cleanliness classes for the different propulsion elements from component to system level in accordance with clause 4.4.",{"$nulls":4},"superseded","Engineering","Level 2"]
["ECSS-S-ST-00C","9.2c","Requirement","ECSS-S-ST-00_1000003","The customer shall produce, as part of the PRD, a documentation identifying the ECSS requirements applicable to the project.\n    ","NOTE An “ECSS applicable requirements matrix” (EARM) is a recommended method for this component of the PRD.",{"$nulls":3},"superseded","System","Level 1"]
["ECSS-E-ST-10-02C Rev.1","5.2.2.3d","Requirement","ECSS-E-ST-10-02_0740022","Similarity analysis shall define differences that can dictate additional verification activities.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.2.2.4a","Requirement","ECSS-E-ST-10-02_0740025","Verification by Review-of design (ROD) shall consist of using approved records or evidence that unambiguously show that the requirement is met.","NOTE \tExamples of such approved records are design documents and reports, technical descriptions, and engineering drawings.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.2.4.4b","Requirement","ECSS-E-ST-10-02_0740045","In the pre-launch stage the verification shall confirm that the product is capable of functioning as planned during launch and early operations.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.2.7c","Requirement","ECSS-E-ST-10-02_0740070","The preliminary verification planning shall cover all products and requirements by the end of phase B.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.3.2.2c","Requirement","ECSS-E-ST-10-02_0740091","The supplier shall provide an Analysis report for the reviews as agreed with the customer.","NOTE\t1\tSee ECSS-E-ST-10 Table A-1 for review deliverables.\nNOTE\t2\tFor each discipline specific analysis reports is covered in the respective ECSS standard. A generic guideline for the content of an Analysis Report is given in Annex S of ECSS-E-ST-10.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.3.2.4b","Requirement","ECSS-E-ST-10-02_0740098","The supplier shall provide the Inspection report in conformance with the DRD in Annex E.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","5.4.2f","Requirement","ECSS-E-ST-10-02_0740191","The supplier's VCB representative shall ensure the Verification Control Board (VCB) includes participation of Engineering and Quality Assurance representatives within its members.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","A.2.1<9>a","Requirement","ECSS-E-ST-10-02_0740138","The VP shall describe high level definitions of the verification tools to be used, such as S/W facilities, special tools, simulators, analytical tools. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","C.2.1<5>a","Requirement","ECSS-E-ST-10-02_0740162","The Test Report shall include the list of deviations to the test procedure, the nonconformance including failures and the problems.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","C.2.1<6>c","Requirement","ECSS-E-ST-10-02_0740165","Separate test analyses shall be cross-referenced.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-02C Rev.1","F.2.1<5>a","Requirement","ECSS-E-ST-10-02_0740186","The Verification Report shall list the requirements to be verified (in correlation with the VCD).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10C Rev.1","5.2.3.4b","Requirement","ECSS-E-ST-10_0790021","The system engineering function shall ensure that for each requirement contained in the technical requirements specification, the verification methods are reflected in the verification matrix.","NOTE\tTechnical requirements specification is defined in ECSS-E-ST-10-06 Annex A.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","5.3.2c","Requirement","ECSS-E-ST-10_0790041","The system engineering function shall ensure that analyses include design induced effects between system components or the system and its external environment and account for analysis uncertainties, in conformance with Annex K.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","5.3.4d","Requirement","ECSS-E-ST-10_0790050","The system engineering function shall ensure that analysis tools are capable of exchanging and using models and data where agreed by customer and supplier.","NOTE \t1\tFor exchange of models and data, see ECSS-E-TM-10-20 and ECSS-E-TM-10-21.\nNOTE \t2\tExchange can be either direct or via interfaces.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","5.4.1.4b","Requirement","ECSS-E-ST-10_0790071","The system engineering function shall establish and maintain a design justification file in conformance with Annex K.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","5.6.1g","Requirement","ECSS-E-ST-10_0790092","The system engineering function shall ensure that the experience gained in past and in parallel activities is systematically considered and support project management in the collection of experience gained for future use.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","6.2a","Requirement","ECSS-E-ST-10_0790112","<<deleted, modified and inserted as informative text in clause 4>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","6.2d","Requirement","ECSS-E-ST-10_0790115","<<deleted, modified and inserted as informative text in clause 4>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","6.9a","Requirement","ECSS-E-ST-10_0790136","<<deleted, modified and inserted as informative text in clause 4>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","D.2.1<4.1>d","Requirement","ECSS-E-ST-10_0790161","The SEP shall contain the Coordinate System Document (as defined in ECSS-E-ST-10-09 Annex A).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","D.2.1<5.1.2>l","Requirement","ECSS-E-ST-10_0790182","The SEP shall define process and control to be put in place to meet requirements for implementation of design selections relating to humans for any item with associated human interface, including computer based system and equipment.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","D.2.1<5.4>a","Requirement","ECSS-E-ST-10_0790189","The SEP shall describe any specific issues, problems requiring dedicated attention, investigations or actions during the current phase and identify risks, and risk mitigation measures.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","F.2.1<4>b","Requirement","ECSS-E-ST-10_0790209","For each technology or technological element, the following information shall be listed:\n1.\tindex of technology readiness and maturity as defined in Table 4-2 of ECSS-E-AS-11;\n2.\tproof of company's maturity concerning the knowledge and expertise of the technology, including a description of the necessary technology acquisition activities;\n3.\tidentification of potential risks, e.g. technology availability, programmatic and financial aspects.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","G.2.1<6>b","Requirement","ECSS-E-ST-10_0790230","The DDF shall contain or refer to the system or product technical budget, the latter conforming to Annex I.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","K.2.1<2>a","Requirement","ECSS-E-ST-10_0790255","The DJF shall list the applicable and reference documents in support to its generation.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","K.2.1<3>a","Requirement","ECSS-E-ST-10_0790258","The DJF shall contain a description of the expected product, its intended mission, architecture and design, and the functioning principles on which it is based.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","K.2.1<10.2>a","Requirement","ECSS-E-ST-10_0790283","The DJF shall present the justification of constraints induced by the system or product design definition on the implementation of the operations e.g. operational allowable envelopes, restrictions on operating modes, and exclusion zones.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","L.2.1<10>b","Requirement","ECSS-E-ST-10_0790304","The trade-off report shall present the identified technical and programmatic risks induced by the choice of the recommended solution, and any additional activity necessary to be performed for risk mitigation.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","O.2.1<5>a","Requirement","ECSS-E-ST-10_0790326","The RJF shall present and justify the different environments and constraints for each life profile situations for the concept presented in the technical requirements specification.","NOTE\tFor justification, reference can be made to the system concept report of the considered project where relevant.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","P.2.1<2>a","Requirement","ECSS-E-ST-10_0790333","The PUM shall list the applicable and reference documents in support of the generation of the document.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","P.2.1<4.9.3>c","Requirement","ECSS-E-ST-10_0790354","Appropriate cross-reference shall be made to product constituent modes and procedures.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10C Rev.1","P.2.1<5.8>b","Requirement","ECSS-E-ST-10_0790375","product constituent modes shall be defined for all distinct nominal and back-up modes of the subsystem including:\n1.\tpurpose (i.e. conditions under which each is used);\n2.\toperational constraints;\n3.\tresource utilization;\n4.\tthe definition of the associated modes for each product constituent and its software functions;\n5.\thigher level monitoring requirements;\n6.\tidentification of the allowable mode transitions and any product constituent operational constraints.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-10-06C","7.2.3c","Requirement","ECSS-E-ST-10-06_0770007","Abbreviated terms used in requirements shall be defined in a dedicated section of the specification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-06C","7.2.4a","Requirement","ECSS-E-ST-10-06_0770010","The specification shall be complete in terms of applicable requirements and reference to applicable documents.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-06C","8.2.9b","Requirement","ECSS-E-ST-10-06_0770035","Verification of technical requirements shall be performed in conformance with ECSS-E-ST-10-02.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-09C","5.2.2a","Requirement","ECSS-E-ST-10-09_0230002","The Coordinate Systems Document (CSD) shall be produced in conformance with Annex A.\n    ","NOTE The CSD is intended for reviews.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-09C","5.3.3b","Requirement","ECSS-E-ST-10-09_0230023","The origin and axes of a coordinate frame shall be identified in figures using the reference mnemonic as indicated in 5.3.2c.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-09C","5.4.1b","Requirement","ECSS-E-ST-10-09_0230030","The derivation of the origin of a frame from reference points shall be defined.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-09C","5.4.7b","Requirement","ECSS-E-ST-10-09_0230051","Permitted parameterisations of a coordinate system shall be specified in the CSD.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-09C","A.2.1<4>a","Requirement","ECSS-E-ST-10-09_0230076","The CSD shall specify the units pertaining to the coordinate systems and parameterisations used within the project.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.2.1.4a","Requirement","ECSS-E-ST-10-11_0780005","The characteristics of a task of the human-machine system shall be characterised in terms of:\n    1. Objectives,\n    2. Availability of Resources,\n    3. Human functions,\n    4. Type (e.g. in case of tasks: cognitive, physical, automated … e.g. in case of operations: autonomous, maintenance, guided, proximity), \n    5. Complexity (e.g. when fast reaction are needed, multiple users are involved, uncertainties may occur, collaboration with autonomous or semi-autonomous systems), \n    6. Mission or life criticality, and\n    7. Plans and Schedules.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.2.2a","Requirement","ECSS-E-ST-10-11_0780010","Context of use analysis shall be performed ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.4.2b","Requirement","ECSS-E-ST-10-11_0780034","During project planning, the capability to interact with and incorporate stakeholder feedback shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.5.2b","Requirement","ECSS-E-ST-10-11_0780055","When the electronic mannequin is used for EVA or for IVA activities analysis where a dedicated suit is worn by the crew member, suit limitations to human movements and its encumbrances shall be characterized. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.7.2b","Requirement","ECSS-E-ST-10-11_0780076","Additional items see from 4.7.3 up to 4.7.9 shall be present to complete the various living areas including, traffic flow and translation paths, hatches and doors.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.7.4c","Requirement","ECSS-E-ST-10-11_0780083","The following architecture complements shall be included in the design of a pressurised spacecraft or habitat according to its mission duration and related constraints.\n    1. Mobility Aids: provided to support human movements.\n    2. Panels and Partitions: provided for flexibility in the organisation of the living areas.\n        NOTE For an orbital or habitation environment: to cover all volumes that are not considered primary living areas, to avoid free objects to drift in areas where their recovery by the on-board crew might be difficult.\n    3. Aesthetic complements and different colours schemes.\n    4. Crew restraint: provided for all pressurised and un-pressurised environments to restrain or support the crew member in their activities.\n    5. Mechanical restraint for loose objects: provided to enable the crew member to attach equipments and other loose items for task execution.\n    6. Ambient illumination, provided to support human presence both inside and outside the pressurised areas.\n        NOTE 1 It is important that ambient illumination is in line with the pressurised environment local orientation scheme.\n        NOTE 2 It is important that ambient illumination is designed accordingly with the pressurised area functions.\n    7. Complements for protection of the crew (e.g. radiation, touch temperature, hazardous atmosphere, sharp edges).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.7.10h","Requirement","ECSS-E-ST-10-11_0780104","When an EVA is supported by a robot, the EVA crew shall have a direct override capability on the robot operations.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.10.1.1c","Requirement","ECSS-E-ST-10-11_0780129","A continuous assessment plan (part of human-centred design process plan) shall be established. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.10.3.1b","Requirement","ECSS-E-ST-10-11_0780150","This assessment shall be used in the evaluation of the results.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","4.10.3.3b","Requirement","ECSS-E-ST-10-11_0780153","All the related affecting environment characteristics that have influence on the test results shall be of representative fidelity. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-11C","A.2.2b","Requirement","ECSS-E-ST-10-11_0780178","The HCD process plan shall consider all human in the loop issues for the space system project regardless if it concerns the space segment or its ground infrastructure.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","5.2b","Requirement","ECSS-E-ST-10-12_0980002","The achieved RDM shall be established by analysis and a justification provided in the applicable radiation hardness assurance programme required by ECSS-Q-ST-60 for Class 1, 2 and 3 components.\n    NOTE For RDM, see Clause 5.1.1.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","5.5.4b","Requirement","ECSS-E-ST-10-12_0980023","The radiation metric used in the achieved RDM shall be chosen as representative of the sensor bandwidth critical to the mission objectives.\n    NOTE 1 It is highly dependent upon the sensor design and application. It can be provided by the customer in the equipment requirements.\n    NOTE 2 As with single event effects, the MRDM required can be dependent upon the phase of the mission, and local environment.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","5.6.2e","Requirement","ECSS-E-ST-10-12_0980030","For parts whose achieved RDM, as determined from the assessment in requirements 5.6.2a, b and 5.6.2c, falls below the MRDM specified in requirement 5.2a shall be:\n    1. declared by the supplier to have failed to meet the specification, \n    2. reported to the customer, and\n    3. either replaced with a part that meets the MRDM or subjected to detailed testing and analysis procedures.\n        NOTE 1 The tests and analysis procedures are specified in the clauses of ECSS-Q-ST-60 relevant to “Radiation Hardness”.\n        NOTE 2 This analysis can be performed after PDR when more detail of the system geometry is available for more accurate shielding analyses.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","7.5.1b","Requirement","ECSS-E-ST-10-12_0980051","The influence of shielding in attenuating the primary particle environment and modification to its spectrum at the component location shall be analysed, including the effects of the component packaging, as specified in Clause 6.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","9.4.1.2a","Requirement","ECSS-E-ST-10-12_0980076","The probability of single event transients, upsets, functional interrupts and multiple-cell upsets due to ions heavier than protons shall be determined as follows:\n    1. If the variation of the ion cross-section with LET is known, by using the Integrated RPP (IRPP) approach described in requirements 9.5.2a.1 and 9.5.2a.3.\n    2. Otherwise, using either of the following RPP methods:\n        (a) The incident particle differential LET spectrum, integrated over the integral chord-length distribution in the sensitive volume for which the energy deposition is above that corresponding to the experimentally-determined LET threshold of the device, and using the formulation of “Bradford” specified in requirement 9.5.2a.2(b).\n        (b) The differential chord-length distribution integrated over the incident particle integral LET spectrum, for which the LET corresponds to energy deposition above the experimentally-determined threshold of the device, and using the formulation of: “Bradford” or of “Pickel” or of “Blandford and Adams” specified in requirement 9.5.2a.2(b).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","9.4.2c","Requirement","ECSS-E-ST-10-12_0980097","The experimental data used for device conditions shall be either those expected for operational conditions, or such that the experiment provide worse SEE-susceptibility data, as follows:\n    1. For SRAMs and DRAMs, SEU-dependent electrical conditions are voltage, clock frequency and refresh rate.\n    2. For SEL, tests are for the maximum power and maximum temperature conditions expected for space application.\n    3. For SEB, tests correspond to the minimum operating temperature for the application, as this corresponds to maximum SEB susceptibility of the device.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","9.5.2a","Requirement","ECSS-E-ST-10-12_0980100","Calculation of the ion contribution to SEE rates shall be performed as follows:\n    1. By using the LET spectra for cosmic rays and heavy ions from solar particle events given by the radiation environmental specification, obtain the cross section experimental curve giving at least LET threshold and saturation cross-section, or the Weibull parameters.\n    2. If using RPP approach:\n        (a) Assume that the sensitive volume is a parallelepiped of the same volume as the sensitive one.\n        (b) Calculate the error rate using one of the following formulae:            \n-\tBradford formula:\n \nwith    \n \n-\tPickel formula:\n \n\n-\tBlandford and Adams formula:\n \nwhere:\nA\t= total surface area of the SV;\nl, w and h\t= length, width and height of the SV;\ndF/d(LET) \t= differential ion flux spectrum expressed as a function of LET (shortened to “differential LET spectrum”);\nPCL(>D(LET))\t= integral chord length distribution, i.e. the probability of particles travelling through the sensitive region with a pathlength greater than D;\nLETMin \t= minimum LET to upset the cell (also referred to as the LET threshold);\nLETMax \t= maximum LET of the incident distribution (~105 MeV×cm2/g).\n                  \n    3. If using IRPP approach:\n        (a) Use the real sensitive volume for the integration.\n        (b) Calculate the error rate using the following formula:\n \n\n\nwith  \nwhere:\ndF/d(LET)\t=\tdifferential LET spectrum;\nPCL(>D(LET))\t=\tintegral chord length distribution;\ndsion/d(LET)\t=\tdifferential upset cross section;\nA\t=\ttotal surface area of the sensitive volume;\nS\t=\tsurface area of the sensitive volume in the plane of the semiconductor die;\nl, w and h\t=\tlength, width and height of the sensitive volume;\nDMax\t=\tmaximum length that can be encountered in the SV;\nLETMax\t=\tmaximum LET of the LET spectrum;\nLETi,Min\t=\tlower bin limit in the differential upset cross section dsion/d(LET);\nLETi,Max \t=\tupper bin limit in the differential upset cross section dsion/d(LET).\n            NOTE For a detailed discussion of the RPP and IRPP approaches, see ECSS-E-HB-10-12 Sections 8.5.2 to 8.5.4. References can be found in [6], [7], [8], [9] and [10].",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","10.4.9.1a","Requirement","ECSS-E-ST-10-12_0980125","Under the conditions specified in requirement 10.4.2a.1, the energy deposition spectrum from direct ionization shall be calculated by using one of the following formulas:\n    1. From direct ionization, by one of the following formulas:\n        (a) Detailed calculation:\n\t \n        (b) Approximated calculation:\n\t \n\twhere\n\tdY/de(e)\t= energy deposition rate spectrum;\n\tA\t= total surface area of the SV or detector;\n\tdF/dE(E)\t= differential incident particle flux spectrum expressed as a function of energy, E;\n\tdPCL/dD(D)\t= differential chord length distribution through the sensitive volume for an isotropic distribution;\n\tdE/dx(E)\t= stopping power for particles of energy E;\n\tEmin\t= minimum energy for the incident particle spectrum;\n\tEmax\t= maximum energy of the incident particle spectrum.\n\tNOTE This expression assumes the incident particle spectrum on the detector is or can be approximated to a isotropic angular distribution. Furthermore, it is assumed that the change in the stopping power of the particle through the sensitive volume and any multiple scattering can be neglected.\n    2. For nucleon-nuclear collision-induced energy, by one of the following methods:\n        (a) If the dimensions of the detector volume are 10 times (or more) smaller than the ranges and mean-free paths of the incident particles, by using the following formula: \n \nwhere:\ndY/de(e), A, dF/dE(E), dPCL/dD(D), dE/dx(E), Emin, and Emax have the same meaning as in Clause 10.4.9.11, and:\nM\t=\tmass of sensitive volume;\nNA\t=\tAvogadro’s constant;\nW\t=\tatomic or molecular mass of the material making up the detector;\ns(E)\t=\tnuclear-interaction cross-section for the material as a whole due to incident particles of energy E;\ndP/de(E,e)\t=\tenergy deposition rate spectrum (or response function) for incident particles of energy E, and energy deposition, e .\n\n        (b) Otherwise, by applying radiation simulation tools agreed with the customer.\n            NOTE 1 Examples of such tools are Geant4, MCNPX, and FLUKA. More examples can be found in Table 2 of ECSS-E-HB-10-12.\n            NOTE 2 For a rational and detailed discussion on energy deposition spectrum from direct ionization calculation and nucleon-nuclear interactions, see ECSS-E-HB-10-12, Section 9.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-12C","11.5h","Requirement","ECSS-E-ST-10-12_0980146","If shielding simulations are performed which include self-shielding, the simulation shall include the variations in a build-up of high LET particles, including the nuclear interactions (“star” events) of these particles.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31C","4.1.2c","Requirement","ECSS-E-ST-31_0800004","Space vehicle and GSE design shall accommodate specific requirements for thermal conditioning. \n    NOTE For example: Battery thermal conditioning, heat pipe panel levelling fixtures, auxiliary fluid cooling loops, pre-launch conditioning of launcher.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.2.3a","Requirement","ECSS-E-ST-31_0800025","The Cryogenic Control System (CCS) shall meet the allowable temperatures defined by the system authority and specified in the CCS specification.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.3.4.2b","Requirement","ECSS-E-ST-31_0800046","In case of a thermally unacceptable attitude, the TCS shall agree with the system authority alternative attitudes and lay out.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.4.9b","Requirement","ECSS-E-ST-31_0800071","The TCS shall demonstrate by analysis and test that the allocated reliability figure is met.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.5.2.3c","Requirement","ECSS-E-ST-31_0800092","For the cases where full verification by test is not performed the following requirements shall apply and agreed with the system authority:\n    1. Introduction of simplified and separated test cases including nominal and worst case scenarios.\n    2. Clear identification of unknown data and justification of assumptions taken for test prediction.\n        NOTE Examples of unknown data: Heat flux, catalycity, emissivity.\n    3. The methods and processes to use test results and extrapolate to actual flight conditions. \n        NOTE 1 In addition to classical means, plasma wind-tunnel (e.g. arc-jet) and high temperature radiation test methods may be used.\n        NOTE 2 This applies to cases, for which flight conditions are not sufficiently specified and where verification by test is not appropriate (e.g. due to the size of the test object or lack of environment representativity).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.5.3.1c","Requirement","ECSS-E-ST-31_0800095","For TCS items controlled by radiative and conductive heat exchange, a thermal balance test shall be performed in order to: \n    1. provide data for the verification of the thermal mathematical model as part of the TCS qualification,\n    2. demonstrate the suitability of the TCS design,\n    3. verify the performance of TCS hardware, and\n    4. provide data about sensitivity of the TCS design with respect to parameter changes.\n        NOTE 1 For example, heat dissipation\n        NOTE 2 TB testing is generally performed on items at high integration levels, such as spacecraft, service module, payload module or instruments. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","4.6.4a","Requirement","ECSS-E-ST-31_0800120","Requirements for implementing a cleanliness and contamination control programme as specified in ECSS-Q-ST-70-01 clause 5.1 shall apply.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","A.2.1<1>a","Requirement","ECSS-E-ST-31_0800144","The TCS mathematical model specification shall contain a description of the purpose, objective, content and the reason prompting its preparation.\n    NOTE For example:\n        · This document specifies the requirements for the delivery of subassembly mathematical models to the system authority to be used for system analysis.\n        · This document specifies requirements for reduced thermal mathematical models to be delivered by sub-contractors and unit suppliers. The models are introduced in the global mathematical model of the spacecraft in order to calculate satellite thermal performance at system level.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","A.2.1<5>b","Requirement","ECSS-E-ST-31_0800151","A method of identification and numbering of nodes shall be presented.\n    NOTE For example: Each node is identified by 5 digits with the following meaning:\n        · X indicates the type of hardware, i.e. 1 for MLI, 2 for primary structure, 3 for secondary structure, etc.\n        · Y indicates the subassembly or the external element, to which the node belongs;\n        · ZZZ indicates the sequence of nodes in the mathematical model.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","B.2.1<5>e","Requirement","ECSS-E-ST-31_0800172","Tools (including version) and computer environment used for establishing thermal models shall be described.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","C.2.1<9>e","Requirement","ECSS-E-ST-31_0800199","Based on analysis results recommendations for design changes and adaptations at subsystem and system level shall be formulated.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-31C","E.2.1<7>a","Requirement","ECSS-E-ST-31_0800219","The TCS thermal balance test specification shall list the applicable test facility requirements together with the instrumentation, data acquisition and test equipment to be used.\n    NOTE Test facility requirements are defined in close cooperation with the TVT authority.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32-01C Rev. 1","5.1e","Permission","ECSS-E-ST-32-01_0810318","For unmanned, single-mission, space vehicles and their payloads, and GSE the reduced fracture control programme, specified in clause 11, may be implemented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","5.3.1a","Requirement","ECSS-E-ST-32-01_0810008","Fracture control activities and status shall be reported during all project reviews.\n    NOTE For project reviews, see ECSS-M-ST-10.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","6.3.3b","Requirement","ECSS-E-ST-32-01_0810033","The structure remaining after failure of any element of the PFCI shall sustain the limit loads with a safety factor of 1,0 for metallic and glass items or 1,15 for composite, bonded and sandwich items, without losing minimum specified performance.\n    NOTE Minimum specified performance includes prevention of large scale yielding.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","6.3.5.3.2a","Requirement","ECSS-E-ST-32-01_0810052","One of the following criteria shall be met:\n    - Low-risk fracture items are not subjected to fatigue loading beyond acceptance or normal protoflight testing (if any), transportation, and one mission (including a potential aborted mission), or\n    - Low-risk fracture items are shown to possess acceptable resistance to crack growth from potential initial defects caused by machining, assembly, and handling, by demonstrating that assumed initial surface cracks of 3 mm depth and 6 mm length and corner cracks of 3 mm radius from holes and edges do not grow to failure in less than four complete service lifetimes.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","7.1a","Requirement","ECSS-E-ST-32-01_0810059","Fracture mechanics analysis shall be performed to determine the analytical life of a safe life metallic item.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","7.2.5f","Requirement","ECSS-E-ST-32-01_0810080","For the derivation of the proof loading to be applied for identification of initial crack sizes, upper boundary values, defined as 1,3 times the mean values, shall be used for the critical stress intensity factor, KIC or KC.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","7.2.8k","Requirement","ECSS-E-ST-32-01_0810101","Shear (i.e. mode II or mode III) loading of the crack shall be considered, using an analysis method agreed with the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","8.3.2b","Requirement","ECSS-E-ST-32-01_0810128","When the material properties specified in 8.3.2a are not available, they shall be derived by means of a test programme covering:\n    1. Ultimate and yield strength for all welding conditions used, including mechanical properties (as in 8.3.2a) in the presence of different misalignments, angles between joints or typical defects, and their consequences.\n    2. Fracture toughness KC, stress-corrosion cracking threshold KISCC, and crack propagation parameters for each type of thickness.\n    3. Young’s modulus for weld material:\n        (a) Evaluated by test only in those cases, where a significant amount of a second phase with a different modulus compared to the base material appears. \n        (b) If the microstructure with respect to the different phases does not change, the base material Young’s modulus applies also for weld material.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","8.4.3.3a","Requirement","ECSS-E-ST-32-01_0810149","In the case where protective devices are used to reduce the effects of events, to avoid some events, or to protect the structure, the effectiveness of the devices shall be demonstrated by test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","8.4.4.2a","Requirement","ECSS-E-ST-32-01_0810156","A safe life item shall meet all the requirements for the safe life approach described in clauses 6.2, 6.3, and 10.7.\n    NOTE See also Figure 6-3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","8.7a","Requirement","ECSS-E-ST-32-01_0810177","The verification of all potential fracture critical glass components, except those verified as fail-safe or contained, shall include an analysis of crack growth under conditions of the stresses and the environments encountered during their service life.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.2b","Requirement","ECSS-E-ST-32-01_0810198","All nonconformances which affect fracture-critical items and primary structural hardware designed to safe life principles shall be dispositioned as “major nonconformances”.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.3.1g","Requirement","ECSS-E-ST-32-01_0810205","Post test NDI shall be performed for all proof-tested items (where the proof test is not the NDI method).\n    NOTE With approval of the customer, the post test NDI can focus on areas with increased probability of defects, e.g. focusing on welds, castings, forgings, bonds, and composite parts. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.3.3i","Requirement","ECSS-E-ST-32-01_0810226","Except for glass items, visual inspection shall not be the only NDI.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.4.3.1c","Requirement","ECSS-E-ST-32-01_0810247","The radiation of the beam shall be within ±5° of the orientation of the plane of the crack to be detected.\n    NOTE Radiographic exposures at different orientations can be needed to ensure that the complete volume of an item is sufficiently inspected for potentially critical cracks that can be in a wide range of orientations.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.5.2.2.1a","Requirement","ECSS-E-ST-32-01_0810272","Applied NDI methods shall provide crack detection to at least 90 % probability level (confidence level 95 %) in conformance with 10.5.2.2.1b.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.7.2.1.1d","Requirement","ECSS-E-ST-32-01_0810293","The analysis or test shall demonstrate ultimate load capability at the beginning of life.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-01C Rev. 1","10.7.2.2c","Requirement","ECSS-E-ST-32-01_0810300","For metallic parts the detected defect shall be verified as crack-like defect, and a fracture mechanics analysis or test shall be performed to verify the acceptability of this defect.\n    NOTE Only in the case of a well-known type of defect (e.g. pores) for which a data base of representative test data is available, an assessment without replacing the defect by a crack can be used.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.2.3.2a","Requirement","ECSS-E-ST-32-02_0260013","Safe operating limits shall be established for pressurized hardware based on analysis and testing employed during its design, development and qualification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.2.4.3d","Requirement","ECSS-E-ST-32-02_0260034","If the demonstration specified in 4.2.4.3c is not performed, it shall be demonstrated that all concerned parts of the pressurized hardware are not affected by the exceeded storage environment.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.3.2.1e","Requirement","ECSS-E-ST-32-02_0260041","In the case specified in 4.3.2.1d, requirements for ‘fatigue analysis’ shall be applied in conformance with ECSS-E-ST-32.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.3.3.1d","Requirement","ECSS-E-ST-32-02_0260062","The failure mode shall be demonstrated by analysis or test or both according to clause 5.3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.3.4.1c","Requirement","ECSS-E-ST-32-02_0260087","A strength and stability demonstration shall be performed by analysis and test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.3.4.2j","Requirement","ECSS-E-ST-32-02_0260108","If external cycling loads are applied, the load shall be cycled to limit for four times the predicted number of operating cycles of the most severe design condition.","NOTE Destabilizing load with constant minimum internal pressure or maximum additive load with a constant MDP.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.4.2.1j","Requirement","ECSS-E-ST-32-02_0260129","For ‘process control’, requirements shall be in conformance with ECSS-Q-ST-70.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.4.2.3a","Requirement","ECSS-E-ST-32-02_0260136","All hardware shall be submitted to the following chronology of operations:\n    1. initial NDI, in order to establish the initial condition of the hardware;\n    2. proof pressure test;\n    3. leak test;\n    4. final NDI.","NOTE The NDI prior to proof test can be substituted for that of the manufacturing process.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.4.3.2f","Requirement","ECSS-E-ST-32-02_0260157","If external cycling loads are applied, the load shall be cycled to limit for four times the predicted number of operating cycles of the most severe design condition.","NOTE Destabilizing load with constant minimum internal pressure or maximum additive load with a constant MDP.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.4.4.1h","Requirement","ECSS-E-ST-32-02_0260169","‘Safe life item’ demonstration shall be performed in conformance with ECSS-E-ST-32-01:\n    1. by test for non-metallic items;\n    2. by analysis or test or both for metallic items (e.g. metallic bosses).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.4.4.3e","Requirement","ECSS-E-ST-32-02_0260186","Final NDI shall be performed on the over-wrap of the COPS as a minimum.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.5.2.2a","Requirement","ECSS-E-ST-32-02_0260207","Clause 5.2 on structural engineering shall be applied.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.5.2.4d","Requirement","ECSS-E-ST-32-02_0260232","Final NDI shall be performed on the over-wrap of the COPC as a minimum.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.5.3.3f","Requirement","ECSS-E-ST-32-02_0260253","NDI operations shall be applied to the over-wrap, in addition to NDI on the liner.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.6.1.2l","Requirement","ECSS-E-ST-32-02_0260274","Inspections shall be applied according to clause 5.7.\n    ","NOTE 1 The development approach for sealed containers is illustrated in Figure 4-10\nNOTE 2 The development approach for cryostats (or Dewars) is illustrated in Figure 4-11\nNOTE 3 The development approach for heat pipes is illustrated in Figure 4-12\nNOTE 4 The development approach for hazardous fluids containers is illustrated in Figure 4-13\nNOTE 5 Failure mode demonstration as per clause 5.3 is sometimes specified for heat pipes by the customer.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.6.1.4b","Requirement","ECSS-E-ST-32-02_0260281","Cryostats shall be NDI inspected prior to the proof pressure test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.6.2.3b","Permission","ECSS-E-ST-32-02_0260461","The first qualification test article specified in 4.6.2.3a may be deleted with customer approval.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.6.3.2h","Requirement","ECSS-E-ST-32-02_0260323","Qualification tests shall be conducted according to clause 4.6.3.3 to demonstrate the structural adequacy of the design.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","4.6.3.3b","Permission","ECSS-E-ST-32-02_0260465","The first qualification test article specified in 4.6.3.3a may be deleted with customer approval.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","5.3.1b","Requirement","ECSS-E-ST-32-02_0260351","The choice of the demonstration methodology (i.e. analysis or test or both) shall conform to the requirements on failure mode demonstration specified in clauses 4.2 to 4.5 according to the type of pressurized hardware.\n    ","NOTE For example:\n        · Failure mode may be demonstrated by similarity with an existing analysis or test with customer approval.\n        · For new designs, without heritage, the demonstration by test is sometimes specified by the customer.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","5.3.5b","Requirement","ECSS-E-ST-32-02_0260376","When LBB is demonstrated by test, a test report shall be prepared in conformance with ECSS-E-ST-10-02.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","5.5.1a","Requirement","ECSS-E-ST-32-02_0260395","‘General requirements’ and ‘Accepting testing’ requirements shall apply in conformance with ECSS-E-ST-10-03.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-02C Rev. 1","5.7.2e","Requirement","ECSS-E-ST-32-02_0260416","For ‘NDI for composite and bonded parts’, requirements shall be in conformance with ECSS-E-ST-32-01.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-03C","4.4d","Requirement","ECSS-E-ST-32-03_0100007","The modal DOFs shall be ordered in the matrices according to the mode numbering sequence. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-03C","5.4.3c","Requirement","ECSS-E-ST-32-03_0100028","The maximum acceptable non-zero terms of the (6x6) matrix KR shall be agreed.\n    ","NOTE 1 All the terms of ER are theoretically equal to zero.\nNOTE 2 For 1 meter or 1 radian rigid motion, typical acceptable values of ER terms are not exceeding 1.E-03 joule.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-08C Rev. 1","4.2.5b","Requirement","ECSS-E-ST-32-08_0220007","If analysis specified in 4.2.5a confirms that creep can occur, the creep testing campaign to be performed shall be agreed with the customer at MPCB.\n    ","NOTE Creep is a time-dependant deformation of a material under an applied load. It usually occurs at elevated temperature, although some materials creep at room temperature. If permitted to continue indefinitely, creep terminates in rupture. Extrapolations from simple to complex stress-temperature time conditions are difficult.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-08C Rev. 1","4.2.7a","Requirement","ECSS-E-ST-32-08_0220010","Thermal mismatch between structural members shall not generate stresses in the specified operational temperature range for the item higher that the specified allowable limit.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-08C Rev. 1","4.3.7b","Requirement","ECSS-E-ST-32-08_0220030","Effectiveness of the moisture barrier shall be demonstrated by test.\n    ","NOTE Coatings can be used to prevent moisture absorption or desorption of dimensionally stable structures or to prevent the release of organic volatiles which can affect the performances of some equipments.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-08C Rev. 1","4.6.2e","Requirement","ECSS-E-ST-32-08_0220055","Composite materials shall be characterized by elementary tests on samples.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","4.1.2a","Requirement","ECSS-E-ST-32-11_0250001","Prior to the execution of the test, the frequencies of interest and the mode shapes of interest shall be identified.\n    NOTE 1 The “frequencies of interest” and the “mode shapes of interest” are those identified as being relevant for achieving the modal survey test objectives.\n    NOTE 2 Instead of specific frequencies of interest, a frequency range of interest can be identified.\n    NOTE 3 In cases where the test article mathematical model is employed for accurate response predictions, the frequency range of interest is usually defined as being the frequency range in which major dynamic excitations from the launch vehicle are expected.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","4.2.4b","Requirement","ECSS-E-ST-32-11_0250022","The test facility shall have a valid (up-to-date) calibration certificate.\n    NOTE 1 The calibration certificate documents the results of the calibration of the measuring instruments or the measurement system. Usually the calibration is performed by an authorized external institution.\n    NOTE 2 It is good practice for test facilities to provide calibration certificates that are less than one year old.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","4.2.5.2b","Requirement","ECSS-E-ST-32-11_0250029","Test operators shall be alerted by automatic facility procedures if there is overloading.\n    NOTE For example, acoustic or optical warnings, automatic shut-down.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","5.3.3a","Requirement","ECSS-E-ST-32-11_0250050","A measurement point plan (MPP) shall be defined for the modal survey test.\n    NOTE 1 The structural dynamic responses can be measured by means of accelerometers. Different types of accelerometers can be applied.\n    NOTE 2 For specific applications, other sensors can also be applied, for example: strain gauges, optical sensors, and displacement meters.\n    NOTE 3 Depending the test requirements, the measurement direction can be either uni-axial, bi-axial, or tri-axial. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","5.4.3a","Requirement","ECSS-E-ST-32-11_0250075","The type of the excitation signal shall be defined. \n    NOTE The most commonly applied excitation signals are given in Annex A. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","5.4.4b","Requirement","ECSS-E-ST-32-11_0250078","Stiffness and damping non-linearities shall be determined by measuring the variation of natural frequencies and damping factors versus different input levels.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","5.8.1.1a","Requirement","ECSS-E-ST-32-11_0250099","The experimental test modal data shall be compared with the analytical modal data, for the following purposes:\n    1. To validate the mathematical model.\n    2. To validate the test data.\n    3. To select reliable test data for the mathematical model update.\n    4. For taking corrective measures in a running test campaign.\n    5. To detect erroneous areas in the mathematical model (error localization).\n        NOTE The correlation methods are given in Table 5-2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32-11C","6.3.5c","Requirement","ECSS-E-ST-32-11_0250124","The pure dynamic characteristics of the test article shall be extracted from the reference FEM after the influence of the test fixtures is removed.\n    NOTE In general, the reference FEM includes the test article and the test fixtures.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-32C Rev. 1","4.2.6b","Requirement","ECSS-E-ST-32_0050017","Load application sequence shall be defined.\n    NOTE For example to account for any non-linear effect depending on load application sequence.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.3.10a","Requirement","ECSS-E-ST-32_0050039","Structural requirements derived from electrical conductivity requirements shall be identified.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.4c","Requirement","ECSS-E-ST-32_0050046","External interfaces shall include:\n    1. spacecraft-launcher interface,\n    2. human factors and ergonomics\n    3. interfaces with equipment, optics and avionics,\n    4. rendezvous and docking, robotics, \n    5. ground support equipment for pre-flight and post-flight operations, and\n    6. support equipment for in-orbit operations. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.5.8e","Permission","ECSS-E-ST-32_0050753","In the cases specified in d) above, preliminary design allowables may be based on the initially small sample size, and upgraded as the sample size increases by tests of newly arriving batches.\n    NOTE 1 For material testing requirements, see ECSS-E-ST-32-08 and ECSS-E-HB-32-20.\n    NOTE 2 Probabilistic descriptions of the strength distribution of materials are usually based on the normal, log-normal or the Weibull distribution. Regardless of the kind of distribution, distribution curves and fractiles cannot be uniquely identified due to the data scatter. The values are assumed to lie within an interval bounded by upper and lower confidence limits. When design allowables are deduced from a regression line based on a small number of test specimens the confidence in such allowables is low. Larger numbers of test specimens generally do not change the shape of the regression line, but the confidence in the statistical evaluation increases.\n    NOTE 3 The test database can be broadened by the inclusion of compatible data from acceptance and development tests.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.5.18a","Requirement","ECSS-E-ST-32_0050092","A scatter factor of four (4) shall be used in fatigue analysis. \n    NOTE 1 The scatter factor is applied to the number of cycles of a certain load level in order to cover the uncertainties of loads and material properties. Usually for metallic materials a scatter factor of 4 is applied. However, for specific applications (e.g. pressure vessels and low cycle fatigue) higher values are commonly used (e.g. 5 for pressure vessels).\n    NOTE 2 For composite materials in some cases a factor on the stress (e.g. 1.15) is defined instead of a scatter factor on the load cycles”\n    NOTE 3 The number of cycles can be based on the number of possible repetitions of tests (e.g. 1 qualification vibration plus 3 possible repetitions) specified by the project.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.6.2.1c","Requirement","ECSS-E-ST-32_0050095","A mathematical model shall be developed and delivered for launcher coupled dynamic analysis (LCDA).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.6.2.8c","Requirement","ECSS-E-ST-32_0050116","The life of the structure shall be verified for the specified service life multiplied by the specified scatter factor considering the most unfavourable load sequence within each event.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.6.3.2c","Requirement","ECSS-E-ST-32_0050141","Checking of the test conformance with regard to the test procedure shall be performed after the test. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.6.3.12b","Requirement","ECSS-E-ST-32_0050162","Structural and acoustic to structural transmissibilities shall be validated by test.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.6.3.16a","Requirement","ECSS-E-ST-32_0050169","Ageing tests shall be performed to identify variations of the material properties as a function of time and environment. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.7.2b","Requirement","ECSS-E-ST-32_0050190","For new and unproven manufacturing technology a development and qualification program shall be performed.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.8.4.1a","Requirement","ECSS-E-ST-32_0050211","All maintenance actions shall be documented, including: \n    1. the specification of inspection methods,\n    2. recording of results, \n    3. category of damage, \n    4. repair methods, and\n    5. compilation of service history documents.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.9.7h","Requirement","ECSS-E-ST-32_0050236","Detailed numbering (nodes and elements) and modelling requirements shall be specified in a finite element model requirements document.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","4.10b","Requirement","ECSS-E-ST-32_0050239","The supplier shall provide Design loads in conformance with Annex B.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","A.2.1<4.1>c","Requirement","ECSS-E-ST-32_0050260","Reference shall be made to the available drawings. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","A.2.1<5.4>a","Requirement","ECSS-E-ST-32_0050285","The CADMDD shall indicate the properties and materials related to the item. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","B.2.1<4.1>a","Requirement","ECSS-E-ST-32_0050306","The DL document shall indicate the consistent unit system and the related unit symbols used by the designer. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","B.2.1<5.1>c","Requirement","ECSS-E-ST-32_0050313","Reference shall be made to the corresponding source documents, according to <2>.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","C.2.1<4.3>b","Requirement","ECSS-E-ST-32_0050334","If no changes have been made w.r.t. previous DSA report issues, it shall be explicitly stated.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","D.2.1<4.1>a","Requirement","ECSS-E-ST-32_0050355","The FA shall describe the structure and introduce to the terminology for major structure components. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","E.2.1<7>a","Requirement","ECSS-E-ST-32_0050380","The types of non-destructive inspection performed on the structural items and the related initial crack sizes adopted shall be reported or referenced.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","E.2.1<8.2>b","Requirement","ECSS-E-ST-32_0050383","It shall be clearly reported the assumptions made in terms of crack model, initial crack size, location and orientation, material data, unitary stresses or loads, scatter factor and the results obtained like final crack size, analytical lifetime and critical crack size. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","F.2.1<11>a","Requirement","ECSS-E-ST-32_0050408","The FCP shall include the type of non-destructive inspection (NDI) to be performed on the PFCI's and the corresponding initial flaw size to be used in the analysis.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","H.2.1<4.2>b","Requirement","ECSS-E-ST-32_0050429","Reference shall be made to the available set of drawings, including their revision status, to explain the actual status of the design and to clearly define the structure to be analyzed.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","I.2.1<6.1>a","Requirement","ECSS-E-ST-32_0050450","The MMDD shall summarize and include a justification of the modelling assumptions and methodology. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","I.2.1<6.6>a","Requirement","ECSS-E-ST-32_0050457","The MMDD shall indicate the pre and post-processor used for modelling, by underlying software limitations and recommendations to properly handle the model.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","I.2.1<8.2>b","Requirement","ECSS-E-ST-32_0050478","The position of the masses shall be indicated also by plotting the model and labelling the masses.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","I.2.1<13.5>a","Requirement","ECSS-E-ST-32_0050499","The MMDD shall report the results of dedicated checks performed to assess adequacy to perform thermal stress analysis. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","J.2.1<5.4>b","Requirement","ECSS-E-ST-32_0050524","An explanation of the use of test results in analysis shall be included (e.g. mathematical models previously validated by modal survey tests).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","J.2.1<6>c","Requirement","ECSS-E-ST-32_0050527","Criteria used to select the significant modes shall be reported and the justification included.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","K.2.1<7.2>b","Requirement","ECSS-E-ST-32_0050552","Reasons for the choice and limitations of the models shall be summarized here.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","K.2.1<9.4>a","Requirement","ECSS-E-ST-32_0050574","The SSA shall define the format to transfer stress data to fracture and fracture mechanics. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","K.2.1<10.3>o","Requirement","ECSS-E-ST-32_0050595","The SSA shall cross-refer any previous issue and summarize the changes.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","L.2.1<4.1>a","Requirement","ECSS-E-ST-32_0050602","The SAB shall describe the structural item and introduce to the terminology for its major components. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","M.2.1<4.1>a","Requirement","ECSS-E-ST-32_0050623","The SB shall indicate the consistent unit system of measures used. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","N.2.1<2>a","Requirement","ECSS-E-ST-32_0050644","The SMS shall list the applicable and reference documents in support to the generation of the document.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","O.2.1<4.3>a","Requirement","ECSS-E-ST-32_0050669","The TAC shall describe all the coordinate systems used.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","O.2.1<6>a","Requirement","ECSS-E-ST-32_0050672","The TAC shall summarize the main aspects of the test performed and reference test documentation shall be indicated. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","P.2.1<5>b","Requirement","ECSS-E-ST-32_0050697","The objectives of the analytical predictions shall be clearly reported.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","P.2.1<6.9>c","Requirement","ECSS-E-ST-32_0050718","The TE shall discuss how the data have been checked during the test to ensure the test validity.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","Q.2.1<4.9>a","Requirement","ECSS-E-ST-32_0050739","A cross-reference between analysis locations and monitoring locations shall be included with reference to the test specification and the measurement plan. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-32C Rev. 1","Q.2.1<5.3>b","Requirement","ECSS-E-ST-32_0050746","The use of test results in analysis shall be explained (e.g. substructure mathematical models previously validated by modal survey tests).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.2.2.1a","Requirement","ECSS-E-ST-34_0830017","The nominal value and the limit values for the total atmospheric pressure in the pressurized volume shall be specified.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.2.3.5c","Requirement","ECSS-E-ST-34_0830042","Exchange of atmosphere between pressurized volumes: atmosphere exchange between connected pressurized volumes shall be specified.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.2.9.4a","Requirement","ECSS-E-ST-34_0830063","The capability to monitor microbial contamination of surfaces shall be provided in the accessible volume.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.2.10.2b","Requirement","ECSS-E-ST-34_0830066","The capability to provide shielding to maintain the ionizing radiation below the specified limits shall be provided.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.4.1.4a","Requirement","ECSS-E-ST-34_0830091","Resupply of inert diluent gas shall be accepted in conformance with the interface specifications.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.4.4.1a","Requirement","ECSS-E-ST-34_0830112","Potable water needs, including water for drinking, oral hygiene, and food preparation (e.g. rehydration), shall be specified. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.4.5.3.1","Requirement","ECSS-E-ST-34_0830219","When food production is specified, it shall be produced in conformance with crew needs, following food requirements specified in 4.4.4.5.1.\n",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.4.5.5.3","Requirement","ECSS-E-ST-34_0830226","Food trash shall be avoided in term of mass and volume.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.5.3.2b","Requirement","ECSS-E-ST-34_0830150","Temporary storage of unprocessed gas, solid and concentrated liquid wastes shall be provided with the capacity to meet the peak and contingency needs specified in 4.4.5.3.2a.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.4.7.2.2a","Requirement","ECSS-E-ST-34_0830175","Requirements for providing medical equipment for diagnostic and treatment purposes shall be specified.\n    ","NOTE This can include means to treat cases of decompression illness.",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.6.3.5.5a","Requirement","ECSS-E-ST-34_0830196","The requirements on ECLSS specific forbidden zones shall be specified at project Phase C (ECLSS design phase). \n    ","NOTE Forbidden zones include outside FOV, and operational range of mechanisms.",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-34C","4.6.3.7a","Requirement","ECSS-E-ST-34_0830199","The requirements for payload in the pressurized volume shall be specified.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35-01C","4.3.2a","Requirement","ECSS-E-ST-35-01_0840006","Support structures of pressure vessels and pressurized components shall allow deformations of the vessels due to pressure or temperature changes and cycles to occur without causing stresses that exceed acceptable limits.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.5.1.8a","Requirement","ECSS-E-ST-35-01_0840027","The system and its components shall be designed for the expected number of cycles during the whole mission life, for both on-ground and in-service operation.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.5.7c","Requirement","ECSS-E-ST-35-01_0840052","Item 4.5.7b shall be supported by analysis, simulation, or testing or all of them.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.5.8a","Requirement","ECSS-E-ST-35-01_0840055","A design assessment for failure tolerance shall be performed for every component.\n    NOTE 1 See ECSS-Q-ST-30-02.\n    NOTE 2 Table 4-1 covers the component failure modes generally encountered in the use of standard components. Failure to operate are not mentioned while external leakage is only reported for tanks and tubing.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.5.14.1a","Requirement","ECSS-E-ST-35-01_0840076","The support structure shall allow the installation of a device to adjust thruster alignment. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.6.1a","Requirement","ECSS-E-ST-35-01_0840105","A verification matrix shall be established indicating the type of verification method to apply for the individual requirements.\n    NOTE 1 For verification of liquid propulsion systems, see ECSS-E-ST-10-02.\n    NOTE 2 2 Verification is performed to demonstrate that the system or subsystem fully conforms to the requirements. This can be achieved by adequately documented analysis, tests, review of the design, inspection, or by a combination of them.\n    NOTE 3 In the following clauses of this clause 4.6, it is considered that:\n        · verification by review of the design is included in verification by analysis, and\n        · verification by inspection is included in verification by test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.6.2.3.2b","Requirement","ECSS-E-ST-35-01_0840123","The risk of propellant adiabatic decomposition shall be analysed.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.6.2.3.5a","Requirement","ECSS-E-ST-35-01_0840126","Oscillations induced by the motion of the propellant in the tanks on the spacecraft structure and stability shall be analysed. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.6.3.7b","Requirement","ECSS-E-ST-35-01_0840151","Cases addressed in 4.6.3.7a shall include at least:\n    1. Water-hammer effects\n    2. Transients during system pressurisation\n    3. Design of flow orifices\n    4. Thruster cross-coupling effects\n    5. Hydrazine detonation due to adiabatic compression when applicable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","4.7.2a","Requirement","ECSS-E-ST-35-01_0840172","Procedures shall be established and maintained to ensure that the production of components, subsystems and systems conforms to all the requirements.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.2.2f","Requirement","ECSS-E-ST-35-01_0840197","The propulsion system shall provide the means for propellant gauging during the mission.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.2.3c","Requirement","ECSS-E-ST-35-01_0840200","Thruster response times shall be defined with respect to:\n    1. Start-up (time to achieve nominal thrust)\n    2. Changes in thrust level during normal operation\n    3. Shut-down (time to transit from nominal to zero thrust).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.1.3a","Requirement","ECSS-E-ST-35-01_0840221","A water-hammer effects analysis shall be performed to support the propulsion system design and ensure proper functioning.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.3.2c","Requirement","ECSS-E-ST-35-01_0840246","Pressurant, propellant and contaminants budgets shall include:\n    1. Their impact on lifetime\n    2. Variation of performance during lifetime\n    3. Quantity for deorbiting\n    4. Residuals.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.9a","Requirement","ECSS-E-ST-35-01_0840267","For pressure vessels design, clause 4.5.10 shall be applied.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.10c","Requirement","ECSS-E-ST-35-01_0840270","For propellant tanks design of EP systems using liquid propellants, clause 4.5.11 shall be applied.\n    NOTE 1 A large variety of propellants are used for electric propulsion thrusters (i.e. gaseous, liquid and solid); therefore different tank design rules are applicable.\n    NOTE 2 Some gaseous propellants, such as xenon, are usually stored in supercritical condition.\n    NOTE 3 The fluid characteristics of supercritical Xenon (e.g. density) can be substantially different from those of a simulant pressurant gas during environmental testing (e.g. vibration testing). Thus, analysing this point during system design can prevent coupling modes between the spacecraft structure, xenon tank and the xenon itself as a free-moving high density fluid. With this objective, selection of the xenon tank and tank shape is done in conformance to the spacecraft eigenfrequencies.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.14.1a","Requirement","ECSS-E-ST-35-01_0840295","For power supply, control and processing equipment, ECSS-E-ST-20 shall be applied.\n    NOTE 1 The purpose of the power supply, control and processing devices in an EP system is to provide the thruster and other electrically-powered components with the adequate electrical input parameters during transient and at steady-state operations. \n    NOTE 2 Depending on the type of EP system, the power supply, control and processing functions can be performed by dedicated equipment or carried out as part of the tasks of the spacecraft power system.\n    NOTE 3 Most commonly, the power conditioning devices of an EP system include also functions to control and process incoming and outgoing data and commands.\n    NOTE 4 For redundancy, operational purposes and mass optimization, thruster switching devices can be introduced in the EP system to provide cross-strapping of electrical power between the power supplies and several thrusters.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.5.18.3d","Requirement","ECSS-E-ST-35-01_0840316","The GSE shall be designed to prevent inadvertent electrical discharge.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.6.3.6a","Requirement","ECSS-E-ST-35-01_0840341","Performance tests, including direct thrust measurement, shall verify that the performances of the system, including the thruster, flow control unit and the power supply and conditioning, conform to the requirements.\n    NOTE Performance tests can be included in the life tests.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-01C","5.6.4a","Requirement","ECSS-E-ST-35-01_0840344","Tests results, as well as all models, shall be established and structured with a commonly agreed structure and format.\n    NOTE Example of these models are: thermal, mechanical, electric, magnetic, performance models.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.3.3a","Requirement","ECSS-E-ST-35-02_1100016","For solid thrusters that provide thrust impulsion, the thrust centroid time shall be characterized. \n    ","NOTE Examples of solid thrusters: separation or braking rockets, control systems.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.5.2.2b","Permission","ECSS-E-ST-35-02_1100161","Dedicated MEOP and MDP may be calculated for each component to take into account the axial gradient of pressure in the bore.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.5.5.2.1a","Requirement","ECSS-E-ST-35-02_1100061","The temperature of the interface between the thermal protection and the propellant shall be defined and justified such that the propellant combustion rate increase remains consistent with SRM safety and reliability requirements.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.5.5.3.1a","Requirement","ECSS-E-ST-35-02_1100068","For the ballistic dimensioning of the propellant grain, the pressure and mass flow rate histories shall be determined, in conformance with the system and subsystem requirements, according to the throat design (i.e. dimensions and erosion).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.7b","Requirement","ECSS-E-ST-35-02_1100088","For solid motors for spacecraft, the outgassing materials shall be characterized after burn-out.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","4.10.2.3b","Requirement","ECSS-E-ST-35-02_1100107","The design of the measurement system and the SRM shall be compliant with the needs identified in 4.10.2.3a.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","A.2.1<7>d","Requirement","ECSS-E-ST-35-02_1100131","In case previous environment analyses are available, the AR-DY shall include:\n    1. comparison of the result of the characteristics of the environment induced by the propulsion system with the previous ones, and \n    2. report including a discussion on the differences.\n        ","NOTE Requirements are not limited to system or subsystem requirements; they can also be “internal” or “derived” requirements.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","B.2.1<1>a","Requirement","ECSS-E-ST-35-02_1100134","The AR-MSDS shall contain the technical or commercial identification of the propulsion system.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-02C","B.2.1<11>a","Requirement","ECSS-E-ST-35-02_1100155","The AR-MSDS shall provide the toxic combustion products generated by the propulsion system in case of fire.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","7.2m","Requirement","ECSS-E-ST-35-03_1110019","The critical technologies, manufacturing and control processes shall be listed and their qualification process described.\n    ","NOTE See ECSS-Q-ST-20.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.4.2b","Requirement","ECSS-E-ST-35-03_1110040","Propulsive system components shall provide inputs to the functional and mechanical models at various steps of the development.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.4.3.2b","Requirement","ECSS-E-ST-35-03_1110047","If in-flight draining cannot be performed through the flow paths for the normal operation of the propulsion system, specific lines or valves shall be incorporated in the liquid propulsion system to enable in-flight draining.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.4.4.2.3a","Requirement","ECSS-E-ST-35-03_1110068","The minimum tank operating pressure shall conform to with the tank structural requirement.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.4.5.3.1c","Requirement","ECSS-E-ST-35-03_1110089","Water-hammer phenomena shall have no detrimental effect on the structural and the functional behaviour of the propulsion system.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.3.1c","Requirement","ECSS-E-ST-35-03_1110103","Contributions to engine thrust shall be analysed and reported in the design justification file as defined in ECSS-E-ST-10 Annex K DRD.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.3.3.5b","Requirement","ECSS-E-ST-35-03_1110118","The extreme envelope shall be reported from the PDR.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.4.2a","Requirement","ECSS-E-ST-35-03_1110139","TCA subsystem fire tests shall be included in the development plan.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.4.7b","Requirement","ECSS-E-ST-35-03_1110164","The stability margin of an engine design shall be determined before the thrust chamber CDR.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.4.8.2f","Requirement","ECSS-E-ST-35-03_1110185","The development logic shall include the demonstration of the reliability requirement for ignition system.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.4.8.3c","Requirement","ECSS-E-ST-35-03_1110192","The frequency range of the dynamic pressure fluctuations measurement shall cover the two first tangential acoustic modes, the two first radial acoustic modes and the two first longitudinal acoustic modes of the combustion chamber.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.6.2g","Requirement","ECSS-E-ST-35-03_1110213","Vibration limits shall be established.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.7.2b","Requirement","ECSS-E-ST-35-03_1110234","The analysis specified in 9.5.7.2a. shall be performed for every physical loop.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.9.2.2a","Requirement","ECSS-E-ST-35-03_1110259","The valve functional characteristics shall be established over the entire extreme envelope.\n    ","NOTE Example of functional characteristics: pressure drop, response times.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.5.9.3.2a","Requirement","ECSS-E-ST-35-03_1110262","The pressure regulator functional characteristics shall be established over the entire extreme envelope.\n    ","NOTE For example downstream pressure versus mass flow rate curve.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","9.6n","Requirement","ECSS-E-ST-35-03_1110287","For margin policy ECSS-E-ST-10 shall apply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-03C","12a","Requirement","ECSS-E-ST-35-03_1110308","For verification ECSS-E-ST-35 clause 4.8 shall apply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","4.2.1b","Requirement","ECSS-E-ST-35-10_1050008","The need for compatibility testing shall be assessed and included in Annex A.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","4.2.4b","Recommendation","ECSS-E-ST-35-10_1050185","Compatibility testing should take place following the logic of Figure 4-1\n    NOTE 1 This guarantees that they are performed with increasing complexity, generation of details, and for the specific applications.\n    NOTE 2 The requirements list needs to be tailored. It depends on the specific application which tests are going to be performed and which by-passed: e.g. if no hydrogen is involved, no hydrogen embrittlement tests are performed.\n    NOTE 3 An example of tailoring the requirements list is given in Annex C and Annex E",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.1.3a","Requirement","ECSS-E-ST-35-10_1050036","The national regulations with regard to pollution and protection of the environment shall be observed when tests are executed.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.2.3.3c","Requirement","ECSS-E-ST-35-10_1050057","The containers shall be prepared according to the compatibility test procedure for the actual tests.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.6.2a","Requirement","ECSS-E-ST-35-10_1050082","Tensile strength and elongation at rupture before and after exposure to the liquid of interest, shall be determined according to either:\n    - ISO 1817 Clauses 3 through 6 and 7.7, or\n    - ASTM- D-638-03 Clauses 5 through 11.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.6.2d","Requirement","ECSS-E-ST-35-10_1050085","Tear strength before and after exposure to the liquid of interest shall be determined according to ASTM D 624-00 Clauses 6 through 10.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.7.3.1e","Requirement","ECSS-E-ST-35-10_1050110","The test temperature shall at least be the upper temperature of the qualification temperature range.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","6.9.1b","Requirement","ECSS-E-ST-35-10_1050131","Exposure to the test environment of samples shall be representative of the specific application in terms of hydrogen concentration, pressure and temperature. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","A.2.1<4>b","Requirement","ECSS-E-ST-35-10_1050153","Reference shall be made to the applicable design definition file, inclusive of its revision status.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-10C","A.2.1<6>c","Requirement","ECSS-E-ST-35-10_1050160","For each build level, lower build level analyses shall be included for reference.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35C Rev. 1","4.2a","Requirement","ECSS-E-ST-35_0850001","The propulsion system shall conform to the mission requirements described in the propulsion system technical specification, including:\n    1. Ground operations (i.e. functional control, testing, propellant, simulant loading and transportation).\n    2. Pre-launch and launch activities (i.e. integration, storage, ageing and transport).\n    3. In-orbit operations (i.e. orbit transfer, orbit maintenance and attitude control) and the complete in-orbit life.\n    4. Disposal operations.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.2.3a","Requirement","ECSS-E-ST-35_0850026","The calculation of Isp,th, of the propulsion system shall include the kinetics, the mixture ratio, the chamber pressure and area ratio.\n    NOTE Not applicable for EP.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.4.3a","Requirement","ECSS-E-ST-35_0850047","During development and qualification phases, the transient performances of the propulsion system shall be tested in the representative conditions with respect to interface conditions and operation in flight.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.5b","Requirement","ECSS-E-ST-35_0850050","The margin policy shall be reported in the design justification file.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.9.3f","Requirement","ECSS-E-ST-35_0850075","Components identified in e. shall be protected by a filter.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.14.1.1c","Requirement","ECSS-E-ST-35_0850096","Proof of qualification of all instrumentation shall be provided.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.5.15c","Requirement","ECSS-E-ST-35_0850117","For the monitoring and control system a FMECA shall performed and the failure modes identified.\n    NOTE For FMECA, see ECSS-Q-ST-30-02. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.8.2.1c","Recommendation","ECSS-E-ST-35_0850410","The effects of these differences on the operation and reliability of the propulsion system should be analysed.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","4.9.2a","Requirement","ECSS-E-ST-35_0850146","It shall be ensured that tooling and test equipment avoid:\n    1. Wrong connections\n    2. Pollution or contamination.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","A.2.1<6.2>b","Requirement","ECSS-E-ST-35_0850171","If experimental input data is used, the data sheet or test results shall be referenced or reproduced in the AR-P.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","B.2.1<4.2>a","Requirement","ECSS-E-ST-35_0850192","The AR-G shall describe the coordinate systems used in the gauging system or subsystem.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","B.2.1<6.1>a","Requirement","ECSS-E-ST-35_0850195","Since analysis covers both model computations and elaboration of measurements, the AR-G shall cover:\n    1. The description of the used assumptions.\n    2. The description of simplifications.\n    3. A brief summary of rationale and software used for the gauging analysis and the related uncertainties.\n        NOTE Uncertainties can result from numerical inaccuracies, measurement inaccuracies, models that are based on simplifications and the conditions under which data have been obtained.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","C.2.1<4.2>a","Requirement","ECSS-E-ST-35_0850220","The thermal analysis shall include a description and a discussion of the following thermal aspects that are typical for propulsion subsystems and systems:\n    1. Thermal conditioning before operation;\n        (a) The initial and final conditions of the thermal state of a propulsion system;\n        (b) How the thermal conditioning is realized.\n            NOTE Thermal conditioning includes pre-heating of cathodes, neutralizers, feed systems, catalyst beds, propellants (e.g. xenon and cesium) and chill-down of cryogenic systems.\n    2. Thermal shock;\n        (a) How the thermal shock effects have been assessed.\n        (b) The demonstration that the propulsion component, subsystem or system can withstand the thermal shocks that are being encountered.\n            NOTE Thermal shocks occur during chill-down (from ambient temperatures to cryogenic temperatures, < 20 K) and start-up of propulsion systems (from ambient or cryogenic temperatures to temperatures often exceeding 3 000 K).\n    3. Propellant evaporation\n        (a) The means by which it is ensured that the amount of propellant evaporation meets the specifications.\n        (b) The passive or active measures that have been or to be implemented to satisfy the requirements.\n            NOTE Propellant evaporation is especially important for cryogenic propellants (boil-off) and for FEEP (evaporation and subsequent condensation of liquid metal).\n    4. Propellant stratification\n        (a) The measures by which it is ensured that the propellant stratification conforms to the requirements.\n            NOTE Propellant stratification especially occurs with cryogenic propellants where the temperature of the upper levels can be substantially higher than the temperature of the lower levels.\n    5. Thermal stresses in solid propellants\n        (a) The analyses of the temperature, temperature gradients, and changes in temperature and temperature gradients after curing of a solid propellant grain.\n        (b) The thermal analyses of propellant grains that have been in orbit a long time before being ignited.\n            NOTE For example, several months up to several years.\n        (c) How the resulting thermal stresses have been calculated;\n        (d) The evidence that the thermal history of the propellant grain does not introduce stresses that transgress the specified stresses\n            NOTE 1 For example shrinkage.\n            NOTE 2 Curing of propellant grains usually takes place at temperatures well above the operational temperature of the propellant.\n            NOTE 3 De-orbiting motors can be in orbit for several years. During this period the solid motors can undergo many temperature changes (thermal cycles).\n    6. Thermal induced aging and damage in solid propellants\n        (a) The evidence that the thermal induced aging of solid propellants conforms to the system and subsystem specifications.\n        (b) The evidence that for solid rocket motors that undergo many temperatures changes (thermal cycling), the coupled thermal-mechanical computations demonstrate that damage to the propellant grain conforms to the system and subsystem specifications.\n            NOTE 1 For example, for thermally non-controlled de-orbiting motors that are a long time in space before being operated.\n            NOTE 2 Aging of solid propellants is accelerated at high temperatures and by temperature cycling. This can especially be important for solid motors that are a long time in before being operated (e.g. de-orbiting motors).\n    7. Radiation cooling\n        (a) The temperature management of propulsion components, subsystems or systems that are cooled by radiation;\n            NOTE Typical examples are mono- and bi-propellant thrusters and electric propulsion systems.\n        (b) The evidence that the propulsion component, subsystem or system temperature conforms to the component, subsystem or system requirements.\n        (c) The evidence that the radiation cooled propulsion components, subsystems or systems conform to the requirements when installed in a spacecraft or launcher where its view factors can have changed substantially, either due to its installation or by the installation of radiation shields.\n    8. Regenerative cooling\n        (a) The evidence that the regenerative cooling keeps the material temperatures within the boundaries specified by the requirements.\n        (b) The evidence that the regenerative cooling keeps the temperature of the regenerative cooling fluid within the boundaries specified by the requirements.\n            NOTE Some rocket engine cycles (e.g. expander cycle, bleed cycle) strongly rely on a proper energy transfer to the cooling fluid.\n        (c) The evidence that thermal expansion and contraction conform to the structural requirements.\n    9. Heat soak-back\n        (a) The evidence that after shutdown of a propulsion subsystem or system the temperature of cold structures of the propulsion subsystem or system and the temperature of structural elements close to the propulsion subsystem or system conform to the subsystem or system requirements.\n            NOTE After shutdown of a rocket engine, there is no active cooling any more, and also cooling of parts and components that are normally cooled by the propellant flow is interrupted. Therefore parts that during the operation of the propulsion system remains cool, heat up mainly due to conduction and radiation.\n    10. Thermal conditions at the start\n        (a) The thermal analyses that have been made to establish the thermal conditions before the starting of a rocket motor.\n        (b) Measurements to be according to the thermal analysis in order to establish the thermal state of the engine.\n            NOTE 1 If regenerative or film-cooled rocket motors are (re)started while hot, it can be impossible to establish a proper regenerative coolant flow (flow blockage) or to establish an appropriate coolant film. In that case, measures are taken to ensure that the proper coolant flow is established or measures are that prevent the motor from being restarted.\n            NOTE 2 In particular for cryogenic upper stage engines, starting the engine at too low temperatures can lead to combustion instability or insufficient power delivery from the regenerative cooling circuit for expander cycle engines.\n    11. Heating of the nozzle and the nozzle throat\n        (a) The thermal analyses for the nozzle and its components e.g. throat-inserts, flexible seal, thermal / ablative materials, temperature gradients and related stresses in regeneratively cooled nozzles.\n        (b) The selection of high temperature materials that are compatible with the environment (composition of the exhaust gases).\n        (c) The associated thermal expansion / contraction, the induced thermal stresses and the effect on clearances.\n        (d) The evidence that the nozzle and nozzle throat meet the subsystem and system thermal requirements.\n            NOTE The highest heat transfer in rocket motors is encountered in the throat region. During start-up the nozzle encounters thermal shocks and strong transient thermal effects.Nozzles of cryogenic systems undergo a thermal shock and cooling down to cryogenic temperatures.Typical stagnation temperatures of the combustion products exceed 3 000 K.\n    12. Change in thermal characteristics (emissivity) due to deposition of sputtering material\n        (a) The effects of the change in irradiative properties of electric propulsion systems due to deposition of sputtering material during long term testing in vacuum chambers.\n        (b) The measures to be taken to ensure that notwithstanding a changing thermal behaviour of the electric propulsion system during long term testing, the tests remain representative for the performance of an electric propulsion system in flight.\n            NOTE During long term testing of an electric propulsion system in a vacuum chamber, coating material from the walls of the vacuum chamber can be deposited on the electric propulsion system. This can cause a change in the thermal characteristics of the electric propulsion system during long term testing.\n    13. Bake-out / thermal cleaning\n        (a) The thermal analysis and temperature evolution of electric propulsion thrusters for bake-out or thermally cleaning these thrusters.\n            NOTE The cleansing of contaminants (e.g. FEEP) of electric propulsion thrusters, to ensure a proper operation, is done by heating the thrusters to high temperatures. These temperatures usually exceed the operational temperature of the electric propulsion thrusters and can be design drivers.Other electric propulsion thrusters can be heated to melt or evaporate particulate material from the grids.\n    14. Thermal analysis for propellant feed systems\n        (a) The thermal analysis and temperature control to maintain the propellant feed system within its specified temperature range.\n            NOTE 1 The propellants are delivered to the thrusters / motors / engines within a specified temperature range.\n            NOTE 2 For some propellants there is the danger of freezing (N) or liquefaction (xenon).\n            NOTE 3 For some propellants there can be a danger of flow blockage or of explosion due to adiabatic compression of propellant vapours during priming.\n    15. Thermal stresses in radiation cooled nozzles\n        (a) The structure of a radiation cooled nozzle or nozzle section can withstand the combination of stresses due to internal pressure, external loads and thermal stresses \n            NOTE 1 Radiation cooled nozzles are often found on satellite engines and attitude control thrusters.\n            NOTE 2 Some large rocket engines have a nozzle extension that is radiation cooled.\n    16. De-stratification\n        (a) The evidence that the amount of usable cryogenic propellant conforms to the requirements when sloshing or rolling of the stage is taken into account.\n            NOTE If cryogenic propellant with high temperatures (that is normally at the top of the tank) due to sloshing enters the propellant feed lines, the entrance conditions for the propellant pump can not longer be satisfied.\n    17. Thermo-mechanical cycling \n        (a) The evidence that engine life requirements are met for the number of thermal cycles the engine undergoes;\n        (b) The demonstration that crack propagation conforms to the engine requirements.\n            NOTE 1 Thermo mechanical cycling is especially important for reusable liquid engines.\n            NOTE 2 Thermo mechanical cycling can be important for engines during development testing.\n            NOTE 3 Crack propagation and crack growth due to thermo-mechanical cycling can especially be important for engines built with a tubular structure for regenerative cooling.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","D.2.1<6.2>c","Requirement","ECSS-E-ST-35_0850241","If experimental input data is used, the test plan, test procedures, individual test item descriptions, and existing deviations from the generic design on which the experimental data is based shall be referenced;",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","E.2.1<4.2>a","Requirement","ECSS-E-ST-35_0850262","The AR-N shall describe the coordinate systems used in the nozzle- discharge system.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","E.2.1<6.2>c","Requirement","ECSS-E-ST-35_0850269","If experimental input data is used, the test plan, test procedures, individual test item descriptions, and existing deviations from the generic design on which the experimental data is based shall be referenced;",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","F.2.1<4.1>c","Requirement","ECSS-E-ST-35_0850290","Reference shall be made to the applicable design definition file, inclusive its revision status. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","G.2.1<4.2>a","Requirement","ECSS-E-ST-35_0850315","The AR-Tr shall describe the coordinate systems used in the propulsion system or subsystem for which a transient analysis is made.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","G.2.1<10>a","Requirement","ECSS-E-ST-35_0850336","In the AR-Tr a summary of the results shall be given containing the following information:\n    1. A summary of the main results.\n    2. Limitations of the performed work. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","H.2.1<3>a","Requirement","ECSS-E-ST-35_0850339","The UM shall use the terms, definitions, abbreviated terms and symbols used in ECSS-E-ST-35.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","H.2.1<5.10>a","Requirement","ECSS-E-ST-35_0850364","For propulsion systems other than solid, the UM shall describe:\n    1. The cases for loading and unloading the propulsion subsystem or system.\n    2. The loading and unloading procedures for every case.\n        NOTE For example, ground tests, satellite loading, loading on the launcher, and related unloading.\n    3. The safety measures to be implemented during loading and unloading.\n    4. The conditions under which loading and unloading can take place.\n    5. The disposal of unloaded fluids.\n    6. The equipment to be used during loading and unloading.\n    7. All measurements during loading and unloading.\n    8. Any limitation for the number of loading and unloading cycles the propulsion subsystem or system can undergo.\n    9. The maximum duration for propellants and working fluids to remain loaded in the propulsion subsystem or system.\n    10. Measures that prevent contamination of the propulsion system during loading and unloading.\n    11. In case of unloading, which components cannot be reused and be replaced.\n        NOTE As solid propellants are usually present in the delivered propulsion subsystem or system they are not considered in this clause.Loading of the propulsion subsystem or system comprises filling the tanks of the propulsion subsystem or system with propellants and working fluids (e.g. water, helium, nitrogen).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","I.2.1<6.2>b","Requirement","ECSS-E-ST-35_0850385","The MM-PA shall state the number of significant digits for all relevant parameters in the mathematical modelling.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-35C Rev. 1","I.2.1<6.3>c","Requirement","ECSS-E-ST-35_0850392","The MM-PA shall list the range and conditions for which the mathematical models are valid.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.2.4.3a","Requirement","ECSS-E-ST-40_0860010","The customer shall specify the external interfaces of the software, including the static and dynamic aspects, for nominal and degraded modes.\n","EXPECTED OUTPUT: External interface requirements specification [RB, IRD; SRR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.3.3.2a","Requirement","ECSS-E-ST-40_0860031","Software project reviews (i.e. joint reviews organized under the responsibility of the customer aiming at defining a customer approved technical baseline) shall be included in the software life cycle, with as a minimum SRR, PDR, CDR, QR and AR as specified in 5.3.4.\n","EXPECTED OUTPUT: Software project reviews included in the software life cycle definition [MGT, SDP; SRR, PDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.4.2.3b","Requirement","ECSS-E-ST-40_0860056","The supplier shall use a method to support the construction of the logical model.\n","EXPECTED OUTPUT: Software logical model method [TS, SRS; PDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.5.2.5b","Requirement","ECSS-E-ST-40_0860077","The supplier shall document and justify all timing and synchronization mechanisms.\n","EXPECTED OUTPUT: Real-time software dynamic design model [DDF, SDD; CDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.5.2.5e","Requirement","ECSS-E-ST-40_0860080","The supplier shall ensure protection against problems that can be induced by the use of dynamic allocation of resources, e.g. memory leaks.\n","EXPECTED OUTPUT: Real-time software dynamic design model [DDF, SDD; CDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.6.4.1c","Requirement","ECSS-E-ST-40_0860105","If it can be justified that validation by test cannot be performed, validation shall be performed by either analysis, inspection or review of design.\n","EXPECTED OUTPUT: Software validation specification with respect to the requirements baseline [DJF, SVS; QR, AR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.8.2.1c","Requirement","ECSS-E-ST-40_0860126","Verification activities and tasks defined in clause 5.8.3, including associated methods, techniques, and tools for performing the tasks, shall be selected for the life cycle activities and software products.\n","EXPECTED OUTPUT: Software verification plan - activities, methods and tools [DJF, SVerP; PDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.8.3.4a","Requirement","ECSS-E-ST-40_0860133","The supplier shall verify the software detailed design ensuring that:\n    1. detailed design is externally consistent with the architecture;\n    2. there is internal consistency between software components and software units;\n    3. the traceability between the architecture and the detailed design is complete;\n    4. the software units that are not traced to the components are justified;\n    5. testing is feasible, by assessing that:\n        (a) commandability and observability features are identified and included in the detailed design in order to prepare the effective testing of the performance requirements;\n        (b) computational invariant properties and temporal properties are added within the design;\n        (c) fault injection is possible.\n    6. operation and maintenance are feasible;\n    7. the design is correct with respect to requirements and interfaces, including safety, security, and other critical requirements;\n    8. the design implements proper sequence of events, inputs, outputs, interfaces, logic flow, allocation of timing and sizing budgets, and error handling;\n    9. the design model has been checked;\n    10. 1the hierarchical breakdown from high level components to terminal ones is provided;\n    11. 1the dynamic features (tasks definition and priorities, synchronization mechanisms, shared resources management) are provided and the real-time choices are justified;\n    12. 1the synchronisation between external interface and internal timing is achieved;\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Detailed design traceability matrices [DJF, SVR or SDD; CDR];\n          b.Detailed design verification report [DJF, SVR; CDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.8.3.13c","Requirement","ECSS-E-ST-40_0860156","As support to the verification of the software detailed design, the supplier shall verify the software behaviour using the software behavioural design model produced in 5.5.2.3a. eo c., by means of the techniques defined in 5.5.2.6.\n","EXPECTED OUTPUT: Software behaviour verification [DJF, SVR;CDR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.10.2.2a","Requirement","ECSS-E-ST-40_0860177","If the spacecraft lifetime goes after the expected obsolescence date of the software engineering environment, then the maintainer shall propose solutions to be able to produce and upload modifications to the spacecraft up to its end of life.\n","EXPECTED OUTPUT: Maintenance plan - long term maintenance solutions [MF, - ; QR, AR, ORR].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","5.10.7.2a","Requirement","ECSS-E-ST-40_0860202","The maintainer shall notify the retirement plan and related activities, including the following items:\n    1. description of the replacement or upgrade with its date of availability;\n    2. statement of why the software product is no longer to be supported;\n    3. description of other support options available, once support is removed.\n","EXPECTED OUTPUT: Retirement notification [MF, - ; - ].",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","B.2.1<5.2>b","Requirement","ECSS-E-ST-40_0860223","Description of capability requirements shall be organized by capability type.\n    NOTE For example, requirements can be organized per controlled subsystem (e.g. AOCS, power, and thermal).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","B.2.1<5.5.1>a","Requirement","ECSS-E-ST-40_0860230","The SSS shall list the requirements on the computer hardware to be used.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","B.2.1<6.4>a","Requirement","ECSS-E-ST-40_0860247","The SSS shall include requirements for \n    1. the installation and acceptance of the software (5.2.3.3,)\n    2. the needed versions, their content and their medium (5.2.4.1,)\n    3. the needed supplier support for system integration (5.2.4.2)\n    4. the format and delivery medium of all exchanged data in the project, including the interface and the system database (5.2.4.9)",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","D.2.1<4.3>c","Permission","ECSS-E-ST-40_0860675","A block diagram may be presented showing the major components of the larger system or project, interconnections, and external interfaces.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","D.2.1<5.2>a","Requirement","ECSS-E-ST-40_0860280","The SRS shall describe the capabilities to be provided by the software item under definition.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","D.2.1<5.13>a","Requirement","ECSS-E-ST-40_0860301","The SRS shall list any safety requirement applicable to the software item.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","E.2.1<5.1>c","Requirement","ECSS-E-ST-40_0860321","The traceability information of each requirement derived from higher level documentation, to the applicable higher level requirement, shall be stated.\n    NOTE The documented trace can be provided automatically by tools when models are used to express requirements.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","F.2.1<5.1>b","Requirement","ECSS-E-ST-40_0860347","The architecture structure of the software item shall be described, identifying the software components, their hierarchical relationships, any dependency and interfaces between them. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","F.2.1<5.4.5>a","Requirement","ECSS-E-ST-40_0860368","The function of a component shall be described in the software architectural design. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","F.2.1<5.4.8>d","Permission","ECSS-E-ST-40_0860703","If the information in <5.4.8>c. is implicit in the definition of the type of component, a description need not be done. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","G.2.1<5.1>a","Requirement","ECSS-E-ST-40_0860396","The SRelD shall \n    1. summarize the main information on the software configuration item, and \n    2. describe the changes implemented since previous version.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","H.2.1<9.7>a","Requirement","ECSS-E-ST-40_0860417","The SUM shall describe the common error conditions that can occur as a result of executing the function, and how to detect that the error has occurred.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","H.2.1<11.1>a","Requirement","ECSS-E-ST-40_0860424","The SUM shall describe how to use the software and what the software does, combining tutorials and reference information for both novices and experts.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","I.2.1<6.3.2>a","Requirement","ECSS-E-ST-40_0860445","The SVerP shall list the required inputs to accomplish the verification activities. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","J.2.1<4.8>a","Requirement","ECSS-E-ST-40_0860466","The SValP shall state (or refer to the SDP) all the identified risks to the software validation campaign.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","K.2.1<5.4>b","Recommendation","ECSS-E-ST-40_0860713","The responsibilities specified in <5.4>a. should be described by identifying the groups responsible for managing, designing, preparing, executing the tests. \n    NOTE Groups can include developers, technical support staff, and product assurance staff. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","K.2.1<8.2.3>d","Requirement","ECSS-E-ST-40_0860512","Configuration of the facility (both hardware and software) to be used to execute the identified test shall be described.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","K.2.1<9.2.2>b","Requirement","ECSS-E-ST-40_0860519","Reference to appropriate documentation shall be performed and traceability information shall be provided.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","L.2.1<5.3>a","Requirement","ECSS-E-ST-40_0860540","The SVS w.r.t. TS or RB shall describe all the features and significant combinations not to be tested.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","L.2.1<7.2.4>a","Requirement","ECSS-E-ST-40_0860561","The SVS w.r.t. TS or RB shall describe, for each test case, the criteria to decide whether the test has passed or failed.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","L.2.1<8.2.1>a","Requirement","ECSS-E-ST-40_0860568","The SVS w.r.t. TS or RB shall identify each test procedure uniquely. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","M.2.1<5.2>a","Requirement","ECSS-E-ST-40_0860589","The status of margins regarding the technical budgets shall be presented in the SVR at each milestone, describing the utilized analytical hypothesis.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","O.2.1<4.3>a","Requirement","ECSS-E-ST-40_0860614","The SDP shall state: \n    1. the assumptions on which the plan is based; \n    2. the external events the project is dependent upon;\n    3. constraints on the project;\n    4. technical issues.\n        NOTE Technical issues are only mentioned if they have an effect on the plan. Assumptions, dependencies and constraints are often difficult to distinguish. The best approach is not to categorize them but to list them. For example:\n            · limitations on the budget;\n            · schedule constraints (e.g. launch dates, delivery dates); \n            · constraints on the location of staff (e.g. the obligation to work at developer’s premises);\n            · commercial hardware or software used by the system;\n            · availability of simulators and others test devices;\n            · availability of external systems with which the system interfaces.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","O.2.1<5.3>g","Requirement","ECSS-E-ST-40_0860635","Any adaptation of the design method (e.g. deviations, extensions, and avoidance of utilization of some methodology features) shall be described or referenced.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","P.2.1<7>a","Requirement","ECSS-E-ST-40_0860656","The SRevP shall include:\n    1. The review entry criteria:\n        (a) Review data package is ready.\n        (b) Review team, organization and plan are agreed and ready. \n    2. Review success criteria:\n        (a) Review objectives are met\n        (b) Actions agreed to be closed before this review have been closed\n        (c) RIDs agreed to be closed before this review have been closed\n        (d) RIDs from this review are dispositioned and actions assigned\n    3. The review conclusion, based on the review success criteria.\n        NOTE Possible review conclusions are:\n            · Successful: review success criteria have been met. Authorization to proceed with next life cycle phase is granted.\n            · Successful with rework to be done: review success criteria have been partially met. There are pending corrections for documents and/or Software. Corrections are done according to open SPRs and actions agreed on RIDs. Authorization to proceed with next life cycle phase is granted. Dates for closure of open SPRs and implementation of actions from RIDs are agreed in the review.\n            · Not successful: review success criteria have not been met. Documents to be baselined at the review cannot be baselined, and Software released for the review cannot be used for follow on activities in their current status. Authorization to proceed with next life cycle phase is not granted.\n    4. The review report, including review minutes of meeting content, presentations, RID status metric, dispositioned RIDs, discussions, actions, review conclusion and any other material used during the review.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-40C","P.2.1<13>a","Requirement","ECSS-E-ST-40_0860663","The SRevP shall include a RID form in conformance with ECSS-M-ST-10-01.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50-01C","6.3.9a","Requirement","ECSS-E-ST-50-01_0240020","The ambiguity between true and complemented data shall be resolved so that only true data is provided to the Reed-Solomon decoder.\n    ","NOTE Data in NRZ-L form is normally resolved using the 32-bit attached sync marker. NRZ-M data is self-resolving.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-01C","8.6.2b","Requirement","ECSS-E-ST-50-01_0240041","If a stream of transfer frames is recorded for insertion in the forward direction into the data fields of the transfer frames of a real-time telemetry channel, then the recorded stream shall use the embedded ASM.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-01C","9.3.2d","Requirement","ECSS-E-ST-50-01_0240048","The pseudo-random sequence shall not be exclusive-ORed with the ASM.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-02C","4.2.2.3a","Permission","ECSS-E-ST-50-02_0870093","Suppressed carrier modulation schemes as defined in ECSS-E-ST-50-05 clause 6.2 may be selected for the telemetry.\n    NOTE Such schemes are not compatible with simultaneous ranging modulation. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-02C","4.5.3c","Requirement","ECSS-E-ST-50-02_0870044","One mode selection shall be accessible by telecommand: ranging modulation on/off.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-02C","4.6.2.2b","Requirement","ECSS-E-ST-50-02_0870065","For a digital implementation of the station transmit carrier generation, any offset from the nominal uplink carrier frequency shall be considered in the Doppler data processing.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-02C","4.6.4.2.2c","Requirement","ECSS-E-ST-50-02_0870087","The station location (antenna phase centre) shall be determined to an accuracy better of than 0,5 m.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.1c","Requirement","ECSS-E-ST-50-03_0880003","The TM Transfer Frame shall be of constant length throughout a specific mission phase.\n    ","NOTE Because a change of frame length also changes the time interval between the start of successive frames, it can result in a loss of synchronization at the data capture element.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.2.3a","Requirement","ECSS-E-ST-50-03_0880024","The Virtual Channel Identifier shall always be present in a Transfer Frame Primary Header.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.2.7.2d","Requirement","ECSS-E-ST-50-03_0880045","The Transfer Frame Secondary Header Flag shall be static in a specific master channel, throughout a mission phase, when the Transfer Frame Secondary Header is associated with a master channel.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.2.7.4b","Requirement","ECSS-E-ST-50-03_0880052","The Packet Order Flag shall be contained in bit 34 of the Transfer Frame Primary Header.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.3.2.1b","Requirement","ECSS-E-ST-50-03_0880073","The Transfer Frame Secondary Header Identification shall be contained in bits 0-7 of the Transfer Frame Secondary Header.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.4.3.4b","Requirement","ECSS-E-ST-50-03_0880098","The packet processing function shall place packets contiguously into the Transfer Frame Data Field.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-03C","5.5.1d","Requirement","ECSS-E-ST-50-03_0880119","The Operational Control Field shall be present in every TM Transfer Frame transmitted through the associated master channel or virtual channel throughout a mission phase.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.1.1.4a","Requirement","ECSS-E-ST-60-30_1160005","If a navigation function is necessary for the mission, the AOCS shall provide the hardware and software means for autonomous on-board determination of the spacecraft orbital state which includes position, velocity and time.\n    ","NOTE Orbit determination can be needed on board and/or on ground.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.1.1.9a","Requirement","ECSS-E-ST-60-30_1160012","The AOCS shall define a strategy for the implementation of the mode transitions and describe how this strategy is applied for each AOCS mode transition, including the following items:\n    1. transition conditions and the check performed by the on-board software,\n    2. actions on software and hardware performed autonomously on board,\n    3. actions to be performed on ground.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.1.3.2a","Requirement","ECSS-E-ST-60-30_1160033","The AOCS shall contribute to the estimation of remaining propellant quantities, through on-board or on-ground algorithms, when the measurement provided by the propulsion system does not cover the mission need.\n    ","NOTE 1 If implemented, the pressure transducer can fail, or have a low accuracy at the end of life. \nNOTE 2 Pulse counting is a common alternative.\nNOTE 3 Fuel gauging requirements are generally related to the estimation of the remaining lifetime and the estimation of satellite MCI evolution.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.2.4b","Requirement","ECSS-E-ST-60-30_1160058","The AOCS shall identify operational constraints in order to meet its calibration needs.\n    ","NOTE Operational constraints include orbit conditions, specific attitude conditions and durations.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.3.1a","Requirement","ECSS-E-ST-60-30_1160061","The AOCS shall be designed to cover the following flight domain along the whole mission:\n    1. worst case launcher separation rate conditions lower than TBS °/s in a TBS angular range,\n    2. mission profile to reach the mission reference orbit,\n    3. mission reference orbit,\n    4. end-of-life disposals.\n        ","NOTE 1 For example, the mission reference orbit can be defined by Keplerian orbital elements.\nNOTE 2 Point 2, point 3 and point 4 can be described as an orbit range, or an altitude range.\nNOTE 3 The launcher conditions specification can refer to another document managed separately.\nNOTE 4 The Flight domain may vary with mission phases. ",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.3.6e","Requirement","ECSS-E-ST-60-30_1160082","For a given duration of the mode of TBS days, the AOCS control of the safe mode shall not generate an orbit degradation greater than:\n    1. TBS m/s along the track,\n    2. TBS m/s along the cross track direction,\n    3. TBS m/s along the direction perpendicular to the orbit plane.\n        ","NOTE It is usually difficult to design a safe mode minimizing the orbit degradation on a specific direction, because of the great variety of attitude profiles, and the verification can be done only a posteriori through simulations. It is also possible to have a requirement on a maximum degradation on any axis.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","5.4.6a","Requirement","ECSS-E-ST-60-30_1160107","End-to-end AOCS tests shall be performed during final verification on the integrated satellite, according to ECSS-E-ST-10-03.\n    ","NOTE The AOCS functional simulator can be used as a reference to support the end-to-end tests.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-30C","A.2.1h","Requirement","ECSS-E-ST-60-30_1160128","The AOCS design definition file shall provide the following sensors and actuators information:\n    1. Datasheet and main features\n    2. Implementation on the satellite : lay out and Field of View\n    3. Operating constraints",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","5.2.2.1c","Requirement","ECSS-E-ST-50-04_0890008","The Segment Header shall consist of two fields, positioned contiguously, in the following sequence:\n    1. Sequence Flags\t\t2 bits\n    2. MAP Identifier\t\t6 bits\n        ","NOTE Both fields are always present in a Segment Header.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","5.2.2.3d","Requirement","ECSS-E-ST-50-04_0890015","If MAP multiplexing is not used on a particular virtual channel of the transfer sublayer, the MAP Identifier shall have a constant value for all TC Segments on that virtual channel.\n    ","NOTE In this case the virtual channel has a single MAP.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","5.4.5b","Requirement","ECSS-E-ST-50-04_0890036","The order of the packets shall not be changed to improve the blocking of the packets into the data units.\n    ","NOTE The order of arrival of the packets is preserved.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","5.5.4.6c","Requirement","ECSS-E-ST-50-04_0890061","The MAP Identifier in the Segment Header of a control segment shall contain the MAP Identifier of a control MAP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","5.5.4.7b","Requirement","ECSS-E-ST-50-04_0890064","When the PAC receives a MAP reset command and the PAC is in lockout state, the PAC shall exit lockout state.\n    ","NOTE The MAP reset command is used, for example, to recover from breaks in the sequence of TC Segments due to link difficulties or unplanned termination of transfer services.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","6.2.2.7a","Requirement","ECSS-E-ST-50-04_0890085","The Virtual Channel Identifier shall always be present in a Transfer Frame Primary Header.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","6.3.1c","Requirement","ECSS-E-ST-50-04_0890110","A CLCW shall be conveyed in the Operational Control Field of a telemetry transfer frame.\n    ","NOTE The telemetry transfer frame can be a version 1 telemetry transfer frame as defined in ECSS-E-ST-50-03 or a version 2 telemetry transfer frame as defined in CCSDS 732.0-B-2.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","6.6.2b","Requirement","ECSS-E-ST-50-04_0890131","After comparison of the length of the candidate frame with the length indicated by the Frame Length field in the Transfer Frame Primary Header, the following actions shall be taken:\n    1. If the length of the candidate frame is less than the length indicated by the Frame Length field, then discard the candidate frame.\n    2. If the length of the candidate frame exceeds the length indicated by the Frame Length field, then remove the fill octets from the end of the candidate frame.\n        ","NOTE 1 The minimum length of a TC Transfer Frame is 8 octets.\nNOTE 2 A candidate frame contains at most one TC Transfer Frame. The TC Transfer Frame is assumed to start at the beginning of the candidate frame.\nNOTE 3 For the purposes of finding the Frame Length field, the frame delimiting and fill removal procedure assumes that the candidate frame is a version 1 TC Transfer Frame, as defined in clause 6.2, although the Transfer Frame Version Number has not yet been validated.\nNOTE 4 Once a candidate frame has successfully passed the frame delimiting and fill removal procedure, it has the length indicated by the Frame Length.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","7.2.3.8.2a","Requirement","ECSS-E-ST-50-04_0890138","The value of W shall be set according to the following rules:\n2 ≤ W ≤ 254\nand\nW is an even integer",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","7.4.3.2c","Requirement","ECSS-E-ST-50-04_0890159","The system of request identifiers shall be able to handle multiple requests awaiting confirm responses at the same time.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","7.6.2c","Requirement","ECSS-E-ST-50-04_0890180","For each frame type (AD, BD or BC), at most one transmit request shall be outstanding, i.e. awaiting a response.\n    ","NOTE FOP-1 uses the AD_Out_Flag, BD_Out_Flag and BC_Out_Flag defined in clause 7.2.2.7 to keep track of outstanding requests.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","7.9.2.9a","Requirement","ECSS-E-ST-50-04_0890205","Transmit Set V(R) type-BC frame shall include the following:\n    1. Creating a new frame with a Set V(R) control command in the Transfer Frame Data Field.\n    2. Performing the Transmit type-BC frame action defined in clause 7.9.2.7 for the frame.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","7.9.2.15a","Requirement","ECSS-E-ST-50-04_0890211","Look for directive shall include the actions shown in Figure 7-4.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","8.2.3.3b","Requirement","ECSS-E-ST-50-04_0890230","The Filler bit shall be contained in bit 63 of the BCH codeblock.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-04C","9.2.1a","Requirement","ECSS-E-ST-50-04_0890255","The length of the acquisition sequence shall be at least 128 bits.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","5.5.2c","Requirement","ECSS-E-ST-50-13_1010016","For Table 5-1 and Table 5-2, there shall be an odd number of straps.\n    NOTE It is then said that the parity is odd.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","6.1a","Requirement","ECSS-E-ST-50-13_1010023","Data link layer requirements, which are not applicable to legacy devices, shall be identified and provided in an applicability matrix and statement of non-compliance. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","7.2.1a","Requirement","ECSS-E-ST-50-13_1010044","For CommunicationSynchronize primitive Table 7-3 shall apply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.2.2.1d","Requirement","ECSS-E-ST-50-13_1010065","The nominal period of TimeSynchronizeSubmit shall be fixed for a mission.\n    NOTE Recommended value for TimeSynchronize.Submit Period is one second.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.3.2.1d","Requirement","ECSS-E-ST-50-13_1010090","The BC shall send the Communication Frame Synchronization Messages in broadcast mode.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.3.2.1g","Requirement","ECSS-E-ST-50-13_1010093","The Communication Frame number shall be 0 in the first frame and incremented by one modulo N for each new Communication Frame.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.6.1.1f","Requirement","ECSS-E-ST-50-13_1010114","The Distribution Transfer Descriptor (DTD) shall be sent to the RT in SA 27R.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.6.2.1g","Requirement","ECSS-E-ST-50-13_1010139","If the Reset flag is ‘0’, the BC shall identify a new Acquisition Transfer Request by evaluation of the Acquisition Block Count value with comparison to the stored one and do the following:\n    1. If these values are not identical:\n        (a) acquire the block using subaddresses as defined in clause.8.6.2.2g, in case the Mode flag in the Acquisition Transfer Request is ‘0’ and the SIZE field indicates a block length between 1 and 1024 in the BC.\n        (b) ignore the request, in case the Mode flag in the Acquisition Transfer Request is ‘0’ and the SIZE field indicates a block length greater than 1024 in the BC.\n        (c) acquire the block using subaddresses as defined in clause 8.6.2.2j in case the Mode flag in the Acquisition Transfer Request is ‘1’.\n    2. If these values are identical, ignore the request (no new data).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.7.1d","Requirement","ECSS-E-ST-50-13_1010160","Word 16 to 32 of SA 1T shall be reserved for RT configuration monitoring data to be defined by the application.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-13C","8.7.3b","Requirement","ECSS-E-ST-50-13_1010167","Word 0 of SA 1R shall be used for RT Health Reset command as defined in clause 8.7.3f. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","4.2.4.1b","Requirement","ECSS-E-ST-50-14_0940008","To achieve full cross-strapping benefits, in terms of reliability, any potential common failure of UNIT_1_A and UNIT_1_B drivers and UNIT_2_A and UNIT_2_B receivers shall be avoided. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","5.3.2b","Requirement","ECSS-E-ST-50-14_0940029","The resulting voltage shall be utilised to feed a dedicated analogue channel.\n    ","NOTE The objective of these requirements is that the receiver is able to directly interface with a passive thermistor:",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","7.1.2.2a","Requirement","ECSS-E-ST-50-14_0940054","The passive state of the HPC_OUT(H) signal shall be low.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","7.1.2.5a","Requirement","ECSS-E-ST-50-14_0940057","The design of the high power pulse command interface shall ensure that no failure mode results in the output being permanently active (high state).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","8.2.2b","Recommendation","ECSS-E-ST-50-14_0940167","The peripheral element should be designed to be compatible with any tb specified in 8.3.4.8 and 8.4.4.9.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","8.4.2.2a","Requirement","ECSS-E-ST-50-14_0940103","Maximum skew measured at core side shall be Dt = 0,02 × tb . ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","8.7.1a","Requirement","ECSS-E-ST-50-14_0940124","A balanced differential pair of circuits called GATE_WRITE+ and GATE_WRITE- shall be provided. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-14C","8.7.4b","Requirement","ECSS-E-ST-50-14_0940131","The balanced differential pair specified in 8.7.4a shall \n    1. be driven by the peripheral element, and \n    2. carry the DATA_IN signal.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.1.1a","Requirement","ECSS-E-ST-50-52_1080001","The Target SpaceWire Address field shall comprise zero or more data characters forming the SpaceWire address which is used to route the command to the target.\n    ","NOTE The Target SpaceWire Address is stripped off by the time the packet reaches the target.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.1.6i","Permission","ECSS-E-ST-50-52_1080401","An RMAP implementation may use an implicit return address or implicit partial return address.\n    ","NOTE For example, a SpaceWire router with an RMAP configuration port can automatically route the reply to an RMAP command out of the same port that the RMAP command arrived on without the need for this being explicitly specified in the Reply Address field.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.1.3a","Requirement","ECSS-E-ST-50-52_1080047","The Target Logical Address field shall be as defined in clause 5.1.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.1.5.2a","Requirement","ECSS-E-ST-50-52_1080050","The Packet Type field shall be 0b01 to indicate that this is a command.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.2.5b","Requirement","ECSS-E-ST-50-52_1080075","The Packet Type field shall be 0b00 to indicate that the RMAP packet is a reply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.3.4.6b","Recommendation","ECSS-E-ST-50-52_1080405","When checking the Header CRC indicates no error present in the header and if the Instruction field contains an unused packet type (0b10 or 0b11), the target should update the error information to reflect the “unused RMAP packet type or command code” error if the target supports error information gathering.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.3.6.7a","Requirement","ECSS-E-ST-50-52_1080117","If the Verify-Data-Before-Write bit is set (1) in the command field of the header and if there is more data in the data field than specified in the Data Length field of the write command header, the target shall:\n    1. Not write data into memory,\n    2. Discard the rest of the packet,\n    3. Return a “too much data” error as specified in clause 5.6 to the node specified in the Reply Address and Initiator Logical Address fields if a reply has been requested, Reply bit set (1).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.3.3.6.11b","Recommendation","ECSS-E-ST-50-52_1080416","If the Verify-Data-Before-Write bit is clear (0) in the command field of the header and if there is less data in the data field than specified in the Data Length field of the write command header when the EOP is reached, the target should:\n    1. Indicate that an “insufficient data” error has occurred to the user application in the target,\n    2. Update the error information to reflect the “insufficient data” error if the target supports error information gathering.\n        ","NOTE If there is a Data CRC in the packet prior to the EOP then it can be incorrectly transferred into memory at the end of the data.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.4.1.5.3c","Requirement","ECSS-E-ST-50-52_1080152","The Reply bit shall be set (1) for a read command.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.4.2.5a","Requirement","ECSS-E-ST-50-52_1080171","The Protocol Identifier field shall be as defined in clause 5.1.3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.4.3.4.2b","Recommendation","ECSS-E-ST-50-52_1080427","If an EEP or EOP is received before the complete header including header CRC has been received the target should update the error information to reflect the “EEP” or “Early EOP” error if the target supports error information gathering.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.4.3.4.4a","Requirement","ECSS-E-ST-50-52_1080195","When an RMAP packet is received at the target the Header CRC shall be checked.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.4.3.9a","Requirement","ECSS-E-ST-50-52_1080220","When the read reply is received at the initiator (or other node specified by the Reply Address), successful completion of the read request shall be indicated to the user application on that node (Read Data Confirmation).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.1.5.4a","Requirement","ECSS-E-ST-50-52_1080241","The Reply Address Length field shall be set to the smallest number of 32-bit words that is able to contain the Reply SpaceWire Address from the target, back to the initiator of the command packet or some other node that is to receive the reply.\n    ","NOTE For example, if ten path Reply SpaceWire Address bytes are used then the Reply Address Length field is set to three (0b11).",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.2.2a","Requirement","ECSS-E-ST-50-52_1080262","The format of the reply to a read-modify-write command shall be as in Figure 5-17.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.2.6c","Requirement","ECSS-E-ST-50-52_1080269","The Command field shall be set to the same value as in the Command field of the read-modify-write command, 5.5.1.5.3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.3.4.4a","Requirement","ECSS-E-ST-50-52_1080290","When an RMAP packet is received at the target the Header CRC shall be checked.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.3.5.3a","Requirement","ECSS-E-ST-50-52_1080375","If the Target Logical Address is not a logical address recognised by the target user application, the target shall\n    1. Discard the command packet,\n    2. Return an “invalid Target Logical Address” error as specified in clause 5.6 to the node specified in the Reply Address and Initiator Logical Address fields.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.5.3.14a","Requirement","ECSS-E-ST-50-52_1080336","When a reply is received by the initiator (or other node specified by the Reply Address) with the reserved bit in the instruction field set (1) or with the command/reply bit clear (0), the initiator shall discard the reply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-52C","5.6.1b","Requirement","ECSS-E-ST-50-52_1080339","If a command executes successfully, then the Error Code 0 shall be used in the Status field of any reply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-53C","5.1.3a","Requirement","ECSS-E-ST-50-53_1090004","The Status code parameter shall be used to indicate the validity of the packet to the receiving service user.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-53C","5.3.2a","Requirement","ECSS-E-ST-50-53_1090025","Target Logical Address field shall be an 8-bit field that contains a logical address of the target.\n    ","NOTE 1 The Target Logical Address field is normally set to a logical address recognised by the target.\nNOTE 2 If the target does not have a specific logical address then the Target Logical Address field can be set to the default value 254 (0xFE).\nNOTE 3 A target can have more than one logical address.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-53C","5.5.4.2a","Requirement","ECSS-E-ST-50-53_1090046","If the CCSDS Packet Transfer Protocol packet arrives at the target with the Reserved field set to 0x00 and is terminated by an EOP, the CCSDS Packet shall be extracted from the SpaceWire packet and passed to the target user application.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50C","5.2.1.3a","Requirement","ECSS-E-ST-50_0970002","As an output from the requirements engineering activity, the customer shall produce the space communication system requirements specification (CSRD) in conformance with the DRD of Annex A.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.2.6.2a","Requirement","ECSS-E-ST-50_0970023","The activities performed during space communication system operations shall include:\n    1. operation of the space communication system as and when specified by the mission to achieve the objectives of the mission;\n    2. maintenance, including planned upgrades of the system and reconfiguration for different phases of the mission;\n    3. provision of additional support for spacecraft trouble shooting and contingency operations;\n    4. execution of the decommissioning procedures at end-of-life, including stopping spacecraft transmissions, and notification of the ITU-R of the availability of the frequencies for re-use.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.5.4a","Requirement","ECSS-E-ST-50_0970048","The space communication system shall enable telemetry-in-the-blind operation, i.e. the down-linking of telemetry data in the absence of any up-link signal to the spacecraft.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.6.11.5a","Requirement","ECSS-E-ST-50_0970069","Uplink budget calculations shall be based on a BER of 10-5 at the input to the telecommand decoder.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.6.11.8a","Recommendation","ECSS-E-ST-50_0970224","The downlink frame rejection rate should be less than 10-5.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.6.14.9a","Requirement","ECSS-E-ST-50_0970097","The space link shall provide an exception reporting function that enables the reporting of all detected errors.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","5.8.5a","Requirement","ECSS-E-ST-50_0970118","The ground network shall enable the hot redundant operation of nodes used for the control and operation of critical mission functions.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","A.2.1<5>b","Requirement","ECSS-E-ST-50_0970125","The CSRD shall summarize the major project milestones relating to the ground segment.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","B.2.1<4>b","Requirement","ECSS-E-ST-50_0970146","The CSBD shall describe all of the assumptions made in establishing the communication system baseline definition.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","C.2.1<1>a","Requirement","ECSS-E-ST-50_0970167","The CSAD shall contain a description of the purpose, objective, content and the reason prompting its preparation.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","D.2.1<7>a","Requirement","ECSS-E-ST-50_0970192","The CSVP shall describe each verification test to be performed, including the following information for each one:\n    1. a statement of the purpose of the verification test;\n    2. a detailed description of the test;\n    3. a list of the tools, equipment, or facilities to perform the test;\n    4. a definition of the configuration of the test environment and the unit under test at the start of the test (i.e. pre-conditions);\n    5. a description of the expected result (i.e. post-conditions);\n    6. pass and fail criteria for the test.\n        ","NOTE The purpose of these test description is to ensure that the verification tests can be repeated.",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","H.2.1<2>a","Requirement","ECSS-E-ST-50_0970213","The CSOM shall list the applicable and reference documents in support to the generation of the document.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50C","H.2.1<4>b","Requirement","ECSS-E-ST-50_0970216","The CSOM shall describe the communication system test procedures used to verify the correct operation of the communication system during the mission;",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-60-10C","4.2.4.2.2a","Requirement","ECSS-E-ST-60-10_1020020","If the total error   is a quadratic sum of two errors   and  , each of which being a linear combination of individual contributing errors, and if the following additional conditions are verified:\n ,  ,  \nthe following condition shall be met to ensure that the budget is compliant with the specification:\n \nwhere\n¾\t  and   are the means of the two errors   and  .\n¾\t  is a positive scalar defined such that for a Gaussian distribution the   confidence level encloses the probability   given in the specification. \n¾\t  and   are the standard deviations of the two errors   and  .\n¾\t  is the maximum value for the total error, given in the specification. \n¾\t‘log’ is the natural logarithm (base e)\nNOTE \t1\tThis condition is based on the properties of a Rayleigh distribution. It is a less conservative formula than the general case (4.2.4.2.1) - see annex A.2.4 for more details.\nNOTE \t2\tThis applies to the case of “directional” pointing errors in which the errors on the perpendicular axes are similar.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-10C","5.2.4c","Requirement","ECSS-E-ST-60-10_1020033","The appropriate stability margin indicators shall be identified and justified by the control designer according to the nature and structure of the uncertainties affecting the system. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.1j","Requirement","ECSS-E-ST-70-01_1060010","It shall be possible to initiate the execution of a local function from anywhere within an OBCP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.2.7a","Requirement","ECSS-E-ST-70-01_1060031","It shall be possible to include the following execution controls within an OBCP:\n    1. simple conditional branching (i.e. if … then … else …);\n    2. multiple conditional branching where the path taken is dependent on the value of a specified parameter (or variable);\n    3. repeated execution of a statement (or a group of statements) with the possibility of repeating the execution a specified number of times, repeating the execution indefinitely whilst a given condition holds true or repeating the execution until a given condition becomes true.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.2.9.3b","Requirement","ECSS-E-ST-70-01_1060052","It shall be possible to access events raised on-board together with their associated parameters.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.4.2.3d","Requirement","ECSS-E-ST-70-01_1060077","The Activate request shall include any necessary parameters to be passed to the OBCP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.4.4.4c","Requirement","ECSS-E-ST-70-01_1060098","The loading policy shall be definable on a per-OBCP basis.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","5.4.4.5c","Requirement","ECSS-E-ST-70-01_1060101","The OBCP engine shall be able to execute several OBCPs in parallel.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-01C","6.2.1h","Requirement","ECSS-E-ST-70-01_1060126","OBAP validation and verification shall be completed prior to system qualification, see Figure 6-3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","4.5c","Requirement","ECSS-E-ST-70-11_0290007","No single unintentional ground command or failure in one space segment element shall cause a failure in another space segment element.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","4.6d","Requirement","ECSS-E-ST-70-11_0290014","For each on-board function, there shall be at least one alternative configuration that can achieve the same function using different on-board units.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.2.3d","Requirement","ECSS-E-ST-70-11_0290035","The capability shall be provided to transmit real-time telemetry data and deferred telemetry data simultaneously.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.3.1t","Requirement","ECSS-E-ST-70-11_0290056","The location of a parameter within a non-variable telemetry source packet shall be fixed and derivable from an implicit knowledge of the packet structure.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.4n","Requirement","ECSS-E-ST-70-11_0290081","If the requirements for timing accuracy are expected to vary during the course of a mission, the capability shall be provided to change the rate of generation of the time packet.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.5.3c","Requirement","ECSS-E-ST-70-11_0290102","Telecommand routing shall ensure that an on-board “blockage” resulting from payload commanding has no impact on platform commanding.\n    ","NOTE For example, an extensive command sequence for the configuration of a payload, which has no impact on the essential commanding of platform subsystems in parallel.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.5.4e","Requirement","ECSS-E-ST-70-11_0290109","Failure of telecommand execution at any of the identified stages shall either be explicitly reported or unambiguously observable in the housekeeping telemetry.\n    ","NOTE ECSS-E-ST-70-41 service 1 can be used for this purpose.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.6.2g","Requirement","ECSS-E-ST-70-11_0290130","With the exception of high-priority commands, all potentially critical configuration change telecommands initiated by the ground segment shall be buffered on-board in such a way that all parameters defining the new configuration can be inspected by the ground segment, via telemetry, before executing the change on-board.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.7.5.2i","Requirement","ECSS-E-ST-70-11_0290151","The reporting of FDIR activities shall contain all information for failure analysis (e.g. time of occurrence, parameter out-of-limit, switching performed). \n    ","NOTE A time delay for this reporting can be accepted if, for example, the reporting uses an operational on-board processor.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.7.5.3b","Requirement","ECSS-E-ST-70-11_0290158","The capability shall be provided to monitor and to define out-of-limit conditions for essential on-board parameters (see clause 5.8.6).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.7.5.7b","Requirement","ECSS-E-ST-70-11_0290179","The on-board fault management function shall autonomously establish a fully operational configuration such that mission operations can continue, including the generation of the mission products. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.8.3a","Requirement","ECSS-E-ST-70-11_0290200","The capability shall be provided for the ground segment to load any changeable memory area.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.8.5g","Requirement","ECSS-E-ST-70-11_0290225","The capability shall be provided for a telecommand released from the on-board operations schedule to set an interlock on (i.e. condition the release of) subsequent telecommands within the same sub-schedule.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.8.6j","Requirement","ECSS-E-ST-70-11_0290246","All changes of monitoring status shall be reported to the ground segment by means of a “check transition” telemetry packet.\n    ","NOTE For example, a check transition telemetry packet produced when a parameter goes out-of-limits and when it subsequently returns back into limits.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.8.7c","Requirement","ECSS-E-ST-70-11_0290253","When transferring a set of data that exceeds the maximum packet size specified for the mission (e.g. memory loading or dumping), the capability shall be provided to transfer this data in more than one packet (part packet).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.8.9p","Requirement","ECSS-E-ST-70-11_0290274","The capability shall be provided to suspend and resume the retrieval of stored telemetry packets.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.9.1c","Recommendation","ECSS-E-ST-70-11_0290360","A processor switchover should not invalidate telecommands not yet released from any ground schedule.\n    ","NOTE This implies that telecommands defined for the prime unit are also valid for the redundant unit, except for any command routing data which the ground system can automatically change when addressing the redundant processor.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.9.1j","Recommendation","ECSS-E-ST-70-11_0290362","Enabling of on-board software should use only a single telecommand.\n    ","NOTE This does not preclude dual-step commanding because only the final command enables the software.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.9.3a","Requirement","ECSS-E-ST-70-11_0290323","Redundant receivers, cross-strapped to redundant decoders, shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-11C","5.9.7g","Recommendation","ECSS-E-ST-70-11_0290365","Any operationally-significant information on the configuration and timing of payload operations should be downlinked in the telemetry.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70C","5.2.2.6b","Requirement","ECSS-E-ST-70_0060021","The OVP shall cover:\n    1. Test preparation activities.\n    2. Technical and managerial resources used for execution of the tests.\n    3. Test strategies, methods and scenarios.\n    4. Test pass or fail criteria.\n    5. Post-test activities.\n        NOTE For example, reporting, handling of non-conformances.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","5.3.3a","Requirement","ECSS-E-ST-70_0060038","The outputs of the mission operations data production process shall be the ones specified in Table 5-4.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","5.5.2e","Requirement","ECSS-E-ST-70_0060050","Training shall comprise theoretical and practical training including realistic simulations, rehearsals of operational scenarios and contingency cases for the ground segment and the space segment.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","5.7.3a","Requirement","ECSS-E-ST-70_0060071","The outputs of the operational configuration management process shall be the ones specified in Table 5-12.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","5.8.2.4d","Requirement","ECSS-E-ST-70_0060092","Performance reports on the space and ground segments (including trend analysis) shall be produced at suitable intervals to determine success in meeting the mission objectives.\n    NOTE 1 For example, mission product throughput and quality from payload data processing facilities.\n    NOTE 2 The reporting requirements of ECSS-Q-ST-10-09 apply in the case that the anomaly is shown to be a nonconformance.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","5.9.2b","Requirement","ECSS-E-ST-70_0060099","The disposal operations analysis shall cover methods for storage, dismantling, reusing, recycling or destruction of the space segment. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","6.2.2.3k","Requirement","ECSS-E-ST-70_0060120","Contributions to the space-to-ground interface control document (SGICD) shall be prepared addressing:\n    1. RF interfaces.\n    2. Voice, video and high-rate data transmission.\n        NOTE See AOS Networks and Data Links: Architectural Specification, CCSDS 701.0-B-2.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","6.4.2.1c","Requirement","ECSS-E-ST-70_0060145","The integrated logistics support systems shall be integrated and validated in conformance with the “Requirements for control of logistic activities” of ECSS-M-ST-70.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","6.5.2.2h","Requirement","ECSS-E-ST-70_0060166","Configuration management shall cover: \n    1. The maintenance of a configuration management database.\n    2. Support of configuration documentation.\n    3. Management of configuration items.\n        NOTE 1 For configuration management see ECSS-M-ST-40.\n        NOTE 2 Configuration items include hardware components, network components, software components including also COTS, documentation, configuration data, mission operations data.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","7.4.2a","Requirement","ECSS-E-ST-70_0060187","The main processes specified in Table 7-3 shall be carried out during phase C.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","7.5.3d","Requirement","ECSS-E-ST-70_0060194","Mission operations data validation shall end with a critical operations review (COR).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","A.2.1<7>b","Requirement","ECSS-E-ST-70_0060215","The requirements shall be organized according to the following operations functional breakdown:\n    1. mission planning and scheduling;\n    2. monitoring and control;\n    3. performance monitoring and evaluation;\n    4. flight dynamics;\n    5. payload operations and data management:\n        (a) payload operations planning;\n        (b) payload operations control;\n        (c) payload data processing;\n        (d) payload data archiving; \n        (e) user services;\n        (f) data product delivery;\n        (g) performance analysis.\n    6. on-board software maintenance;\n    7. other mission-specific operations functions.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","C.2.1<3.5>a","Requirement","ECSS-E-ST-70_0060236","The MOCD shall describe the relationship of the mission with other missions or programmes, including:\n    1. membership of a family of missions of the same or similar design or based on the same spacecraft platform;\n    2. membership of a multi-national or coordinated multi-mission programme;\n    3. agreements for the ground segment to support other concurrent missions or programmes or to process data from other missions.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","C.2.1<5.3>a","Requirement","ECSS-E-ST-70_0060243","The MOCD shall describe the concept for the implementation of scheduled operations for the space and ground segment, including:\n    1. schedule execution;\n    2. procedure execution;\n    3. manual commanding;\n    4. command pre-transmission validation and uplink management;\n    5. command verification;\n    6. schedule and command history archiving;\n    7. space and ground segment health monitoring;\n    8. failure detection, isolation and recovery (FDIR).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","E.2.1<4.5>a","Requirement","ECSS-E-ST-70_0060264","Provide a cross-reference to the applicable version of the SGICD.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","E.2.1<5.7>f","Requirement","ECSS-E-ST-70_0060289","For contingency procedures, the same details shall be provided as for nominal operational procedures in E.2.1<5.7>d. ",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","G.2.1<3.3>c","Requirement","ECSS-E-ST-70_0060310","The following shall also be defined:\n    1. mechanisms for confirming the readiness to proceed with operations (briefing) and for reviewing the progress of execution of operations (de-briefing;\n    2. the reporting channels for routine operations and the mechanisms deployed for anomaly reporting;\n    3. mechanisms for on-call support and the procedures for invoking them.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","I.2.1a","Requirement","ECSS-E-ST-70_0060331","Each operations procedure shall have a unique identification number.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","I.2.2<6>b","Permission","ECSS-E-ST-70_0060403","An operations procedure may also indicate conditions under which start of the procedure is prohibited",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-70C","J.2.1<10>a","Requirement","ECSS-E-ST-70_0060359","The CFISRD shall identify the requirements for post-launch technical support from the OC, covering:\n    1. On-site participation of project support teams during LEOP and commissioning phase operations, including responsibilities, required skills, schedule for support;\n    2. On-call engineering support to mission operations at the mission control centre: response time as a function of mission phase;\n    3. Call-out engineering support for satellite anomaly recovery operations at the mission control centre, including response time as a function of mission phase;\n    4. Off-site support for analysis of satellite anomalies, including inputs to be provided to the OC (in particular anomaly reports, in accordance with Annex H), definition of close-out report, and response times.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-50-05C Rev. 2","4.3.2a","Requirement","ECSS-E-ST-50-05_0900026","The project manager shall provide, to the frequency coordinator, the data regarding the frequencies used by the spacecraft to enable the advance publication, coordination and notification procedures of ITU/RR/9 and ITU/RR/11 no later than three years before the planned launch date.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","4.3.2d","Requirement","ECSS-E-ST-50-05_0900029","The procedures of ITU/RR/9 and ITU/RR/11 shall be carried out by the frequency coordinator for the satellites and Earth stations, in conformance with frequency management procedures.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","5.5.4a","Requirement","ECSS-E-ST-50-05_0900050","Satellites in Sun-synchronous orbit or in an orbit that is proximate to the orbits of the DRS user satellites shall not produce a power-flux-density greater than -155 dB(W/m2) in 1 MHz at any location on the geostationary orbit (GSO) for more than 0,1 % of the time.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","6.1.4.1.3e","Requirement","ECSS-E-ST-50-05_0900075","Telemetry subcarrier frequencies shall conform to the following requirements:\n    1. carrier acquisition by the ground receivers, as specified in clause 7.1;\n    2. occupied bandwidth, as specified in clause 5.4;\n    3. compatibility between ranging and telemetry.\n        NOTE For compatibility between ranging and telemetry, see ECSS-E-ST-50-02.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","6.1.7a","Requirement","ECSS-E-ST-50-05_0900096","A positive-going video signal shall result in an advance of the phase of the radio frequency carrier.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","6.2.2b","Requirement","ECSS-E-ST-50-05_0900117","If the ground stations network for the mission concerned has the capability for using the synchronization marker(s) to resolve the phase ambiguity, such techniques shall be used without performing differential encoding for BPSK, QPSK, OQPSK and UQPSK signals.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","6.2.3.2b","Requirement","ECSS-E-ST-50-05_0900124","The phase angle between the two quadrature carriers shall be (90 ±5)°.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","6.2.3.4k","Requirement","ECSS-E-ST-50-05_0900145","In the case of digital implementation, the FIR filter impulse response shall be at least 16 bits long.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","7.1.1.2a","Requirement","ECSS-E-ST-50-05_0900174","For safe acquisition, a period of time commensurate with a triangular frequency search in the worst case condition on link margin shall be allowed.\n    NOTE This is independent of the methods used for the acquisition of the Earth station receivers and demodulators. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","7.1.3a","Requirement","ECSS-E-ST-50-05_0900177","If the coherent mode of the spacecraft transmitter is used, this shall be activated automatically or by telecommand, in the latter case, after acquisition of the Earth-space link is confirmed. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","7.2.3a","Requirement","ECSS-E-ST-50-05_0900197","The acquisition procedure shall be the same as that described in 7.2.2, except that the sweep parameters are:\n    1. Sweep rate: 1 Hz/s to 10 kHz/s.\n    2. Maximum sweep range: ±1 MHz.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","9.1a","Requirement","ECSS-E-ST-50-05_0900224","The modulated RF carrier shall conform to the following expressions: \n \nwhere\nP  is the power of the carrier;\nf  is the centre frequency;\nj(t) is the phase of the modulated carrier;\nj0  is a constant random phase;\nand, \n \nwhere\nak = (-1)k dk dk-1 are the pre-coder output symbols; \ndk = { ±1 } is the k-th information symbol to be transmitted.\n\nThe instantaneous frequency pulse g(t) is obtained through a linear filter with impulse response defined by: \n \nwhere\n \n* means convolution,\nh(t) is the Gaussian density function:\n \nwhere\n \nwith \nln (n) = natural logarithm (base = e);\nB = one-sided 3-dB bandwidth of the filter with impulse response h(t);\nTs = the duration of one input symbol as defined in Figure 6-1 and Figure 6-2.\n    NOTE The specified pre-coding suppresses the need for differential decoding at the receiver side and improves the receiver performances.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-05C Rev. 2","9.2.6.3b","Recommendation","ECSS-E-ST-50-05_0900302","The output filtering should be obtained with a 4 poles/2 zeros elliptic filter characterized with the normalized transfer function given in Figure 9-7.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-32C","5.2a","Requirement","ECSS-E-ST-70-32_0950019","The capability shall be provided to request the execution of any space system activity.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-32C","5.2h","Requirement","ECSS-E-ST-70-32_0950026","To ensure that any service provided by the EMCS is accessible within a procedure, the following capabilities shall be provided:\n    1. to request any operation defined for any space system object;\n    2. to acquire the value of any property of any space system object.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-32C","B.2c","Recommendation","ECSS-E-ST-70-32_0950062","Multiples and submultiples of an engineering unit should be formed using the simple engineering unit symbol combined with a decimal prefix, as specified in Table B-2. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","4.3.2.3c","Requirement","ECSS-E-ST-10-03_0750021","The following parties shall participate to the PTR:\n    1. product assurance;\n    2. project engineer;\n    3. AIT;\n    4. facility representative;\n    5. other, including specialist, as relevant.\n        ","NOTE For example launcher authority for tests related to launcher interface or other company representative that will take over the responsibility of the hardware after delivery. ",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","4.3.2.4c","Requirement","ECSS-E-ST-10-03_0750024","The following parties shall participate to the TRB:\n    1. product assurance;\n    2. project engineer;\n    3. AIT;\n    4. facility representative;\n    5. other, including specialist, as relevant.\n        ","NOTE For example launcher authority for tests related to launcher interface or other company representative that will take over the responsibility of the hardware after delivery.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","4.4.1d","Requirement","ECSS-E-ST-10-03_0750045","Cleanliness and contamination control for test programmes shall conform to ECSS-Q-ST-70-01.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","4.5.3c","Requirement","ECSS-E-ST-10-03_0750070","The acceptance programme shall be performed, after a qualification programme has been completed (as per clause 4.5.2 or clause 4.5.4). \n    ","NOTE The FM is built from the same design file than the QM or the PFM used for qualification, as specified in the ECSS-E-ST-10-02 clause 5.2.4.3.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.1d","Requirement","ECSS-E-ST-10-03_0750091","Any unusual or unexpected behaviour shall be evaluated to determine the existence of any trend potentially leading to anomaly or failure situation.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.2a","Requirement","ECSS-E-ST-10-03_0750098","The space segment equipment qualification test baseline shall consist of the tests specified in Table 5-1 in line with requirement 5.1b, according to the type of the space segment equipment.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.1.3b","Requirement","ECSS-E-ST-10-03_0750119","The space segment equipment shall be set up to operate under the environmental conditions expected during actual operation.\n    ","NOTE Environments include e.g. ambient, thermal, vacuum, and various combinations of these.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.2.4e","Requirement","ECSS-E-ST-10-03_0750140","For space segment equipment which is designed to be re-flown, the qualification test duration shall be in conformance with Table 5-2 plus 50 seconds per additional flight. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.3.1g","Requirement","ECSS-E-ST-10-03_0750165","When temperature potentially affects the sealing materials or surfaces, an evaluation of the hardware design and operational characteristics shall be performed and, if technically warranted, the leak test conducted at the minimum and maximum qualification or acceptance temperature limits for respectively qualification or acceptance test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.3.2b","Requirement","ECSS-E-ST-10-03_0750168","The proof pressure acceptance test shall be performed to demonstrate absence of workmanship problem leading to leak above the specification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.4.1o","Requirement","ECSS-E-ST-10-03_0750189","The space segment equipment operative configuration during the test shall be the most severe one in the power time domain and from the power consumption point of view.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","5.5.6.1.2a","Requirement","ECSS-E-ST-10-03_0750214","The space segment equipment sound power measurements shall be performed in accordance with ISO 3740:2000.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.1.2.1f","Recommendation","ECSS-E-ST-10-03_0750460","The FFT activities should follow the expected mission sequence, properly involving the interested functions, with the element correct configuration for the particular mission phase.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.1.2.3b","Requirement","ECSS-E-ST-10-03_0750242","The following protection functions shall be tested:\n    1. over-voltage protection functions;\n    2. over-current protection functions;\n    3. inter-locks, if any;\n    4. overriding capabilities of protection functions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.1.5c","Requirement","ECSS-E-ST-10-03_0750263","During the polarity test the AOCS shall be operated in the mode where the chain is used in the control loop.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.2.5e","Requirement","ECSS-E-ST-10-03_0750284","A resonance search shall be performed before and after the transient vibration tests to determine resonance frequencies to evaluate the product integrity.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.2.8d","Requirement","ECSS-E-ST-10-03_0750309","Notching criteria and implementation shall be approved by the customer and, if relevant, by the launcher authority.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.2.8g","Requirement","ECSS-E-ST-10-03_0750312","A resonance search shall be performed before and after the sinusoidal vibration tests to determine resonance frequencies to evaluate the product integrity and to compare the resonance frequency distribution with that of the mathematical model or modal survey.","NOTE 1 Any significant shift in resonance frequencies from those analytically determined is an indication of improper assembly or materials defects.\nNOTE 2 This resonance search can be used to update the Finite Element Model in case of design modification w.r.t. the previously tested model.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.4.1d","Requirement","ECSS-E-ST-10-03_0750337","The sequence of functional tests shall be defined in the test specification such that all space segment equipment are tested.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","6.5.5.2.1a","Requirement","ECSS-E-ST-10-03_0750358","The space segment element shall be subjected to EMC tests, specified in the ECSS-E-ST-20-07 clause 5.3 and in conformance with the Annex A of ECSS-E-ST-20.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","7b","Requirement","ECSS-E-ST-10-03_0750379","Pre-launch tests results shall result in the authorizing the next pre-launch activities to be carried out.\n    ","NOTE For example leak test is performed to authorize fuelling.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","7i","Requirement","ECSS-E-ST-10-03_0750386","If the pyro connections are planned in the launch facility, circuit continuity, insulation shall be checked, at the level of the safe and arm plug connector, prior to connection.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","B.2.1<2>a","Requirement","ECSS-E-ST-10-03_0750407","The TSPE shall list the applicable and reference documents in support to the generation of the document.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-03C","C.2.1<11>a","Requirement","ECSS-E-ST-10-03_0750431","The TPRO shall describe how the applicable documentation is used to support the test activity.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.2.3c","Requirement","ECSS-E-ST-70-31_0270017","Mathematical, time and string functions shall be supported.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.2.3f","Requirement","ECSS-E-ST-70-31_0270020","The capability to mix compatible units freely within an expression shall be supported",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.2.6n","Requirement","ECSS-E-ST-70-31_0270045","Engineering units shall be supported.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.4.2a","Requirement","ECSS-E-ST-70-31_0270066","All monitoring and control data shall be considered as case-insensitive, with the exception of engineering units.\n    ","NOTE Engineering units are defined in Annex B of ECSS-E-ST-70-32.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.5.4.2a","Requirement","ECSS-E-ST-70-31_0270087","For system elements of type “application process”, the additional data specified in Table 6-15 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.5.5.4.1a","Requirement","ECSS-E-ST-70-31_0270094","For the definition of the tailoring of the housekeeping and diagnostic data reporting service, the additional data shown in Table 6-22 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.5.5.10.2a","Requirement","ECSS-E-ST-70-31_0270115","For the data types of the packet fields of the on-board operations scheduling service, the additional data shown in Table 6-43 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.5.7a","Requirement","ECSS-E-ST-70-31_0270136","For system elements of type “VC”, the additional data specified in Table 6-64 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.6.6.2a","Requirement","ECSS-E-ST-70-31_0270161","For reporting data that is delta-checked, the additional data specified in Table 6-86 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-31C","6.7.1.2a","Requirement","ECSS-E-ST-70-31_0270164","For each activity, the data specified in Table 6-89 shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","4.2b","Requirement","ECSS-E-ST-20-08_0090002","The data specified in requirement 4.2a shall be determined during the development phase of a new component and need not be repeated during the qualification program.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.3.2.1b","Requirement","ECSS-E-ST-20-08_0090023","The PMP list shall include the RML and CVCM values for all materials used.\n    NOTE The mission specification can specify an absolute limit to the total mass loss and volatile condensable material of the solar array sub-system. The fulfilment of this system requirement can be verified either by analysis using the total amount of the applied materials, the individual material RML and CVCM data, outgassing field of view and temperature distribution, or by test of the representative subsystem and measurement of the outgassing product.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.3.3.4a","Requirement","ECSS-E-ST-20-08_0090044","Sections shall not be included at the coupon level. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.3.3.9d","Requirement","ECSS-E-ST-20-08_0090051","No failure shall be propagated from one solar array wiring group to another.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.4.3.5a","Requirement","ECSS-E-ST-20-08_0090072","A visual inspection shall be made after stringing.\n    NOTE This is to determine, as early as possible, defects in the rear sides of solar cells and, when feasible, the front sides.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.1.3.3e","Requirement","ECSS-E-ST-20-08_0090097","The number of (non-cell) components shall correspond to the number in a flight configuration of the unit they belong to, but with a minimum of two. \n    NOTE For example, it can be one blocking diode per string, one shunt diodes per shunt interval, and two bleed resistors per panel, but in accordance with this requirement, in all these cases the minimum number is two.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.1.4.4d","Requirement","ECSS-E-ST-20-08_0090119","The duration of the test shall be 30 days.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.1.4.4g","Requirement","ECSS-E-ST-20-08_0090122","Water condensation on the surface of the test sample shall be prevented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.2.6c","Requirement","ECSS-E-ST-20-08_0090147","Any defect in conformance with requirement 5.5.3.2.6b, raised after acceptance shall be reported and traced throughout the qualification sequence.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.2.14a","Requirement","ECSS-E-ST-20-08_0090168","Welding of wires at string terminations and terminals shall be in conformance with the SCD-PVA.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.3.5b","Requirement","ECSS-E-ST-20-08_0090189","The resistance shall be the value stated in the SCD-PVA.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.3.7c","Requirement","ECSS-E-ST-20-08_0090196","When all the cells are protected by shunt diodes, during the test, the temperature increase of the shunt diode shall be uniform and shall not exceed the value stated in the SCD-PVA.\n    NOTE If the measured voltage is outside the sum of the individual diode forward voltages at the maximum current ±1 %, techniques such as thermographic photo recordings may be used to locate the failed shunt diodes.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.7.3a","Requirement","ECSS-E-ST-20-08_0090217","The panels shall be exposed to the number of thermal cycles for acceptance as stated in the SCD-PVA.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","5.5.3.11.3b","Requirement","ECSS-E-ST-20-08_0090242","No open circuit conditions shall be recorded during continuity testing.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.3.1c","Requirement","ECSS-E-ST-20-08_0090263","The data documentation corresponding to the tests referred to in requirement 6.3.1b shall be delivered together with the delivered SCAs and the qualification test lot as part of the DDP.\n    NOTE For the DDP, see clause 6.6.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.3.3.2b","Requirement","ECSS-E-ST-20-08_0090266","The predicted operational voltage (Vop) shall be defined in the SCD-SCA.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.4.3.1.4c","Requirement","ECSS-E-ST-20-08_0090292","Defects of the types specified in requirement 6.4.3.1.4a occurring in the contact weld area shall be prevented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.4.3.3.2a","Requirement","ECSS-E-ST-20-08_0090313","The electrical current of SCA under 1 S.C. (AM0) shall be measured and recorded digitally at least at 50 points, at a solar cell temperature of 25 °C +/- 0,5 °C or operating temperature. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.4.3.5.2c","Requirement","ECSS-E-ST-20-08_0090329","The monochromatic irradiation shall be generated by one of the following methods: \n    1. With the aid of narrow-band interference filters, having the following characteristics:\n        (a) for silicon solar cells, at least, at 14 discrete wavelength intervals between 0,3 mm and 1,1 mm; \n        (b) for single-junction GaAs solar cells at least, at 14 discrete wavelength intervals between 0,3 mm and 1,1 mm and at least 3 narrow band interference filters in the range 0,75 mm to 1,1 mm.\n        (c) for multi-junction GaAs solar cells, the number of narrow band interference filters and their wavelength are stated in the SCD-SCA.\n    2. By means of a high-intensity monochromator for continuous recording between 0,3 mm and at least 1,8 mm.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.4.3.8.2g","Requirement","ECSS-E-ST-20-08_0090343","Water condensation on the surface of the SCAs shall be prevented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.4.3.13.2b","Requirement","ECSS-E-ST-20-08_0090364","The measurement specified in requirement 6.4.3.13.2a shall be performed between the cover contact dots or by the method described in the SCD-SCA.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","6.5.2c","Requirement","ECSS-E-ST-20-08_0090390","Failure analysis of these SCAs shall be performed by the supplier and the results provided to the customer, as part of an NRB documentation.\n    NOTE For NRB, see ECSS-Q-ST-10-09.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.3.1a","Requirement","ECSS-E-ST-20-08_0090411","Acceptance tests shall be performed on the following:\n    1. components for delivery;\n    2. components used for qualification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.3.1d","Requirement","ECSS-E-ST-20-08_0090414","The sample size shall be in conformance with Table 7-1, but it may be modified depending on the specific project requirements as stated in SCD-BSC.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.4.2.2e","Requirement","ECSS-E-ST-20-08_0090440","Facilities shall be available to safely store the qualification lot including failed samples for a minimum of 6 years (equivalent to five years in storage and one year in orbit).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.5.1.5.3b","Requirement","ECSS-E-ST-20-08_0090461","The maximum total length of missing grids, short grids or non-continuous grids shall not exceed a total length of 3 grids.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.5.6.3a","Requirement","ECSS-E-ST-20-08_0090486","For single junction solar cells, the coverglass gain-loss stated in the SCD-BSC shall be determined by using n-Amyl alcohol in order to simulate the optical properties of the adhesive. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.5.6.3d","Requirement","ECSS-E-ST-20-08_0090489","The solar cells shall be submitted to an electrical performance test before and after applying the coverglass, as defined in requirements 7.5.6.3a to 7.5.6.3c, according to clause 7.5.3 under the following test conditions:\n    1. at an illumination of 1 S.C. (AM0);\n    2. a temperature, as stated in the SCD-BSC.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.5.8.2d","Requirement","ECSS-E-ST-20-08_0090510","Any visible delamination of parts of the contacts or the anti-reflection coating shall not exceed the limits specified in clauses 7.5.1.4 and 7.5.1.5.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","7.5.15.2c","Requirement","ECSS-E-ST-20-08_0090535","After the tests, the cells shall be kept at temperatures below 50 °C until they are electrically measured.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.3.1.2b","Requirement","ECSS-E-ST-20-08_0090556","The SCD-CVG shall be prepared by the supplier in conformance with Annex D and provided to the customer for reviewing and agreement.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.3.1.3a","Requirement","ECSS-E-ST-20-08_0090559","The supplier shall ensure that the tests and inspections are performed.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.7.1.1a","Requirement","ECSS-E-ST-20-08_0090585","All the coverglasses shall be visually inspected with the naked eye to verify the requirements for defects on coverglasses in conformance with clause 8.7.1.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.7.4.3b","Requirement","ECSS-E-ST-20-08_0090606","The thickness shall be measured using a calibrated micrometer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.7.11.1.2f","Requirement","ECSS-E-ST-20-08_0090631","Water condensation on the surface of the coverglasses shall be prevented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.7.11.2.2b","Requirement","ECSS-E-ST-20-08_0090634","The chamber temperature shall then be increased from ambient temperature to 50 °C at a minimum.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","8.7.15a","Requirement","ECSS-E-ST-20-08_0090655","The coverglass breaking strength shall exceed the limits set in the SCD-CVG.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.2.2.1a","Requirement","ECSS-E-ST-20-08_0090680","Delivered integral protection diodes shall be processed and inspected in conformance with the requirements of the process identification document (PID) defined in clause 7.2, and ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.4.6a","Requirement","ECSS-E-ST-20-08_0090701","Documentation on acceptance tests shall conform to clause 9.8.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.5.2e","Requirement","ECSS-E-ST-20-08_0090708","The integral protection diodes shall be equipped with front interconnectors as step 7 in Table 7-2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.6.2.5.1b","Requirement","ECSS-E-ST-20-08_0090730","Peeling, blistering and delamination of contacts shall not be present.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.6.7.3a","Requirement","ECSS-E-ST-20-08_0090751","The uniformity of the contact thickness of the metal layers of the cell contact shall conform to the requirements of the interconnection process (as stated in the SCD-EPD) and the procurement specification of the supplier.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.6.15.2b","Requirement","ECSS-E-ST-20-08_0090776","The forward and reverse I/V characteristic of the diode shall be recorded: \n    1. in darkness\n    2. under illumination, unless it is demonstrated that the protection diode has a negligible photovoltaic response.\n    3. with a limiting power supply (to avoid destructive breakdown), and \n    4. with temperature control imposed (to avoid thermal runaway),",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.6.15.2e","Requirement","ECSS-E-ST-20-08_0090779","In case of an integral protection diode the electrical isolation of cell and diode shall be tested by measuring the current when a voltage (as stated in the SCD-BSC) is applied between the front contacts of the protection diode and of the cell at the temperatures as stated in the SCD-BSC.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","9.6.18.2e","Requirement","ECSS-E-ST-20-08_0090800","The test duration and parameter settings for each individual diode shall be as in Table 9-5 and mission requirements.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","10.1.3b","Requirement","ECSS-E-ST-20-08_0090825","For multi-source simulators used for characterizing multijunction solar cells, the relevant class of solar simulator in Table 10-4 shall be determined for each junction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","10.2.3a","Requirement","ECSS-E-ST-20-08_0090846","The following data shall be reported when using a standard cell:\n    1. Cell description (identification, type, size), \n    2. Calibration data with uncertainty budget, \n    3. calibration type, \n    4. calibration laboratory, \n    5. calibration light source class spectrum, \n    6. If primary standard and SWS have a different size, stability and uniformity, \n    7. Normalized spectral response curve, \n    8. Temperature Coefficients and calibration date.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","11.1.4.2.2a","Recommendation","ECSS-E-ST-20-08_0091094","From the capacitance measurements at several bias voltages, the following parameters of the model of capacitance should be determined with respect to the cell junction voltage and temperatures: \n    1. C0 (capacitance at 0 V), \n    2. C1 (diffusion parameter), and \n    3. F (voltage barrier at measurement temperature), ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","11.2.2.4b","Recommendation","ECSS-E-ST-20-08_0091104","The voltage determined in requirement 11.2.2.4a should be used to calculate the capacitance according to the expression and conditions specified in clause 11.2.1.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","A.2.1<8.3>e","Requirement","ECSS-E-ST-20-08_0090898","For blocking diode test, in conformance with clause 5.5.3.3.6, the SCD-PVA shall state:\n    1. The IFORWARD in A, and the VREVERSE in V, of the blocking diode.\n    2. The values for VFORWARD, in V, and IREVERSE, in A, to be obtained from the test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","B.2.1<6.8>a","Requirement","ECSS-E-ST-20-08_0090923","In case of coverglass with conductive coating, in conformance with clause 6.4.3.9, the SCD-SCA shall specify which of the two standards ISO 9211-4 or ECSS Q-ST-70-13 shall be applied",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","B.2.1<6.11>a","Requirement","ECSS-E-ST-20-08_0090926","In conformance with clause 6.4.3.13, the SCD-SCA shall describe:\n    1. The method to perform the surface conductivity test that shall be between the contact dots or an alternative one to be specified here n the SCD-SCA.\n    2. The minimum value, in W, and the maximum variation after any test, in W, of the cover conductivity before and after qualification tests of SCA of subgroup D (in conformance with Table 6-1).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","C.2.1<6.10>a","Requirement","ECSS-E-ST-20-08_0090947","In conformance with clause 7.5.6.3, the SCD-BSC shall include:\n    1. the agent used to simulate the properties of the adhesive;\n    2. the coverglass used for the test;\n    3. for the test conditions, the temperature, in °C;\n    4. for the pass-fail criteria, the maximum ISC, in %. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","D.2.1<7.2>a","Requirement","ECSS-E-ST-20-08_0090972","The SCD-CVG shall include the same provisions as for the transmission into air for qualification tests (in conformance with clause D.2.1<8.3>).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","E.2.1<1>a","Requirement","ECSS-E-ST-20-08_0090993","The SCD-EPD shall contain a description of the purpose, objective, content and the reason prompting its preparation.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","E.2.1<6>c","Requirement","ECSS-E-ST-20-08_0091000","For contact thickness, in conformance with clause 9.6.8, the SCD-EPD shall include the maximum and minimum values of the contact thickness in mm.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-08C Rev. 1","G.3.1a","Requirement","ECSS-E-ST-20-08_0091021","The DDP for SCA, BSC, CVG and protection diode shall consist of cover sheet or sheets, including as a minimum the following:\n    1. reference to the corresponding SCD, including issue and date;\n    2. reference to this Standard, including issue and date; \n    3. component type (for SCDs, BSCs, coverglasses and protection diodes); \n    4. procurement SCA, BSC, CVG and protection diode identification; \n    5. manufacturing SCA, BSC, CVG and protection diode identification; \n    6. number of purchase order or contract; \n    7. deviations from, or additions to, the corresponding SCD and this Standard, if so specified in the order; \n    8. manufacturer’s name and address; \n    9. location of the manufacturing plant; \n    10. signature on behalf of the manufacturer; \n    11. total number of pages of the data package. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","4.2.6b","Requirement","ECSS-E-ST-20-07_0080013","When specifying limits and frequency ranges, the following issues shall be included:\n    1. sensitivity of possible victim receiver subsystems including out-of-band response,\n    2. no limits apply to transmit frequencies and information carrying modulation bandwidths,\n    3. highest and lowest intentional frequency used by space system receivers,\n    4. antenna port attachments, gain/loss characteristics.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","4.2.13.2a","Requirement","ECSS-E-ST-20-07_0080038","Cable shields shall not be used as an intentional current carrying conductor, except coaxial cables in radiofrequency circuits and high-speed data links using coaxial cables.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","4.2.13.2d","Requirement","ECSS-E-ST-20-07_0080041","Bonding of cable shields shall be as following:\n    1. Bonding to chassis ground is performed at both ends:\n        (a) through the equipment connector body,\n        (b) using a backshell that provides for circumferential bonding of shields, or using a halo-ring.\n            NOTE No grounding inside the equipment through a connector ground pin in order to prevent any perturbation inside the equipment.\n    2. Connection to electrical reference is performed through dedicated pins.\n        NOTE This case typically appears in the design of detection chains.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.2.4c","Requirement","ECSS-E-ST-20-07_0080066","The LISNs shall be located at the power source end of the exposed length of power leads specified in 5.2.6.6.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.2.6.6.2a","Requirement","ECSS-E-ST-20-07_0080087","Individual leads shall be grouped into cables in the same manner as in the actual installation.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.2.7.1c","Requirement","ECSS-E-ST-20-07_0080108","When the EUT has several available modes (including software controlled operational modes), the number of modes to be tested for emission and susceptibility shall be such that all circuitry is evaluated. \n    NOTE It is expected that the customer defines or agrees operating modes.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.2.8.3a","Requirement","ECSS-E-ST-20-07_0080115","When current measurements are performed on the central line of a coaxial transmission line a transmission line with 50 W characteristic impedance, coaxial connections on both ends, and space for an injection probe around the centre conductor shall be used for calibration.\n    NOTE Figure 5-4 represents an arrangement described in MIL-STD-461E.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.2.10.1c","Requirement","ECSS-E-ST-20-07_0080136","Step sizes shall be decreased such to permit observation of a response.\n    NOTE For receivers, it can make use of the frequency plan to adjust the number of points.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.3.3d","Requirement","ECSS-E-ST-20-07_0080238","The EMISM between the launch system RF emissions and the spacecraft RF receivers’ damage threshold shall be verified.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.4.5.2b","Requirement","ECSS-E-ST-20-07_0080180","A right-handed orthogonal coordinate system XYZ shall be assigned to the EUT geometric centre. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.4.5.2e","Requirement","ECSS-E-ST-20-07_0080183","The magnetic field shall be positive when orientated from the centre of the EUT towards the magnetometer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.4.9.2a","Requirement","ECSS-E-ST-20-07_0080208","The test equipment shall be as follows:\n    1. Spike generator with following characteristics:\n        (a) Pulse width of 10 µs and 0,15 µs,\n        (b) Pulse repetition rate capability up to 10 pulses per second,\n        (c) Voltage output as required, positive then negative,\n        (d) Output control,\n        (e) Adequate transformer current capacity commensurate with line being tested,\n        (f) Output impedance 5 W or less for 0,15 µs and 1 W or less for 10µs transient,\n        (g) External synchronization and triggering capability.\n    2. Oscilloscope with 50 MHz bandwidth or greater.\n    3. Differential high-voltage probe.\n    4. Isolation transformer.\n    5. 5 W resistor power metal film resistor with inductance lower 100 nH and peak power capability.\n    6. LISN defined in 5.2.4, with added inductor for a total inductance not less than 20 µH for parallel injection.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-07C Rev. 1","5.4.12.3a","Requirement","ECSS-E-ST-20-07_0080229","The test setup shall be as follows:\n    1. Maintain a basic test setup for the EUT as specified in 5.2.6. and Figure 5-3.\n        NOTE It is important at this point to assess the test area for potential high-voltage hazards and take necessary precautionary steps to assure safety of test personnel.\n    2. When using an ESD generator as a high-voltage power supply as shown Figure 5-30 or Figure 5-31, it is set in the contact discharge mode.\n    3. Connect the high-voltage electrode to the discharge circuit at the node between the spark gap and the capacitor.\n    4. The discharge circuit length is not larger than what is necessary to place in series the 20 cm long coupling wire, the damping resistor, the discharge capacitor, the spark gap and the current probe.\n        NOTE It is important to ensure that the discharge loop is as small as possible for achieving the transient pulse duration objective defined in 5.4.12.4a.2(d).\n    5. For calibration the test equipment is configured as shown Figure 5-30, and meeting following provisions:\n        (a) the discharge circuit is not coupled to the EUT,\n        (b) choke resistors are near the capacitor,\n        (c) the current probe monitoring the primary current from the ESD source is near the damping resistor, at the capacitor side,\n        (d) the high voltage probe is measuring the voltage across the capacitor, grounded at the damping resistor side.\n            NOTE The high-voltage probe is not meant to measure the voltage during the discharge but the voltage reached before discharge\n    6. Test the EUT by configuring the test equipment as specified in Figure 5-31 and meeting the following provisions:\n        (a) the high voltage probe used for calibration is removed,\n        (b) the EUT is mounted on a conductive ground plane using the space vehicle mount and attach points, and operated using the actual electrical harness, or an EMC test harness of identical construction to the actual harness.\n            NOTE It is preferable to use the actual electrical harness.\n        (c) the discharge circuit is supported 5 cm above the ground plane by a non-conductive standoff with high-voltage insulation capability,\n        (d) from calibration, the discharge circuit is kept unchanged in size and shape, and tightly electromagnetically coupled 20 cm along an EUT bundle, held by dielectric bonds\n            NOTE A maximum separation distance of 1 cm between the injection wire and the outer circumference of the bundle under test is a condition for achieving a tight electromagnetic coupling.\n        (e) a current probe is monitoring the primary current from the ESD source near the damping resistor,\n        (f) a current probe is monitoring the current in the EUT harness, 5 cm from the EUT connector.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","5.2.1.4a","Requirement","ECSS-E-ST-50-15_1270019","All data cables shall use shielded twisted-pair cables.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","5.2.2.2b","Requirement","ECSS-E-ST-50-15_1270026","Receptacles shall be equipped with male contacts.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","5.3.3.2.3g","Requirement","ECSS-E-ST-50-15_1270040","If CAN_H shorted to ground, upon fault removal the CAN network shall resume communication with no ill effects to CAN nodes.","NOTE\tIf CAN_H is shorted to ground the CAN network cannot communicate.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","5.6.2b","Recommendation","ECSS-E-ST-50-15_1270254","The indication of Error Active and Error Passive should be provided to the application. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","6.9d","Requirement","ECSS-E-ST-50-15_1270083","Only one device within the network shall act as SYNC producer by issuing periodically the SYNC object.","NOTE\tBus redundancy management uses SYNC object exchange as described in 8.3.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","6.10b","Requirement","ECSS-E-ST-50-15_1270086","COB-IDs restricted for a specific purpose in CANopen shall not be used other than for that particular purpose.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","7.1.2f","Requirement","ECSS-E-ST-50-15_1270107","The Local SCET Set and Local SCET Get objects shall be mapped into the CAN frame according to Figure 7-1.","NOTE\tIt is up to the designer to decide the implemented size of the Fine Time counter in a particular device.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","7.2.3h","Requirement","ECSS-E-ST-50-15_1270134","Each Time consumer shall map the Local SCET Get object (7.1.2) or the Local UTC Get object (7.1.3) to a dedicated Local Time PDO transmit PDO.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","8.3.3g","Requirement","ECSS-E-ST-50-15_1270157","When an NMT message is detected on a particular bus, the slave shall consider that bus the active one. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","9.1b","Requirement","ECSS-E-ST-50-15_1270164","Slave node address ID(6).. ID(0) assigned to each node shall conform to clause 10 of this document.","NOTE\tNODE-ID 0 is used to broadcast all nodes in the network. It does not use it.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","9.4.7.1a","Requirement","ECSS-E-ST-50-15_1270193","Slaves shall not produce or consume Time Stamp messages. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-15C","10.3.2a","Requirement","ECSS-E-ST-50-15_1270224","The connector shall be compliant to specification: MIL-C D38999 Series 3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-24C","5.1e","Requirement","ECSS-E-ST-10-24_1290004","The interface management plan shall define at least the:\n1.\tapplicability domain,\n2.\tmanagement logic, \n3.\tresponsibility and approval authorities, \n4.\tinterface consolidation approach and life cycle, \n5.\tschedule,\n6.\tdocumentation tree,\n7.\tinternal documentation organization approach (contractual, discipline or product decomposition), and\n8.\tchange management approach.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-24C","5.2c","Requirement","ECSS-E-ST-10-24_1290007","For each interface identified in the list of 5.2b, the following shall be provided:\n1.\tinvolved interface ends, \n2.\tcontractual responsibilities, \n3.\ttechnical documentation and their version specifying and defining the interface. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-24C","5.6f","Requirement","ECSS-E-ST-10-24_1290032","If validation is included, the customer and suppliers shall agree on the interface validation approach.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-24C","B.2.1<2>b","Requirement","ECSS-E-ST-10-24_1290052","The document approval authority (including change approval authority) shall be defined. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-24C","C.2.2<1>a","Permission","ECSS-E-ST-10-24_1290075","The IDD may take different forms depending on the kind of interface end it documents.","NOTE \tExamples of different forms are: a mechanical drawing, interface 3D CAD model, electrical circuit schematic, software API, software architectural or detailed design document.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.2.1.1.1b","Requirement","ECSS-E-ST-20-20_1320010","The HLCL class shall be selected among one shown in Table 3-3 and comply with related class performance.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.2.7.6.1a","Requirement","ECSS-E-ST-20-20_1320029","Requirement 5.2.7.5.1a shall apply both in case of the LCL/HLCL being commanded ON by telecommand and when the bus voltage rises for the RLCL.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.2.14.2.1a","Requirement","ECSS-E-ST-20-20_1320048","In case the LCL/RLCL/HLCL switch fails in a dissipative failure and in case the \"on board system\" removes the failure by reducing the load or commanding OFF an additional switch, all the surrounding components shall be within rating during the on board system reaction time.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.4.1.1.1b","Requirement","ECSS-E-ST-20-20_1320068","The worst case overload condition applied for the verification shall be a sudden short-circuit applied at the LCL Distribution Unit connector interface.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.4.1.1.1e","Requirement","ECSS-E-ST-20-20_1320071","The maximum LCL/RLCL input overshoot charge due to any overload shall be limited to 1 mC maximum.","NOTE \tRefer to Figure 3-1 and/or Figure 3-2.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.4.6.1.1a","Requirement","ECSS-E-ST-20-20_1320096","Minimum phase margin for LCL/RLCL/HLCL shall be 50°, under the following conditions:\n1.\ta zero Ohm impedance load is applied, and\n2.\tthe DC voltage across the LCL/RLCL/HLCL equals (4 ±1) V.","NOTE \tThe zero Ohm impedance is implemented by a voltage source with current sink capability.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-20C","5.5.4.1.1a","Requirement","ECSS-E-ST-20-20_1320116","In case of an LCL/RLCL failure causing a sudden application of nominal voltage to the load, the relevant peak current shall be lower than 20 A or 5 times the class current, whichever is greater.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.3.2a","Requirement","ECSS-E-ST-70-41_1330005","Each service type shall define at least one subservice type.","NOTE\tThis Standard introduces the concept of subservices that group and isolate the functions of a service.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.3.3.3a","Requirement","ECSS-E-ST-70-41_1330026","Each report type shall either be:\n1.\ta data report type,\n2.\ta verification report type, or\n3.\tan event report type.","NOTE 1\tFor item 1, an example of a data report type is the housekeeping parameter report type specified in clause 6.3.3.3. \nNOTE 2\tFor item 2:\n·\tthe verification report types are those specified in clause 6.1, i.e. the request verification service type.\n·\tthe verification reports are used in the request related transactions, refer to clause 5.3.5.2.\nNOTE 3\tFor item 3, the event report types are those specified in clause 6.5.4, see also clause 5.3.5.4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.3.5.2.3i","Requirement","ECSS-E-ST-70-41_1330047","For each instruction type, the functionality that the subservice performs when executing an instruction of that type shall be declared when specifying that instruction type.","NOTE\tAn example of such subservice functionality can be found in 6.3.5.6.1i.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.4.3.3.1e","Requirement","ECSS-E-ST-70-41_1330072","For each on-board memory, whether scrubbing that memory is supported shall be declared when specifying that memory.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.4.7.1b","Requirement","ECSS-E-ST-70-41_1330093","Each subservice shall belong to exactly one service.","NOTE\tThe type of a subservice is one of the subservice types defined for the related service type.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.4.7.2.1c","Requirement","ECSS-E-ST-70-41_1330096","Each subservice entity shall be either a subservice user or a subservice provider.","NOTE\tA subservice entity is identified by the subservice that it belongs to and the application process that hosts it.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","5.4.11.3.3a","Requirement","ECSS-E-ST-70-41_1330121","For each data report that can be generated in an autonomous data reporting transaction, the destination of the data report in that case shall be declared when specifying the related subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.1.4.2c","Requirement","ECSS-E-ST-70-41_1330141","Each successful acceptance notification shall contain:\n1.\tthe identifier of the request that successfully passed the acceptance verification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.1.4.3f","Requirement","ECSS-E-ST-70-41_1330148","For each request that fails its acceptance verification, the acceptance and reporting subservice shall:\n1.\tgenerate a single failed acceptance notification and associated report for that request;\n2.\tdiscard that request.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.2.4.2c","Requirement","ECSS-E-ST-70-41_1330169","Each instruction to distribute an on/off device command shall contain:\n1.\tthe device address.","NOTE\tFor item 1, refer to requirement 6.2.4.1b.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.2.5.3f","Requirement","ECSS-E-ST-70-41_1330190","The device access subservice shall process any valid instruction that is contained within a request to distribute register dump commands regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.2.7.1.3f","Requirement","ECSS-E-ST-70-41_1330216","For each request to acquire data from physical devices that contains only valid instructions, the device access subservice shall execute those instructions in the order of their appearance in that request.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.2.7.2.3i","Requirement","ECSS-E-ST-70-41_1330237","For each request to acquire data from logical devices that results in at least one data acquisition failure, the device access subservice shall generate a single failed completion of execution verification report that includes the first failed progress of execution notification generated for that request.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.3.1a","Requirement","ECSS-E-ST-70-41_1330244","The housekeeping reporting subservice shall be able to collect and report the sampled values of each on-board parameter that is accessible to the application process that hosts that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.3.4.2e","Requirement","ECSS-E-ST-70-41_1330265","For each instruction to disable the periodic generation of a housekeeping parameter report that it rejects, the housekeeping reporting subservice shall generate the failed start of execution notification for that instruction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.3.6f","Requirement","ECSS-E-ST-70-41_1330286","The housekeeping reporting subservice shall process any valid instruction that is contained within a request to report housekeeping parameter report structures regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.3.7f","Requirement","ECSS-E-ST-70-41_1330293","The housekeeping reporting subservice shall process any valid instruction that is contained within a request to generate a one shot report for housekeeping parameter report structures regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.3.10g","Requirement","ECSS-E-ST-70-41_1330314","For each valid instruction to report the periodic generation properties of a housekeeping parameter report structure, the housekeeping reporting subservice shall generate a single housekeeping parameter report periodic generation properties notification that includes:\n1.\tthe housekeeping parameter report structure identifier;\n2.\tthe related periodic generation action status;\n3.\tthe related collection interval.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.4.5c","Requirement","ECSS-E-ST-70-41_1330335","Each instruction to disable the periodic generation of a diagnostic parameter report shall contain:\n1.\tthe diagnostic parameter report structure identifier to disable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.4.9a","Requirement","ECSS-E-ST-70-41_1330360","The diagnostic reporting subservice capability to generate a one shot report for diagnostic parameter report structures shall be declared when specifying that subservice.","NOTE\tThe corresponding requests are of message type \"TC[3,28] generate a one shot report for diagnostic parameter report structures\". The responses, one for each instruction, are data reports of message type \"TM[3,26] diagnostic parameter report\".\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.4.12b","Requirement","ECSS-E-ST-70-41_1330381","Each request to report the periodic generation properties of diagnostic parameter report structures shall contain one or more instructions to report the periodic generation properties of a diagnostic parameter report structure.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.5.1a","Requirement","ECSS-E-ST-70-41_1330388","The parameter functional reporting configuration subservice shall be able to control the generation of each housekeeping parameter report generated by the housekeeping reporting subservices of the parent housekeeping service.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.5.4.2a","Requirement","ECSS-E-ST-70-41_1330409","The parameter functional reporting configuration subservice shall provide the capability to delete parameter functional reporting definitions if the capability to create a parameter functional reporting definition is provided by that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[3,39] delete parameter functional reporting definitions\".\nNOTE 2\tFor the capability to create a parameter functional reporting definition, refer to clause 6.3.5.4.1.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.5.6.1h","Requirement","ECSS-E-ST-70-41_1330430","The parameter functional reporting configuration subservice shall process any valid instruction that is contained within a request to add parameter report definitions to a parameter functional reporting definition regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.3.5.6.2f","Requirement","ECSS-E-ST-70-41_1330437","The parameter functional reporting configuration subservice shall reject any instruction to remove a parameter report definition from a parameter functional reporting definition if:\n1.\tthat instruction refers to a parameter report definition that is not in that parameter functional reporting definition.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.4.3.3a","Requirement","ECSS-E-ST-70-41_1330458","For each parameter that statistics are evaluated, the default sampling interval that the parameter statistics reporting subservice uses for that parameter shall be declared when specifying that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.4.6.2b","Requirement","ECSS-E-ST-70-41_1330479","Each request to enable the periodic parameter statistics reporting shall contain exactly one instruction to enable the periodic parameter statistics reporting.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.4.7.2h","Requirement","ECSS-E-ST-70-41_1330504","For each valid instruction to delete all parameter statistics definitions, the parameter statistics reporting subservice shall:\n1.\tremove all parameter statistics definitions from the list of evaluated parameters, if any.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.5.5.2c","Requirement","ECSS-E-ST-70-41_1330525","Each instruction to enable the report generation of an event definition shall contain:\n1.\tthe event definition identifier of the event definition to enable.","NOTE\tFor the event definition identifier, refer to requirement 6.5.3b.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.5.5.3c","Requirement","ECSS-E-ST-70-41_1330532","Each instruction to disable the report generation of an event definition shall contain:\n1.\tthe event definition identifier of the event definition to disable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.3.2d","Requirement","ECSS-E-ST-70-41_1330553","For each writeable memory that it manages, whether the raw data memory management subservice has write access to that memory shall be declared when specifying that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.3.4a","Requirement","ECSS-E-ST-70-41_1330574","The raw data memory management subservice shall provide the capability to dump raw memory data.","NOTE\tThe corresponding requests are of message type \"TC[6,5] dump raw memory data\". The responses are data reports of message type \"TM[6,6] dumped raw memory data report\".\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.3.4h","Requirement","ECSS-E-ST-70-41_1330581","The raw data memory management subservice shall process any valid instruction that is contained within a request to dump raw memory data regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.3.6i","Requirement","ECSS-E-ST-70-41_1330602","If an error occurs during the writing to memory of the data related to an instruction to load a raw memory data area by reference, the raw data memory management subservice shall:\n1.\timmediately abort the execution of the related request;\n2.\tgenerate a failed execution notification for that instruction.","NOTE\tFor example, an error can occur when the memory becomes write-protected by hardware during the course of the load operation.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.4.4e","Requirement","ECSS-E-ST-70-41_1330627","The structured data memory management subservice shall reject any request to load object memory data if any of the following conditions occurs:\n1.\tthat request refers to a memory identifier that is unknown;\n2.\tthe subservice does not have write access to the memory referred to in that request;\n3.\tthat request refers to a memory that is write protected;\n4.\tthat request refers to a memory object that is write protected;\n5.\tthe base identifier in that request refers to a memory object that is unknown;\n6.\tthat request contains an instruction that refers to an offset that exceeds the maximum memory size of the memory object identified by the base identifier;\n7.\tloading the data contained in any related instruction exceeds the maximum memory size of the memory object identified by the base identifier;\n8.\tthe size of the data contained within any of the related instruction is not a multiple of the memory access alignment constraint.","NOTE\tThe checking of instructions that follow a faulty instruction is optional. For some failures, e.g., the variable octet-string size of the data does not comply with the actual data, any processing of the remaining instructions in the request does not make sense.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.4.6e","Requirement","ECSS-E-ST-70-41_1330648","Each instruction to check an object memory data shall contain:\n1.\tthe byte offset within the memory object identified by the base identifier;\n2.\tthe octet length of the memory area to check.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.4.8i","Requirement","ECSS-E-ST-70-41_1330669","If an error occurs during the writing to memory of the data related to an instruction to load an object memory data area by reference, the structured data memory management subservice shall:\n1.\timmediately abort the execution of the related request;\n2.\tgenerate a failed execution notification for that instruction.","NOTE\tFor example, an error can occur when the memory becomes write-protected by hardware during the course of the load operation.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.4.9e","Requirement","ECSS-E-ST-70-41_1330676","Each instruction to dump an object memory data area to file shall contain:\n1.\tthe byte offset within the memory object identified by the base identifier;\n2.\tthe octet length of the memory area to dump.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.6.6.1.5b","Requirement","ECSS-E-ST-70-41_1330697","Each request to disable the scrubbing of a memory shall contain exactly one instruction to disable the scrubbing of a memory.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.8.2.1.1a","Requirement","ECSS-E-ST-70-41_1330718","Each function management service shall contain at least one function management subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.9.2.1a","Requirement","ECSS-E-ST-70-41_1330729","Each spacecraft shall contain exactly one time management service.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.9.4.2c","Requirement","ECSS-E-ST-70-41_1330747","If the time reporting subservice does not include the P-field in the CUC time reports, the implicit P-field value shall be declared when specifying that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.4.2a","Requirement","ECSS-E-ST-70-41_1330772","Each scheduled activity definition shall consist of:\n1.\tthe request;\n2.\tthe release time of that request;\n3.\tif sub-schedules are supported, the identifier of the sub-schedule to which that scheduled activity is associated;\n4.\tif groups are supported, the identifier of the group to which that scheduled activity is associated.","NOTE 1\tFor item 3, refer to requirement 6.11.4.1a.\nNOTE 2\tFor item 4, refer requirement 6.11.4.1b.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.4.5f","Requirement","ECSS-E-ST-70-41_1330793","The list of verification checks that the time-based scheduling subservice shall perform on the requests associated to the new scheduled activities shall be declared when specifying that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.5.2.2c","Requirement","ECSS-E-ST-70-41_1330814","Each instruction to disable a time-based sub-schedule shall contain:\n1.\tthe identifier of the sub-schedule to disable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.5.2.3b","Requirement","ECSS-E-ST-70-41_1330821","Each request to report the status of each time-based sub-schedule shall contain exactly one instruction to report the status of each time-based sub-schedule.","NOTE\tThe instructions to report the status of each time-based sub-schedule contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.6.3.1b","Requirement","ECSS-E-ST-70-41_1330842","Each request to enable time-based scheduling groups shall contain:\n1.\tone or more instructions to enable a time-based scheduling group, or\n2.\texactly one instruction to enable all time-based scheduling groups.","NOTE\tThe instructions to enable all time-based scheduling groups contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.7.1c","Requirement","ECSS-E-ST-70-41_1330863","The notifications contained in a time-based schedule summary report shall be ordered according to the release time of the reported scheduled activities.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.8.1d","Requirement","ECSS-E-ST-70-41_1330870","The time-based scheduling subservice shall reject any request to time-shift all scheduled activities if:\n1.\tthe time obtained by adding the time offset to the release time of the earliest activity contained within the time-based schedule is earlier than the time obtained by adding the time-based schedule time margin to the current time.","NOTE\tIf the time offset is sufficient to result in a scheduled activity with a release time in the past or with a release time that is too close to the current time, that instruction is rejected and no activities are time-shifted.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.9.3c","Requirement","ECSS-E-ST-70-41_1330891","The time-based scheduling subservice shall reject any request to time-shift scheduled activities identified by request identifier if:\n1.\tthe time obtained by adding the time offset to the release time of the earliest activity identified by an instruction in the request is earlier than the time obtained by adding the time-based schedule time margin to the current time.","NOTE\tIf the time offset is sufficient to result in a scheduled activity with a release time in the past or with a release time that is too close to the current time, that request is rejected and no activities are time-shifted.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.10.2.2b","Requirement","ECSS-E-ST-70-41_1330916","The set of scheduled activities identified by the \"select all activities scheduled from time tag to time tag\" filtering mechanism shall be all activities that are scheduled between and including the specified \"from time tag\" and \"to time tag\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.11.10.5d","Requirement","ECSS-E-ST-70-41_1330937","The time-based scheduling subservice shall reject any request to summary-report the time-based scheduled activities identified by a filter if any of the following conditions occurs:\n1.\tthat request contains an instruction that refers to an invalid time window type;\n2.\tthat request contains an instruction that refers to a \"from time tag\" that is greater than a \"to time tag\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.2.2a","Permission","ECSS-E-ST-70-41_1333510","The parameter monitoring subservice may support the evaluation of the delta-check type.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.3e","Requirement","ECSS-E-ST-70-41_1330964","If the parameter monitoring subservice uses a subservice-specific monitoring interval, that monitoring interval shall be declared when specifying that subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.6.1d","Requirement","ECSS-E-ST-70-41_1330985","The parameter monitoring subservice shall reject any instruction to enable a parameter monitoring definition if any of the following conditions occurs:\n1.\tthat instruction refers to a parameter monitoring definition identifier that is not in the PMON list;\n2.\tthat instruction refers to a parameter monitoring definition that is used by a protected functional monitoring definition.","NOTE\tFor item 2, the existence of protected functional monitoring definitions depends on the presence of a functional monitoring subservice with support for protecting functional monitoring definitions. See also clause 6.12.4.6.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.8b","Requirement","ECSS-E-ST-70-41_1331010","Each request to change the maximum transition reporting delay shall contain exactly one instruction to change the maximum transition reporting delay.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.9.1a","Requirement","ECSS-E-ST-70-41_1331013","The parameter monitoring subservice capability to add parameter monitoring definitions shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[12,5] add parameter monitoring definitions\".\nNOTE 2\tFor the capability to delete all parameter monitoring definitions, refer to clause 6.12.3.9.2.\nNOTE 3\tFor the capability to delete parameter monitoring definitions, refer to clause 6.12.3.9.3.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.9.4b","Requirement","ECSS-E-ST-70-41_1331034","Each request to modify parameter monitoring definitions shall contain one or more instructions to modify a parameter monitoring definition.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.3.12g","Requirement","ECSS-E-ST-70-41_1331059","For each valid request to report the out-of-limits, the parameter monitoring subservice shall generate a single out-of-limits report that includes all related out-of-limit notifications.","NOTE\tFollowing the generation of an out-of-limits report, the reported transitions are not removed from the check transition list. The transitions are removed when they are reported in a check transition report, see clause 6.12.3.7.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.4.5.1a","Requirement","ECSS-E-ST-70-41_1331080","For each functional monitoring definition, whenever a new PMON checking status has been established for one of its parameter monitoring definitions, the functional monitoring subservice shall perform the following:\n1.\tIf the FMON function status is \"enabled\" and the FMON status is \"enabled\" and the current FMON checking status is not \"failed\":\n(a)\tthe check validity condition, if any, is computed;\n(b)\tIf the computed check validity condition yields false, the FMON checking status is set to \"invalid\".\n2.\tIf the FMON function status is \"enabled\", the FMON status is \"enabled\" and the current FMON checking status is neither \"failed\" nor \"invalid\":\n(a)\tcheck if the number of related parameter monitoring definitions that are contemporaneously in violation equals or exceeds the minimum PMON failing number;\n(b)\tif the check yields true, the FMON checking status is set to \"failed\" and the associated event is raised;\n(c)\tif the check yields false, the FMON checking status is set to \"running\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.4.6.1g","Requirement","ECSS-E-ST-70-41_1331101","For each valid instruction to protect a functional monitoring definition, the functional monitoring subservice shall:\n1.\tset the FMON protection status of the functional monitoring definition to \"protected\".","NOTE\tWhen a functional monitoring definition is protected, it cannot be deleted and it prevents the enabling, disabling or modifying of any parameter monitoring definition that is used in that functional monitoring definition. See clauses 6.12.4.7.2, 6.12.3.6.1, 6.12.3.6.2 and 6.12.3.9.4. \n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.4.6.2g","Requirement","ECSS-E-ST-70-41_1331108","For each valid instruction to unprotect a functional monitoring definition, the functional monitoring subservice shall:\n1.\tset the FMON protection status of the functional monitoring definition to \"unprotected\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.12.4.8e","Requirement","ECSS-E-ST-70-41_1331129","For each instruction to report a functional monitoring definition that it rejects, the functional monitoring subservice shall generate the failed start of execution notification for that instruction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.13.3.3.2b","Requirement","ECSS-E-ST-70-41_1331154","The receiving entity of the large packet downlink subservice shall initiate the downlink operation when it receives the first part report of the large packet.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.13.3.3.2e","Requirement","ECSS-E-ST-70-41_1331157","The receiving entity of the large packet downlink subservice shall end the downlink operation when the last part report of the large packet has been successfully received.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.13.4.3.2i","Requirement","ECSS-E-ST-70-41_1331178","For each large packet uplink that is aborted, the receiving entity of the large packet uplink subservice shall:\n1.\tgenerate a single large packet uplink abortion notification that includes the reason of that abortion;\n2.\tdiscard that large packet and the related uplink part requests.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.2.5c","Requirement","ECSS-E-ST-70-41_1331203","The maximum number of event definition identifiers that can be contained within an event report blocking forward-control definition shall be declared when specifying that real-time forwarding control subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.4.1l","Requirement","ECSS-E-ST-70-41_1331224","For each valid instruction to add all report types of a service type to the application process forward-control configuration, the real-time forwarding control subservice shall:\n1.\tadd, for the specified application process identifier, an application process forward-control definition if not already existing;\n2.\tadd, for the related application process forward-control definition and the specified service type identifier, a service type forward-control definition to the related application process forward-control definition, if not already existing;\n3.\tdelete, if any, all report type forward-control definitions of the related service type forward-control definition.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.4.2f","Requirement","ECSS-E-ST-70-41_1331231","Each instruction to delete a service type from the application process forward-control configuration shall contain:\n1.\tthe application process identifier addressed by that instruction,\n2.\tthe service type identifier. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.5.2e","Requirement","ECSS-E-ST-70-41_1331260","For each instruction to delete a structure identifier from the housekeeping parameter report forward-control configuration that it rejects, the real-time forwarding control subservice shall generate the failed start of execution notification for that instruction. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.6.1c","Requirement","ECSS-E-ST-70-41_1331274","Each instruction to add a structure identifier to the diagnostic parameter report forward-control configuration shall contain:\n1.\tthe application process identifier addressed by that instruction;\n2.\tthe diagnostic parameter report structure identifier;\n3.\tif subsampling is supported, the subsampling rate.","NOTE\tFor item 3, refer to requirement 6.14.3.2.1d.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.7.1b","Requirement","ECSS-E-ST-70-41_1331299","Each request to delete event definition identifiers from the event report blocking forward-control configuration shall include exactly one of:\n1.\tany combination of one or more instructions:\n(a)\tto delete an event definition identifier from the event report blocking forward-control configuration,\n(b)\tto delete an application process from the event report blocking forward-control configuration;\n2.\tan instruction to empty the event report blocking forward-control configuration.","NOTE\tThe instructions to empty the event report blocking forward-control configuration contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.7.1e","Requirement","ECSS-E-ST-70-41_1331302","For each instruction to delete an event definition identifier from the event report blocking forward-control configuration that it rejects, the real-time forwarding control subservice shall generate the failed start of execution notification for that instruction. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.14.3.7.3d","Requirement","ECSS-E-ST-70-41_1331323","For each valid request to report the content of the event report blocking forward-control configuration, the real-time forwarding control subservice shall generate a single event report blocking forward-control configuration content report that includes all related event report blocking forward-control definition notifications.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.3.2d","Requirement","ECSS-E-ST-70-41_1331348","The storage and retrieval subservice shall reject any instruction to enable the storage function of a packet store if:\n1.\tthat instruction refers to a packet store that does not exist.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.4.2f","Requirement","ECSS-E-ST-70-41_1331369","The storage and retrieval subservice shall reject any instruction to change the open retrieval start time tag of a packet store if any of the following conditions occurs:\n1.\tthat instruction refers to a packet store that does not exist;\n2.\tthe packet store open retrieval status of that packet store is in-progress.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.4.3c","Requirement","ECSS-E-ST-70-41_1331376","Each instruction to resume the open retrieval of a packet store shall contain:\n1.\tthe identifier of the packet store;\n2.\tif the storage and retrieval subservice supports prioritizing the packet retrievals from packet stores, the retrieval priority.","NOTE\tFor item 2, refer to requirements 6.15.3.1m and 6.15.3.1n.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.5.2e","Requirement","ECSS-E-ST-70-41_1331397","For each instruction to start the by-time-range retrieval of a packet store that it rejects, the storage and retrieval subservice shall generate the failed start of execution notification for that instruction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.7.1g","Requirement","ECSS-E-ST-70-41_1331418","For each valid instruction to delete the content of a packet store up to the specified time, the storage and retrieval subservice shall:\n1.\tdelete the contents of the packet store specified in that instruction, from the earliest packet in that store up to and including the last packet with a time stamp less than or equal to the time specified in that request.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.8.4c","Requirement","ECSS-E-ST-70-41_1331443","Each instruction to copy the packets contained in a packet store selected by time window shall contain:\n1.\tthe time window;\n2.\tthe source packet store identifier;\n3.\tthe destination packet store identifier.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.8.4f","Requirement","ECSS-E-ST-70-41_1331446","The set of packets identified by the \"select all packets stored after time tag\" filtering mechanism shall be all packets that are stored at and after that specified \"from time tag\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.3.9.3d","Requirement","ECSS-E-ST-70-41_1331467","The storage and retrieval subservice shall reject any request to change a packet store type to bounded if any of the following conditions occurs:\n1.\tthat request contains an instruction that refers to a packet store that does not exist;\n2.\tthat request contains an instruction that refers to a packet store whose packet store storage status is \"enabled\";\n3.\tthat request contains an instruction that refers to a packet store whose packet store by-time-range retrieval status is \"enabled\";\n4.\tthat request contains an instruction that refers to a packet store whose packet store open retrieval status is \"in-progress\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.2.1d","Requirement","ECSS-E-ST-70-41_1331492","If the packet selection subservice provides the capability to control, per housekeeping parameter report structure, the storage of housekeeping parameter reports or the capability to control, per diagnostic parameter report structure, the storage of diagnostic parameter reports, the subservice capability to subsample the storage of the parameter reports shall be declared when specifying that subservice.","NOTE\tRefer to requirements 6.15.4.2.1a and 6.15.4.2.1b. \n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.3h","Requirement","ECSS-E-ST-70-41_1331513","If the packet selection subservice provides the capability to control, per event definition, the storage of event reports, the subservice shall block the storage of an event report to a packet store if that report fulfils all of the following conditions:\n1.\tthe application process identifier of that report is contained within an event report blocking storage-control definition for that packet store, and\n2.\tthat event report blocking storage-control definition has no event definition identifier.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.4.1f","Requirement","ECSS-E-ST-70-41_1331520","Each instruction to add all report types of a service type to the application process storage-control configuration shall contain:\n1.\tif the packet selection subservice controls more than one application process, the application process identifier addressed by that instruction,\n2.\tthe service type identifier. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.4.2l","Requirement","ECSS-E-ST-70-41_1331541","The packet selection subservice shall reject any instruction to delete an application process from the application process storage-control configuration if:\n1.\tthat instruction refers to an application process identifier that is not in the application process storage-control configuration.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.5.1h","Requirement","ECSS-E-ST-70-41_1331562","For each instruction contained within a request to add structure identifiers to the housekeeping parameter report storage-control configuration that it rejects, the packet selection subservice shall generate the failed start of execution notification for that instruction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.6.1d","Requirement","ECSS-E-ST-70-41_1331587","Each instruction to add a structure identifier to the diagnostic parameter report storage-control configuration shall contain:\n1.\tif the packet selection subservice controls more than one application process, the application process identifier addressed by that instruction;\n2.\tthe diagnostic parameter report structure identifier;\n3.\tif subsampling is supported, the subsampling rate.","NOTE 1\tFor item 1, refer to requirement 6.15.4.1.1a.\nNOTE 2\tFor item 3, refer to requirement 6.15.4.2.1d.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.6.1g","Requirement","ECSS-E-ST-70-41_1331590","The packet selection subservice shall reject any instruction to add a structure identifier to the diagnostic parameter report storage-control configuration if:\n1.\tthe maximum number of diagnostic parameter report structure identifiers that can be contained within a diagnostic parameter report storage-control definition is already reached;\n2.\tthe corresponding diagnostic parameter report storage-control definition has no structure identifier already defined.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.7.1c","Requirement","ECSS-E-ST-70-41_1331615","The packet selection subservice shall reject any request to add event definition identifiers to the event report blocking-control configuration if:\n1.\tthat request refers to a packet store that does not exist.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.15.4.7.3a","Requirement","ECSS-E-ST-70-41_1331636","The packet selection subservice capability to report the content of the event report blocking storage-control configuration of a packet store shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[15,39] report the content of the event report blocking storage-control configuration\". The responses are data reports of message type \"TM[15,40] event report blocking storage-control configuration content report\".\nNOTE 1\tThat capability requires the capability for that subservice to control, per event definition, the storage of event reports, refer to requirement 6.15.4.2.1c.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.2.1.1a","Requirement","ECSS-E-ST-70-41_1331657","Each on-board control procedure service shall contain exactly one OBCP management subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.3.1a","Requirement","ECSS-E-ST-70-41_1331664","The list of application processes that can be addressed by the on-board control procedure service shall be declared when specifying that service.","NOTE 1\tThe application process that hosts the on-board control procedure service is always part of that list.\nNOTE 1\tThis Standard assumes that all requests of addressable application processes can be used by the on-board control procedure service.\nNOTE 2\tWhen the on-board control procedure service releases a request, the request is processed by an executing service, indicated by the service type and the application process identifier within the request. The generation of verification reports for the request is the responsibility of the executing service. The destination of the generated verification reports is the application process that hosts that on-board control procedure service.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.4.2g","Requirement","ECSS-E-ST-70-41_1331685","For each valid instruction to direct-load an OBCP, the OBCP management subservice shall:\n1.\tload the OBCP code in the OBCP engine;\n2.\tset the execution status of the OBCP to \"inactive\".","NOTE\tThe OBCP identifier and the OBCP checksum (if used) are also stored in the OBCP engine.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.4.6b","Requirement","ECSS-E-ST-70-41_1331706","Each request to load by reference and activate an OBCP shall contain exactly one instruction to load by reference and activate an OBCP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.4.9d","Requirement","ECSS-E-ST-70-41_1331731","The OBCP management subservice shall reject any request to abort an OBCP if any of the following conditions occurs:\n1.\tthe OBCP engine is not running;\n2.\tthat request contains an instruction that refers to an OBCP identifier that is not loaded in the OBCP engine.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.4.10a","Requirement","ECSS-E-ST-70-41_1331734","The OBCP management subservice capability to abort all OBCPs and report shall be declared when specifying that subservice.","NOTE\tThe corresponding requests are of message type \"TC[18,17] abort all OBCPs and report\". The responses are data reports of message type \"TM[18,18] aborted OBCP report\".\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.6.2f","Requirement","ECSS-E-ST-70-41_1331759","For each valid instruction to resume an OBCP, the OBCP management subservice shall:\n1.\tif the execution status of the OBCP is \"active and held\", unfreeze the execution of the OBCP at the position where it was frozen;\n2.\tset the execution status of the OBCP to \"active and running\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.18.4.7.1b","Requirement","ECSS-E-ST-70-41_1331773","Each request to communicate parameters to an OBCP shall contain exactly one instruction to communicate parameters to an OBCP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.19.3.1b","Requirement","ECSS-E-ST-70-41_1331802","The event-action subservice shall be associated to at least one event reporting subservice.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.19.5.2a","Requirement","ECSS-E-ST-70-41_1331809","If the event-action function is disabled, the event-action subservice shall not trigger the action for any event-action definition.","NOTE\tWhen the event-action function is disabled, the service does not react to any event reports.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.19.7.2f","Requirement","ECSS-E-ST-70-41_1331830","The event-action subservice shall process any valid instruction that is contained within a request to disable event-action definitions regardless of the presence of faulty instructions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.19.8.4c","Requirement","ECSS-E-ST-70-41_1331851","For each valid instruction to delete all event-action definitions, the event-action subservice shall:\n1.\tset the event-action function status to \"disabled\";\n2.\tdelete all event-action definitions.","NOTE\tEach event-action definition is deleted without regard to its enabled or disabled event-action status.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.20.4.1g","Requirement","ECSS-E-ST-70-41_1331876","For each valid instruction to report a parameter value, the parameter management subservice shall generate a single parameter value notification that includes:\n(a)\tthe parameter identifier;\n(b)\tits value.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.20.4.2b","Requirement","ECSS-E-ST-70-41_1331879","Each request to set parameter values shall contain one or more instructions to set a parameter value.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.20.5.4d","Requirement","ECSS-E-ST-70-41_1331904","The parameter management subservice shall reject any instruction to report a parameter definition if:\n1.\tthat instruction refers to an unknown parameter.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.21.5.2f","Requirement","ECSS-E-ST-70-41_1331925","For each valid instruction to direct-load a request sequence, the request sequencing subservice shall:\n1.\tload the request sequence;\n2.\tset the execution status of the request sequence to \"inactive\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.21.5.6c","Requirement","ECSS-E-ST-70-41_1331946","Each instruction to load by reference and activate a request sequence shall contain:\n1.\tthe identifier of the request sequence; \n2.\tif the request sequence is not to be loaded according to the loading policy, the file path of the on-board file that contains the request sequence to load and activate.","NOTE\tWhen the loading policy is used, the policy determines which on-board file contains the request sequence to load, refer to requirement 6.21.5.1b.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.21.5.7d","Requirement","ECSS-E-ST-70-41_1331953","The request sequencing subservice shall reject any request to abort a request sequence if any of the following conditions occurs:\n1.\tthat request contains an instruction with a request sequence identifier that refers to a request sequence that is not loaded;\n2.\tthat request contains an instruction that refers to a request sequence whose execution status is \"inactive\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.21.8d","Requirement","ECSS-E-ST-70-41_1331974","The request sequencing subservice shall reject any request to report the content of a request sequence if:\n1.\tthat request contains an instruction with a request sequence identifier that refers to a request sequence that is not loaded.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.6.3.3b","Requirement","ECSS-E-ST-70-41_1331999","Each request to disable the position-based schedule execution function shall contain exactly one instruction to disable the position-based schedule execution function.","NOTE\tThe instructions to disable the position-based schedule execution function contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.6.7b","Requirement","ECSS-E-ST-70-41_1332020","The position-based schedule execution process shall consider a scheduled activity is disabled if:\n1.\tthe position-based schedule execution function is disabled,\n2.\tthat scheduled activity is associated to a disabled sub-schedule,\n3.\tthat scheduled activity is associated to a disabled group.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.7.1b","Requirement","ECSS-E-ST-70-41_1332023","For each sub-schedule, the position-based scheduling subservice shall maintain a status indicating whether the schedule execution function for that sub-schedule is enabled or disabled.","NOTE\tThis status is named \"sub-schedule status\".\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.8.2.1d","Requirement","ECSS-E-ST-70-41_1332048","The position-based scheduling subservice shall reject any instruction to create a position-based scheduling group if any of the following conditions occurs:\n1.\tthat instruction refers to an already existing group;\n2.\tthe maximum number of groups that can be contemporaneously managed is already reached.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.8.3.2b","Requirement","ECSS-E-ST-70-41_1332069","Each request to disable position-based scheduling groups shall contain:\n1.\tone or more instructions to disable a position-based scheduling group, or\n2.\texactly one instruction to disable all position-based scheduling groups.","NOTE\tThe instructions to disable all position-based scheduling groups contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.10.2e","Requirement","ECSS-E-ST-70-41_1332090","For each request to position-shift all scheduled activities that is rejected, the position-based scheduling subservice shall generate a failed start of execution notification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.10.4b","Requirement","ECSS-E-ST-70-41_1332097","Each request to detail-report all position-based scheduled activities shall contain exactly one instruction to detail-report all position-based scheduled activities.","NOTE\tThe instructions to detail-report all position-based scheduled activities contain no argument.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.11.4b","Requirement","ECSS-E-ST-70-41_1332118","Each request to summary-report position-based scheduled activities identified by request identifier shall contain one or more instructions to summary-report a position-based scheduled activity identified by request identifier.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.12.3c","Requirement","ECSS-E-ST-70-41_1332143","Each instruction to delete the position-based scheduled activities identified by a filter shall contain:\n1.\ta position window, consisting of:\n(a)\tthe type of the position window that is one of \"select all\", \"from position tag\", \"to position tag\", \"from position tag to position tag\";\n(b)\tfor \"from position tag\" and \"from position tag to position tag\", the from position tag;\n(c)\tfor \"to position tag\" and \"from position tag to position tag\", the to position tag;\n2.\tif sub-schedules are supported, zero or more sub-schedules;\n3.\tif groups are supported, zero or more groups.","NOTE 1\tFor the filtering mechanism, including the interaction of the parts of the filter, refer to clause 6.22.12.2.\nNOTE 1\tFor sub-schedule support, refer to requirement 6.22.6.1a.\nNOTE 2\tFor group support, refer to requirement 6.22.6.1b.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.12.6e","Requirement","ECSS-E-ST-70-41_1332164","For each request to detail-report the position-based scheduled activities identified by a filter that is rejected, the position-based scheduling subservice shall generate a failed start of execution notification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.22.13a","Requirement","ECSS-E-ST-70-41_1332167","The following observables shall be defined for the position-based scheduling subservice:\n1.\tthe current orbit number;\n2.\tthe position-based schedule execution function status (enabled or disabled);\n3.\tthe current number of scheduled activities in the position-based schedule;\n4.\tif sub-schedules are supported, the current number of sub-schedules;\n5.\tif groups are supported, the current number of groups.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.4.2d","Requirement","ECSS-E-ST-70-41_1332192","The file handling subservice shall reject any request to report the attributes of a file if:\n1.\tthat request contains an instruction that refers to an object path that is invalid.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.4.4f","Requirement","ECSS-E-ST-70-41_1332213","Each instruction to find files shall contain:\n1.\tthe repository path;\n2.\tthe search pattern.","NOTE\tWildcards are limited to the search pattern. The find files request cannot be used to search for files in multiple repositories by means of wildcard characters in the repository path.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.4.5.1c","Requirement","ECSS-E-ST-70-41_1332220","Each instruction to create a directory shall contain:\n1.\tthe object path of the directory.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.4.6d","Requirement","ECSS-E-ST-70-41_1332241","Each instruction to summary-report the content of a repository shall contain:\n1.\tthe repository path.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.5.2.3d","Requirement","ECSS-E-ST-70-41_1332262","The file copy subservice shall reject any request to move a file if any of the following conditions occurs:\n1.\tthat request contains a file copy operation identifier that is already allocated to another on-going file copy operation;\n2.\tthat request contains an instruction that refers to an object path for the source file that is invalid;\n3.\tthat request contains an instruction that refers to an object path for the target file that is invalid;\n4.\tthe source object path and the target object path in the instruction each identify a remote file system.","NOTE\tThe move a file request cannot be used to move a file from a remote source to a remote target.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.5.3.4b","Requirement","ECSS-E-ST-70-41_1332287","Each request to resume all file copy operations involving a repository path shall contain exactly one instruction to resume all file copy operations involving a repository path.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.5.5.2b","Requirement","ECSS-E-ST-70-41_1332305","Each request to enable the periodic reporting of the file copy status shall contain exactly one instruction to enable the periodic reporting of the file copy status.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","6.23.5.5.3c","Requirement","ECSS-E-ST-70-41_1332312","For each valid instruction to disable the periodic reporting of the file copy status, the file copy subservice shall:\n1.\tset the file copy status periodic reporting status to \"disabled\".",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","7.3.7c","Requirement","ECSS-E-ST-70-41_1332345","The variable­length bit­string shall have the structure specified in Figure 7-3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","7.3.10c","Requirement","ECSS-E-ST-70-41_1332371","If the absolute time parameter has CDS format, the standard CCSDS epoch of 1958 January 1 shall be used.","NOTE\tThe CDS format is specified in CCSDS 301.0-B-4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","7.3.12c","Requirement","ECSS-E-ST-70-41_1332380","For each packet field whose structure and format is deduced, the deduction of the structure and format shall only result from the content of one or more preceding fields of the same packet, of one or more mission constants or a combination of both.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","7.4.3.2f","Requirement","ECSS-E-ST-70-41_1332404","If checksumming telemetry packets is used for the mission, for each telemetry packet that it generates, each application process shall:\n1.\tcalculate the checksum of that packet, and \n2.\tset the calculated value in the packet error control field of that packet.","NOTE 1\tThe telemetry packet checksum is calculated when all other fields of the packet are complete, and prior to downloading the packet.\nNOTE 1\tThe telemetry packet checksum is used by the ground system to verify the checksum of the complete telemetry packet.\nNOTE 2\tChecksumming telemetry packets includes also checksumming large telemetry packets, see clause 6.13.3.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.1.2.4b","Requirement","ECSS-E-ST-70-41_1332430","For each telemetry packet transporting a failed start of execution verification report, the source data field shall have the structure specified in Figure 8-4.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.2.2.7b","Requirement","ECSS-E-ST-70-41_1332467","For each telecommand packet transporting a request to acquire data from physical devices, the application data field shall have the structure specified in Figure 8-16.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.3.2.6b","Requirement","ECSS-E-ST-70-41_1332498","For each telecommand packet transporting a request to disable the periodic generation of housekeeping parameter reports, the application data field shall have the structure specified in Figure 8-26.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.3.2.8a","Requirement","ECSS-E-ST-70-41_1332503","Each telecommand packet transporting a request to disable the periodic generation of diagnostic parameter reports shall be of message subtype 8. ","NOTE\tFor the corresponding system requirements, refer to clause 6.3.4.5.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.3.2.20b","Requirement","ECSS-E-ST-70-41_1332540","For each telecommand packet transporting a request to modify the collection interval of diagnostic parameter report structures, the application data field shall have the structure specified in Figure 8-40.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.3.2.31a","Requirement","ECSS-E-ST-70-41_1332572","Each telecommand packet transporting a request to remove parameter report definitions from a parameter functional reporting definition shall be of message subtype 43. ","NOTE\tFor the corresponding system requirements, refer to clause 6.3.5.6.2.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.4.2.1a","Requirement","ECSS-E-ST-70-41_1332583","Each telecommand packet transporting a request to report the parameter statistics shall be of message subtype 1. ","NOTE\tFor the corresponding system requirements, refer to clause 6.4.5.2.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.5.2.1a","Requirement","ECSS-E-ST-70-41_1332610","Each telemetry packet transporting an informative event report shall be of message subtype 1. ","NOTE\tFor the corresponding system requirements, refer to clause 6.5.4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.6.2.2b","Requirement","ECSS-E-ST-70-41_1332639","For each telecommand packet transporting a request to load raw memory data areas, the application data field shall have the structure specified in Figure 8-67.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.6.2.15a","Requirement","ECSS-E-ST-70-41_1332676","Each telecommand packet transporting a request to enable the write protection of a memory shall be of message subtype 15. ","NOTE\tFor the corresponding system requirements, refer to clause 6.6.6.2.4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.9.1c","Requirement","ECSS-E-ST-70-41_1332706","For each spacecraft time packet, the secondary header flag in its packet primary header shall be set to 0.","NOTE\tSetting the secondary header flag to 0 indicates that the packet secondary header field is not present in the packet.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.9.2.3b","Requirement","ECSS-E-ST-70-41_1332715","For each telemetry packet transporting a CDS time report, the source data field shall have the structure specified in Figure 8-90.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.11.2.10b","Requirement","ECSS-E-ST-70-41_1332743","For each telemetry packet transporting a time-based schedule detail report, the source data field shall have the structure specified in Figure 8-97.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.11.2.20c","Requirement","ECSS-E-ST-70-41_1332772","To enable all time-based sub-schedules, N shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.11.2.23b","Requirement","ECSS-E-ST-70-41_1332781","For each telecommand packet transporting a request to delete time-based scheduling groups, the application data field shall have the structure specified in Figure 8-107.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.12.2.3b","Requirement","ECSS-E-ST-70-41_1332811","For each telecommand packet transporting a request to change the maximum transition reporting delay, the application data field shall have the structure specified in Figure 8-113.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.12.2.9a","Requirement","ECSS-E-ST-70-41_1332843","Each telemetry packet transporting a parameter monitoring definition report shall be of message subtype 9. ","NOTE\tFor the corresponding system requirements, refer to clause 6.12.3.10.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.12.2.19b","Requirement","ECSS-E-ST-70-41_1332875","For each telecommand packet transporting a request to enable functional monitoring definitions, the application data field shall have the structure specified in Figure 8-131.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.12.3.1b","Requirement","ECSS-E-ST-70-41_1332906","The values of the PMON checking status shall be:\n1.\tfor expected-value-checking, as specified in Table 8-7.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.13.2.1b","Requirement","ECSS-E-ST-70-41_1332918","For each telemetry packet transporting a first downlink part report, the source data field shall have the structure specified in Figure 8-140.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.14.2.2d","Requirement","ECSS-E-ST-70-41_1332944","To delete an application process from the application process forward-control configuration, N2 shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.14.2.8d","Requirement","ECSS-E-ST-70-41_1332969","To report that no housekeeping parameter report type of the related application process is in the housekeeping parameter report forward-control configuration, N2 shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.14.2.10d","Requirement","ECSS-E-ST-70-41_1332978","To delete an application process from the diagnostic parameter report forward-control configuration, N2 shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.2.1b","Requirement","ECSS-E-ST-70-41_1333003","For each telecommand packet transporting a request to enable the storage function of packet stores, the application data field shall have the structure specified in Figure 8-159.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.2.10a","Requirement","ECSS-E-ST-70-41_1333038","Each telemetry packet transporting a packet store content summary report shall be of message subtype 13. ","NOTE\tFor the corresponding system requirements, refer to clause 6.15.3.10.1.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.2.18b","Requirement","ECSS-E-ST-70-41_1333066","For each telecommand packet transporting a request to delete packet stores, the application data field shall have the structure specified in Figure 8-175.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.2.27c","Requirement","ECSS-E-ST-70-41_1333096","To empty the housekeeping parameter report storage-control configuration, N1 shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.2.29c","Requirement","ECSS-E-ST-70-41_1333105","To empty the diagnostic parameter report storage-control configuration, N1 shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.15.3a","Requirement","ECSS-E-ST-70-41_1333134","The values of the packet store type shall be as specified in Table 8-14.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.18.2.4c","Requirement","ECSS-E-ST-70-41_1333164","To stop an OBCP at the end of current step, the step ID field shall be set to 0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.18.2.7b","Requirement","ECSS-E-ST-70-41_1333173","For each telecommand packet transporting a request to communicate parameters to an OBCP, the application data field shall have the structure specified in Figure 8-202.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.18.2.18a","Requirement","ECSS-E-ST-70-41_1333203","Each telecommand packet transporting a request to stop and unload an OBCP shall be of message subtype 20. ","NOTE\tFor the corresponding system requirements, refer to clause 6.18.4.4.8.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.19.2.8b","Requirement","ECSS-E-ST-70-41_1333236","For each telecommand packet transporting a request to enable the event-action function, the application data field shall be omitted.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.20.2.6a","Requirement","ECSS-E-ST-70-41_1333265","Each telecommand packet transporting a request to report parameter definitions shall be of message subtype 6. ","NOTE\tFor the corresponding system requirements, refer to clause 6.20.5.4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.21.2.7b","Requirement","ECSS-E-ST-70-41_1333296","For each telemetry packet transporting a request sequence execution status report, the source data field shall have the structure specified in Figure 8-233.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.21.2.11a","Requirement","ECSS-E-ST-70-41_1333307","Each telecommand packet transporting a request to report the content of a request sequence shall be of message subtype 11. ","NOTE\tFor the corresponding system requirements, refer to clause 6.21.8.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.22.2.5b","Requirement","ECSS-E-ST-70-41_1333333","For each telecommand packet transporting a request to delete position-based scheduled activities identified by request identifier, the application data field shall have the structure specified in Figure 8-241.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.22.2.16a","Requirement","ECSS-E-ST-70-41_1333365","Each telecommand packet transporting a request to detail-report all position-based scheduled activities shall be of message subtype 16. ","NOTE\tFor the corresponding system requirements, refer to clause 6.22.10.4.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.22.2.19b","Requirement","ECSS-E-ST-70-41_1333372","For each telemetry packet transporting a position-based sub-schedule status report, the source data field shall have the structure specified in Figure 8-252.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.22.2.27b","Requirement","ECSS-E-ST-70-41_1333400","For each telemetry packet transporting a position-based scheduling group status report, the source data field shall have the structure specified in Figure 8-259.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.23.2.9a","Requirement","ECSS-E-ST-70-41_1333439","Each telecommand packet transporting a request to create a directory shall be of message subtype 9. ","NOTE\tFor the corresponding system requirements, refer to clause 6.23.4.5.1.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","8.23.2.19b","Requirement","ECSS-E-ST-70-41_1333470","For each telecommand packet transporting a request to suspend all file copy operations involving a repository path, the application data field shall have the structure specified in Figure 8-279.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","9.2.2b","Requirement","ECSS-E-ST-70-41_1333498","For each CPDU, the application process identifier used to refer to that CPDU shall be declared when specifying the spacecraft architecture.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-70-41C","9.2.3c","Requirement","ECSS-E-ST-70-41_1333505","The duration exponential value in a command pulse instruction shall be an unsigned integer greater than or equal to 0, and less than or equal to 7.","NOTE\tWhen the CPDU executes a command pulse instruction, it generates a pulse on the specified output line of a duration equal to:\n\t \n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","4.5.1b","Requirement","ECSS-E-ST-60-21_1350019","The data output of each gyro channel shall have its own date measurement related to a clock reference.","NOTE\tThe clock reference can be either internal or external.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","4.9.1c","Requirement","ECSS-E-ST-60-21_1350044","If internal filtering or compensation is applied to the measurement, both raw and filtered or compensated data shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","4.10.1a","Requirement","ECSS-E-ST-60-21_1350047","The gyro shall provide a Test mode. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.1.2a","Requirement","ECSS-E-ST-60-21_1350068","The worst-case performances shall be assessed by using the worst-case sensor of the statistical ensemble.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.2.2.3a","Requirement","ECSS-E-ST-60-21_1350093","The bias repeatability from switch-on to switch-on shall be specified by the customer denoting the performance type in terms of maximum, 1 sigma, 68% confidence level or peak to peak.","NOTE\tThe on and off durations are specified.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.3.1b","Requirement","ECSS-E-ST-60-21_1350114","The statistical interpretation of the gyro noise terms shall be defined by the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.4.2.3e","Requirement","ECSS-E-ST-60-21_1350135","the scale factor repeatability between before and after irradiation shall be specified by the customer denoting the performance type in terms of maximum, 1 sigma, 68% confidence level or peak to peak.","NOTE\tDepending of the gyro use, the repeatability values can be combined into a single specification. \n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.4.3c","Requirement","ECSS-E-ST-60-21_1350142","The estimation of the scale factor shall include considerations on the bias knowledge and the applied input rate.","NOTE\t1\tFor example the orientation of the gyro input axis w.r.t. the motion table axis and the Earth rotation axis. \nNOTE\t2\tIt is good practice to align the gyro sensing axis with the motion table rotation axis and to perform measurement over complete revolutions, in order to limit to second order of magnitude the contribution of alignment error and of Earth rotation projection along the gyro perpendicular axes.\nNOTE\t3\tDepending on the orientation of the sensing axis on the motion table and on the measurement required accuracy, an estimate of the alignment error can be required prior or simultaneously to the scale factor estimate.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.5.2.4b","Requirement","ECSS-E-ST-60-21_1350167","The relative gyro axes alignment, one w.r.t. another, stability over a customer-defined time period shall be specified by the customer denoting the performance type in terms of maximum, 1 sigma, 68% confidence level or peak to peak, taking into consideration environmental conditions between the alignment measurements.","NOTE\tMultiple time intervals with associated operating conditions can be specified.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.6.3b","Permission","ECSS-E-ST-60-21_1350231","The time tag scale factor may be characterised by test by monitoring of the time tag evolution on a significant period versus an external time reference.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.7.2a","Requirement","ECSS-E-ST-60-21_1350190","The measured rate error, or the measured angular increment error over the time interval between the two measurements, at the end of the unit start-up shall be specified by the customer as a ratio of the input angular rate with a specified maximum absolute error.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-21C","5.4.13.2a","Requirement","ECSS-E-ST-60-21_1350209","The stimulation performance requirements shall be verified by test.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.1.2a","Requirement","ECSS-E-ST-31-02_1190005","The specification shall be identifiable, referable and related to a TPHTE product.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.1.3m","Requirement","ECSS-E-ST-31-02_1190024","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.5.3.2a","Requirement","ECSS-E-ST-31-02_1190047","Verification by test shall be compliant with requirement 5.2.2.2a of ECSS-E-ST-10-02.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.5.3.3.1d","Requirement","ECSS-E-ST-31-02_1190054","Discrepancies between analytical prediction and test results shall be analysed in order to demonstrate that the objective of the qualification is not compromised.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.6.2c","Requirement","ECSS-E-ST-31-02_1190074","The delta qualification sequence shall be agreed with the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.6.8a","Requirement","ECSS-E-ST-31-02_1190102","Leak test shall be performed at ambient temperature using a detection method agreed with the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.6.8d","Requirement","ECSS-E-ST-31-02_1190105","During the leak test, the pressure level shall be maintained for 30 minutes as a minimum.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.6.9.5a","Requirement","ECSS-E-ST-31-02_1190126","Start-up with low power shall be verified by testing with and without thermal inertia on the evaporator heater system.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","5.6.14.4a","Requirement","ECSS-E-ST-31-02_1190154","For HP diode, tests shall be performed as specified in clause to 5.6.9.4 at one vapour temperature and with a heat load of 50 % of Qmax.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","6.2.3d","Requirement","ECSS-E-ST-31-02_1190279","Calibration of laboratory equipment shall be verified prior to their use.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","6.2.7a","Requirement","ECSS-E-ST-31-02_1190286","Declared Materials List, Declared, Process List and Declared Mechanical Parts List, as established during the qualification process, shall be confirmed to be applicable to the hardware submitted to the acceptance process. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","B.2.1<6>a","Requirement","ECSS-E-ST-31-02_1190183","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","D.2.1<4>a","Requirement","ECSS-E-ST-31-02_1190204","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","F.2.1<7>a","Requirement","ECSS-E-ST-31-02_1190229","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","F.2.1<10>a","Requirement","ECSS-E-ST-31-02_1190232","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-02C Rev.1","H.2.1<2>a","Requirement","ECSS-E-ST-31-02_1190253","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.2.3d","Requirement","ECSS-E-ST-33-11_0280019","The basis of the time shall be specified and justified.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.4b","Requirement","ECSS-E-ST-33-11_0280040","The explosive subsystem shall react only to a specified stimulus and be insensitive to all others.","NOTE\tSpecified stimulus: e.g. nature, range of values.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.4i","Requirement","ECSS-E-ST-33-11_0280047","If loss of function is safety critical or catastrophic, the explosive subsystem shall avoid single-point failures and include at least two initiators.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.5.2.4a","Requirement","ECSS-E-ST-33-11_0280068","The arm function shall be the second-last action in the sequence.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.7.4b","Requirement","ECSS-E-ST-33-11_0280089","In case 4.7.4a is not met, it shall either: \n1.\tbe agreed with the end-user to change the on-board subsystem requirements, or \n2.\tbe agreed with the end-user to provide protection against the environmental conditions or to reduce the external loads on the explosive subsystem.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.8.2.5b","Requirement","ECSS-E-ST-33-11_0280113","Protective features shall be provided to\n1.\tprevent initiation, \n2.\tprevent change of state of the safety barriers,\n3.\tprevent parasitic paths,\n4.\tbe tested to verify effectiveness.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.8.2.5e","Requirement","ECSS-E-ST-33-11_0280116","Measures to satisfy requirement 4.8.2.5d shall respect single point grounding implementation.","NOTE\tSingle point grounding implementation is described in ECSS-E-HB-20-07 section 6.1.3.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.8.3.1c","Requirement","ECSS-E-ST-33-11_0280139","Build-up of heat shall be prevented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.9f","Requirement","ECSS-E-ST-33-11_0280159","The nature and condition of age-sensitive materials shall be identified and documented in the DMPL.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.10.1e","Requirement","ECSS-E-ST-33-11_0280169","Initiator connector shall be terminated by male contacts.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.10.5c","Requirement","ECSS-E-ST-33-11_0280187","It shall not be possible to install an explosive device with the safety cap mounted.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.10.11.1f","Requirement","ECSS-E-ST-33-11_0280208","Remote operation and status indication shall be provided.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.11.1.1b","Requirement","ECSS-E-ST-33-11_0280230","For other elements of the subsystem, which can be fully tested before flight, the equipment environmental test conditions of the end-user shall apply.","NOTE\tThe requirements for explosive components are given below as measurements to be made after specific preconditioning and under survival and operational conditions identified in 4.6.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.11.2.7b","Requirement","ECSS-E-ST-33-11_0280270","Under the conditions in column E of Table 4-9, the properties in column A, expressed in the units specified in column B, shall be between the values in column C (maximum) and column D (minimum).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.11.3.2a","Requirement","ECSS-E-ST-33-11_0280256","The connector thread or closing mechanism shall be self locking.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.12.1a","Requirement","ECSS-E-ST-33-11_0280283","For any explosively actuated device which incorporates initiation and explosive charges the requirements of Clause 4.11 shall apply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.12.6d","Requirement","ECSS-E-ST-33-11_0280304","The flow direction shall be marked on the device.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.14.3.1a","Requirement","ECSS-E-ST-33-11_0280325","Test specification (TSPE) shall be in conformance with the DRD in Annex B of ECSS-E-ST-10-03.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.14.3.5a","Requirement","ECSS-E-ST-33-11_0280332","It shall be verified by test that the correct stimulus arrives at the correct initiator and no other.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.15.2b","Recommendation","ECSS-E-ST-33-11_0280433","If it is not possible to exclude explosive devices of class 1, according to UNECE regulations ST/SG/AC.10/1, Chapter 2.1 par. 2.1.3.6, the explosive devices are assigned to Class 1 and the required transport classification should be 1.4 S.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-11C Rev.1","4.15.4g","Requirement","ECSS-E-ST-33-11_0280372","The correctness of all connections shall be confirmed and a record of all connections be maintained.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-04C","5.3d","Requirement","ECSS-E-ST-31-04_1370005","If a STEP-TAS reader encounters an invalid entity in the input dataset, the reader shall not fail unless the resulting model is unrealisable in the target tool.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-31-04C","5.4a","Requirement","ECSS-E-ST-31-04_1370007","Software tools that implement STEP-TAS interfaces shall document the conformance classes reached.","NOTE \tThe STEP-TAS conformance classes are enumerated in Table 4-1.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.2.5a","Requirement","ECSS-E-ST-50-11_1410013","The SpaceFibre Lane layer shall provide three services: \n1.\tA Transfer Word service which sends data and control words over a SpaceFibre lane and which receives data and control words over a SpaceFibre link.\n2.\tA Control service which controls the operation of the lanes in a link, using the TxOnly, RxOnly, FarEndActive, and LaneReset signals for each lane and which provides the current state of the Lane Initialisation state machine.\n3.\tA Capabilities service which sets the capabilities of each lane at the near-end of a link and reports the capabilities of each lane at the far-end of the link.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.3.2a","Requirement","ECSS-E-ST-50-11_1410037","The SKIP control word shall begin with a comma, K28.7, which is in the least significant symbol position of the control word and is sent first.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.3.7a","Requirement","ECSS-E-ST-50-11_1410058","The Inverse INIT2 control word, iINIT2, shall begin with an initialisation comma, K28.5, which is in the least significant symbol position of the control word and is received first.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.3.8c","Requirement","ECSS-E-ST-50-11_1410065","The third symbol in the INIT3 control word, which has the value D24.1, shall identify the Lane Layer Control Word as being an INIT3 control word.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.4.2a","Requirement","ECSS-E-ST-50-11_1410086","The ACTIVE control word shall begin with a comma, K28.7, which is in the least significant symbol position of the control word and is sent first.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.5.1.3e","Requirement","ECSS-E-ST-50-11_1410111","The fourth and final symbol in the SDF control word is reserved and shall be set to D0.0.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.5.1.7e","Requirement","ECSS-E-ST-50-11_1410132","The fourth symbol of the SIF control word shall be a data symbol with any value from D0.0 to D31.7 and encode a data character containing an 8-bit CRC covering the first three characters of the control word, excluding the 8-bit CRC field itself, which is used to confirm the integrity of the SIF control word before its contents are acted upon.","NOTE\t1\tThere is no end of idle frame control word. Idle frames are ended by an SDF, SBF or SIF. \nNOTE\t2\tThe CRC includes the data value of the K-code in the SIF control word, i.e. ignoring the value of the D/K flag.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.5.2c","Requirement","ECSS-E-ST-50-11_1410135","The FCT control word shall begin with the K28.3 control character which is in the least significant symbol position of the control word and is sent first.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.5.3.5d","Requirement","ECSS-E-ST-50-11_1410160","The third and fourth symbols in the RETRY control word are reserved and shall be set to D0.0 when transmitted and ignored when received.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.8.1b","Requirement","ECSS-E-ST-50-11_1410181","Three types of frame shall be supported: data frame, broadcast frame, idle frame.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.8.4a","Requirement","ECSS-E-ST-50-11_1410202","A broadcast frame shall start with a start of broadcast frame, SBF, control word.","NOTE\tThe broadcast frame is illustrated in Figure 5-7.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.8.4h","Requirement","ECSS-E-ST-50-11_1410209","The Reserved sub-field in the EBF shall be set to zero when transmitted and ignored when received.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.3.10i","Requirement","ECSS-E-ST-50-11_1410230","A RETRY control word shall be able to be inserted within a broadcast, data or idle frame.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.2.1e","Recommendation","ECSS-E-ST-50-11_1410257","The clock-data recovery circuit should indicate, in a status register, when bit synchronisation is achieved.","NOTE\tThis is for status information only.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.3.2i","Requirement","ECSS-E-ST-50-11_1410281","For data signalling rates in the range above 3,125 Gbit/s to 6,25 Gbit/s, the serial eye pattern mask shall have the intervals specified in Table 5-15.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.3.3g","Permission","ECSS-E-ST-50-11_1410299","An equivalent form of termination of the input signal may be used, when needed by a particular receiver device.","NOTE\tFor example, see Nick Holland, “Interfacing Between LVPECL, VML, CML, and LVDS Levels”, Texas Instruments, Application Report SLLA120, December 2002.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.4.2b","Requirement","ECSS-E-ST-50-11_1410314","Two pairs of differential PCB tracks shall be used for a bi-directional SpaceFibre lane, one pair for each direction.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.4.4.3b","Requirement","ECSS-E-ST-50-11_1410337","Flight cable shall contain one or several signal wires or pairs of signal wires with individual shields or an overall shield or both individual and overall shields.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.4.6.1a","Requirement","ECSS-E-ST-50-11_1410362","Type-D EGSE electrical medium from and including the Type-D connector at one end of a lane to and including the Type-D connector at the other end of that lane, shall:\n1.\tMaintain a signal path of 50 ohm ± 5 ohm single-ended impedance or 100 ohm ± 10 ohm differential impedance.\n2.\tHave an insertion loss of less than 2,2 dB/m plus 2 dB per connector pair at a maximum operating bit rate specified for the SpaceFibre electrical medium.\n3.\tHave a return loss of more than 9 dB.\n4.\tHave a near-end crosstalk isolation of better than 30 dB.\n5.\tHave a far-end crosstalk isolation of better than 30 dB.\n6.\tHave a signal skew between TXp and TXn of less than the larger of:\n(a)\t±20 ps.\n(b)\t±10% of the shortest bit interval that the medium is used for.","NOTE\t±20 ps corresponds to a difference in path length of around ±2 mm and is Signal skew 10 Gbit/s = 100 ps bit time, around 15 mm signal length, 10 % is 1,5 mm which is difficult to manufacture.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.4.6.3b","Requirement","ECSS-E-ST-50-11_1410369","Type-D EGSE cable shall contain one or several signal wires or pairs of signal wires with individual shields or an overall shield or both individual and overall shields.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.5.2k","Requirement","ECSS-E-ST-50-11_1410393","Multi-rate transmitters operating over the range 1 Gbit/s to 10 Gbit/s, shall follow the specifications for 10 Gbit/s transmitters.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.6.2.1a","Requirement","ECSS-E-ST-50-11_1410421","A specific Type-B flight fibre optic medium shall be referred to by a unique descriptive name based on the type of insert and connector used in the following format: SpFi-TypeB-Insert-Connector, where Insert is the type of insert and Connector is a unique name for the type of connector and its specific contact allocation.","NOTE\t1\tFor example, a Type-B flight fibre optic medium using MT inserts in a 38999 connector with a specific contact allocation (D) is given the name SpFi-TypeB-MT-38999D.\nNOTE\t2\tThe Type-B fibre optic medium is intended to be a generic specification of a cable assembly without defining the insert or connector body to be used.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.6.3.2d","Permission","ECSS-E-ST-50-11_1410444","When more than one lane is provided in an active optical cable assembly, the power connection may be shared provided that it can provide sufficient power for all of the transceivers.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.4.6.3.3b","Requirement","ECSS-E-ST-50-11_1410447","The Type-C fibre optic cable assembly shall contain one or more pairs of fibre with each pair connected as specified in Table 5-33.","NOTE\tA Type-C fibre optic cable assembly containing two fibres is illustrated in Figure 5-26.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.5.2.3c","Requirement","ECSS-E-ST-50-11_1410473","For a single lane link FarEndActive shall be de-asserted.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.5.2.8b","Requirement","ECSS-E-ST-50-11_1410494","When in the InvertRxPolarity state the Lane Initialisation state machine shall initiate the following actions:\n1.\tWhen RxOnly is not asserted, enable the transmitter driver.\n2.\tWhen TxOnly is not asserted, enable the receiver and CDR.\n3.\tInvert received bits.\n4.\tSend INIT1 control words.\n5.\tReceive Lane layer control words, LLCW.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.5.2.12e","Requirement","ECSS-E-ST-50-11_1410519","The Lane Initialisation state machine shall leave the PrepareStandby state on one of the following conditions, which are evaluated in the order given:\n1.\tWhen LaneReset is asserted, move to the ClearLine state.\n2.\tWhen 32 STANDBY control words have been sent, move to the ClearLine state.\n3.\tWhen three consecutive LOST_SIGNAL or three consecutive STANDBY control words have been received, move to the ClearLine state.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.5.2.13c","Recommendation","ECSS-E-ST-50-11_1410522","When in the LossOfSignal state and RxOnly is asserted the Lane Initialisation state machine should disable the transmitter driver. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.5.7a","Requirement","ECSS-E-ST-50-11_1410543","A symbol word shall comprise four symbols.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.1d","Requirement","ECSS-E-ST-50-11_1410568","The Multi-Lane layer shall pass data words and Data Link layer control words received from the Lane layer to the Data Link layer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.4.1a","Requirement","ECSS-E-ST-50-11_1410589","Data and control words to be sent over a multi-lane link shall be distributed across the data-sending lanes of the link.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.4.1d","Requirement","ECSS-E-ST-50-11_1410592","When sending data link control words, each data link control word shall be replicated and sent over all data-sending lanes forming a row filled with the same control word, with the exception of the EDF control words which have different CRC values.","NOTE\t1\tThe data link control words can then be generated and processed at a rate that is independent of the number of lanes being used. This lower, fixed rate simplifies the implementation.\nNOTE\t2\tThe CRC16 field of an EDF is different for each lane according to the data sent in that lane.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.6.2a","Requirement","ECSS-E-ST-50-11_1410617","A valid receiving row shall fulfil one of the following conditions:\n1.\tContain only data words or a mix of data words and PAD control words.\n2.\tContain only control words without any PAD control words.","NOTE\t1\tSee clause 5.6.4.2 for details of Pads.\nNOTE\t2\tIt is possible that some invalid rows, for example \"SDF SDF EDF\", is considered a valid row even if it is not legal. However, in this case, detecting this sequence as invalid row is not necessary because the error is detected later in the Data Link layer. Control words are only received from one of the lanes. In this example, if first lane or third lane is used, everything is fine and no retry is needed. If the second lane is used, the word identification state machine detects the error. Therefore, it is not necessary to check that control words in all lanes are equivalent, which requires increasing logic when the number of lanes is increased. \n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.7.1b","Requirement","ECSS-E-ST-50-11_1410638","The Aligned condition shall arise when all of the following conditions occur:\n1.\tAll lanes are aligned.\n2.\tThe far-end lanes in the active state are the same as the near-end lanes in the active state.","NOTE\tLane alignment is specified in requirement 5.6.6.4f.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.9.5b","Requirement","ECSS-E-ST-50-11_1410663","The reset for lane L, LaneReset(L), shall be de-asserted when the following condition occurs:\n1.\tLaneState(L) = ClearLine AND LinkReset is de-asserted.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.6.10c","Requirement","ECSS-E-ST-50-11_1410666","Once initialised a hot redundant lane shall send Lane layer and Multi-Lane layer control words, and not send any Data Link layer word.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.2.1a","Requirement","ECSS-E-ST-50-11_1410687","The network layer interface to the SpaceFibre port shall comprise one or more output virtual channel buffers and one or more input virtual channel buffers.","NOTE\tNormally, there is the same number of output and input virtual channel buffers.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.3.1f","Requirement","ECSS-E-ST-50-11_1410712","On LaneReset, the FCT credit counter shall not be modified. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.4.3d","Requirement","ECSS-E-ST-50-11_1410733","Several virtual channels shall be able to be scheduled to send data in the same time-slot.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.4.4b","Requirement","ECSS-E-ST-50-11_1410740","The medium access controller shall use the precedence of each virtual channel to determine which ready virtual channel is permitted to send a data segment.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.4.5q","Requirement","ECSS-E-ST-50-11_1410761","Bandwidth Credit shall be set to zero on interface reset.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.5k","Requirement","ECSS-E-ST-50-11_1410782","The Broadcast Bandwidth Credit shall be increased by one after the interval equal to the time it takes to send the number of words of 4 divided by the Normalised Expected Broadcast Bandwidth.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.6.3.1d","Requirement","ECSS-E-ST-50-11_1410807","The Transmit Sequence Counter shall be cleared to zero on link reset of the SpaceFibre port.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.6.3.1g","Requirement","ECSS-E-ST-50-11_1410810","The Transmit Sequence Counter and associated polarity flag shall provide Sequence Numbers for data frames, FCTs, broadcast frames, idle frames and FULL words.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.6.3.2o","Requirement","ECSS-E-ST-50-11_1410827","If the Sequence Count of the SEQ_NUM of a received SIF or FULL is not the same as the Receive Sequence Counter or the polarity flag of the SEQ_NUM is not the same as the Receive Polarity Flag, a sequence error has occurred and the idle frame or FULL shall be discarded.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.6.7f","Requirement","ECSS-E-ST-50-11_1410857","When an FCT is received with a CRC error or out of sequence, it shall be discarded.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.7.2.1b","Requirement","ECSS-E-ST-50-11_1410878","ACKs shall be sent as soon as possible after being requested, while respecting control word precedence.","NOTE\t1\tControl word precedence is specified in clause 5.3.10.\nNOTE\t2\tACKs are not buffered before they are sent.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.7.2.2c","Requirement","ECSS-E-ST-50-11_1410885","A NACK requested to be sent shall be sent as soon as possible, while respecting control word precedence.","NOTE\t1\tA NACK that is requested to be sent which cannot be sent immediately means that a NACK is pending to be sent. The pending NACK is sent as soon as possible.\nNOTE\t2\tSee clause 5.3.9 for the specification of precedence.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.7.3.4c","Requirement","ECSS-E-ST-50-11_1410906","The Receive Error state machine shall leave the Error Positive state on the following conditions:\n1.\tWhen an ACK is requested to be sent, move to the Valid Positive state, before sending the ACK. \n2.\tWhen a data frame, broadcast frame, FCT, SIF or FULL is received containing a positive Sequence Number but an incorrect, out of sequence, Sequence Count, move to the Error Negative state, before sending any NACK in response to this error.","NOTE\tNote the ACK is therefore sent with a positive Sequence Number.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.7.8.7a","Requirement","ECSS-E-ST-50-11_1410927","FCT, ACK, NACK, FULL and RETRY control words shall be able to be received in any state.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.1i","Requirement","ECSS-E-ST-50-11_1410952","The Network layer shall be controlled by the following management parameters from the Management Information Base:\n1.\tRouting switch virtual network to virtual channel mapping.\n2.\tRouting switch routing table.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.2.1b","Requirement","ECSS-E-ST-50-11_1410955","The SpaceFibre ports of nodes and SpaceFibre routing switches shall be interconnected with links. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.3k","Requirement","ECSS-E-ST-50-11_1410976","Each virtual network shall have an identifier from VN0 to VN63.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.5c","Requirement","ECSS-E-ST-50-11_1411001","The end of a packet shall be indicated by an EOP or EEP.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.8.1k","Requirement","ECSS-E-ST-50-11_1411022","All ports, except for the configuration port, shall contain at least two virtual channels in a port.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.8.1r","Requirement","ECSS-E-ST-50-11_1411029","A routing switch configuration port shall be accessed using path addressing only. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.8.4a","Requirement","ECSS-E-ST-50-11_1411051","A configurable virtual channel time-out shall be used by all virtual channels to detect a packet that has become stuck.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.9.3b","Requirement","ECSS-E-ST-50-11_1411072","A routing switch shall be configurable to remove the logical address character at the start of a packet and replace it with a Fill character when a packet is forwarded. ","NOTE\t1\tThe deletion of a logical address is used to expand the number of nodes that can be accessed using logical addressing. A large network is divided into regions where a logical address applies. When crossing a boundary between regions, the logical address is deleted exposing a new logical address that applies to the next region. Regions using logical addressing can be connected to regions using path addressing. This mechanism enables more than 223 nodes to be accessed using a series of logical addresses.\nNOTE\t2\tA regional logic address can be used wherever a logical address is used.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.12.2d","Requirement","ECSS-E-ST-50-11_1411097","A broadcast message shall be broadcast through the ports of the routing switch, excluding the port on which the broadcast message arrived.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.8.13b","Requirement","ECSS-E-ST-50-11_1411100","A SpaceFibre node shall comprise the following:\n1.\tOne or more SpaceFibre ports or parallel ports, which each contain one or more virtual channels.\n2.\tOne or more end-points, each of which provides an interface between a virtual channel of a port and the host system.\n3.\tZero or one broadcast mechanism, which broadcasts broadcast-messages over the ports and broadcast-interface of the node.\n4.\tZero or one broadcast interface, which provides the interface from applications hosted by the node to the broadcast mechanism.","NOTE\tThe UML diagram in Figure 5-56 illustrates the components and specialisations of a SpaceFibre node.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","5.9.4c","Permission","ECSS-E-ST-50-11_1411126","Implementations may provide additional status information for debugging purposes.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","6.2.3.3.4a","Requirement","ECSS-E-ST-50-11_1411148","The effect on receipt of the BROADCAST_MESSAGE.indication primitive by the SpaceFibre user shall be for the user to read the broadcast message.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","6.3.4.2.1a","Requirement","ECSS-E-ST-50-11_1411169","The SCHEDULE.request primitive shall be used by the SpaceFibre network layer to pass current time-slot information to the Data Link layer in order to synchronise the scheduled QoS in each Data Link of a network.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","6.4.2.2.2a","Requirement","ECSS-E-ST-50-11_1411176","The TX_SYMBOL.request primitive shall provide the following parameters:\n1.\tTX_SYMBOL.request (Symbol).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-11C","6.5.2.2.4a","Requirement","ECSS-E-ST-50-11_1411197","The effect on receipt of the SET_MANAGEMENT_PARAMETER.request primitive shall be to update the specified management parameter with the new value provided in the request.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.2.5c","Requirement","ECSS-E-ST-50-12_1420017","The SpaceWire Physical layer shall be responsible for transmitting and receiving the data and strobe signals over PCB tracks, connectors and cable assemblies.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.2.5d","Requirement","ECSS-E-ST-50-12_1420044","For a SpaceWire cable constructed in accordance with 5.3.2.2a and 5.3.2.2b and with differential pairs consisting of 26 AWG wires, the constants in Table 5-3 shall be used in conjunction with equation [5-1] to determine the upper limit of the average insertion loss in decibel per meter.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.2.6a","Requirement","ECSS-E-ST-50-12_1420049","The SpaceWire cable shall conform to the PSNEXT and PSELFEXT values in Table 5-5 and Table 5-6 respectively.","NOTE\tThese values are achievable on cable alone. On assemblies with MDM 9-pin connectors these values cannot be achieved. This performance can be met with EMI and crosstalk optimised connectors.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.4.1a","Requirement","ECSS-E-ST-50-12_1420078","Cable assemblies shall consist of one of the following alternatives:\n1.\tTwo Type A connectors with male contacts joined by a length of cable;\n2.\tTwo Type B connectors joined by a length of cable;\n3.\tA Type A connector with male contacts and a Type B connector joined by a length of cable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.4.3.3d","Requirement","ECSS-E-ST-50-12_1420101","The individual shields of the differential signal pairs carrying the output signals Dout+, Dout- and Sout+ and Sout- shall be connected together and to pin 3 of the connector at the transmitting end.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.6.2.1b","Requirement","ECSS-E-ST-50-12_1420124","SpaceWire using LVDS line drivers and line receivers shall be referred to as SpW-LVDS.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.6.2.2g","Requirement","ECSS-E-ST-50-12_1420133","The steady state difference in magnitude of VOUTp or VOUTn when transmitting logic 1 compared to when transmitting logic 0 shall be less than 50 mV.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.3.6.2.5h","Recommendation","ECSS-E-ST-50-12_1420155","A single fault should not lead to a driver emitting a voltage outside the range 0 V to +3,6 V relative to the driver ground reference.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.4.3.1b","Requirement","ECSS-E-ST-50-12_1420182","The data­control flag shall be set to zero to indicate that the current symbol holds a data character. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.4.4f","Requirement","ECSS-E-ST-50-12_1420207","The SpaceWire receiver shall be tolerant of simultaneous transitions on the Data and Strobe lines. ","NOTE\t1\tBeing tolerant of simultaneous transitions means that there is no lock-up of the receiver when a simultaneous transition occurs.\nNOTE\t2\tSimultaneous transitions on the Data and Strobe lines are not part of the normal operation of SpaceWire. They can occur, however, either when a SpaceWire cable is plugged in while the transmitter is trying to make a connection, or when the LVDS driver or receiver circuits are enabled while the transmitter is trying to make a connection.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.4.6b","Requirement","ECSS-E-ST-50-12_1420210","The gotNull condition shall only be cleared when the RX Enable flag is de-asserted",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.5.2e","Requirement","ECSS-E-ST-50-12_1420235","The data link layer shall indicate to the Network layer when it is able to accept another N-Char for sending.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.5.4o","Permission","ECSS-E-ST-50-12_1420256","When the data link layer can only hold fewer than 56 received N-Chars, the receive credit count may have a maximum value of less than 56..","NOTE\tIt is possible for the data link layer to hold more received N-Chars than the maximum receive credit count value.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.5.7.5b","Requirement","ECSS-E-ST-50-12_1420277","The Link state machine shall leave the Started state on one of the following conditions:\n1.\tWhen LinkDisabled is asserted, move to the ErrorReset state.\n2.\tWhen a disconnect occurs, move to the ErrorReset state.\n3.\tWhen a parity error occurs, move to the ErrorReset state.\n4.\tWhen an ESC error, move to the ErrorReset state.\n5.\tWhen an FCT, N-Char or broadcast code is received from the Encoding Layer, move to the ErrorReset state.\n6.\tWhen enable is asserted, at least one Null has been sent and gotNull is asserted, move to the Connecting state.\n7.\t12,8 µs after entering the Started state, move to the ErrorReset state.","NOTE\tThe Null that is received causing the gotNull condition to be asserted, can occur in the ErrorWait, Ready or Started state.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.5.8.2a","Requirement","ECSS-E-ST-50-12_1420284","When Port Reset is asserted, the Link Error Recovery state machine shall enter the Normal state.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.4.2a","Requirement","ECSS-E-ST-50-12_1420305","The value field of a time-code shall contain a 6-bit time-code value, which is an unsigned binary integer.","NOTE\tThe network layer time-code is illustrated in Figure 5-23.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.5.3b","Requirement","ECSS-E-ST-50-12_1420330","Bits 0 to 4 of the value field of an interrupt acknowledgement code shall contain an interrupt identifier, which has a value between 0 and 31.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.5.6a","Requirement","ECSS-E-ST-50-12_1420351","A node supporting distributed interrupts in the interrupt with acknowledgement mode shall conform to clause 5.6.5.4.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.5.6d","Recommendation","ECSS-E-ST-50-12_1420354","A node not supporting sending of interrupt acknowledgements should discard any host requests to send interrupt acknowledgements.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.8.1a","Requirement","ECSS-E-ST-50-12_1420379","A SpaceWire routing switch shall forward a packet, arriving at one port, towards its required destination, through another port or back through the same port as determined by the first data character of the packet and the contents of the routing table.","NOTE\tA packet can be forwarded through two or more ports when packet multicast is being used, see clause 5.6.8.10.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.8.5b","Recommendation","ECSS-E-ST-50-12_1420400","A packet arriving with a leading data character that references a non-existent port should result in an invalid address error being registered.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.8.9d","Permission","ECSS-E-ST-50-12_1420421","When using a legacy routing switch, that routing switch may also support group adaptive routing for path addresses.","NOTE\tThis clause is included because ECSS-E-ST-50-12C (31 July 2008) allows group adaptive routing with path addresses. This is, however, not recommended as it makes path addressing non-deterministic, thus making it difficult to reliably configure a network, using device configuration ports.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.6.8.12b","Permission","ECSS-E-ST-50-12_1420428","When logic resources permit, a separate configurable port time-out may be used for each port.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","5.7.5a","Requirement","ECSS-E-ST-50-12_1420449","The data link layer management parameters detailed in clause 5.5.3 shall be incorporated in the SpaceWire Management Information Base. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.1.3.2.4a","Requirement","ECSS-E-ST-50-12_1420474","On receipt of the DISTRIBUTED_INTERRUPT.request primitive the SpaceWire end-point shall immediately send the interrupt code through its port.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.2.1.3.4a","Requirement","ECSS-E-ST-50-12_1420495","The effect on receipt of the READ_NCHAR.request primitive by the data link layer shall be that an N-Char from the specified port is read by the network layer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.2.2.2.2a","Requirement","ECSS-E-ST-50-12_1420498","The BROADCAST_CODE.request primitive shall have the following parameters:\n1.\tBROADCAST_CODE.request (Port, Broadcast code value).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.3.2.4.1a","Requirement","ECSS-E-ST-50-12_1420523","The function of the DISCONNECT.indication primitive shall be to indicate to the data link layer that the SpaceWire link is disconnected. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.4.2.2.4a","Requirement","ECSS-E-ST-50-12_1420544","On receipt of the DS_RX.request primitive the physical layer shall pass the data and strobe signals received over the physical medium to the encoding layer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-50-12C Rev.1","6.5.2.2.1a","Requirement","ECSS-E-ST-50-12_1420551","The GET_PARAMETER.request primitive shall be used to read the current value of a SpaceWire management parameter and status information.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","6.3.3.1a","Requirement","ECSS-E-ST-20-06_0070017","The applicability of the electrical continuity requirements shall be established in accordance with the diagram in Figure 6-1.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","6.6.1c","Requirement","ECSS-E-ST-20-06_0070036","The tests shall either:\n1.\treproduce the physical process of concern, i.e. charging, in a worst-case environment, or \n2.\tyield electrostatic material properties enabling the materials response to such an environment to be assessed.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","6.8.1a","Requirement","ECSS-E-ST-20-06_0070060","Electrical continuity and grounding shall be verified by inspection and testing. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","7.2.3.1d","Requirement","ECSS-E-ST-20-06_0070077","A series of tests shall be performed with the inter-connector covered with an insulator to observe discharges in solar cell assembly (SCA) gaps areas.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","7.2.3.2b","Requirement","ECSS-E-ST-20-06_0070080","The test shall be performed using inverted voltage gradient conditions. ","NOTE \tAn IVG configuration can be obtained by using keV electron beams or filament vaporization or neutralized or non neutralized ion source (cf reference [39]).\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","9.2.2c","Recommendation","ECSS-E-ST-20-06_0070170","Cables running external to the main spacecraft body, should have the minimum thickness of dielectric insulation consistent with their primary function. ","NOTE \tThis arises from the general rule that higher electric fields can arise in thicker dielectrics.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","10.2.2b","Requirement","ECSS-E-ST-20-06_0070125","Sputtering and surface contamination which can occur if current is collected through ion impacts shall be within a level agreed with the customer. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","11.2.1b","Requirement","ECSS-E-ST-20-06_0070137","If neutral plasma thrusters have an integral cathode (effectively an integral neutralizer) which neutralizes the beam and is used as part of the ionization process, the neutralizer requirements in 11.2.1a shall be applied to these cathodes.","NOTE \tHall effect thrusters are neutral plasma thrusters.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-06C Rev.1","11.3.1a","Requirement","ECSS-E-ST-20-06_0070154","If ground testing is used for ESD validation of electrical propulsion systems, the effects of vacuum chamber limitations used in the test shall be established through modelling.","NOTE \t1\tFor example, by computer simulation.\nNOTE \t2\tDetailed requirements for ground testing, e.g. size of chamber, and accuracy of diagnostics depend on the thrusters under test. Thrust range, plasma density and ion energy varies strongly from one thruster to another.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-32-10C Rev.2 Corr.1","4.1.5.3a","Requirement","ECSS-E-ST-32-10_0110012","A “margin policy” factor KMP shall be applied for launch vehicles.","NOTE \tThis factor, used to give confidence to the design, covers (not exhaustive list):\n·\tthe lack of knowledge on the failure modes and associated criteria.\n·\tthe lack of knowledge on the effect of interaction of loadings.\n·\tthe non-tested zones.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.2.4.3a","Requirement","ECSS-E-ST-33-01_0820009","All items having the same identification number shall be functionally and dimensionally interchangeable.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.4.2b","Requirement","ECSS-E-ST-33-01_0820030","Mechanical interface, position accuracy or velocity tolerances shall be specified and verified that they conform to the functional needs.","NOTE \tMechanical interfaces include assembly and test rigging and other installation and integration conditions.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.5.2.1a","Requirement","ECSS-E-ST-33-01_0820033","Materials shall be selected in conformance with ECSS-Q-ST-70 clause 5, or be verified that they conform to requirements, approved by the customer.","NOTE \t1\tFor general requirements on materials used for space mechanisms, see ECSS-E-ST-32-08. The material requirements in 4.5.2.2 to 4.5.2.7 are specific to mechanisms.\nNOTE \t2\tFor selection of materials, see ECSS-Q-ST-70-71.\nNOTE \t3\tFor additional requirements relating to tribology, see clause 4.7.3.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.3.1a","Requirement","ECSS-E-ST-33-01_0820058","Mechanisms shall be designed with a lubrication function between surfaces in relative motion in order to ensure they conform to the mechanism performance requirements specified in the specific mechanism specification, throughout the specified lifetime.","NOTE \tThe lubrication function aims to provide the motorization margins and minimize wear.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.3.4.1a","Requirement","ECSS-E-ST-33-01_0820079","The life of tribological contacts shall be verified under worst case ground and flight conditions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.3.4.2g","Recommendation","ECSS-E-ST-33-01_0820459","Bearing preload should be measured after final mechanism assembly.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.5.2.5a","Requirement","ECSS-E-ST-33-01_0820106","For structural margin of safety requirements, ECSS-E-ST-32 shall apply.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.5.3.1f","Requirement","ECSS-E-ST-33-01_0820123","The kinetic energy of the mechanism moving parts, and its effects, shall not be taken into account to meet the specified motorization factor.","NOTE \tSuch effects are acceleration and deceleration force and torque of moving parts.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.5.4.3g","Requirement","ECSS-E-ST-33-01_0820143","Latches shall be resettable for ground testing.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.5.4.6b","Requirement","ECSS-E-ST-33-01_0820162","The sizing of ball bearings made of materials other than hardened steel shall be proposed by the supplier and agreed by the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.5.4.8d","Recommendation","ECSS-E-ST-33-01_0820464","Clearances should be at least 3 times its associated tolerance.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.7.1.1e","Requirement","ECSS-E-ST-33-01_0820188","Generated electrical disturbances shall conform to the project specific EMC requirements.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.7.6a","Requirement","ECSS-E-ST-33-01_0820207","Mechanisms containing electrical parts and circuitry shall be protected against overcurrent due to abnormal applied voltage or internal conditions in conformance with ECSS-E-ST-20, clause 5.8.1.","NOTE \tThe current protection can be provided externally.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.7.7.8a","Requirement","ECSS-E-ST-33-01_0820214","Mechanisms shall conform to the spacecraft system requirements on magnetic cleanliness in conformance with ECSS-E-ST-20-07, and conductivity of surfaces for electrostatic discharge (ESD) protection in conformance with ECSS-E-ST-20-06. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.2.1b","Requirement","ECSS-E-ST-33-01_0820235","If any of the analysis specified in requirement 4.8.2.1a is not performed, justification shall be provided by the supplier and agreed by the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.2.11a","Requirement","ECSS-E-ST-33-01_0820256","The conformity of the mechanism to the requirements for shock generation and susceptibility specified in the SMS shall be verified by analysis.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.3.1f","Requirement","ECSS-E-ST-33-01_0820281","The mechanism shall be subjected to a thermal verification.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.3.3.8a","Requirement","ECSS-E-ST-33-01_0820301","The EMC performance of mechanisms shall be verified by testing when:\n1.\tEMC sensitive components are used on the mechanism, or \n2.\tspacecraft specific EMC requirements are applicable to the mechanism.","NOTE \tEMC comprises susceptibility and emissivity.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.3.3.10a","Requirement","ECSS-E-ST-33-01_0820307","The mathematical model used to analyse the dynamic behaviour of the control system shall be correlated with measurements performed on representative hardware agreed by the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","4.8.3.4.2c","Requirement","ECSS-E-ST-33-01_0820327","The acceptance level testing shall be carried out at levels, which are higher than expected in flight but less than the qualification levels.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","A.2.1<3>d","Requirement","ECSS-E-ST-33-01_0820344","The SMS shall describe the redundancy concepts for the mechanism.","NOTE \tSee 4.2.5.2d.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","A.2.1<6>a","Requirement","ECSS-E-ST-33-01_0820351","The SMS shall list the handling, storage and operational requirements for all lubricated parts.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","C.2.1<1>b","Requirement","ECSS-E-ST-33-01_0820372","The MAV shall list:\n1.\tall the applicable documents regarding requirements related to design and performance; \n2.\tthe design definition file reference of the mechanism being analysed;\n3.\tthe list of documents providing inputs to analyses presented in this document; \n4.\tany other applicable and reference documents to support the generation of the document.","NOTE 1 \tto item 3: For example, thermal analysis, structural analysis, and test reports.\nNOTE 2\tto item 3: Subsystems and parts data to be included.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","F.2.1<2>a","Requirement","ECSS-E-ST-33-01_0820428","The MSVP shall describe the mission and the role of the mechanism in achieving the mission.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-33-01C Rev.2","G.2.1<5>b","Requirement","ECSS-E-ST-33-01_0820449","The MSVR shall state and describe any open issues.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","4.1.6.1d","Requirement","ECSS-E-ST-60-20_0920018","The supplier shall document whether the star sensor initialization uses either:\n1.\tInternal initialization, or \n2.\tDirect initialization.","NOTE \t1\tFor internal initialization, the information to initialize the sensor is provided by the attitude determination function of the star sensor.\nNOTE \t2\tFor direct initialization, the information to initialize the sensor is supplied by an external source e.g. AOCS.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","4.2.4b","Requirement","ECSS-E-ST-60-20_0920031","The supplier shall document whether the autonomous attitude determination capability is repetitively used to achieve the autonomous attitude tracking.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.1.2b","Requirement","ECSS-E-ST-60-20_0920043","The statistical ensemble shall be characterized and agreed with the customer.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.4e","Requirement","ECSS-E-ST-60-20_0920052","The supplier shall identify the worst case projection in BRF of the value de-fined in 5.4d. ","NOTE \tDifferent angular accelerations can be specified with associated required performance.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.4l","Requirement","ECSS-E-ST-60-20_0920059","The impact of individual star errors on the overall rate accuracy shall be provided via simulation.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.5.5.1c","Requirement","ECSS-E-ST-60-20_0920079","The performance shall be specified under the related performance general conditions.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.8.1b","Requirement","ECSS-E-ST-60-20_0920102","The following additional performance metrics shall be established: track maintenance probability, as specified in 5.7.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.9.4.3b","Requirement","ECSS-E-ST-60-20_0920183","The probability of invalid attitude determination shall be estimated under the conditions given in given in 5.4 and 5.9.2.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.12e","Requirement","ECSS-E-ST-60-20_0920135","The functional mathematical model shall be validated against the actual temporal performances of the sensor.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-60-20C Rev. 2","5.13.4b","Requirement","ECSS-E-ST-60-20_0920190","The complete immunity of star tracker to flux levels shall be demonstrated. ","NOTE \tBy tolerance it is meant that determined error rates/probabilities are compliant with customer requirements\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-21C","5.1.1d","Requirement","ECSS-E-ST-20-21_1400004","An end to end test shall be performed to ensure that the actuator pulses are effectively present at actuator interface when a system level verification is done.","NOTE\tThe end to end test is performed with the actual flight actuator if resettable and safe. Alternatively, it is performed with a flight representative actuator or - if not possible for safety or practical reasons - with a load of the same impedance as the flight actuator.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-21C","5.2.2k","Requirement","ECSS-E-ST-20-21_1400025","No cross-strapping shall be present between electronics of nominal and redundant actuators chains.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-21C","5.2.3g","Requirement","ECSS-E-ST-20-21_1400032","The fire commands of the actuator electronics shall be inhibited by dedicated external inhibition straps.","NOTE\tstrap closed equals to commands disable, strap open equals to commands enable.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-21C","5.4.1e","Requirement","ECSS-E-ST-20-21_1400053","The current timing profile for voltage-driven actuators shall be provided by the system integrator.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-21C","5.6.3d","Recommendation","ECSS-E-ST-20-21_1400078","The maximum inductance of voltage-driven actuators should be 20 mH.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.2.2.2b","Recommendation","ECSS-E-ST-35-06_0200382","Tubings and manifolds should avoid blind holes and dead ends,",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.2.3c","Requirement","ECSS-E-ST-35-06_0200040","Filtration rate and capacity requirements shall include the flight operation and the contamination introduced by integration and testing at higher build level. \n    ","NOTE See Annex A.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.2.4d","Requirement","ECSS-E-ST-35-06_0200047","The GSE shall provide sampling interfaces and sampling equipment to verify cleanliness.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.3.4o","Requirement","ECSS-E-ST-35-06_0200068","The joining process shall not introduce contamination into the critical surface area or bring contaminants into contact with propellants, pressurants or simulation fluids.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.4.1b","Requirement","ECSS-E-ST-35-06_0200093","The results of 4.4.1a shall be reported in Annex A and Annex C.\n    ","NOTE Practical experience with standard hydraulic and pneumatic systems has shown that particles below 5 µm are not critical.",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.4.1e","Requirement","ECSS-E-ST-35-06_0200096","For systems, subsystems and components allowing the presence of particulate matter up to and including 5 mm, the particulate cleanliness requirements shall be based on the following three classes, the basis of each being a range of flow system external tube sizes:\n    1. Class 1, which applies for propulsion systems, or sections thereof with external tube sizes up to 20 mm (¾”).\n    2. Class 2, which applies for propulsion systems, or sections thereof with external tube sizes between 20 mm and 50 mm (¾” - 2”).\n    3. Class 3, which applies for propulsion systems, or sections thereof with external tube sizes exceeding 50 mm (>2”).",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","4.4.4j","Requirement","ECSS-E-ST-35-06_0200117","It shall be verified that the cleaning fluids meet their specifications. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","5.2.2b","Requirement","ECSS-E-ST-35-06_0200142","Decontamination shall take place in an approved facility.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","5.3.3.1b","Requirement","ECSS-E-ST-35-06_0200163","Alkaline cleaners and organic or water-based solvents shall be used for degreasing and removal of organic and inorganic contamination, e.g. scale and soluble metal oxides, see Annex D.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","5.5.1e","Requirement","ECSS-E-ST-35-06_0200184","The selected temperature for drying from liquids shall be within the operational temperature range of the liquid.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","5.5.3.1a","Requirement","ECSS-E-ST-35-06_0200191","The reliability of the dryness shall be verified by clause 5.5.3.2 or 5.5.3.3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","5.5.5.3d","Requirement","ECSS-E-ST-35-06_0200212","The oven shall be closed, purged and filled with inert test gas if required for the specific application.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","6.2.2e","Requirement","ECSS-E-ST-35-06_0200237","Polymer components for oxidiser systems shall be cleaned with a water-based process and blown dry with type A nitrogen conforming to ISO 14951-3:2000. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","6.2.3a","Requirement","ECSS-E-ST-35-06_0200240","The test fluid volume required for analysis shall depend upon the analytical methods employed. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","6.3.2a","Requirement","ECSS-E-ST-35-06_0200261","All temporary hardware necessary to perform or validate the cleaning process shall be compatible with the processing materials and the subsystem, system or other related field equipment that is to be cleaned.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","6.4.3d","Requirement","ECSS-E-ST-35-06_0200399","The method used for vaccum dryness shall be defined in the CTS DRD in conformance with Annex B.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","8.1g","Requirement","ECSS-E-ST-35-06_0200307","The item shall be double-bagged and packed to prevent damage during storage and handling.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","8.3b","Requirement","ECSS-E-ST-35-06_0200314","If the label cannot be placed between the inner and outer packaging film, the label shall be enclosed in a plastic bag or between layers of plastic film and secured to the outside of the package. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","11.1.3b","Requirement","ECSS-E-ST-35-06_0200335","A suitable test liquid, e.g. IPA, HFE or water, in conformance with Annex D, shall be passed through the item at a average velocity exceeding 1,25 m/s and not exceeding the operational flow rate.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-35-06C Rev.2","A.2.1<5>f","Requirement","ECSS-E-ST-35-06_0200356","In addition to particulate and NVR specifications the definition of the required dryness level and packaging requirements (protections) shall be presented.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.1.2a","Requirement","ECSS-E-ST-40-07_1440010","Simulation time shall be used for keeping the progress of time with respect to the start of the simulation, with the following properties:\n1.\tSimulation time is a non-negative Duration type;\n2.\tSimulation time is initialised to 0 at the beginning of the Building state as per Table 4-1;\n3.\tSimulation time changes only when:\n(a)\tThe simulation is progressing in the Executing state;\n(b)\tAs a result of a restore of a breakpoint in restoring state;\n(c)\tAs a result of ITimeKeeper SetSimulationTime.\n4.\tIt is not specified how quickly simulation time is progressed when the simulator is in Executing state;\n5.\tSimulation time is stored and restored in the storing and restoring states;",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.1.2d","Requirement","ECSS-E-ST-40-07_1440013","Epoch time shall be time dependent on the Simulation time with a fixed offset using the DateTime type.","NOTE\t1\tEpoch time progresses with Simulation time.\nNOTE\t2\tEpoch time is changed with the ITimeKeeper SetEpochTime (See 5.3.2).\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.3.1e","Requirement","ECSS-E-ST-40-07_1440035","The IComponent Connect method shall allow the components to connect to the simulator environment and other components, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“simulator” giving a pointer to the ISimulator interface as per ISimlator.h in [SMP_FILES] to access services from the simulation environment. \n2.\tBehaviour:\n(a)\tIf the Component is not in Configured state, it throws an InvalidComponentState exception as per InvalidComponentState.h in [SMP_FILES];\n(b)\tIf called in Configured state, the component enters Connected state;\n(c)\tAfter entering Connected state, it connects to simulation services used by the component, if any.","NOTE\tIt is guaranteed that all models have been created, published and configured before the Connect method of any component is called.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.5.2b","Requirement","ECSS-E-ST-40-07_1440060","The IContainer GetComponent method shall return the component matching the given name, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“name” giving the name of the component to be returned.\n2.\tBehaviour:\n(a)\tIf no component matching the given name is found, it returns nullptr.","NOTE\tAs the container does not support component name duplication, it is not possible to get naming conflict when performing query.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.7.1b","Requirement","ECSS-E-ST-40-07_1440081","The IEntryPoint Execute method shall be called when the triggering event is emitted.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.8.1d","Requirement","ECSS-E-ST-40-07_1440088","The IDynamicInvocation Invoke method shall invoke the method referenced, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“request” giving the identification of the callable method, as a fully populated request object implementing IRequest (see 5.2.8.2).\n2.\tBehaviour:\n(a)\tIf the operation specified by the request parameter is not callable through dynamic invocation, it throws an InvalidOperationName exception as per InvalidOperationName.h in [SMP_FILES];\n(b)\tIf the number of arguments specified by the request object does not match the number of parameters of the callable operation, it throws an InvalidParameterCount exception as per InvalidParameterCount.h in [SMP_FILES];\n(c)\tIf the types of the arguments specified by the request object do not match the types of parameters of the callable operation, it throws an InvalidParameterType exception as per InvalidParameterType.h in [SMP_FILES];\n(d)\tIf called with a valid request object, it calls the operation identified in the request, passing the parameters provided in the request which are of parameter direction In or InOut; \n(e)\tAfter invoking the request, it stores the parameter values of parameters with parameter direction InOut, Out or Return into the requests object.","NOTE\tThe Invoke operation is a void operation as the result of the invocation is stored in the IRequest object (see 5.2.8.2.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.10.2a","Requirement","ECSS-E-ST-40-07_1440109","All Simulation models which can be failed through a list of possible failures shall implement the IFallibleModel interface as per IFallibleModel.h in [SMP_FILES].","NOTE\t1\tThis is an optional interface. \nNOTE\t2\tThe simulation environment does not automatically persist the state of each failure, as it is the responsibility of the models to store the failure state in persisted data.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.2.11.5b","Requirement","ECSS-E-ST-40-07_1440130","The IField GetView method shall return the View Kind for the field. ","NOTE\tSee Table 4-2 for specification of View Kind.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.1f","Requirement","ECSS-E-ST-40-07_1440157","The ILogger Log method shall log a message, with the following arguments:\n1.\t“sender” giving the originator of the message;\n2.\t“message” giving the text to be logged;\n3.\t“kind” giving the registered log message kind for this message as returned from ILogger::QueryLogMessageKind method.\n(a)\tIf the LogMessageKind ID was not previously registered by using ILogger::QueryLogMessageKind, then it registers the passed LogMessageKind with text set to the passed number, followed by the sender’s Name and the string “undefined log message kind”. ","NOTE\tThis implicit registration of a new LogMessageKind ID allows to quickly identify models in a simulation that are logging using custom unregistered LogMessageKinds.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.2c","Requirement","ECSS-E-ST-40-07_1440160","The ITimeKeeper SetMissionStartTime method shall set a new start time for Mission time, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“missionStart” giving the new Epoch time for which the Mission time is zero.\n2.\tBehaviour:\n(a)\tAfter changing the MissionStartTime, it emits the SMP_MissionTimeChanged global SMP Event.","NOTE\tThis method changes the offset between the Epoch time and the Mission time.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.3m","Requirement","ECSS-E-ST-40-07_1440181","The IScheduler SetEventMissionTime method shall update the Mission time of the next execution of an Event with the following arguments and behaviour:\n1.\tArguments:\n(a)\t“eventId” giving the unique identifier of the Event;\n(b)\t“missionTime” giving the time of the next execution of the Event.\n2.\tBehaviour:\n(a)\tIf the given EventId is not currently on the scheduler, it throws an InvalidEventId exception as per InvalidEventId.h in [SMP_FILES]; \n(b)\tIf the Event identified by the given EventId is not scheduled on Mission time, it throws an InvalidEventId exception as per InvalidEventId.h in [SMP_FILES];\n(c)\tIf the mission time is before the current mission time, the Event is never executed but instead removed immediately from the scheduler;\n(d)\tWhen the Mission time of the next execution of an Event is updated, it takes effect on all future repeats of this Event as per the remaining “repeat” count and respecting the given cycle-time between each repeat.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.6c","Requirement","ECSS-E-ST-40-07_1440207","The ILinkRegistry GetLinkCount method shall return the link count between the given source and target, with the following arguments:\n1.\t“source” giving the source component;\n2.\t“target” giving the target component.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.7q","Requirement","ECSS-E-ST-40-07_1440228","The ISimulator AddModel method shall add a model to the models collection of the simulator, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“model” giving the model to be added.\n2.\tBehaviour:\n(a)\tIf the Simulation is not in Standby, Building, Connecting or Initializing state, it throws an InvalidSimulatorState exception as per InvalidSimulatorState.h in [SMP_FILES];\n(b)\tIf the name of the new model conflicts with the name of an existing model already added via AddModel, it throws a DuplicateName exception as per DuplicateName.h in [SMP_FILES];\n(c)\tIf the name of the new model conflicts with the name of an existing service already added via AddService, it throws a DuplicateName exception as per DuplicateName.h in [SMP_FILES].","NOTE\t1\tThe container for the models has no upper limit and thus the ContainerFull exception will never be thrown.\nNOTE\t2\tThe method will never throw the InvalidObjectType exception, as it gets a component implementing the IModel interface.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.7x","Requirement","ECSS-E-ST-40-07_1440235","The ISimulator GetResolver method shall return the interface to the mandatory resolver service.","NOTE\tThis is a type-safe convenience method, to avoid having to use the generic GetService() method. For the standardised services, it is recommended to use the convenience methods, which are guaranteed to return a valid reference.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.9.1b","Requirement","ECSS-E-ST-40-07_1440256","The IPublication GetTypeRegistry method shall return a reference to the Type Registry.","NOTE\tSee clause 5.3.10 for details on the Type Registry.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.3.10.1d","Requirement","ECSS-E-ST-40-07_1440277","The ITypeRegistry GetType method shall return the interface to the requested type, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“typeUuid” giving the Uuid for which the type are returned.\n2.\tBehaviour: \n(a)\tIf no type with the registered Uuid are found, it returns nullptr.","NOTE\tThis method can be used to find out whether a specific type has been registered before.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.1a","Requirement","ECSS-E-ST-40-07_1440302","The Catalogue file shall be in conformance with thc Catalogue file DRD of Annex A.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.2.1c","Requirement","ECSS-E-ST-40-07_1440305","Types that are used in another Type shall be visible for that Type.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.2.4d","Requirement","ECSS-E-ST-40-07_1440330","The Type link of an Association shall point to a Model, Interface or Value Type.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.2.9d","Requirement","ECSS-E-ST-40-07_1440351","A Field of a Structure shall be public.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.3g","Requirement","ECSS-E-ST-40-07_1440372","Each Field of a model or service that is of a type defined in a catalogue shall be defined in a catalogue.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","5.4.1.3n","Requirement","ECSS-E-ST-40-07_1440379","Each Reference of a model or service shall be defined in a catalogue.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.4.3d","Requirement","ECSS-E-ST-40-07_1440403","The Static attribute as per ecss.smp.smpcat in [SMP_FILES] shall have the following effect for the Field C++ mapping:\n1.\tIf set to “true”, then the C++ field includes the ‘static’ specifier as per “Field” template in Table 6-1;\n2.\tIf not set, then it has no effect;\n3.\tIf set to “false”, then it has no effect.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.4.6j","Requirement","ECSS-E-ST-40-07_1440427","The Const attribute as per ecss.smp.smpcat in [SMP_FILES] shall have the following effect for the Property C++ mapping:\n1.\tIf set to “true”, then the C++ mapping includes the ‘const’ specifier at the beginning, as per “Property Getter” and \"Property Setter\" templates in Table 6-1;\n2.\t2. If not set, then it has no effect;\n3.\t3. If set to “false”, then it has no effect.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.4.11c","Requirement","ECSS-E-ST-40-07_1440451","The Container member variable shall point to an implementation of the Smp::IContainer interface.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.5.1a","Requirement","ECSS-E-ST-40-07_1440457","For each type, a universally unique identifier (UUID) variable shall be declared as per “Uuid” template in Table 6-1.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.6.4a","Requirement","ECSS-E-ST-40-07_1440482","Exception types shall be mapped to ISO/ANSI C++ classes as follows:\n1.\tSyntax as per “Exception” template in Table 6-1;\n2.\tIf the Base element is defined, the class inherits from the Base class;\n3.\tIf the Base element is not defined, the class inherits from the default Exception class.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.1.7.4b","Requirement","ECSS-E-ST-40-07_1440503","Service classes shall have a default constructor.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.2.3j","Requirement","ECSS-E-ST-40-07_1440525","Packages shall map to either static or dynamic libraries.","NOTE\t1\tTwo dynamic library implementations are currently mapped\n·\tUnix Shared Object (SO)\n·\tWindows Dynamic Link Library (DLL)\nNOTE\t2\tThe requirements for the static library are common to all the dynamic library implementations, therefore they are not repeated in the corresponding clauses. The clauses on the dynamic library implementations cover only the specific delta specifications applicable to the case at hand.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-40-07C","6.2.5b","Requirement","ECSS-E-ST-40-07_1440532","A SMP bundle shall be composed by one or more package dynamic libraries, directly related to the SMDL packages.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20C Rev.1","4.1.2e","Requirement","ECSS-E-ST-20_0020005","An undetermined status at the interfaces of a powered unit shall not cause damage to an un-powered interface. ","NOTE \tUndetermined status includes: non-nominal operating modes, permanent and non-permanent failure modes, powered and un-powered interfaces.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","4.2.1f","Requirement","ECSS-E-ST-20_0020026","For redundant functions implemented on the same PCB, any deviation of the physical separation specified in 4.2.1e shall be tracked in the Critical item List.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","4.2.3b","Requirement","ECSS-E-ST-20_0020050","All external test connectors on a unit and spacecraft skin connectors shall be covered for flight.","NOTE \tUmbilical connectors (detached during launch) are not part of skin connectors (detached or connected before launch).\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","4.2.3e","Requirement","ECSS-E-ST-20_0020053","It shall be ensured that erroneous mating is avoided by connector keying or marking.","NOTE \tThe requirement is met either by harness routing, or by using keyed connectors, or adequate positioning of connectors, or connectors of different type or size, or connector marking.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","4.2.4o","Requirement","ECSS-E-ST-20_0020078","Protection functions within a unit protecting other units shall be verified by test at system level or at unit level with representative interfaces.","NOTE\t1\tThis is the case e.g. of a battery discharge regulator switching OFF autonomously at low input voltage to protect a Li-ion battery against irreversible damage to overdischarge.\nNOTE\t2\tIn the case of the LCL in power distribution, the limitation of current at turn-on is considered representative for validation of the protection at system level.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.3b","Requirement","ECSS-E-ST-20_0020097","It shall not be possible to inhibit a protection feature if such an inhibition can lead to the loss of the main primary power bus in case of a single failure at spacecraft level.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.5.2n","Requirement","ECSS-E-ST-20_0020118","<<deleted>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.5.3d","Requirement","ECSS-E-ST-20_0020125","The EOL solar cell I(V) curve shall be derived from measurements performed at the temperatures specified in 5.5.3c after irradiation with particles in conformance with the “Electron irradiation” and “Proton irradiation” tests for “Bare solar cells” specified in ECSS-E-ST-20-08 clause 7, and agreed with the customer.","NOTE \tThe irradiated particles can either electrons or protons. The irradiation particles can be electrons or protons, chosen in order to facilitate the calculation of degradation, ideally using the particle type that dominates the degradation during the mission.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.6.2k","Requirement","ECSS-E-ST-20_0020146","Provisions for interfacing the battery with the ground support equipment during pre-launch operations shall be made.","Such provisions can include:\n· signal lines for monitoring battery voltage,\n· signal lines for monitoring battery temperature,\n· capability to charge the battery,\n· capability to discharge the battery.",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.7.2a","Requirement","ECSS-E-ST-20_0020170","No single failure shall result in the loss of the power subsystem capability to the extent that the minimum mission requirements, in any of its phases, cannot be fulfilled.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.7.3b","Requirement","ECSS-E-ST-20_0020190","<<deleted>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.7.3e","Requirement","ECSS-E-ST-20_0020193","<<deleted>>",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.8.1c","Requirement","ECSS-E-ST-20_0020218","All non-protected sections of a primary bus generation and distribution system shall be protected as a minimum by double insulation (including harness, connector, wiring and PCB) up to the first protection device (fuse, current breaker or current limiter).",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","5.8.1x","Requirement","ECSS-E-ST-20_0020422","The requirement 5.8.1k shall be verified by worst case analysis, in accordance with ECSS-Q-ST-30 Annex J, and test.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","6.2.1a","Requirement","ECSS-E-ST-20_0020252","The supplier shall establish an overall EMC programme.","NOTE\t1\tThe EMC programme is an activity the purpose of which is to provide for spacecraft-level compatibility with the minimum impact to programme cost, schedule and operational capabilities. The role of the customer in the EMC programme is that of top-level oversight.\nNOTE\t2\tThe EMC programme is based on requirements of this standard, the statement of work, spacecraft specification, and other applicable contractual documents.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","6.2.3c","Requirement","ECSS-E-ST-20_0020258","The supplier shall chair the EMCAB, with customer oversight. ","NOTE\t1\tThe EMCAB members are representatives of the Spacecraft Supplier and payload suppliers and users.\nNOTE\t2\tEMCAB members can invite associate suppliers or independent experts. \nNOTE\t3\tThe EMCAB accomplishes its duties and document its activities mainly through the use of the system-level EMC documentation.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","6.3.6c","Requirement","ECSS-E-ST-20_0020279","The RF compatibility analysis, if used instead of test, shall include the effects of inter-modulation products.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","7.2.2.2.3c","Requirement","ECSS-E-ST-20_0020304","Deformations of array antennas, which parts are physically attached to different portions of the spacecraft platform, shall be quantified ant their impact on antenna performance assessed.","NOTE \tFor large array antennas that use hold-down and release, deployment mechanisms as well as pointing devices, ECSS-E-ST-33-11 can be applied.\n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","7.2.2.3.5a","Requirement","ECSS-E-ST-20_0020325","The circuit characteristics of the antenna RF chain shall be independently quantified and their impact on antenna performances assessed at least up to CDR.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","7.2.2.3.5d","Requirement","ECSS-E-ST-20_0020328","For antenna RF chain the design and manufacturing shall be performed to avoid discharge phenomena according to Paschen curves valid for its specified pressure range and gas properties.","NOTE \tSee clause 7.3 for further details. \n",{"$nulls":3},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","7.3.4a","Requirement","ECSS-E-ST-20_0020353","The following criteria shall be met for qualification for power handling and gas discharge:\n1.\tthe RF component and equipment has no physical degradation,\n2.\tthe RF component and equipment has no degradation of the RF performance during and after the test.",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20C Rev.1","B.2.1e","Requirement","ECSS-E-ST-20_0020373","An intra-system compatibility culprit/victim test matrix shall be included in the EMEVP, showing all combinations of individual equipment/subsystems to be tested in order to verify overall intra-system compatibility;",{"$nulls":4},"active","Engineering","Level 1"]
["ECSS-E-ST-20-01C","4.1a","Requirement","ECSS-E-ST-20-01_1450001","The process of verification of the equipment with respect to multipactor performance shall demonstrate conformance to the margin requirements defined in clauses 4.6 and 4.7.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","4.3.1.3d","Recommendation","ECSS-E-ST-20-01_1450024","For multipactor design and verification, failure modes that are not recoverable should not be taken.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","4.7.3.1a","Requirement","ECSS-E-ST-20-01_1450052","The test margin shall be defined according to the equipment or component type and the heritage.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","5.3.2.2.4d","Requirement","ECSS-E-ST-20-01_1450078","The customer and supplier shall agree on the method for the computation of the multipactor threshold voltage, specified in 5.3.2.2.4c. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","5.3.3.3a","Requirement","ECSS-E-ST-20-01_1450099","SEY data used in the analysis shall be representative of the material in the critical part of the equipment and come from either measured SEY or ECSS SEY. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","5.3.3.3d","Requirement","ECSS-E-ST-20-01_1450102","If no ad-hoc SEY measurement data are available, and the material is not listed in Table 9-1, no analysis is possible and the equipment or component shall be classified as P3.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","6.4.3.1a","Requirement","ECSS-E-ST-20-01_1450128","A test with a single carrier, applying an equivalent power as specified in clause 6.4.3.2. shall be performed. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","6.5.5d","Requirement","ECSS-E-ST-20-01_1450149","At least one of the following seeding sources shall be used: \n1.\tUV light source, which produces electrons by the photoemission mechanism. \n2.\tAn electron gun, which produces a known beam of electrons where both the energy and flux can be characterised.\n3.\tA charged wire probe, which produces electrons by the point discharge mechanism.\n4.\tRadioactive β source, which produces high-energy electrons that, after impacting with metal surfaces or propagation though metallic or dielectric walls, yield a supply of secondary low energy seed electrons.","NOTE\tIf a metallic or dielectric wall is too thick, the high-energy electrons will not be able to propagate and the supply of secondary low energy electrons will not be sufficient. Recommendations for wall thickness are provided in the Multipactor handbook ECSS-E-HB-20-01.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","7.3.2a","Requirement","ECSS-E-ST-20-01_1450156","When phase nulling is used as a detection technique, it shall be tuned regularly throughout the test campaign by minimising the null level, in order to maximise detection sensitivity.","NOTE\tIt is good practice that the lowest residual level of the nulling system is kept at least 45 dB below the level obtained with only one of the two nulling paths connected to the detection system.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","8.3c","Requirement","ECSS-E-ST-20-01_1450177","The second step shall be performed immediately after the multipactor test of the equipment, depending on its outcome.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","8.5.3b","Requirement","ECSS-E-ST-20-01_1450198","The results of the investigation of 8.5.3a.9 shall be reported to the customer to conclude on the nature of the discharge or event.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-20-01C","9.4.2.4b","Requirement","ECSS-E-ST-20-01_1450223","For each incident energy, this reference condition shall be recovered.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","6.2.1a","Requirement","ECSS-E-ST-10-04_0760014","The values in Table 6-2 shall be used for the electromagnetic radiation. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","6.2.2a","Requirement","ECSS-E-ST-10-04_0760017","For daily and 81-day averaged values of F10.7, S10.7 and M10.7 the values given in Table A-1 shall be used.","NOTE\t1\tAp is only weakly correlated with the solar activity indices. It has a seasonal variation and is higher at the equinoxes.\nNOTE\t2\t81 days corresponds to 3 solar rotations and 81 day averaged values are used as input for atmosphere models.\nNOTE\t3\tAlternative daily and 81-day average values and forecast methods are available [ISO 27852:2016]. Their values can be more appropriate depending on the use-case.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","8.2.2d","Requirement","ECSS-E-ST-10-04_0760041","For future dates not covered by the default files, for F10.7 and ap the activity indices defined in clause 6 and corresponding values for IG12 and Rz12 shall be used. ","NOTE \tInformation on the accuracy of the IRI-2016 model and typical ionospheric density profiles are given in Annex H.3.1\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","9.2.1.2.1c","Requirement","ECSS-E-ST-10-04_0760059","The mission duration parameter used with the IGE2006 model shall be rounded up to the nearest integral year.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","9.2.1.2.2f","Permission","ECSS-E-ST-10-04_0760130","For trapped electron fluxes at altitudes between 20 500 km and 24 000 km and the Inclination range of 55° ± 5°, either the AE-8 or the MEOv2 model may be used.","NOTE \tIf used above 20 500 km altitude the MEOv2 model can provide conservative results. More information on this model is given in Annex I.\n",{"$nulls":3},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","9.2.7a","Requirement","ECSS-E-ST-10-04_0760143","The interplanetary environment shall apply for the energetic particle environment at L2 and the deep tail.",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","10.2.2.2b","Requirement","ECSS-E-ST-10-04_0760092","The models specified in 10.2.2.2a and 10.2.2.2h shall be used for all mission durations. ",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-E-ST-10-04C Rev.1","11.2b","Requirement","ECSS-E-ST-10-04_0760112","<<deleted>>",{"$nulls":4},"active","Engineering","Level 2"]
["ECSS-M-ST-10-01C","5.3.3a","Requirement","ECSS-M-ST-10-01_0310019","The supplier shall support the customer in providing all facilities and logistics for the review meetings and sessions as required by the customer.",{"$nulls":4},"active","Management","Level 2"]
["ECSS-M-ST-10-01C","5.3.5a","Requirement","ECSS-M-ST-10-01_0310026","The review team shall:\n    1. Review the documentation\n    2. Identify problems, make recommendations or request explanations by means of RIDs\n    3. Assess the adequacy of the responses to RIDs\n    4. Support the review team leader in preparing the report.",{"$nulls":4},"active","Management","Level 2"]
["ECSS-M-ST-10-01C","A.2.1<1>a","Requirement","ECSS-M-ST-10-01_0310047","The review procedure shall provide an overview of the status of the project under review and the purpose and scope of the review.",{"$nulls":4},"active","Management","Level 2"]
["ECSS-M-ST-10C Rev. 1","5.2.1.2a","Requirement","ECSS-M-ST-10_0010014","The supplier shall set up the project management organization in such a way that adequate resources are allocated to the project to ensure timely completion of the business agreement.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-10C Rev. 1","5.2.1.2h","Requirement","ECSS-M-ST-10_0010021","The first level supplier shall establish, maintain and distribute a project directory including key personnel, as a minimum.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-10C Rev. 1","5.2.3.3b","Requirement","ECSS-M-ST-10_0010042","The supplier shall have the right to demand that the audit be performed by a third party, and that the third party obtain authorization each time the audit necessitates access to information concerning patent rights or confidentiality associated with defence secrecy.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-10C Rev. 1","5.3r","Requirement","ECSS-M-ST-10_0010063","The supplier shall maintain the approved OBS, keep it up-to-date, and issue it to the lower tier suppliers and the customer.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-10C Rev. 1","B.2.1<3>d","Requirement","ECSS-M-ST-10_0010088","Each product item selected as configuration item shall be identified in the product tree.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.2.1.3d","Requirement","ECSS-M-ST-40_0320010","Classified information shall be used only in a secure environment or location.\n    NOTE For example: area limited in access.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.2.2c","Requirement","ECSS-M-ST-40_0320017","Configuration management processes shall interface with IDM for defining rules for documentation identification and processing, control and distribution.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.1.6e","Requirement","ECSS-M-ST-40_0320043","The system shall be able to manage check-in/check-out, multiple versions.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.2.2e","Requirement","ECSS-M-ST-40_0320060","Major planned departures shall be processed as for class 1 changes.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.2.4a","Requirement","ECSS-M-ST-40_0320067","Both customer and supplier shall establish procedures for the analysis, review and disposition of proposed changes.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.3.2d","Requirement","ECSS-M-ST-40_0320088","The complete CIDL for an individual CI, model or deliverable item shall be available at project reviews.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.7.2.1a","Requirement","ECSS-M-ST-40_0320109","Responsibility for the information/documentation content shall lie with the organization closest to the data source.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.7.3.2a","Requirement","ECSS-M-ST-40_0320134","Information/documentation shall be signed using digital signature.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","5.3.7.5d","Requirement","ECSS-M-ST-40_0320155","Information/documentation shall be protected against environmental and accidental risks and against unauthorized access.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","A.2.1<3.1>b","Requirement","ECSS-M-ST-40_0320162","The configuration management plan shall also describe the interface with other CM organizations (customer and supplier) and the CM relationship to other internal organization elements.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","A.2.1<4.7>c","Requirement","ECSS-M-ST-40_0320183","The configuration management plan shall identify how the recording, reporting and tracking of action items and incorporation of review recommendations are maintained.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","B.2.1<1>a","Requirement","ECSS-M-ST-40_0320204","The introduction shall describe the purpose and objective of the configuration item list.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","D.2.1<1>a","Requirement","ECSS-M-ST-40_0320211","The introduction shall describe the purpose and objective of the as-built configuration list.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-40C Rev. 1","F.2.1<2>a","Requirement","ECSS-M-ST-40_0320232","The configuration status accounting reports shall list the applicable and reference documents in support to the generation of the document",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","8.2f","Requirement","ECSS-M-ST-60_0300020","The supplier shall notify the customer, independently from the nominal reporting cycle, within a short time notice agreed upon between the parties\n    1. any event that can significantly affect the achievement of the agreed schedule objectives, and\n    2. any situation resulting in a substantial schedule change.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","9.3.1.1a","Requirement","ECSS-M-ST-60_0300041","The supplier shall provide the Original Baseline Cost Plan (OBCP) for himself and for all his suppliers in conformance with Annex K, OBCP and CBCP DRD for Cost Reimbursement, for customer approval.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","9.4.2b","Requirement","ECSS-M-ST-60_0300062","The supplier shall dispose of items under his custody according to the Customer’s requirements in conformance with the approved Inventory Control Plan.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","C.2.1a","Requirement","ECSS-M-ST-60_0300069","The schedule progress report shall provide following information:\n    1. baseline schedule and associated key milestones;\n    2. current working schedule;\n    3. milestone trend analysis for the key milestones;\n    4. clarification and justification on deviations with respect to the baseline schedule;\n    5. proposal of remedy actions;\n    6. validity assessment of defined sequences, relationships and constrains of the planned activities;\n    7. status of deliverable items.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","G.2.1<2>a","Requirement","ECSS-M-ST-60_0300089","The cost estimate report shall contain the list of applicable and reference documents, used in support to the generation of the document. ",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","J.2.1<1>a","Requirement","ECSS-M-ST-60_0300110","The header shall include:\n    1. Project title and business agreement number\n    2. Date of issue\n    3. Currency\n    4. Current economic conditions considered\n    5. Applicable project schedule\n    6. Control work package reference",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-60C","K.2.1<5>a","Requirement","ECSS-M-ST-60_0300117","The up to date price variation mechanism information, taking into account all agreed CCNs for the CBCP (price escalation formula, indices, agreed amounts serving as the basis for escalation computation), shall be provided for all lower-tier suppliers under the supplier’s responsibility.",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-80C","7.2.8a","Requirement","ECSS-M-ST-80_0340008","Options for acceptance of resolved, acceptable and overall risks shall be defined where appropriate and presented to the appropriate management level, as defined in the risk management plan, for disposition.","NOTE The aim is determination and implementation of the appropriate risk resolution options. ",{"$nulls":3},"active","Management","Level 1"]
["ECSS-M-ST-80C","A.2.1<14>a","Requirement","ECSS-M-ST-80_0340033","The risk management policy document shall describe the risk management process to be employed i.e. the review, decision and implementation flow within the project concerning the risk planning, identification, assessment and identification, handling, monitoring and documentation functions. ",{"$nulls":4},"active","Management","Level 1"]
["ECSS-M-ST-80C","B.2.2a","Permission","ECSS-M-ST-80_0340078","The response to this DRD may be combined with the response to the risk management policy document DRD, ECSS-M-ST-80 Annex A",{"$nulls":4},"active","Management","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.2.3a","Requirement","ECSS-Q-ST-20_0380009","The supplier shall manage alerts in conformance with ECSS-Q-ST-10, clause 5.2.9.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.2.5a","Requirement","ECSS-Q-ST-20_0380017","The supplier shall ensure that a bidirectional and unequivocal relationship between parts, materials or products and associated documentation or records is established and maintained.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.2.6q","Requirement","ECSS-Q-ST-20_0380038","The supplier shall make the measurement design data available to the customer upon request.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.3.2.1e","Requirement","ECSS-Q-ST-20_0380059","The supplier shall ensure that appropriate reference to the verification documentation is recorded and status updated at project reviews up to final acceptance.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.3.2.3a","Requirement","ECSS-Q-ST-20_0380062","The supplier shall ensure that design reviews are conducted in accordance with project requirements and written procedures.","NOTE\tDesign reviews address the following items:\n·\tQuality requirements and criteria for design, producibility, repeatability, testability and operability are adequately considered in design documentation.\n·\tMethods and data required for procurement, manufacturing, inspection and test are available and validated.\n·\tRisks of not achieving requirements are highlighted and adequately controlled.\n",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.4.1.3b","Requirement","ECSS-Q-ST-20_0380079","The supplier shall submit to the customer, upon request, the list of procurement sources, including all the information in the records 5.3.1.3a, for information.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.5.3.1a","Requirement","ECSS-Q-ST-20_0380104","The supplier shall monitor all processes used for manufacturing, assembly and integration, and enforce all applicable process requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.5.5c","Requirement","ECSS-Q-ST-20_0380115","Sensitive items shall be processed or manufactured, inspected and tested in a controlled environment to prevent any degradation. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.5.9.1b","Requirement","ECSS-Q-ST-20_0380145","The control shall be initiated upon installation or removal of the first temporarily installed or removed item and be maintained through delivery and use of the end item.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.5.9.2e","Requirement","ECSS-Q-ST-20_0380152","The receiving organization shall maintain the logbook up-to-date.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.6.5b","Requirement","ECSS-Q-ST-20_0380170","The QA organization shall be represented in the formal boards established for the review of readiness for testing and testing accomplishment.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.8.3.2b","Requirement","ECSS-Q-ST-20_0380240","If supplier or lower level suppliers deviate from standard practices, as required per 5.7.3.2a, the new practices shall be validated.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","5.8.4.2b","Requirement","ECSS-Q-ST-20_0380197","The acceptance process shall include:\n1.\tacceptance plan,\n2.\tinspection and test procedures, and\n3.\tinspection and test reports.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-20C Rev.2","C.2.1b","Requirement","ECSS-Q-ST-20_0380216","The logbook shall contain the “hardware configuration and traceability” table, which reports all the identification references of single elements composing the CI. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70-54C","5.2.2b","Requirement","ECSS-Q-ST-70-54_1360017","The critical contaminants shall be representative for the expected hardware contamination in terms of type, amount, and surface interaction.","NOTE \tCorrelation between model and real contamination can be made, e.g. by estimation of cleaning efficacy via adhesion forces.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-54C","5.2.7.1c","Requirement","ECSS-Q-ST-70-54_1360037","The statistical confidence level of the cleaning efficacy shall be derived using a customer agreed statistical approach.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-04C","5.1.1e","Requirement","ECSS-Q-ST-10-04_0180005","The supplier shall define evaluation points for assessing the implementation of critical-item control measures.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-04C","5.2.2.1a","Requirement","ECSS-Q-ST-10-04_0180012","The supplier shall identify the applicable requirements for CI control and document the implementation approach chosen in the project’s Product Assurance Plan ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-04C","5.2.4.4d","Requirement","ECSS-Q-ST-10-04_0180033","The supplier shall iterate task 7 (requirements 5.2.4.2a to 5.2.4.2c) and task 8 (requirements 5.2.4.3a to 5.2.4.3b) for non-successfully controlled critical items until they become successfully controlled or - if failing to do so - request disposition by higher management. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-04C","A.2.1<7>a","Requirement","ECSS-Q-ST-10-04_0180058","This list shall contain planned activities to reduce or control the risk as defined in 5.2.4.2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-04C","A.2.1<9>a","Requirement","ECSS-Q-ST-10-04_0180061","The list shall provide the status of action as “Open” or “Closed”.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.2.1.3d","Requirement","ECSS-Q-ST-20-10_1120021","The supplier shall identify all the OTS item functions which can lead to negative effects.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.3.2.1.5c","Requirement","ECSS-Q-ST-20-10_1120046","The supplier shall verify the possibility that the manufacturer can provide spares throughout the project duration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.3.2.3.1f","Requirement","ECSS-Q-ST-20-10_1120067","The supplier shall perform PCB inspection to identify used parts.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.3.2.4.1a","Requirement","ECSS-Q-ST-20-10_1120074","The supplier shall perform inspection on OTS item.","NOTE This inspection aims at improving confidence on provided part list and when no list is provided to identify constituent materials and mechanical parts.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.4.3.2b","Requirement","ECSS-Q-ST-20-10_1120095","AC/DC shall not be used in space applications.","NOTE This constraint forces to remove or to exclude the unit power supply and redesign it. ",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-10C","5.5a","Requirement","ECSS-Q-ST-20-10_1120116","Based on the data collected and on the results achieved during the characterization phase, the supplier shall decide if to propose the final buy approach, not later than the system PDR.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","4.1a","Requirement","ECSS-Q-ST-30-02_0390001","The FMEA shall be initiated for each design phase as indicated in clause 6 and updated to reflect design changes along the project life cycle.\n    NOTE The FMEA is an integral part of the design process as one tool to drive the design along the project life cycle.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","4.1d","Requirement","ECSS-Q-ST-30-02_0390004","The FMEA shall be used in the definition of:\n    1. failure tolerance design provisions (i.e. redundancy, inhibits, FDIR),\n    2. special test considerations,\n    3. maintenance actions (preventive or corrective),\n    4. operational constraints.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","4.6a","Requirement","ECSS-Q-ST-30-02_0390025","All mission phases and related operational modes (including “safe mode”), unless otherwise agreed with the customer, shall be addressed by the FMEA.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","5.2m","Requirement","ECSS-Q-ST-30-02_0390050","The CN for a specific failure mode shall be developed from the severity of the failure effects and the probability of the failure mode occurrence. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","6.5d","Requirement","ECSS-Q-ST-30-02_0390071","The FMEA/FMECA shall provide the following results:\n    1. Identification of the methods for preventing or compensating failure effects of critical items.\n        NOTE Examples of these methods are: redundancies and inhibits.\n    2. Verification that the anticipated actions are able to prevent or control the consequences.\n    3. Identification of remaining single point failures and identification of compensating features if the elimination is not possible or impractical.\n    4. Input to safety analyses.\n        NOTE An example of this input is the identification of the implemented preventing or compensating methods for each identified hazardous consequence.\n    5. Input to the critical function list or critical item list.\n        NOTE An example of this input is the identification of the items (component or equipment) to be considered critical according to the provided criticality definition.\n    6. Input to the FDIR system activity:\n        (a) list of specific monitor parameters that allow the failure to be detected;\n        (b) verification of the effectiveness of the recovery methods or proposal of alternative methods;\n        (c) identification of failure modes that are not monitored.\n    7. Input to operation definition activity,\n        NOTE Examples of these inputs are the identification of crew and system operations implemented to prevent or control critical dependability and safety events and verification of their capability to effectively control the failure consequences.\n    8. Input to test definition activity (if required at the analysed integration level).\n        NOTE Examples of input to test definition activity are:\n            · List of failure modes with relevant effects and observable symptoms provided for generating test requirements and procedures.\n            · Identification of functional paths and redundancies that cannot be tested.\n            · Identification of tests to verify the assumptions used within the FMEA/FMECA that the system reacts according to the anticipated manner.\n    9. Input to user manual and operation procedures.\n        NOTE For example, at system level the list of failure modes with relevant effects and observable symptoms are provided for establishing data recording requirements, and to determine the required frequency of monitoring in testing, check-out and mission use.\n    10. Input to contingency analysis. \n        NOTE The FMEA/FMECA provide input such as failure detection means-observable symptoms and compensating provisions for the implementation of the contingency analysis.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","7.2a","Requirement","ECSS-Q-ST-30-02_0390078","The HSIA shall be performed concurrently with the FMEA/FMECA to influence the hardware design and the software requirements.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","8.5a","Requirement","ECSS-Q-ST-30-02_0390100","If the process step is regarded as critical (according to the criteria in clause 8.4) a recommendation shall be given.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","A.2.1<7>c","Requirement","ECSS-Q-ST-30-02_0390121","Description and listing of any incomplete design areas shall be identified.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","C.2.1<3>a","Requirement","ECSS-Q-ST-30-02_0390146","The FMECA worksheet shall contain an assessment of the probability of occurrence of the assumed failure mode and the relevant probability number (PN)\n    NOTE The PNs applied at the different probability levels are given in Table 5-2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","D.2.1<13>a","Requirement","ECSS-Q-ST-30-02_0390161","The HSIA form shall contain recommendations in case of insufficient S/W actions or in case of adverse effect on H/W.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-02C","F.2.1<6>a","Requirement","ECSS-Q-ST-30-02_0390175","Depending on the process analyzed and on the purpose of the analysis, the Process FMECA worksheet shall contain the description of all possible effects of the assumed failure modes on: \n    1. Safety,\n    2. Product (i.e. final result of the process),\n    3. Process,\n    4. Programmatic \n        NOTE For example, impact on costs schedule.\n    5. Others, if any\n        NOTE For example, company image.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-09C","5.2.3.2b","Requirement","ECSS-Q-ST-30-09_0400014","For non-maintainable systems, the availability at a specific time requirement shall specify by a single requirement both the availability and reliability characteristic.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-09C","6.4a","Requirement","ECSS-Q-ST-30-09_0400035","The availability analysis performed in each project phase shall contribute to the preparation of the following:\n    1. specifications,\n    2. trade-off reports, and\n    3. availability assessment reports.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-09C","7.2.1a","Requirement","ECSS-Q-ST-30-09_0400042","During Phase A, the availability analysis shall cover the following aspects:\n    1. Identification of the methodology for the most realistic evaluation of the availability figures.\n        NOTE The methodology can be improved or even changed in the following phases.\n    2. Support to the preliminary design definition in terms of trade-off studies, rough availability estimations, identification of critical areas.\n    3. Evaluation of the availability performance of the selected reference system or equipment baseline.\n    4. Allocation (where necessary) of the applicable requirements at lower level.\n    5. Planning of the availability tasks for the design definition phase (Phase B or Phase C).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-40-12C","5.1.3a","Requirement","ECSS-Q-ST-40-12_0430007","When using a computer program to support the FTA, the supplier shall use a computer program which fulfils the following criteria:\n    1. it supports the functionality which is necessary to perform the FTA;\n    2. it is compatible with project requirements for electronic data transfer and the interchange of data between interacting programs or tools.\n        NOTE Although there are several proprietary software programs available for various platforms designed to assist the FT analyst, this ECSS Standard does not endorse any particular product.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.3.3.1b","Requirement","ECSS-Q-ST-60-02_0450021","As a minimum, the following tasks shall be performed and documented:\n    1. Estimate design complexity;\n    2. Estimate power consumption;\n    3. Assess feasibility of speed requirements by a preliminary timing analysis;\n    4. Select a radiation hardening approach that ensures compliance with radiation tolerance requirements. Determine a rough estimate of impact on chip area and circuit speed;\n    5. Select a production test approach and its feasibility against all requirements;\n    6. Identify and evaluate the suitability and qualification status of the ASIC technologies or FPGA available to implement the device, fulfilling all functional and non-functional requirements including the specified derating factors. Make a baseline selection;\n    7. Identify packages, fulfilling all requirements. Make a baseline selection;\n    8. Ensure that the baseline technology and package or FPGA have a remaining lifetime, so that flight and compatible prototype parts can be manufactured and are available during the expected procurement phase(s);\n    9. Ensure that technical support for the device can be guaranteed during the expected lifetime;\n    10. Determine availability and status of the required design and test tools (H/W & S/W) and libraries;\n    11. Determine availability of the necessary human resources;\n    12. Determine availability, licensing, support, legal and economical aspects of using IP cores from third parties;\n    13. Ensure that no patents are infringed or agreements exist or can be made with the patent holder.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.4.6e","Requirement","ECSS-Q-ST-60-02_0450046","The reviewers shall check that the architectural design documentation (see clause 7.3.4) together with the documentation of previous development phases is complete, traceable and documented in a level of detail that allow to proceed with the detailed design.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.5.2a","Requirement","ECSS-Q-ST-60-02_0450049","Influences from layout such as cross talk and matching shall be accounted for during the design work. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.6.1a","Requirement","ECSS-Q-ST-60-02_0450074","The layout shall generate the placement and routing information to meet the design rules, timing and other constraints. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.7.2g","Requirement","ECSS-Q-ST-60-02_0450095","The correctness of the FPGA programming shall be verified (checksum test). \n    NOTE This is only applicable for FPGA designs.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","5.8.5d","Requirement","ECSS-Q-ST-60-02_0450116","An application note (see clause 7.4.2) shall be established.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","6.1a","Requirement","ECSS-Q-ST-60-02_0450123","ECSS-Q-ST-20 clause “QA status reporting” shall apply.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","6.3d","Requirement","ECSS-Q-ST-60-02_0450144","A check of the risk mitigation activities shall be a major item of the agenda of every review meeting.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","7.4.2a","Requirement","ECSS-Q-ST-60-02_0450165","If requested by the customer, an application note shall be established for components that are regarded as standard parts for a variety of system applications. This note shall provide information to guide the reader through the possible configurations the device or module can be operated with examples for the corresponding bias circuitry, supply voltages and configuration signals shall be provided.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","G.2.1e","Requirement","ECSS-Q-ST-60-02_0450190","All signal interfaces shall be described in detail including for instance a description of all signals, test and power pins, specifying e.g. the usage of the signals and the signal polarity. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-02C","G.2.1h","Requirement","ECSS-Q-ST-60-02_0450193","A preliminary data sheet shall contain all parts of a final data sheet, with the same level of detail. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","6.2.4.2c","Permission","ECSS-Q-ST-60-05_0160236","In case of confidentiality of particular materials or processes, claimed by category 2 manufacturers, the HTIF attached to the PAD may leave undisclosed the confidentiality elements, provided that these aspects are covered and discussed during the quality and technical audit as described in clause 6.3.3.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","7.3.4b","Permission","ECSS-Q-ST-60-05_0160238","A “recurrent” hybrid circuit may be manufactured without any further design validation. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","8.2.3b","Requirement","ECSS-Q-ST-60-05_0160064","The LAT acceptance criteria shall be as given in Table 8-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","8.3.2c","Requirement","ECSS-Q-ST-60-05_0160071","For bimetallic bonding (gold-aluminium) ageing (1 h at 300 °C or the equivalent time-temperature combination with a 0,92 eV activation energy basis) shall be performed before the pull test.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","9.4b","Requirement","ECSS-Q-ST-60-05_0160092","The definition of the materials and piece parts shall be specified in the procurement specification.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","10.3.3d","Requirement","ECSS-Q-ST-60-05_0160118","The total burn-in time shall not be less than 240 h.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","10.4.1.4b","Permission","ECSS-Q-ST-60-05_0160249","Background noise may be excluded, except those caused by the shock blows, during the monitoring periods.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","10.4.2b","Requirement","ECSS-Q-ST-60-05_0160142","If the cumulative total of parameter drift failures (see clause 10.4.1.2) and parameter limit failures (see clause 10.4.1.3) exceeds 10 % PDA of the number of hybrids submitted to the burn-in and electrical measurements, the lot shall be rejected.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","11c","Requirement","ECSS-Q-ST-60-05_0160167","The customer shall be invited to the following key inspections: \n    1. pre-cap visual inspection;\n    2. final acceptance of the hybrids after the performance of all tests including LAT.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","13.1a","Requirement","ECSS-Q-ST-60-05_0160188","The delivery of hybrid items shall be agreed with the customer at the contract negotiation stage. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","B.2.2<2>a","Requirement","ECSS-Q-ST-60-05_0160209","This table shall list the parameters measured, their units, symbol, measurement conditions, and minimum and maximum values.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-05C Rev. 1","B.2.2<7>a","Requirement","ECSS-Q-ST-60-05_0160216","This table shall list the oven temperature and power applied to comply with ECSS-Q-ST-60-05, clause 10.3.9.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","5.3b","Requirement","ECSS-Q-ST-60-12_0190012","Any non-standard models and design tools shall be justified, and approved by the customer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","7.2.8c","Requirement","ECSS-Q-ST-60-12_0190041","For a cascaded structure, as a minimum, the stability of each block shall be checked individually.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","7.2.11c","Requirement","ECSS-Q-ST-60-12_0190062","For all the points not covered by requirements 7.2.11a and 7.2.11b, the supplier shall demonstrate that the design is made within a domain for which the selected process is fully proven. \n    NOTE E.g. frequency range of applicability of models, biasing ranges.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","7.3.1c","Requirement","ECSS-Q-ST-60-12_0190065","When the design is completed, the designer shall send the file to the manufacturer for assembly of the final reticule and performance of the DRC. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","7.3.12a","Requirement","ECSS-Q-ST-60-12_0190090","The development plan of the circuit(s) defining the planning of manufacturing and testing shall be agreed upon by the entity in charge of the procurement of the MMIC.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.1.2b","Requirement","ECSS-Q-ST-60-12_0190111","Dies incoming inspection (hybrid manufacturer responsibility), in conformance with requirements in clause 10.3.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.2.4.4d","Requirement","ECSS-Q-ST-60-12_0190132","For requirement 10.2.4.4c, a document shall be issued by the user stating that the assembly process used by the manufacturer is representative of the hybrid process.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.2.6b","Requirement","ECSS-Q-ST-60-12_0190139","If a data package is not delivered, all data shall be retained by the manufacturer for a minimum of 5 years during which time it shall be available to the customer for review, upon request.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.4.1.2g","Requirement","ECSS-Q-ST-60-12_0190160","The screening of the assembled devices shall include the following:\n    1. visual inspection (if specified);\n    2. sealing and serialization;\n    3. hermeticity (if applicable) (fine and gross leak test) as per MIL-STD-883 method 1014;\n    4. DC and RF initial electrical measurement at room temperature (including one control device for reproducibility verification) under nominal DC biasing and nominal RF input;\n    5. DC burn in at Tch = 175 °C, for 96 h under nominal biasing condition (no RF);\n    6. DC and RF final electrical measurement at room temperature (including one control device for reproducibility verification) under nominal DC biasing and nominal RF input.\n        NOTE See clause 9 for requirements on issuing a specification for user LAT.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.4.4g","Requirement","ECSS-Q-ST-60-12_0190185","100% final electrical measurement at room temperature and delta calculation shall be made.No failure allowed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","10.5h","Requirement","ECSS-Q-ST-60-12_0190206","In the case of requirement 10.5g the lot shall be treated using the nonconformance procedure. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-12C","A.2.1a","Requirement","ECSS-Q-ST-60-12_0190209","The MMIC electrical design specification shall contain, as a minimum, the following: \n    1. electrical performances and application, \n    2. die dimension, \n    3. in and out interfaces.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60C Rev. 2","4.1.4f","Requirement","ECSS-Q-ST-60_0480016","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval before mounting.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.2.2.3a","Requirement","ECSS-Q-ST-60_0480036","Parts shall be chosen from the EPPL part I.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.2.3.2.2b","Requirement","ECSS-Q-ST-60_0480061","The complete manufacturer assessment, including the survey report and the associated corrective actions, shall be part of the evaluation report.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.2.3.3c","Requirement","ECSS-Q-ST-60_0480064","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.3.2f","Requirement","ECSS-Q-ST-60_0480084","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.3.8a","Requirement","ECSS-Q-ST-60_0480105","Radiation sensitive components, as defined in clause 4.2.2.4, and for which applicable existing test data is insufficient shall be subjected to RVT.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.4b","Requirement","ECSS-Q-ST-60_0480126","The procedures shall be applicable at any facility dealing with components for flight application.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.5.1a","Requirement","ECSS-Q-ST-60_0480129","The supplier shall establish and implement the requirements of this document including methods, organizations and documents used to control the selection and procurement of components in accordance with the requirements of ECSS-Q-ST-20.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","4.6.4f","Requirement","ECSS-Q-ST-60_0480152","The supplier shall prepare a post-programming procedure for customer’s approval, depending on part types (including when necessary electrical tests, programming conditions and equipment, programming software version qualified by the supplier, burn-in conditions, additional screening tests and specific marking after programming) as applicable per 4.6.4d.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.1.5a","Requirement","ECSS-Q-ST-60_0480173","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall be:\n    1. Fit Form and Function compatible, \n    2. manufactured from materials identical to the flight opposite part, and\n    3. ensured to be visibly clean before each connection to flight hardware.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.2.2.4a","Requirement","ECSS-Q-ST-60_0480197","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.2.3.1b","Requirement","ECSS-Q-ST-60_0480200","The supplier shall plan and carry out the evaluation.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.3.1b","Requirement","ECSS-Q-ST-60_0480221","Class 2 components shall meet the quality levels and supplementary conditions specified in Table 7-2.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.3.5b","Requirement","ECSS-Q-ST-60_0480459","The sample size for lot acceptance which may be reduced in some cases, shall be submitted to the customer for approval through the PAD process (see clause 5.2.4).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.3.9g","Permission","ECSS-Q-ST-60_0480510","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.3.11c","Requirement","ECSS-Q-ST-60_0480270","For non qualified parts, the documentation minimum storage period shall be 10 years after delivery of components by the manufacturer. \n    ","NOTE For qualified parts, the documentation storage period is under the responsibility of the manufacturer and the qualifying authority.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","5.6.3b","Requirement","ECSS-Q-ST-60_0480462","Design of hybrids shall conform to clause 7 of the ECSS-Q-ST-60-05.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.1.4f","Requirement","ECSS-Q-ST-60_0480311","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval before mounting.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.2.2.4g","Requirement","ECSS-Q-ST-60_0480335","The supplier shall implement a Radiation Hardness Assurance Programme, in conformance with the requirements of the ECSS-Q-ST-60-15, documented by a plan to be approved by the customer, for radiation sensitive components, covering the collection of all relevant information and specifying the necessary actions in terms of evaluation and procurement testing, planning and control.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.2.2.5a","Requirement","ECSS-Q-ST-60_0480338","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.2.4c","Requirement","ECSS-Q-ST-60_0480359","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.3.5b","Requirement","ECSS-Q-ST-60_0480380","The sample size for lot acceptance which may be reduced in some cases, shall be submitted to the customer approval through the PAD process (see clause 6.2.4)",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.3.9j","Requirement","ECSS-Q-ST-60_0480401","The results of DPA shall be documented by a report sent to the customer, on request, for information.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.4b","Requirement","ECSS-Q-ST-60_0480408","The procedures shall be applicable at any facility dealing with components for flight application.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60C Rev. 2","6.6.4a","Requirement","ECSS-Q-ST-60_0480427","For FPGA, ECSS-Q-ST-60-02 shall apply. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70-01C","5.1.2.2a","Requirement","ECSS-Q-ST-70-01_0500007","In reply to the CRS, the supplier shall establish a cleanliness and contamination control plan (C&CCP) in conformance with the DRD in Annex B (C&CCP DRD), to be provided at the latest at PDR, as part of the review data package.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.2.1.2k","Requirement","ECSS-Q-ST-70-01_0500032","Volatile metals shall not be used.\n    NOTE 1 This is especially the case when the temperatures are above room temperatures.\n    NOTE 2 Some metals such as cadmium and zinc have high vapour pressures and deposit metallic films can occur on adjacent surfaces.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.2.2.1c","Requirement","ECSS-Q-ST-70-01_0500035","Cleaning and packaging operations for all elements shall be processed according to procedures approved by the customer for the specific application/product.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.2.3.1b","Requirement","ECSS-Q-ST-70-01_0500056","The space system shall be shipped to the launch base under clean conditions as defined in the CRS and controlled by the C&CCP.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.3.1.5a","Requirement","ECSS-Q-ST-70-01_0500081","The cleanroom air shall be monitored with dust counters.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.3.1.7f","Requirement","ECSS-Q-ST-70-01_0500102","Molecular contamination in controlled environments shall not exceed 0,5 ´ 10-7 g/cm2 during a continuous period of one week.\n    NOTE 1 In case of contamination sensitive equipment, a lower level can be required, based on the contamination budget (including exposure time).\n    NOTE 2 In a normal cleanroom (without charcoal filters) levels can be achieved that are 10 to 100 times better.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.3.1.9d","Requirement","ECSS-Q-ST-70-01_0500109","Pressure in all areas shall be monitored continuously\n    NOTE In order to take timely corrective actions in case of a pressure drop.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.3.1.13g","Requirement","ECSS-Q-ST-70-01_0500130","Barriers or similar means separating clean and not clean zones inside the airlock shall be placed.\n    NOTE Similar means can be tacky mats.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.3.2e","Requirement","ECSS-Q-ST-70-01_0500151","During the pre-test, test equipment and cabling shall be included in the facility.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.4.2.6a","Recommendation","ECSS-Q-ST-70-01_0500262","Contamination of external surfaces should be monitored.\n    NOTE 1 particulate contamination can be measured by light scattering (e.g. using the Sun or a laser as the a light source) or using QCMs with a crystal having a surface to which particles stick.\n    NOTE 2 Molecular contamination can be measured using QCM located near a sensitive item and maintained at the same temperature as the item or using a mass spectrometer.\n    NOTE 3 Measurements of contamination in space are not often made because the policy of cleanliness control is based upon the basic principle of achieving the lowest possible contamination levels with existing knowledge and within the allocated financial budgets. However, it is advisable to implement an “in space contamination monitoring” as part of the spacecraft housekeeping. When appropriate sensor elements are applied it is possible to predict design life-times at system, subsystem, component or equipment levels.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.4.3.1b","Requirement","ECSS-Q-ST-70-01_0500179","The cleanliness verification shall include all the activities intended to ensure that the actual cleanliness conditions of the space system, the cleanrooms or the vacuum chambers conform to the applicable standards or the applicable CRS (specific to a certain project).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","5.4.4f","Requirement","ECSS-Q-ST-70-01_0500204","Containers carrying sensitive items shall be pressurized with gaseous nitrogen.\n    NOTE Optical units and payloads are examples of sensitive units ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","A.2.1<3>c","Requirement","ECSS-Q-ST-70-01_0500225","The CRS shall specify the transport mechanisms of the potential contaminants from the sources under <3>a. to the contamination sensitive items or areas to be considered in the contamination analysis.\n    NOTE For example: direct flux, reflected flux, ambient scatter, self-scatter and creeping.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","B.2.1<7.4>a","Requirement","ECSS-Q-ST-70-01_0500246","The C&CCP shall describe the provisions for the transportation of critical items. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-01C","B.2.1<8>b","Requirement","ECSS-Q-ST-70-01_0500253","As minimum, the following forms shall be defined:\n    1. PAC and MOC measurement report.\n    2. Cleanliness declaration of conformity (see ECSS-Q-ST-20).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.2.3.2a","Requirement","ECSS-Q-ST-70-02_0510021","During the conditioning of the prepared material samples, the supplier shall ensure an ambient temperature of (22 ± 3) °C with a relative humidity of (55 ± 10) %.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.3.2.1a","Requirement","ECSS-Q-ST-70-02_0510042","The supplier shall clean specimen cups and collector plates with a compatible solvent.\n    NOTE Solvent compatibilities with different materials are provided in ECSS-Q-ST-70-01.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.3.2.11b","Requirement","ECSS-Q-ST-70-02_0510067","The supplier shall reweigh them afterwards.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.3.2.13b","Requirement","ECSS-Q-ST-70-02_0510070","The supplier shall perform baking at 25 °C above the specified test temperature if the blank collectors indicate a mass increase > 30 mg  during the previous test.\n    NOTE It is a good practice to bake the system once every four months.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.6.2b","Requirement","ECSS-Q-ST-70-02_0510095","The supplier shall record any suspected or actual equipment failure as a project nonconformance report in conformance with ECSS-Q-ST-10-09.\n    NOTE This is to ensure that previous results are examined to ascertain whether or not re-inspection or retesting is necessary.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","5.7.4.1a","Requirement","ECSS-Q-ST-70-02_0510116","The supplier shall report all modifications of the apparatus or associated equipment. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","A.2.1<4>a","Requirement","ECSS-Q-ST-70-02_0510123","The materials identification card shall contain the following outgassing screening properties:\n    1. TML\n    2. RML\n    3. CVCM.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-02C","D.2.1<3>a","Requirement","ECSS-Q-ST-70-02_0510145","The report shall contain identification of size, area and mass of test specimen, together with an indication of whether the sample was of the substrate or sandwich type.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-03C","5.3a","Requirement","ECSS-Q-ST-70-03_0520014","The work area shall be clean and free of dust.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-03C","5.5.2d","Requirement","ECSS-Q-ST-70-03_0520035","Coated surfaces shall be shielded from contact by using polyethylene or polypropylene bags or sheets.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-03C","5.7.2.3c","Requirement","ECSS-Q-ST-70-03_0520060","The customer shall be notified of the non-conformance details.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-03C","5.7.2.5a","Requirement","ECSS-Q-ST-70-03_0520063","Trained and competent personnel shall be employed for all operations and inspections related to the black- anodizing process.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-04C","5.2.2.2b","Requirement","ECSS-Q-ST-70-04_0530024","It shall be agreed with the customer that the material samples are representative of batch variance.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-04C","5.3.2b","Requirement","ECSS-Q-ST-70-04_0530045","The supplier shall apply ECSS-Q-ST-20, clause 5.6.3.2 for the establishment of the test.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-06C","5.1.2.2b","Requirement","ECSS-Q-ST-70-06_0550008","The supplier shall identify the parameters that can influence the “seen” fluence.\n    NOTE 1 These parameters can be shielding, view factors or mean sunlight incidence angle.\n    NOTE 2 For example: During one year (8760 hours) the solar irradiation is: \n                  · on a Geostationary cylindrical satellite whose axis is parallel to earth revolution axis, 1112 ESH on the N/S faces and about 2500 ESH on the periphery, \n                  · on the LEO ISS orbit, 2500 ESH on Ram and anti Ram, 250 ESH on nadir, 2200 ESH on zenith, and 1500 ESH on the side faces.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-06C","5.1.2.5a","Requirement","ECSS-Q-ST-70-06_0550015","The supplier shall provide (in the radiation test proposal) the methodology for measuring the defined properties to be investigated.\n    NOTE 1 Materials suffer damage inducing different types of physical properties changes under radiation:\n        \t   · Stable changes: changes are independent of time and measurement conditions.\n        \t   · Unstable changes: changes are dependent of time and measurement conditions.\n    NOTE 2 Stable changes of physical properties can be assessed by ex-situ measurements. These can be mechanical or thermo-mechanical properties. They are of permanent nature.\n    NOTE 3 Unstable changes of physical properties are generally related to electrical and (thermo-) optical properties. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-06C","5.2.1a","Requirement","ECSS-Q-ST-70-06_0550036","The customer shall approve the radiation test proposal including the procedures.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-06C","5.3.3d","Requirement","ECSS-Q-ST-70-06_0550061","Traceability shall be maintained throughout the process from incoming inspection to final measurements and calculations, including details of the test equipment and personnel employed in performing the task.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","5.1.1b","Requirement","ECSS-Q-ST-70-07_0560002","The design constraint specification specified in 5.1.1a shall, at least, include the following statements: \n    1. To avoid solder bridging, orient circuit tracks that are spaced close together in line with the pass direction.\n    2. Avoid large heat sink areas for ground planes and large leads closely connected to massive metal parts.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","5.2.1a","Requirement","ECSS-Q-ST-70-07_0560005","The supplier shall establish a request for verification of the automatic wave soldering process in conformance with Annex B- DRD",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","5.4.2f","Requirement","ECSS-Q-ST-70-07_0560030","Only component types utilized during the verification programme shall be regarded as process approved.\n    NOTE Owing to the high cost of some components, the approval authority can agree to the use of non-functional, or commercial-quality components.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","5.6i","Requirement","ECSS-Q-ST-70-07_0560051","Toxic or volatile vapours shall be exhausted.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","B.2.1f","Requirement","ECSS-Q-ST-70-07_0560072","The request for verification of the automatic wave soldering process shall outline company test capabilities.\n    NOTE Test capabilities like thermal cycling chambers, metallography, chemical analysis, failure analysis.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-07C","C.2.1e","Requirement","ECSS-Q-ST-70-07_0560079","The automatic wave soldering process verification report shall contain a list of findings and recommendations in order to optimize the automatic wave soldering process specifications and control parameters for a given assembled PCB. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","5.4a","Requirement","ECSS-Q-ST-70-08_0570016","Lighting intensity shall be a minimum of 1080 lux on the work surface.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","5.6.2a","Requirement","ECSS-Q-ST-70-08_0570041","Medium-stiff natural- or synthetic bristle, ESD-safe, brushes shall be used for cleaning provided that they do not damage any surface to be cleaned or adjacent materials.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","5.6.7c","Requirement","ECSS-Q-ST-70-08_0570062","Files shall not be used for dressing plated copper soldering-iron tips.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","5.6.7f","Requirement","ECSS-Q-ST-70-08_0570065","The soldering iron or resistance-heating electrode shall maintain the soldering temperature at the joint throughout the soldering operation.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","6.3.1b","Requirement","ECSS-Q-ST-70-08_0570090","For the pretinning of component leads, metallised terminations and terminal posts mildly-activated, rosin-based fluxes (e.g. ROL1) shall be used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","6.4j","Requirement","ECSS-Q-ST-70-08_0570111","Water-based solvents containing saponifiers shall not be used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","6.6.1c","Requirement","ECSS-Q-ST-70-08_0570118","Terminals shall be tin/lead coated with an alloy containing a maximum of 97 % tin.\n    NOTE Example: Hot-dipped or reflowed electro-deposited coatings.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","6.10f","Requirement","ECSS-Q-ST-70-08_0570139","The adhesives, encapsulants and conformal coatings used shall not damage substrate materials or attached devices.\n    NOTE 1 The effects of some conformal coatings on the reliability of solder joints are described in ESA SP 1173.\n    NOTE 2 Adhesion to fused tin-lead finishes is poor, see also ECSS-Q-ST-70-28.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","7.2.2.1b","Requirement","ECSS-Q-ST-70-08_0570160","Conducting surfaces to be soldered shall be cleaned using solvents specified in clause 6.4.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","7.2.4d","Requirement","ECSS-Q-ST-70-08_0570185","Liquid solder shall not come into contact with the component body or its glass meniscus.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","7.3.2b","Requirement","ECSS-Q-ST-70-08_0570206","Plated tips shall be examined for cracking.\n    NOTE Cracked platings allow the liquid solder to alloy with and erode the underlying copper, forming intermetallics which reduce heat transfer and lead to unacceptable joints.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","7.6.1a","Requirement","ECSS-Q-ST-70-08_0570217","Storage facilities shall protect components from contamination and damage. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","8.1.1c","Permission","ECSS-Q-ST-70-08_0570561","Components may be mounted not more than 3,5 mm above the mounting surface, see Figure 8-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","8.1.8a","Requirement","ECSS-Q-ST-70-08_0570256","Solder terminations shall not be cut after the soldering operation.\n    NOTE Component leads and wires are cut and shaped before soldering.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","8.2.1b","Requirement","ECSS-Q-ST-70-08_0570263","The inside radius of a bend shall not be less than the lead diameter or ribbon thickness.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","8.4.3a","Requirement","ECSS-Q-ST-70-08_0570284","For unsupported holes, the cut stud leads shall protrude beyond the PCB surface by 1,5 mm ± 0,8 mm, see Figure 8-9 (a).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","9.1.2b","Requirement","ECSS-Q-ST-70-08_0570305","Terminals shall be selected to fit the conductors.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","9.4.3f","Requirement","ECSS-Q-ST-70-08_0570330","Conductors shall be wrapped a minimum of ¼ turn (Figure 9-3 (a)) to a maximum of ½ turn (Figure 9-3 (c)) around the post.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","9.7f","Requirement","ECSS-Q-ST-70-08_0570351","Conductors shall not misalign floating contacts.\n    NOTE Example: Solid, rigid conductor wire into connectors.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","9.8c","Requirement","ECSS-Q-ST-70-08_0570354","A component shall not move within the sleeving when the sleeving is mechanically supported.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","9.9.4.2f","Requirement","ECSS-Q-ST-70-08_0570379","For shield terminations, the conductor of the grounding wire shall be positioned on the exposed shield.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","10.1.1b","Requirement","ECSS-Q-ST-70-08_0570400","Conductors shall not be temporarily constrained against spring-back force during solder solidification.\n    NOTE Residual stresses are produced in the lead material or solder joint.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","10.2.3a","Requirement","ECSS-Q-ST-70-08_0570407","The workmanship shall be in accordance with clause 15.7.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","10.3.4g","Requirement","ECSS-Q-ST-70-08_0570428","The process of additional heating shall be documented.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","12.1b","Requirement","ECSS-Q-ST-70-08_0570449","Inspection shall be aided by magnification appropriate to the size of the connections between 4 times and 10 times.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","13.3e","Requirement","ECSS-Q-ST-70-08_0570474","The rate of temperature change during the temperature cycle shall not exceed 10 °C per minute.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","14.7b","Requirement","ECSS-Q-ST-70-08_0570495","Inspection shall be in accordance with clause 12.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-08C","14.8g","Requirement","ECSS-Q-ST-70-08_0570502","Operators performing hand soldering and inspectors shall be trained and certified at a school authorized by the Approval authority.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-09C","4.1.2.4a","Requirement","ECSS-Q-ST-70-09_0580010","The supplier shall use a completed “Material identification card” in conformance with DRD in ECSS-Q-ST-70-02 for samples submitted for testing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-09C","A.2.1a","Requirement","ECSS-Q-ST-70-09_0580031","The report shall contain the trade names and batch numbers of the materials under test.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-09C","B.2.1b","Requirement","ECSS-Q-ST-70-09_0580038","The audit report shall describe the test on a defined set of materials.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.1.4.2b","Requirement","ECSS-Q-ST-70-18_0620018","The supplier shall not use files on surface-treated tips or pretinned items.\n    NOTE Nickel plated is an example for surface-treatment.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.2.1a","Requirement","ECSS-Q-ST-70-18_0620039","The supplier shall use solder ribbon, wire and preforms, provided that the alloy and flux conform to the requirements on “material selection” of ECSS-Q-ST-70-08.\n    NOTE 1 The following solder alloys are approved:\n        · 60 Sn (remainder lead): For degolding operations, coating and pretinning.\n        · 96 Sn (remainder silver): For making coaxial-cable outer-conductor-to connector solder joint.\n        · 96 Sn or 63 Sn (remainder lead): For contact-pin soldering and cover soldering of right angle connectors.\n    NOTE 2 Refer also to the table of “Chemical composition of spacecraft solders” in ECSS-Q-ST-70-08.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.3.3b","Requirement","ECSS-Q-ST-70-18_0620064","The supplier shall then add approximately 10 mm to the length to allow for bending, preconditioning and end dressing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.3.7a","Requirement","ECSS-Q-ST-70-18_0620085","The supplier shall use milling tools for stripping the cable ends.\n    NOTE See also clause 5.1.4.5.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.4.1a","Requirement","ECSS-Q-ST-70-18_0620092","The supplier shall establish written procedures which define the various process steps including as a minimum the requirements of clause 5.4.2 and 5.4.3.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.5.1.1.1c","Requirement","ECSS-Q-ST-70-18_0620113","The gap between the rear/end of the centre contact and the face of the dielectric/outer conductor shall be as specified in the assembly instructions for the type of cable-end connector being used.\n    NOTE An example is given in Figure C-5.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.5.1.2k","Requirement","ECSS-Q-ST-70-18_0620134","The supplier shall now solder the outer conductor of the cable to the body of the connector with the aid of the solder specified in clause 5.2.1 and the equipment specified in clause 5.1.4.7.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.5.1.2r","Requirement","ECSS-Q-ST-70-18_0620141","The supplier shall inspect the cover solder joint with respect to the following criteria:\n    1. The solder joint extends around the complete periphery of the cover.\n    2. The cover is fully inserted into the shoulder of the hole \n        NOTE See Figure 5-2.\n    3. The solder joint conforms to the “Final inspection” requirements of ECSS-Q-ST-70-08.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.6.1k","Requirement","ECSS-Q-ST-70-18_0620162","During the nut mating and torquing operations, the supplier shall ensure that no rotation of the cable-end connector body or of the cable takes place.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-18C","5.7.3c","Requirement","ECSS-Q-ST-70-18_0620182","The severity of the vibration tests shall not be inferior to that shown in the following tables of ECSS-Q-ST-70-08:\n    1. Sine survey\n    2. Minimum severity for sine vibration testing\n    3. Minimum severity for random vibration testing for all applications except launchers\n    4. Minimum severity for random vibration testing for launchers.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-20C","5.1.1b","Requirement","ECSS-Q-ST-70-20_0630002","The supplier shall store the samples before and after testing in a clean area.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-20C","5.4.1a","Requirement","ECSS-Q-ST-70-20_0630023","The supplier shall establish an evaluation report in conformance with Annex A",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-20C","A.2.1c","Requirement","ECSS-Q-ST-70-20_0630030","The evaluation report shall list the inspection and test results as described in 5.3.1a6 and 5.3.1b.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.1b","Requirement","ECSS-Q-ST-70-21_0640017","Materials failing to meet the requirements of the applicable screening test shall be subject to testing in configuration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.2.7a","Requirement","ECSS-Q-ST-70-21_0640038","Ignition of the sample shall be accomplished by employing a regulated energy source.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.2.9b","Requirement","ECSS-Q-ST-70-21_0640045","If the supplier uses a different procedure, the supplier shall submit it for customer approval.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.3.4d","Requirement","ECSS-Q-ST-70-21_0640066","The mass of the glass fibres shall not exceed 1,6 g (20 % of the mass of the sample).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.4.7a","Requirement","ECSS-Q-ST-70-21_0640091","The burner shall be of a Bunsen or Tirrill type, with a 9,5 mm bore modified to supply an external supply of air to the burner collar as outlined in Figure D-7.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","5.1.2.5.3a","Requirement","ECSS-Q-ST-70-21_0640112","Ignition shall be either by electrical overload (simulating worst-case conditions) or by open flame.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","A.2.1<1.8>a","Requirement","ECSS-Q-ST-70-21_0640133","The test report shall contain the maximum specified temperature.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-21C","A.2.1<6>a","Requirement","ECSS-Q-ST-70-21_0640140","The test report shall contain percentage oxygen remaining at the end of test.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-22C","4.1.4a","Requirement","ECSS-Q-ST-70-22_0170014","To extend the shelf-life of a material that has exceeded its shelf-life, the following activities shall be performed:\n    1. Re-certify the material for the first time by using the relevant tests in conformance with clause 4.1.6;\n    2. If the first re-certification is successful, extend the shelf-life equal to half the initial shelf-life;\n    3. Re-certify the material for the second time on a case-by-case basis depending on product, application, storage and user experience;\n    4. If the second re-certification is successful, extend the shelf-life to half of the first extension.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","5.3.2f","Requirement","ECSS-Q-ST-30-11_0140007","The derating requirements are not applicable to test conditions (e.g. circuit or equipment level qualification and EMC) for which the maximum ratings shall not be exceeded. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","5.4.2b","Requirement","ECSS-Q-ST-30-11_0140014","For transient or surge conditions, if ratings are not provided, then it shall be assured that the transient or surge values are below the steady-state specified maximum ratings.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.4.2a","Requirement","ECSS-Q-ST-30-11_0140033","Parameters of capacitors from family-group code 01-04 shall be derated as per Table 6-3.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.12.3c","Requirement","ECSS-Q-ST-30-11_0140061","Maximum mating and de-mating cycles shall be limited to 50 cycles.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.20.3a","Requirement","ECSS-Q-ST-30-11_0140090","Some devices can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.26.2.4a","Requirement","ECSS-Q-ST-30-11_0140118","Parameters of Wire-wound high precision resistor (type RBR 56) shall be derated as per Table 6-27.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.28.2a","Requirement","ECSS-Q-ST-30-11_0140131","Parameters of Transistors from family-group code 12-01 to 12-04 and 12-09 shall be derated as per Table 6-33.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-30-11C Rev.1","6.34.3b","Requirement","ECSS-Q-ST-30-11_0140158","RF power shall be limited such that a 6 dB margin exists before the onset of multipactor.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.5a","Requirement","ECSS-Q-ST-70-28_0150022","The supplier shall not reuse components removed because of malfunction or mechanical damage or because of damage to the conductor track in the vicinity of the component but replace them by new identical or equivalent components.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.5d","Requirement","ECSS-Q-ST-70-28_0150025","For chip components, the number of replacements in one location shall not exceed three.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.9.1a","Requirement","ECSS-Q-ST-70-28_0150046","The damage shall not involve a length of track in excess of five times the conductor width.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.12.3c","Requirement","ECSS-Q-ST-70-28_0150071","Where components have been removed and subsequently replaced, the supplier shall inspect the soldered joints in conformance with the accept/ reject criteria of clause 12 in ECSS-Q-ST-70-08. \n    ","NOTE For example: Inspection of the pad or track area to ensure that no lifting has occurred and that no damage has been sustained by the base material is one of the required inspections.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.15.2a","Recommendation","ECSS-Q-ST-70-28_0150145","The supplier should use method J.3.1 and J.3.2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.19.1a","Requirement","ECSS-Q-ST-70-28_0150113","ECSS-Q-ST-20 shall apply.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-28C","4.19.5a","Requirement","ECSS-Q-ST-70-28_0150120","The supplier shall maintain traceability from incoming inspection to final test, including details of test equipment, serial numbers and personnel employed in performing the task.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-40C Rev.1","5.4.6b","Requirement","ECSS-Q-ST-40_0440018","The safety function shall be further represented at all boards dealing with health matters where exposure or endurance limits are defined for flight and ground crews.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","5.7.2a","Requirement","ECSS-Q-ST-40_0440042","The supplier shall hold regular safety status and progress meetings with the customer and his lower tier suppliers as part of the project progress meetings as specified in ECSS-M-ST-10. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","5.7.3d","Requirement","ECSS-Q-ST-40_0440047","Safety reviews shall be performed, and the review objectives achieved, in conformance with clause 5.7.1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","5.11.2b","Requirement","ECSS-Q-ST-40_0440068","The safety data package shall contain at least the following safety related documentation:\n1.\tSafety analysis report (in accordance with Annex D);\n2.\tSupporting analysis (if applicable);\n3.\tSafety risk assessment (if applicable);\n4.\tHazardous ground operations list and procedures;\n5.\tSafety verification tracking log (SVTL, in accordance with Annex C).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.3.3.4.3a","Requirement","ECSS-Q-ST-40_0440093","Hazard which cannot be controlled by compliance to failure tolerance shall be reduced to an accepted level by compliance with specific safety related properties and characteristics of the design. ","NOTE \tExamples are: structures, pressures vessels, mechanisms, material compatibility, flammability.\n",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.3.6h","Requirement","ECSS-Q-ST-40_0440115","Dedicated safing functions shall be provided for emergency situations.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.3.10f","Requirement","ECSS-Q-ST-40_0440136","The space system shall provide an on-board medical facility and the capability for handling a permanently impaired or deceased crewmember.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.4.1f","Requirement","ECSS-Q-ST-40_0440143","These categories shall not violate the safety policy and principles as defined in clause 4.2.1 for the protection of human life or the principles of categorization in accordance with the definition of consequence severity categories in Table 6-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.4.3.3b","Requirement","ECSS-Q-ST-40_0440159","For unmanned systems, only pressure vessels shall be designed in accordance with ECSS-E-ST-32-01, when required by launch site safety authority.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.5.6.4c","Requirement","ECSS-Q-ST-40_0440178","The level of required software product assurance effort shall be determined in accordance with the criticality of the software product.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.6.1c","Requirement","ECSS-Q-ST-40_0440181","Operating ranges and performance limits for safe operation shall be established and specified.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","6.6.3.3a","Requirement","ECSS-Q-ST-40_0440202","To verify conformance to safety requirements, readiness reviews and inspections shall include safety review and assessment of facilities, equipment (incl. GSE), test articles, operating, test and contingency procedures, access controls, and personnel capabilities to comply with the safety requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","7.5.2d","Requirement","ECSS-Q-ST-40_0440227","The following potential initiator events shall be considered:\n1.\thardware failure (random or time dependent);\n2.\tlatent software error;\n3.\toperator error;\n4.\tdesign inadequacies, including:\n(a)\tinadequate margins;\n(b)\tunintended operating modes caused by sneak-circuits;\n(c)\tmaterial inadequacies and incompatibilities;\n(d)\thardware-software interactions;\n5.\tnatural and induced environmental effects;\n6.\tprocedural deficiencies.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","7.5.4.6a","Requirement","ECSS-Q-ST-40_0440248","Whenever safety analyses identify operator errors as a cause of catastrophic or critical hazards, a dedicated analysis shall be carried out.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","8.1b","Requirement","ECSS-Q-ST-40_0440255","For common techniques for verification of design features used to control hazards, the requirements of ECSS-E-ST-10 shall apply. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","8.3.4.3a","Requirement","ECSS-Q-ST-40_0440276","Inflight inspections shall be entered into flight procedures and operation manuals.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-40C Rev.1","B.2.1<4>a","Requirement","ECSS-Q-ST-40_0440297","The plan shall make provisions for assuring conformance to safety requirements and regulations that are applicable to any other facilities and service that are utilized during the course of the project. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70-29C","4.1.1.2c","Requirement","ECSS-Q-ST-70-29_0650004","Coatings and finishes shall be coated on a clean aluminium substrate. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-29C","4.1.1.2f","Requirement","ECSS-Q-ST-70-29_0650007","Heat shrinkable tubing or boots shall be applied and shrunk to simulate actually used configuration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-29C","4.2.2e","Requirement","ECSS-Q-ST-70-29_0650028","For cleaning purposes, the chamber shall have the capability to be evacuated to a pressure of 1,3 Pa or less, or to be purged with clean gas not below 80 °C.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-29C","4.5.2b","Requirement","ECSS-Q-ST-70-29_0650053","The toxic hazard index T shall be determined by calculating the ratio of the projected concentration of each offgassed product to its SMAC value and summing the ratios for all offgassed products without separation into toxicological categories. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.1.3.1b","Requirement","ECSS-Q-ST-70-30_0120007","Any tool not conforming with requirement 5.1.3.1a shall be removed from the work area.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.1.3.3e","Requirement","ECSS-Q-ST-70-30_0120014","The tool and associated accessories shall be checked for cleanliness and general satisfactory condition under up to ×10 magnification as follows:\n    1. The extremity of the bit is perfectly clean and smooth without blockages or faults.\n    2. The sleeve does not have any sharp blockage in its neck, and manual check ensures that the bit runs perfectly in the sleeve, without any hard or rough points of contact. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.1.6.2b","Requirement","ECSS-Q-ST-70-30_0120037","Soak time at each temperature extreme shall be 15 minutes, such that the duration of each cycle averaging one hour.\n    NOTE These conditions can be modified to conform with the particular environmental qualification conditions for the assembly being verified.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.2.2.1a","Requirement","ECSS-Q-ST-70-30_0120058","The material shall be selected from the following list:\n    1. grades of copper or nickel alloys, such as copper-zinc, phosphor bronze,\n    2. copper-nickel-zinc,\n    3. beryllium-copper, nickel-copper (Monel), and\n    4. nickel-clad copper (Kulgrid).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.3.2.1c","Requirement","ECSS-Q-ST-70-30_0120083","In case of necessary rework, the wrapped wire shall be uncoiled using an approved hand tool (see clause 5.1.3.4), to preserve the corners of the terminal post.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.3.2.2a","Requirement","ECSS-Q-ST-70-30_0120086","The distribution of the wraps on the same post shall depend on the level of wiring.\n    NOTE Terminal post length is designed to receive a maximum of three levels of wrap joint.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.4.2h","Requirement","ECSS-Q-ST-70-30_0120111","The jaws shall engage at 90° to the axis of the terminal post, creating a flat surface contact with the wire at the base of the wrap connection. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.4.7d","Requirement","ECSS-Q-ST-70-30_0120132","The failed wire-wrap combination shall be submitted to process certification tests, detailed in clause 5.1.5, to determine cause of the process failure.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.6.2a","Requirement","ECSS-Q-ST-70-30_0120153","Traceability shall be maintained throughout the process from incoming inspection to final test, including details of test equipment, tools and personnel employed in performing the task.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.6.5f","Requirement","ECSS-Q-ST-70-30_0120162","Recalibration shall be carried out at intervals of 12 months or whenever the tool is repaired.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-30C","5.6.8.3c","Requirement","ECSS-Q-ST-70-30_0120182","In both cases of requirement 5.6.8.3b, the samples shall be first visually inspected (see clause 5.5.1).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-36C","5.3a","Requirement","ECSS-Q-ST-70-36_0670017","The directional variation of the alloy shall be considered in the design of the manufactured product.\n    NOTE 1 The directional variation can be appreciable with respect to SCC. \n    NOTE 2 This is necessary for the evaluation of the susceptibility to stress corrosion cracking.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-36C","C.2.1<11>f","Requirement","ECSS-Q-ST-70-36_0670042","Any special precautions taken to control stresses shall be noted.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-36C","C.2.1<13>b","Requirement","ECSS-Q-ST-70-36_0670045","All information relevant for the stress-corrosion cracking evaluation shall be submitted: \n    1. alloy, form and temper of the parent metal;\n    2. filler alloy, if any;\n    3. welding process;\n    4. weld bead removed;\n    5. post-weld thermal treatment or stress relief.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-37C","5.2.2.1c","Requirement","ECSS-Q-ST-70-37_0680015","For turned stress-corrosion test specimen, the supplier shall use a letter height of 1.5 mm for the identification of the sample.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-37C","5.2.4c","Requirement","ECSS-Q-ST-70-37_0680036","The supplier shall make provision for automatic recording of the time of failure of the stress-corrosion specimen.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-37C","5.4.1b","Requirement","ECSS-Q-ST-70-37_0680057","The supplier shall provide the test report in conformance with Annex A for customer approval.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-37C","A.2.1<3>a","Requirement","ECSS-Q-ST-70-37_0680064","The report shall describe the used stress level.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-45C","5.3.3b","Requirement","ECSS-Q-ST-70-45_0690014","A minimum number of three valid tests, in conformance with the validity criteria of ASTM E 561, shall be carried out for each set of material and test condition.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-45C","5.5.2.1a","Requirement","ECSS-Q-ST-70-45_0690035","Determination of operational values of DKth shall be carried out according to the test procedure of ASTM E 647, clause 9.4. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-45C","5.12.2b","Requirement","ECSS-Q-ST-70-45_0690060","Calibration of tensile testing machines and extensometers shall be carried out in conformance to EN 10002-2 and EN 10002-4, respectively.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-45C","5.12.3b","Requirement","ECSS-Q-ST-70-45_0690063","The supplier of raw materials shall include a raw material certificate (RMC) in each test report in conformance with the DRD of Annex C.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-45C","C.2.1<3>c","Requirement","ECSS-Q-ST-70-45_0690088","The RMC shall include:\n    1. batch supplier’s name and code,\n    2. material standard designation and heat treatment,\n    3. date of batch manufacturing,\n    4. specified chemical composition,\n    5. material and heat treatment specifications,\n    6. product form, quantity, dimensions and grain orientation,\n    7. surface treatment,\n    8. description of manufacturing processes.\n        NOTE For example: welding, cutting and milling. \n    9. non-destructive inspection.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.1.4b","Requirement","ECSS-Q-ST-70-46_0700011","Forged blanks belonging to the same batch shall be heat treated in one batch.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.1.8b","Requirement","ECSS-Q-ST-70-46_0700032","Silver plating shall not be used on titanium alloy fasteners.","NOTE Silver and cadmium plating are not used because they can cause embrittlement of titanium alloys, as per requirement in ECSS-Q-ST-70-71C. ",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.2.1a","Requirement","ECSS-Q-ST-70-46_0700039","Dimensional and metallurgical controls shall be carried out in accordance with the sampling procedures and acceptance criteria specified in 4.4.2.1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.2.5e","Requirement","ECSS-Q-ST-70-46_0700060","Fastener microstructure shall be visually inspected for internal defects at a magnification of ´100 or higher in un-etched condition. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.3.3.2f","Requirement","ECSS-Q-ST-70-46_0700085","The nut threads shall be fully engaged. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.3.5.3g","Requirement","ECSS-Q-ST-70-46_0700106","For fasteners with fatigue lives less than the expected mean fatigue life, failure shall not occur in the head-to-shank fillet.","NOTE No restrictions in failure location apply for fasteners with fatigue lives exceeding the expected mean fatigue life.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.3.6.2a","Requirement","ECSS-Q-ST-70-46_0700109","The percent elongation after fracture, the reduction of area at failure and the time to fracture shall be within the values specified in the customer specification document for threaded fasteners.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-46C Rev. 1","4.4.2.4e","Requirement","ECSS-Q-ST-70-46_0700134","The supplier shall remove all nonconforming units or replace them by conforming units. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-53C","5.1.2.1c","Requirement","ECSS-Q-ST-70-53_0990008","The supplier shall use sterilization facilities as described in Annex B.\n    NOTE 1 Dry heat sterilization is described in ECSS-Q-ST-70-57, vapour phase (e.g. hydrogen peroxide) sterilization is described in ECSS-Q-ST-70-56.\n    NOTE 2 Sterilization compatibility tests need to be conducted with the same process parameters intended for the flight hardware. For example compatibility with dry heat sterilization under ambient pressure does not compare to a vacuum process because of differences in thermal gradients.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-53C","5.2.3a","Requirement","ECSS-Q-ST-70-53_0990029","The inspection and test methods as well as the relevant parameters to verify the functionality of equipment after sterilization shall be specified by the customer before the application of each sterilization process.\n    NOTE The extent of physical, chemical, mechanical or electrical properties to be verified before and after sterilization depend on the intended application of the hardware (e.g. materials, components, parts, and assemblies).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-53C","5.2.4e","Requirement","ECSS-Q-ST-70-53_0990036","The specified sterilization time shall start after all surfaces of a hardware item are exposed to the minimum sterilization condition.\n    NOTE 1 Examples of sterilization conditions are: Temperature, radiation dose, or chemical reagent.\n    NOTE 2 Sterilization is a time dependent process.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-55C","5.1.1b","Requirement","ECSS-Q-ST-70-55_1030002","ECSS-Q-ST-20 shall be made applicable in the request for microbiological examination.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-55C","5.4.2b","Requirement","ECSS-Q-ST-70-55_1030027","The supplier shall submit the test report to the customer for approval.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-58C","5.2.1b","Requirement","ECSS-Q-ST-70-58_1040012","Bioburden controlled environments shall be continuously monitored in conformance with ISO 14644- Part 2.\n    NOTE 1 In some cases, aseptic operations can only be ensured if a more stringent particulate control (e.g. ISO 5) is applied. Normally such conditions are provided by laminar air flow environments with a controlled environment in the background.\n    NOTE 2 For commissioning of bioburden controlled environment, see Annex E.1",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-58C","5.2.3.1b","Requirement","ECSS-Q-ST-70-58_1040015","The return to use of all equipment used for bioburden control shall be subject to approval of appropriate representatives responsible for the bioburden control of the environment and/or formal revalidation of the environment.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-58C","5.2.5.6a","Requirement","ECSS-Q-ST-70-58_1040046","Quantitative results shall be expressed as colony-forming-units (CFU) per m3 (volume) or m2 (surface area).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-58C","5.3e","Requirement","ECSS-Q-ST-70-58_1040062","The supplier shall submit the Cleanroom commissioning report in conformance with Annex D to the customer for approval ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-58C","C.2.1a","Requirement","ECSS-Q-ST-70-58_1040069","The WP shall include or refer to the following information:\n    1. A proposed work description giving:\n        (a) the objectives of the cleanroom commissioning activity,\n        (b) cleanroom facilities to be commissioned,\n        (c) test facilities, test procedures and reference to standards,\n        (d) test conditions (i.e. environment, properties evaluated and measurement techniques),\n        (e) expected test output.\n    2. A proposed settlement describing the test procedures and any deviation from the conditions initially requested by the customer.\n    3. A financial and administrative proposal including:\n        (a) responsible person for the activity,\n        (b) list of deliverable items,\n        (c) work breakdown structure defining the required operations (i.e., preparation of specimens, testing, evaluation of results, reporting) and responsibilities,\n        (d) time schedule,\n        (e) travel and subsistence plan (if applicable),\n        (f) itemized cost list, and\n        (g) milestone payment plan.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-13C Rev. 1","5.1.2.3e","Requirement","ECSS-Q-ST-70-13_0610020","The supplier shall label limited-life materials with their shelf lives and dates of manufacture, or date of delivery if date of manufacture is not known.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-13C Rev. 1","5.2.1.1c","Requirement","ECSS-Q-ST-70-13_0610041","The supplier shall ensure that there is no physical or chemical interaction between any adhesive employed during sample preparation and the sample materials.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-13C Rev. 1","A.2.1f","Requirement","ECSS-Q-ST-70-13_0610066","The test result sheet shall contain details of the test parameters outlined in Annex B.\n    ","NOTE This also includes any variation in testing environment conditions.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.1.1.4d","Requirement","ECSS-Q-ST-70-50_1140013","The removal of the adhesive tape from the surface to be analysed shall be conducted as follows:\n    1. Approximately 5 cm of tape are removed from the surface being analysed using a constant speed of less than 1 cm/s, at approximately 45 degrees to the sample surface.\n    2. Sudden or uneven forces are not used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.1.1.4g","Requirement","ECSS-Q-ST-70-50_1140016","The remainder of the tape shall be removed from the surface using a constant speed of less than 1 cm/s.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.1.2.6g","Requirement","ECSS-Q-ST-70-50_1140040","Any witness handling, deployment and measurement, shall be performed wearing non-shedding and lint-free gloves.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.1.3.5.2a","Requirement","ECSS-Q-ST-70-50_1140058","The apparatus shall be as specified in 5.1.2.3, with the following additional items:\n    1. Clean container with lid to collect the solvent after rinsing,\n    2. Petri dish.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.2.1.4.1c","Requirement","ECSS-Q-ST-70-50_1140064","All cleaned equipments shall be stored in a clean area with openings covered with a non-shedding and lint-free cover.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.3.3a","Requirement","ECSS-Q-ST-70-50_1140085","The following apparatus shall be used to perform a tape-lift or a silicon wafer analysis:\n    1. An optical microscope with x50, x100 and x200 magnification.\n    2. Standard linear and globe and circle reticules.\n    3. Flexible high intensity fibre optic light source or homogenously distributed razing light source.","NOTE The optical microscope can be equipped with a motorized stage and auto-focus capabilities for automated counting.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","5.4.5d","Requirement","ECSS-Q-ST-70-50_1140100","Having been placed in this intimate packing, the sensors shall be stored in a container for transport. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","6.2d","Requirement","ECSS-Q-ST-70-50_1140123","Any handling procedures and contamination control requirements (as described in the C&CCP) for the item to be inspected shall be followed during the inspection, paying particular attention to contamination sensitive items.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","6.3.1.2.3c","Recommendation","ECSS-Q-ST-70-50_1140220","The black light should be moved to illuminate the whole surface to be inspected.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","6.3.2.2a","Requirement","ECSS-Q-ST-70-50_1140142","The following apparatus shall be used for the inspection of small items:\n    1. Inspection booth with white-light, 10 W - 20 W fluorescent lamp.\n    2. Matte black background.","NOTE A typical clean air, laminar flow bench can be used as an inspection booth as long as external lighting is switched off and a matte black background is used.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","B.2.1<6>a","Requirement","ECSS-Q-ST-70-50_1140166","The work proposal shall include the procedure for the handling of problem and nonconformance as described in ECSS-Q-ST-10-09.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","D.2.1<3>a","Requirement","ECSS-Q-ST-70-50_1140187","The report shall contain the name of the project for which the inspection has been carried out.\n    ","NOTE A project can be either related to the monitoring of spacecraft systems or controlled areas.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-50C","D.2.1<10>a","Requirement","ECSS-Q-ST-70-50_1140194","The report shall contain a description and unique reference for each spacecraft system that has been inspected.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-15C","5.1o","Requirement","ECSS-Q-ST-60-15_1150016","Mitigation shall be verified by analysis or test.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-15C","5.2l","Requirement","ECSS-Q-ST-60-15_1150037","Component type TNIDS shall be calculated either as\n    1. Total non-ionizing dose level at which the worst case part of the worst case lot exceeds its limits as defined in requirement 5.2k (worst case approach), or\n    2. Total dose level at which the one sided tolerance limit as defined in MIL-HDBK-814 exceeds its limits as defined in requirement 5.2k (statistical approach)",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-15C","5.3i","Requirement","ECSS-Q-ST-60-15_1150064","All SEE testing shall be performed in conformance to requirements of clause 5.3f.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-15C","5.3dd","Requirement","ECSS-Q-ST-60-15_1150086","All data and analysis shall be documented in Radiation Analysis report in conformance with the DRD in Annex B.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-15C","A.2.1<2>c","Requirement","ECSS-Q-ST-60-15_1150093","Total non-ionizing dose curves for Silicon and GaAs materials versus Aluminium shield thickness for a solid sphere geometry shall be presented with figure and table.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-56C","5.1e","Requirement","ECSS-Q-ST-70-56_1230005","The supplier shall provide a hydrogen peroxide bioburden reduction report in conformance with the DRD in Annex C.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-56C","5.3.1.3b","Requirement","ECSS-Q-ST-70-56_1230026","The hydrogen peroxide vapour concentration for surface bioburden overkill under controlled ambient conditions shall be from 6 mg/L to 8,6 mg/L.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-56C","5.4c","Requirement","ECSS-Q-ST-70-56_1230033","The provider of the bioburden reduction service shall demonstrate that the installation and operational qualifications are valid for the activities duration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-57C","5.2.3c","Requirement","ECSS-Q-ST-70-57_1240011","The packaging shall maintain the bioburden level of the product until it is used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-57C","5.4h","Requirement","ECSS-Q-ST-70-57_1240032","Instrumentation used to monitor the process parameters shall be only used within the valid range and time period of the calibration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.1.4a","Requirement","ECSS-Q-ST-60-13_0460011","For each equipment, its supplier shall issue a DCL in an editable and sortable electronic format, as a minimum compatible with CSV, identifying all component types needed.","NOTE CSV is a common file format that can be used to transfer data between database or spreadsheet tables (a spreadsheet program is for example Excel®).",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.2.2.4c","Requirement","ECSS-Q-ST-60-13_0460041","For this demonstration, the supplier shall consider all types of radiation including cosmic (Heavy Ions), electromagnetic, trapped (charged particles - electrons, protons - in radiation belts) and solar (flares). ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.2.2.5a","Requirement","ECSS-Q-ST-60-13_0460048","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.2.3.3c","Requirement","ECSS-Q-ST-60-13_0460064","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.3.2e","Requirement","ECSS-Q-ST-60-13_0460083","The use of any new specification shall be submitted to the customer for approval through the PAD process (see clause 4.2.4) ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.3.3d","Requirement","ECSS-Q-ST-60-13_0460089","For commercial parts, screening tests shall be performed in accordance with Table 4-2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.3.9i","Requirement","ECSS-Q-ST-60-13_0460118","For health and safety reasons, any test producing beryllium oxide dust shall be omitted.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","4.5.3b","Requirement","ECSS-Q-ST-60-13_0460135","If alerts become available at a later stage, the supplier shall analyse the alerts, analyse the project risk and propose an action plan for customer approval.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.1.3d","Requirement","ECSS-Q-ST-60-13_0460164","Depending on the progress of the program, the main PCB activities shall be:\n    1. Review and approval of the supplier's compliance matrix to the clause of section 5 of this standard and any associated documents\n    2. Parts approval including evaluation activities,\n    3. Problem assessment (e.g. alerts, nonconformances, RFD, RFW and  delivery delays).\n    4. Upon customer’s request, assessment activities (by sampling) including: \n        (a) conformity of procurement conditions, \n        (b) conformity of procurement data,\n        (c) post-procurement data, and\n        (d) application of alerts recommendations","NOTE 1 Customer request depends on from the criticality of the equipment or supplier.\nNOTE 2 For (a) to (c), assessment of the procurement conditions, conformity of procurement and post-procurement data is performed versus approval document.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.2.2.2c","Requirement","ECSS-Q-ST-60-13_0460182","With respect to health and safety, beryllium oxide (except if identified in the procurement specification), cadmium, lithium, magnesium, mercury, zinc, radioactive material and all material which can cause safety hazard shall not be used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.2.2.3b","Requirement","ECSS-Q-ST-60-13_0460189","The supplier who is responsible for the design of the piece of hardware shall demonstrate the compliance of its components selection with the radiation constraints of the project. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.2.3.1i","Requirement","ECSS-Q-ST-60-13_0460207","The supplier shall review the evaluation results to determine their impact on the content of the screening and lot acceptance tests.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.3.1e","Requirement","ECSS-Q-ST-60-13_0460224","The supplier shall ensure the compatibility of the change with its application.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.3.2a","Requirement","ECSS-Q-ST-60-13_0460227","The supplier shall procure EEE components according to controlled specifications.","NOTE It can be procurer’s in-house specification, a manufacturer’s drawing or a datasheet as a minimum.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.3.7b","Requirement","ECSS-Q-ST-60-13_0460248","The incoming inspection shall include the following items:\n    1. For any part:\n        (a) Marking control,\n        (b) Quantity verification,\n        (c) Packing checking,\n        (d) Review of the manufacturer delivered documentation,\n        (e) In case of not golden termination finish, check the lead finish as per ESCC 25500 basic specification,\n        (f) Additional tests based on the type of component, criticality and heritage with the manufacturer (e.g. solderability tests, electrical tests).\n    2. For the non-space qualified parts, when the final customer source inspection has not been performed, the following additional items: \n        (a) External visual inspection by sampling (AQL 0,65% level II or 20 parts min) \n        (b) Electrical measurements at room temperature on 20 parts or 100% (if lot size < 20 parts), or a datapackage review.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.4d","Requirement","ECSS-Q-ST-60-13_0460274","As a minimum, the following areas shall be covered:\n    1. Control of the environment in accordance with ESCC Basic Specification No. 24900.\n    2. Measures and facilities to segregate and protect components during receiving inspection, storage, and delivery to manufacturing. \n    3. Control measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","5.6.4f","Requirement","ECSS-Q-ST-60-13_0460296","The supplier shall prepare a post-programming procedure for customer’s approval, depending on part types (including when necessary electrical tests, programming conditions and equipment, programming software version qualified by the supplier, burn-in conditions, additional screening tests and specific marking after programming) as applicable per 5.6.4d.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.2.2.1c","Requirement","ECSS-Q-ST-60-13_0460318","Preference shall be given to components which necessitate the least evaluation or qualification effort. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.2.2.2d","Requirement","ECSS-Q-ST-60-13_0460323","For limited life duration, known instability, safety hazards or reliability risk reasons, EEE components listed below shall not be used:\n1.\tEEE components with pure tin (less than 3% Pb in case of SnPb alloy) used as a finish on the leads, terminations and external surfaces of components and packages.\nNOTE\tFor EEE components with pure tin, see also requirements 6.2.2.2h and 6.2.2.2i.\n2.\tHollow core resistors\n3.\tPotentiometers (except for mechanism position monitoring)\n4.\tNon-metallurgically bonded diodes\n5.\tSemiconductor dice with unglassivated active area\n6.\tWet slug tantalum capacitors other than capacitor construction using double seals and a tantalum case\n7.\tAny component whose internal construction uses metallurgic bonding with a melting temperature not compatible with the end-application mounting conditions\n8.\tWire link fuses < 5A\n9.\tTO5 relays without double welding of the mechanism to the header or with any type of integrated diodes inside.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.2.3.1d","Requirement","ECSS-Q-ST-60-13_0460343","An evaluation plan shall be sent to the customer for approval, and include the following elements:\n    1. Constructional Analysis (as per clause 6.2.3.3),\n    2. Radiation Hardness (as per clause 6.2.3.4b.5). ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.3.1f","Requirement","ECSS-Q-ST-60-13_0460542","Each procured EEE part shall be traceable to a manufacturer assigned trace code.","NOTE The procurement of a single trace code per delivery lot should be preferred and encouraged.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.3.2h","Requirement","ECSS-Q-ST-60-13_0460545","If additional requirements are specified to the manufacturer, they shall be identified in a procurement specification.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.3.9d","Requirement","ECSS-Q-ST-60-13_0460395","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review.","NOTE Annex H provides guidelines for the construction analysis and destructive physical analysis.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","6.5.4a","Requirement","ECSS-Q-ST-60-13_0460418","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-13C","C.2.1a","Requirement","ECSS-Q-ST-60-13_0460440","The internal supplier’s specification shall include or refer to the following information:\n    1. A description of the purpose, content and the reason prompting its preparation, \n    2. A list of the applicable and reference documents,\n    3. Any additional terms, definitions or abbreviations,\n    4. Electrical and mechanical parameters and limits,\n    5. Screening, burn-in, and acceptance requirements,\n    6. Delta limits when applicable.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","6.2.2b","Requirement","ECSS-Q-ST-70-12_1200011","The material selection for all types of PCBs shall be in compliance with the requirements from the clauses 7.1 to 7.6 of the ECSS-Q-ST-70-11.\nNOTE \tExamples of types of PCBs are: single sided, double sided, multilayer, sequential, rigid, rigid-flex, flexible, sculptured flex, HDI, RF.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","6.4d","Requirement","ECSS-Q-ST-70-12_1200018","The serial number shall identify the position of the PCB on the panel.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","7.1.3g","Requirement","ECSS-Q-ST-70-12_1200031","Double-sided copper clad laminate with a thickness as-designed of 5 mil (~125 µm) shall not be used above 30 V unless:\n1.\tthe thickness of laminate as-manufactured is in conformance with the Table 13-3,\n2.\tthe laminate batch is screened by the PCB manufacturer to have a nominal thickness of the etched laminate of ≥ 4,8 mil,\n3.\tthe as-manufactured insulation distance is verified by the PCB manufacturer to be in compliance with requirement 7.1.3g.1,\n4.\tit is recorded as a Review Item in the PCB definition dossier.\nNOTE \t1\tThe thickness value of the requirement 7.1.3g.1 is ≥100 µm.\nNOTE \t2\tThis value specified in the requirement 7.1.3g.2 can be read from the CoC. It does not indicate worst-case thickness as mentioned in the requirement 7.1.3g.1. This prohibits the use of 5 mil laminate on the lower end of the tolerance between 4,5 mil and 4,8 mil.\nNOTE \t3\tPrecautions specified in this requirement are defined to prevent a worst-case insulation value of less than 100 µm due to high tolerances with rough copper surface treatment as indicted in Table 7-2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","7.4.3f","Requirement","ECSS-Q-ST-70-12_1200048","The basic copper foil thickness of fine pitch shall be 17 µm.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","7.4.6c","Requirement","ECSS-Q-ST-70-12_1200064","Widening of tracks shall occur close to AAD footprint to provide a wider track where no other circuitry is adjacent that requires the use of fine pitch.\nNOTE \tSee example of nonconformance indicated by yellow arrow in Figure 7-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","7.5.2c","Requirement","ECSS-Q-ST-70-12_1200069","Except the case specified in the requirement 7.5.3b.2, the annular ring as-manufactured on solder side of external layers shall be in conformance with the requirement 9.5.b.15(a) of ECSS-Q-ST-70-10.\nNOTE \tThis requirement specifies 200 µm",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","8.3.2a","Requirement","ECSS-Q-ST-70-12_1200081","Flex PCBs shall be manufactured with copper clad flexible polyimide laminate without adhesive between copper and laminate. \nNOTE \t1\tThis laminate type is named “adhesiveless”.\nNOTE \t2\tThe laminate typically used is of type Pyralux AP from DuPont.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","8.4i","Requirement","ECSS-Q-ST-70-12_1200095","Tracks shall not change direction within the bending zone, as specified in Figure 8-2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","8.6.2d","Requirement","ECSS-Q-ST-70-12_1200113","Bending of the flex PCB shall be designed not to occur on the termination zone and on an additional distance of 2 mm.\nNOTE \t1\tIn the Figure 8-4 the additional distance is indicated as X.\nNOTE \t2\tEven though no bending is designed to occur on the termination zone, some bending can still occur on the assembled PCB due to the stress on the flex section. A stiffening of the termination zone by implementing double cover layer or adhesive can decrease the bending locally.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","8.7.3d","Requirement","ECSS-Q-ST-70-12_1200120","The build-up, initial and etched copper thickness, track width and insulation distance shall be in conformance with the minimum dimensions specified in Table 8-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","9.3f","Requirement","ECSS-Q-ST-70-12_1200137","Three flex laminates or more in the build-up shall be recorded as Review Item in the PCB definition dossier.\nNOTE \tThree flex laminates can include 6 copper layers.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","10.3.3b","Requirement","ECSS-Q-ST-70-12_1200158","Distance between 2 clearances shall be ≥ 1,5 mm along straight edges.\nNOTE \tDistance along straight edges is indicated as “Iz1” in Figure 10-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","10.3.3e","Requirement","ECSS-Q-ST-70-12_1200161","Distance between pads on the PCB and the edge of the clearance of the heat sink shall be ≥ 0,3 mm.\nNOTE \tDistance between pads on the PCB and the edge of the clearance of the heat sink is indicated as “i” in Figure 10-1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","10.4.4c","Requirement","ECSS-Q-ST-70-12_1200179","Heat sinks that are aligned with the edge of the PCB or exposed on one side by depth controlled milling shall have a protective coating for corrosion protection.\nNOTE \tExample of protective coating is nickel plating.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","11.4.2g","Requirement","ECSS-Q-ST-70-12_1200199","The diameter of the area connecting to layer 2 shall be ≥ 100 µm as-manufactured.\nNOTE \tThis is less than 150 µm as-designed to allow for conical shape of microvia.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","12.2a","Requirement","ECSS-Q-ST-70-12_1200212","The build-up of RF PCBs shall be in conformance with requirements from clause 7.1, except the cases specified in the requirements from 12.2b to 12.2e.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","12.4c","Recommendation","ECSS-Q-ST-70-12_1200460","The number of layers for RF PCBs should be ≤ 8.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","12.7a","Requirement","ECSS-Q-ST-70-12_1200230","The surface finish for RF PCBs shall be in conformance with the requirements from clause 7.8.1.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.6.3e","Permission","ECSS-Q-ST-70-12_1200469","The temperature rise of a track may be reduced when it is superimposed by a copper plane, in conformance with requirements specified in chapter A.4.6.2. of IPC-2152.\nNOTE \tThis chapter specifies that the presence of copper planes is recommended to be used to calculate temperature and to be considered as design margin.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.8.3a","Requirement","ECSS-Q-ST-70-12_1200266","The spacing of conductors on flex laminate in the rigid section shall be in conformance with values for X,Y internal specified in the Table 13-3.\nNOTE \tConductors on flex laminate in rigid section are covered by prepreg.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.8.4a","Recommendation","ECSS-Q-ST-70-12_1200475","Conductors on external layers should be covered with conformal coating.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.9.3.3c","Requirement","ECSS-Q-ST-70-12_1200289","A critical net shall be covered with conformal coating including the track, pads and component leads.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.12.2e","Recommendation","ECSS-Q-ST-70-12_1200491","Ground planes should be used in all digital applications. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.13.3c","Recommendation","ECSS-Q-ST-70-12_1200501","The track length of high impedance signals should be minimized.\nNOTE \tThis is done to reduce crosstalk and pickup noise.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","13.14d","Requirement","ECSS-Q-ST-70-12_1200315","In case planes of analog and digital circuitries are combined, power supply decoupling shall be implemented.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","14.3.4a","Requirement","ECSS-Q-ST-70-12_1200333","The track length between SMT pad and via shall be in conformance with values specified in Table 14-4\nNOTE \t1\tIn Figure 14-4: LT is the track length between SMT and via.\nNOTE \t2\tThe through going via can absorb all tin-lead away from the pad during assembly. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","14.5.8c","Recommendation","ECSS-Q-ST-70-12_1200519","The pad design for components of type AAD should be with via-in-pad technology.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-12C","B.2.1a","Requirement","ECSS-Q-ST-70-12_1200372","The PCB manufacturing dossier shall contain following information:\n1.\tReference to the purchase order including the following items:\n(a)\tID number\n(b)\tLine item numbers for each required PCB type\n(c)\tLine item numbers for each required PCB tooling\n(d)\tLine item numbers for other required services like FAI\n(e)\tRequired quantities for each line item\n(f)\tRequired delivery dates for each line item\n2.\tReference to the PCB definition dossier for each PCB type.\n3.\tTooling files\n(a)\tImaging\n(b)\tDrilling\n(c)\tMilling or routing\n(d)\tPlating\n(e)\tLamination\n(f)\tAOI\n(g)\tElectrical testing\n(h)\tProcess route card or traveller information\n(i)\tInspection drawings\n4.\tMRR checklist\nNOTE \tAn example of an MRR checklist is provided in Annex G.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.1b","Requirement","ECSS-Q-ST-20-07_0370002","The space test centre shall establish, document, implement and maintain a quality and safety management system, and continually improve its effectiveness.","NOTE\tFor example, the effectiveness of the continual improvement of the quality and safety management system can be demonstrated through a reduction of customer complaints and nonconformances, increased customer satisfaction, proactive identification of risks affecting the quality and safety of space test centre operations.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.3.4a","Requirement","ECSS-Q-ST-20-07_0370023","Top management shall appoint a quality representative with defined authority:\n1.\tto ensure that the quality management system is established, implemented and maintained,\n2.\tto report its performance to the space test centre management and any needs for improvement, and\n3.\tto ensure quality assurance awareness throughout the space test centre.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.5.2b","Requirement","ECSS-Q-ST-20-07_0370048","In addition to environmental parameters specified in the requirement 5.5.2a, the space test centre shall assess the impacts of other parameters specified by the customer that affect the test specimen's environmental conditions or the test results.","NOTE\tThese parameters can include among others the following: light level, electromagnetic radiation, magnetic cleanliness, vibration, ionising radiation, and acoustic environment.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.6.1e","Requirement","ECSS-Q-ST-20-07_0370068","The space test centre shall demonstrate that personnel are trained on the maintenance and operation of the new or modified test facility.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.6.2c","Requirement","ECSS-Q-ST-20-07_0370075","The configuration item list specified in the requirement 5.6.2b shall include as a minimum:\n1.\tall software used, \n2.\tall critical items, and \n3.\tall facility items that are under maintenance control and whose replacement by a different part number changes the facility configuration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.6.4a","Requirement","ECSS-Q-ST-20-07_0370094","The space test centre shall establish a maintenance plan for infrastructure, test facilities, environmental monitoring, and software used in the test process.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.7.3c","Requirement","ECSS-Q-ST-20-07_0370118","The space test centre shall demonstrate that processes specified in the requirement 5.7.3a are carried out under controlled conditions, including the following:\n1.\tdocumented procedures specifying test design, test planning, test preparation, test execution and management, test data acquisition and storage, format and contents of test reports, test reviews and inspections, tracking of the test specimen throughout each test campaign;\n2.\tconformance to applicable standards specified in the business agreements, codes, legislation, quality and safety plans or documented procedures;\n3.\tmonitoring and control of test process parameters and test facility characteristics;\n4.\tthe approval of test processes, procedures, facilities and equipment;\n5.\tinspection and maintenance of test facilities, infrastructure, and software to demonstrate continuing test process capability;\n6.\tapplicable competence, training and certification of test personnel and lower tier suppliers in conformance with the requirements of clause 5.4. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.8.1a","Requirement","ECSS-Q-ST-20-07_0370143","The space test centre shall establish and maintain documented procedures for the assessment of readiness of the test facility and the test set-up to verify that the applicable requirements are met. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.8.1d","Requirement","ECSS-Q-ST-20-07_0370146","The FRR shall address, as a minimum, the following topics:\n1.\ttest documentation, including test methods and procedures and acceptance criteria, \n2.\ttest facility status, including: \n(a)\tfacility configuration for the test, \n(b)\ttest facility data handling, \n(c)\ttest facility measurement equipment, \n(d)\tequipment calibration, \n(e)\tenvironmental conditions,\n(f)\tcleanliness status,\n(g)\tmaintenance status, \n(h)\tsafety status,\n(i)\tnonconformances, waiver and deviations that can affect the test,\n3.\tpersonnel qualification and availability, \n4.\tground support equipment (GSE) dedicated to the test and infrastructure readiness, \n5.\ttest specimen (in case responsibility has been contractually transferred to the space test centre), \n6.\tresults from pre-tests (dry-runs, rehearsals), and \n7.\tfinal test preparation actions status. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-07C","5.9.2c","Requirement","ECSS-Q-ST-20-07_0370167","The space test centre shall demonstrate that the safety policy is known and supported by all space test centre personnel.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","4.2h","Requirement","ECSS-Q-ST-20-08_1170009","It shall be ensured that the environment seen by the flight hardware during transportation is not exceeding the acceptance level.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","5.4.1c","Requirement","ECSS-Q-ST-20-08_1170029","The configuration of the hardware under storage shall be known and documented into the storage documentation.","NOTE \tFlight and no flight item are identified in the ABCL.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","5.4.3a","Requirement","ECSS-Q-ST-20-08_1170036","Prior storage under his responsibility, the supplier shall demonstrate that the actual environmental conditions are in accordance with the ones specified in the Storage Plan in conformance with the DRD from Annex A.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","6.2.2c","Requirement","ECSS-Q-ST-20-08_1170057","For MGSE fulfilling the requirement 6.2.2a condition automatism, alert and warning shall be defined by risk analysis and implemented to avoid reaching the hazard or unsafe conditions.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","6.3.2e","Requirement","ECSS-Q-ST-20-08_1170077","The operation leader shall define and implement a safety perimeter.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","7.5a","Requirement","ECSS-Q-ST-20-08_1170102","In order to co-ordinate a smooth dispatch process, the supplier in charge of the transport shall conduct an internal CTT meeting for the shipment of all the P1 and P2 products to be dispatched.","NOTE \t1\tExample of CTT document is given in Annex C.\nNOTE \t2\tExample of packing, shipping, transportation and delivery checklist is presented in Annex D.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","7.5d","Requirement","ECSS-Q-ST-20-08_1170105","The CTT review shall take place to enable transport to be arranged at the right time and to ensure the products arrive at the destination safely and securely.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-20-08C","7.8.2d","Requirement","ECSS-Q-ST-20-08_1170133","The container for the units shall be labelled, tagged or marked to allow detailed identification of the contents of the container, with at least the following:\n1.\tName of manufacturer and customer of the flight hardware\n2.\tProject name\n3.\tUnit name and model\n4.\tConfiguration Item number\n5.\tPart number\n6.\tQuantity or weight (kg)",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","6.2.1e","Permission","ECSS-Q-ST-70-39_1280238","Qualification of a process given to a welding operator may be extended indefinitely provided the three following conditions are met: \n1.\ta qualification record is maintained from the date of the initial qualification,\n2.\tregular audit of the records specified in the 6.2.1e.1 is performed,\n3.\tthe welder and welding operator use the process within every six month period. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","7.2e","Requirement","ECSS-Q-ST-70-39_1280034","Re-acceptance of an equipment shall be performed in the following cases:\n1.\tafter severe repair operation,\n2.\tafter relocation of the welding equipment,\n3.\tafter installation of electrical components which can affect any welding parameter.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","7.3.2a","Requirement","ECSS-Q-ST-70-39_1280041","The filler metal shall be procured with an inspection certificate of type 3.1 from the requirements from clause 4.1 of EN 10204:2004.","NOTE\tThis is a certificate issued by the manufacturer in which the manufacturer declares that the products supplied are in compliance with the requirements of the order made be the customer and in which the manufacturer supplies test results.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","8.1.3a","Requirement","ECSS-Q-ST-70-39_1280060","All welding processes shall be in accordance with ISO 4063:2009.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","8.1.7a","Requirement","ECSS-Q-ST-70-39_1280080","Backing and shielding gases shall be used in conformance with the requirements from DRD from Annex A.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","9.2.1a","Requirement","ECSS-Q-ST-70-39_1280105","When metallographic examinations are required for cross-section examination, samples shall be prepared in accordance with ASTM E3:2007, ASTM E340:2013 and ASTM E407:2007.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","9.2.1d","Requirement","ECSS-Q-ST-70-39_1280108","For circumferential welds, one cut shall be done at 0° position of the weld seam and a second cut at 180° position of weld seam.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","11.1.2a","Requirement","ECSS-Q-ST-70-39_1280134","To verify the weld data set, the assessment of the weld samples for safety classes 1 and 2 shall be as follows:\n1.\tfor manual arc welding the minimum number of weld samples in conformance with Table 11-1.\n2.\tfor all other welding processes the minimum number of weld samples in conformance with Table 11-2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","11.5e","Requirement","ECSS-Q-ST-70-39_1280157","Repair welding shall be performed using a WPS which is approved for weld repair.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","12.2.3b","Requirement","ECSS-Q-ST-70-39_1280179","The application of the inspection criteria specified in the requirement 12.2.3a shall be in conformance with DIN 29595:2007-04 and depends on the Safety Class of the weld.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","13.1c","Requirement","ECSS-Q-ST-70-39_1280187","Modifications to welding parameters which fall outside the WPS shall lead to the issue of a new weld configuration.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","A.2.1<1.2>c","Requirement","ECSS-Q-ST-70-39_1280208","The weld run sequence shall be given on the engineering drawing. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-39C","B.2.1<4>a","Requirement","ECSS-Q-ST-70-39_1280233","Pre-heating and post-weld heat treatments shall be in conformance with the requirements specified in the clause A.2.1<1.6>.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10C Rev.1","5.1.3c","Requirement","ECSS-Q-ST-10_0360017","The Product Assurance plan shall be submitted to the customer for approval.","NOTE \t1\tThe Product Assurance plan can refer to Clauses of the Company Quality Manual and to in-house procedures.\nNOTE \t2\tInformation on the schedule for delivery of PA management documents is given in Annex D.\n",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-10C Rev.1","5.2.1c","Requirement","ECSS-Q-ST-10_0360020","The PA manager shall ensure that the PA disciplines perform the tasks described in the PA Plan in line with the project schedule.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-10C Rev.1","5.2.5b","Requirement","ECSS-Q-ST-10_0360041","The PA manager shall ensure that invalid or obsolete documents and data are removed from all points of issue or use, or assured against unintended use.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-10C Rev.1","A.2.2b","Permission","ECSS-Q-ST-10_0360073","The response to this DRD may be performed by reference to separate discipline plans addressing some of the above clauses of this DRD.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70-14C","5.4.4a","Requirement","ECSS-Q-ST-70-14_1340018","In Class 3 environments, the protective finish shall be tested by a combination of UV and NSST.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-14C","5.5.1a","Requirement","ECSS-Q-ST-70-14_1340025","For processes used for corrosion protection the supplier shall implement a verification programme.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-14C","5.6.2d","Permission","ECSS-Q-ST-70-14_1340072","Nickel plating may be used for applications up to 538 °C.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-14C","5.9.4b","Requirement","ECSS-Q-ST-70-14_1340066","Galvanic couples shall be in conformance with values from Table 5-1 of ECSS-Q-ST-70.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-80C Rev.1","5.2.1.5b","Requirement","ECSS-Q-ST-80_0720019","For each software product assurance requirement, the compliance matrix shall provide a reference to the document where the expected output of that requirement is located.","NOTE For compliance with the required DRDs a general statement of compliance is acceptable.\nEXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR, PDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","5.2.2.3a","Requirement","ECSS-Q-ST-80_0720022","The supplier shall deliver at each milestone review a software product assurance milestone report, covering the software product assurance activities performed during the past project phases.\n","EXPECTED OUTPUT: Software product assurance milestone report [PAF, SPAMR; SRR, PDR, CDR, QR, AR, ORR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","5.5.1a","Requirement","ECSS-Q-ST-80_0720046","For procurement documents, ECSS-Q-ST-20 clause 5.4.2 shall apply.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.1.1a","Requirement","ECSS-Q-ST-80_0720067","The software development life cycle shall be defined or referenced in the software product assurance plan.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.2.2.6a","Requirement","ECSS-Q-ST-80_0720088","The supplier shall update the software dependability and safety analysis at each software development milestone, to confirm the criticality category of software components.\n","EXPECTED OUTPUT: Software dependability and safety analysis report [PAF, -; CDR, QR, AR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.2.3.2a","Requirement","ECSS-Q-ST-80_0720094","The supplier shall define, justify and apply measures to assure the dependability and safety of critical software.","NOTE \tThese measures can include:\n·\tuse of software design or methods that have performed successfully in a similar application;\n·\tinsertion of features for failure isolation and handling (ref. ECSS-Q-HB-80-03, software failure modes and effects analysis);\n·\tdefensive programming techniques, such as input verification and consistency checks;\n·\tuse of a “safe subset” of programming language;\n·\tuse of formal design language for formal proof;\n·\t100 % code branch coverage at unit testing level;\n·\tfull inspection of source code;\n·\twitnessed or independent testing;\n·\tgathering and analysis of failure statistics;\n·\tremoving deactivated code or showing through a combination of analysis and testing that the means by which such code can be inadvertently executed are prevented, isolated, or eliminated.\nEXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.2.5.3a","Requirement","ECSS-Q-ST-80_0720115","The following basic process metrics shall be used within the supplier’s organization: \n    1. duration: how phases and tasks are being completed versus the planned schedule;\n    2. effort: how much effort is consumed by the various phases and tasks compared to the plan.\n","EXPECTED OUTPUT: Internal metrics report.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.2.7.8b","Requirement","ECSS-Q-ST-80_0720140","For software products whose life cycle data from previous development are not available and reverse engineering techniques are not fully applicable, the following methods shall be applied:\n    1. generation of validation and verification documents based on the available user documentation (e.g. user manual) and execution of tests in order to achieve the required level of test coverage;\n    2. use of the product service history to provide evidence of the product’s suitability for the current application, including information about:\n        (a) relevance of the product service history for the new operational environment;\n        (b) configuration management and change control of the software product;\n        (c) effectiveness of problem reporting;\n        (d) actual error rates and maintenance records;\n        (e) impact of modifications.\n","EXPECTED OUTPUT: Software reuse file [DJF, SRF; SRR, PDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.3.3.3a","Requirement","ECSS-Q-ST-80_0720161","For software in which numerical accuracy is relevant to mission success specific rules on design and code shall be defined to ensure that the specified level of accuracy is obtained.","NOTE For example: for an attitude and orbit control subsystem, scientific data generation components.\nEXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.3.3.5b","Requirement","ECSS-Q-ST-80_0720164","The design evaluation shall be performed in parallel with the design process, in order to provide feedback to the software design team.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.3.5.13a","Requirement","ECSS-Q-ST-80_0720189","The supplier shall confirm in writing that the tests are successfully completed.\n","EXPECTED OUTPUT: Testing and validation reports [DJF, -; CDR, QR, AR, ORR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","6.3.6.2a","Requirement","ECSS-Q-ST-80_0720210","The installation shall be performed in accordance with the installation procedure.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","7.1.8a","Requirement","ECSS-Q-ST-80_0720235","The supplier shall define the organization and means implemented to collect and analyse data required for the study of software maturity.","NOTE For example: failures, corrections, duration of runs.\nEXPECTED OUTPUT: Software product assurance reports [PAF, -; -].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","7.2.1.3a","Requirement","ECSS-Q-ST-80_0720238","For each requirement the method for verification and validation shall be specified.\n","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR].",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","7.4.5a","Requirement","ECSS-Q-ST-80_0720259","Taking account of the provider’s maintenance and product policy, it shall be ensured that the hardware and support services can be maintained throughout the specified life of the software product within the operational constraints.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","B.2.1<6.2>b","Requirement","ECSS-Q-ST-80_0720284","The relationship between the project plans and a timely planning for their preparation and update shall be described.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","C.2.1<5>b","Requirement","ECSS-Q-ST-80_0720305","The SPAMR shall include reporting on the correct use of methods and tools.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-80C Rev.1","C.2.1<7>b","Requirement","ECSS-Q-ST-80_0720308","The results of the software maturity analysis shall also be reported.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","4.8a","Requirement","ECSS-Q-ST-30_0410021","The supplier shall report dependability progress to the customer as part of product assurance activities in conformance with ECSS-Q-ST-10.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","5.4a","Requirement","ECSS-Q-ST-30_0410042","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","5.7b","Requirement","ECSS-Q-ST-30_0410053","All recommendations from 5.7a shall be justified, documented and tracked.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","6.1a","Requirement","ECSS-Q-ST-30_0410056","The supplier shall identify undesirable events that lead to the loss or degradation of product performances, together with their classification into categories related to the severity of their failure consequences (see Table 5-1).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","6.4.2.2c","Requirement","ECSS-Q-ST-30_0410077","Measures shall be proposed in the analysis and introduced in the product design and in the control of processes to render all such consequences acceptable to the project.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","6.4.4e","Requirement","ECSS-Q-ST-30_0410102","The availability analysis shall be carried out at system level using the system reliability and maintainability models as well as the data from the outages. ","NOTE \tFor availability analysis, refer to ECSS-Q-ST-30-09.\n",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-30C Rev.1","7.2a","Requirement","ECSS-Q-ST-30_0410110","Availability testing and demonstration shall be performed according to the project requirements in order to validate or justify data bases used for theoretical demonstrations (duration of outages and probability of occurrence).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.1.1.2b","Requirement","ECSS-Q-ST-70-26_0130002","Production facilities where high reliability crimping is performed shall be maintained in a clean and tidy condition.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.1.2.2a","Requirement","ECSS-Q-ST-70-26_0130022","The supplier shall provide the tooling necessary to avoid damage to the conductor.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.2.1j","Requirement","ECSS-Q-ST-70-26_0130042","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.2.5f","Requirement","ECSS-Q-ST-70-26_0130064","For separate conductors introduced straight into the barrel the following shall apply: \n1.\tthe actual strength measurement is performed on one of the wires (the smaller, if two different sizes are used);\n2.\tthe axial strength requirement is determined as specified in requirements of clause 5.4.3.2 for the actual size of wire pulled, assuming a barrel size equal to that wire’s gauge.","NOTE \tExamples of crimping parameters are given in Table A-3 and an example of a typical connector barrel and multi-wire crimping is shown in Figure 5-3.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.2.5i","Requirement","ECSS-Q-ST-70-26_0130173","For 28 AWG up to 16 AWG wire sizes the maximum insulation clearance shall be maintained between 0,3 mm and 1,0 mm.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.3.1f","Requirement","ECSS-Q-ST-70-26_0130179","In case the mission environment exceeds the temperature range for which the materials are qualified, a qualification shall be performed and agreed with the customer ","NOTE \tExamples of materials include cables and crimp items.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.4.3.2d","Requirement","ECSS-Q-ST-70-26_0130188","If two different wire gauges are used then the test specified in 5.4.3.2c shall be performed on the smaller of the two.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.4.4j","Recommendation","ECSS-Q-ST-70-26_0130225","The laboratory for the metallographic tests should be certified with ISO 17025.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.5.2.2c","Requirement","ECSS-Q-ST-70-26_0130111","Operators or inspectors shall be re-certified in cases of repeatedly unacceptable quality levels and changes in crimping techniques, parameters or required skills.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.5.5b","Requirement","ECSS-Q-ST-70-26_0130128","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.5.6.2d","Requirement","ECSS-Q-ST-70-26_0130144","This traceability shall be established by periodic analysis of the corresponding data from the performance inspection and tests (in conformance with clause 5.5.5 requirements), ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","5.6b","Requirement","ECSS-Q-ST-70-26_0130158","The format of the documents shall be in accordance with the deliverables item list defined in the business agreement.","NOTE \tNo specific DRD requirements emerge from this Standard.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","5.1.2c","Requirement","ECSS-Q-ST-70-38_0210282","The first issue of the PID shall fully comply to this standard.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","6.4a","Requirement","ECSS-Q-ST-70-38_0210020","Requirements from clause 5.5 from ECSS-Q-ST-70-08 shall apply for “Precautions against static charges”.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","6.8.1a","Requirement","ECSS-Q-ST-70-38_0210042","Equipment shall not generate, induce or transmit electrostatic charges to devices being placed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","7.2.4a","Requirement","ECSS-Q-ST-70-38_0210062","When purchased premixed or mixed in house, the purity of solder paste shall be maintained.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","7.3.1a","Requirement","ECSS-Q-ST-70-38_0210069","Requirements from clause 6.3.1 from ECSS-Q-ST-70-08 shall apply for \"Rosin based flux\".",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","7.9.1d","Requirement","ECSS-Q-ST-70-38_0210087","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","7.9.4e","Requirement","ECSS-Q-ST-70-38_0210102","<<deleted and moved to 7.9.1n>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","8.5b","Requirement","ECSS-Q-ST-70-38_0210119","Baking of moisture sensitive devices shall be implemented before any reprocessing or assembly process in conformance with JEDEC classification.","NOTE\tThis is to counteract the “popcorn” effect in soldering using oven or vapour phase reflow techniques. \n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","8.5e","Requirement","ECSS-Q-ST-70-38_0210305","Baking of populated PCBs shall be performed when the PCB has been kept under clean room conditions for more than 72 hours.","NOTE\tStorage of PCBs in dry cabinet interrupts the accumulated baking time.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","9.7.6b","Requirement","ECSS-Q-ST-70-38_0210140","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","11.5.1a","Requirement","ECSS-Q-ST-70-38_0210158","Devices shall not be mounted on flexible substrates as defined “flexible printed boards” in ECSS-Q-ST-70-10. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","11.5.4b","Requirement","ECSS-Q-ST-70-38_0210324","Solder joints to devices having square terminations shall meet the dimensional and solder fillet requirements of Table 11-4 and Figure 11-4.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","11.5.8c","Requirement","ECSS-Q-ST-70-38_0210328","X-ray techniques shall be used to verify the acceptable wetting, the absence of bridge, solder balls and minimum electrical clearance.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","13.1b","Requirement","ECSS-Q-ST-70-38_0210182","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.1g","Requirement","ECSS-Q-ST-70-38_0210197","The supplier’s repair process including removing and replacing of one of each type of mounted device shall be submitted to verification testing.","NOTE\t1\tVerification of the number of repairs as permitted in ECSS-Q-ST-70-28.\nNOTE\t2\tThe supplier has the option to perform more than one repair for each type of device.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.2h","Requirement","ECSS-Q-ST-70-38_0210210","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.3a","Requirement","ECSS-Q-ST-70-38_0210214","The verification programme as shown in Figure 14-1 shall consist of:\n1.\tVisual inspection in conformance with clause 13.\n2.\tVibration and shock testing in conformance with clause 14.5.\n3.\tTemperature cycling in conformance with clause 14.6 except for area array devices .\n4.\tMicrosectioning in conformance with clause 14.7.\n5.\tFor area array devices, temperature cycling in conformance with requirements from clause 14.9.\n6.\tCleanliness in conformance with requirement 14.14b.","NOTE\t1\tNote to item 2: Mechanical testing according to this standard gives an indication of the reliability of the product in actual applications. It is unlikely that the test vehicle represents every flight configuration (size of the board, damping of the board, stiffening of board, number of board layers). The deflections, amplitudes, transmissibilities, radii of curvature experienced by SMDs under shock and vibration are totally dependent on the board to which they are mounted. Because each space project has its own unique shock and vibration requirements it is impossible to determine appropriate test levels without testing actual electronic boxes.\nNOTE\t2\tNote to item 3: Temperature cycling is performed to ensure that the SMDs, substrates, solder alloys and associated stacking compounds and conformal coatings are suitable for the operational lifetime of the spacecraft. \n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.3r","Requirement","ECSS-Q-ST-70-38_0210389","NRBs shall be organised by the supplier.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.5g","Requirement","ECSS-Q-ST-70-38_0210405","The levels and duration of the shock shall be provided by supplier.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.7.2f","Requirement","ECSS-Q-ST-70-38_0210416","In case the microsection shows a crack more than 75% of acceptable crack, a second device shall be microsectioned.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.7.2m","Recommendation","ECSS-Q-ST-70-38_0210510","The microsection for devices with small stand-off should be inspected with magnification up to 500 times.","NOTE\tExamples of small stand-off devices are LCCs, chip resistors.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.9.4i","Requirement","ECSS-Q-ST-70-38_0210436","After environmental tests completion, microsectioning of the device shall be performed to demonstrate PCB integrity in the AAD area with respect to:\n1.\tECSS-Q-ST-70-10,\n2.\tDamage to the device outside the procurement specification,\n3.\tFootprint lifts,\n4.\tCracks in laminate,\n5.\tCracks in via,\n6.\tCracks in track,\n7.\tDelamination’s in the PCB,\n8.\tMeasling in the PCB,\n9.\tCracks in bonding if used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.10h","Requirement","ECSS-Q-ST-70-38_0210449","The devices shall be in conformance with the assembly requirements of clause 11.5.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.15.1b","Requirement","ECSS-Q-ST-70-38_0210467","RFA shall be issued.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","14.15.2b","Permission","ECSS-Q-ST-70-38_0210517","The qualifying authority may waive the need for technology sample.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","15.9a","Requirement","ECSS-Q-ST-70-38_0210259","<<deleted, requirement modified in 15.9d>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","5.3.2b","Requirement","ECSS-Q-ST-70-60_1390004","In case the flexible PCB is not qualified in conformance with ECSS-Q-ST-70-60, the project qualification of flexible PCB shall be reviewed under RFA in conformance with clause 7.7.2.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","5.7b","Requirement","ECSS-Q-ST-70-60_1390025","The qualification vehicle shall be representative of the highest technological complexity for which qualification is requested.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","5.8a","Requirement","ECSS-Q-ST-70-60_1390031","The requirements of clause 5.7 shall apply to the evaluation samples.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","5.10c","Requirement","ECSS-Q-ST-70-60_1390051","The PCB manufacturer shall issue the qualification test report in conformance with the DRD in Annex C.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","5.15e","Requirement","ECSS-Q-ST-70-60_1390071","Upon successful qualification renewal, the qualification authority shall approve the qualification in conformance with the clause 5.12 and issue a new qualification letter in conformance with requirement 5.12a.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.3b","Requirement","ECSS-Q-ST-70-60_1390086","The PCB manufacturer shall include coupons on the panel for in-house quality control.","NOTE \tThe panel also includes coupons for batch release and spare coupons. These are described in clause 8.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.3e","Requirement","ECSS-Q-ST-70-60_1390089","Work instructions shall specify the methodology for final inspection in conformance with clause 8.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.6c","Requirement","ECSS-Q-ST-70-60_1390111","Electrolytic soft gold plating shall have a purity of ≥ 99,8 % gold, except for the case of electrolytic hard gold plating.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.7.2j","Requirement","ECSS-Q-ST-70-60_1390126","The PCB manufacturer shall provide instructions to operators on the measures specified in its cleanliness control procure.","NOTE \tExamples of instructors to operators can include labels on the work floor, photographic instructions on best practices, identification of critical areas, and training.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.10.2g","Permission","ECSS-Q-ST-70-60_1390748","In case SnPb is missing on the surface, it may be added with a solder iron and flux on bare surface copper in case all the following conditions are met:\n1.\tthe documented repair operation includes limits for temperature, duration and flux in conformance with ECSS-Q-ST-70-08;\n2.\tthe PCB manufacturer has inspected plated holes to verify the absence of missing SnPb inside them;\n3.\tthe PCB manufacturer has verified that the copper is non-etched in the area of missing SnPb.","NOTE \tNon-etched copper has a flat surface, whereas etched copper has a concave surface. In case copper is affected by etching, the missing SnPb is a process indicator of a problem that can affect plated holes, which cannot be repaired.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.10.2n","Requirement","ECSS-Q-ST-70-60_1390147","Other repairs that are not specified in this clause shall not be performed.","NOTE \tExamples of such repairs are:\n·\trepair of burrs;\n·\tbrushing of overhang of Ni/Au or Au;\n·\trepair of PTH with too small diameter due to excessive SnPb thickness.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","6.13b","Requirement","ECSS-Q-ST-70-60_1390165","Shelf-life shall include storage at the procurement authority and storage at the PCB manufacturer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","7.2b","Requirement","ECSS-Q-ST-70-60_1390186","For initial qualification of a PCB manufacturer or a PCB technology, all tests of groups 1, 2, 3, 4, and 5 shall be performed on PCB and coupon.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","7.7.2b","Requirement","ECSS-Q-ST-70-60_1390206","Project qualification shall provide approval of a PCB technology for the batch used on that project only. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","7.7.2e","Recommendation","ECSS-Q-ST-70-60_1390763","The group 6 from the qualification test plan should be performed on one spare PCB from the FM batch.","NOTE \tThe advantage of testing the FM batch is to ensure representativity. This is important when using non-qualified PCB manufacturers for whom batch-to-batch QA has not been verified by an audit in conformance with ECSS-Q-ST-70-60. The disadvantage of testing the FM batch is that any nonconformances are discovered at a late stage of the procurement.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","8.2.2i","Requirement","ECSS-Q-ST-70-60_1390231","The term “coupon Bn” shall indicate all coupons B1, B2 … Bn for all plating sequences.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","8.2.4g","Requirement","ECSS-Q-ST-70-60_1390250","The microsections of the as-received coupons for plated holes shall be submitted to microscopic inspection in as-polished and micro-etched conditions.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","8.2.5b","Permission","ECSS-Q-ST-70-60_1390773","The IST coupon may be send later than the other coupons, due to its logistics of test and shipment.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.2.2a","Requirement","ECSS-Q-ST-70-60_1390271","Standard bake-out shall be minimum 8 hours at 120 ˚C in ambient pressure.","NOTE\t1\tBaking is performed to remove humidity from the dielectric materials prior to thermal excursions. PCB laminates are known to be hygroscopic.\nNOTE\t2\tFor sensitive PCB technology such as rigid-flex, this bake-out can cause damage when the heating rate is high. In this case a tailoring of the bake-out profile is good practice as per requirement 9.2.2b.\nNOTE\t3\tThis bake-out is in conformance with clause 8.5d of ECSS-Q-ST-70-38.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.3.1a","Requirement","ECSS-Q-ST-70-60_1390284","Visual inspection shall be performed using 10x to 40x magnification.","NOTE \tExamples of equipment used for visual inspection are: binoculars, loups, single scope.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.3.3.3i","Permission","ECSS-Q-ST-70-60_1390783","The procurement authority may specify a more stringent requirement for twist in the PCB definition dossier.","NOTE\t\tSee the notes 1, 2, 3 and 4 from clause 9.3.3.2.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.3.7.2n","Permission","ECSS-Q-ST-70-60_1390787","In case the test fails because the set voltage is not achieved due to high capacitance caused by presence of plane layers, one further re-test may be performed with adjusted parameters.","NOTE \tSuch adjustment can include longer sustain time or longer ramp-up time.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.3.8.2b","Requirement","ECSS-Q-ST-70-60_1390334","The test voltage shall be maximum 10 VDC.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.4.3e","Requirement","ECSS-Q-ST-70-60_1390356","Flexural fatigue test shall cover only static applications.","NOTE \tDynamic applications are project qualified in conformance with requirement 8.6.2b of ECSS-Q-ST-70-12.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.4.6c","Permission","ECSS-Q-ST-70-60_1390793","Another method resulting in the same degree of precision may be used.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.4.8b","Requirement","ECSS-Q-ST-70-60_1390380","Temperature of decomposition, Td, shall be measured in conformance with test method 2.4.24.6 of IPC-TM-650 using TGA.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.4.11.4d","Requirement","ECSS-Q-ST-70-60_1390395","The solderability test shall be performed in not less than one minute, and not more than five minutes after application of flux.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.5.2.5a","Requirement","ECSS-Q-ST-70-60_1390412","Quality of metallisation shall be inspected in bright field.","NOTE \tBright field achieves the best contrast in the metallised areas.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.5.4.3h","Recommendation","ECSS-Q-ST-70-60_1390810","Sample with high thermal mass should be submitted to pre-heating during the rework simulation test.","NOTE \tThis is done to limit the soldering time to maximum 5 seconds.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.5.5.4.1b","Requirement","ECSS-Q-ST-70-60_1390448","Bake-out of IST coupons shall be performed in conformance with requirement 9.2.2a.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.5.5.4.1e","Recommendation","ECSS-Q-ST-70-60_1390817","Correct soldering of connectors should be verified by measuring again the resistance of IST coupons.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.5.5.5.2c","Recommendation","ECSS-Q-ST-70-60_1390824","Specific IST coupons for interconnect verification should include all drill sizes for holes that interconnect on RF laminate.","NOTE \tThis does not include non-functional pads.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.6.3i","Requirement","ECSS-Q-ST-70-60_1390479","The intralayer insulation resistance as received shall be ≥ 10 GΩ.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.6.4d","Requirement","ECSS-Q-ST-70-60_1390486","Visual inspection shall show no evidence of breakdown, flashover or sparking.","NOTE\t1\tTest coupon E of IPC-2221B can be used for intralayer DWV. For interlayer DWV, test coupon E is modified as per requirement 9.6.4b.\nNOTE\t2\tAdvanced test equipment are capable to monitor voltage or leakage current continuously during the applied test voltage. A sudden drop in voltage is indicative of a discharge. This is relevant because visual inspection is not fully efficient on internal layers covered by plane layers.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.7.3.2b","Requirement","ECSS-Q-ST-70-60_1390507","The build-up of the test vehicle for CAF test shall meet all the following conditions:\n1.\tRepresentative of the PID for material and PCB technology;\n2.\t≥ 10 copper layers;\n3.\t1,6 mm ± 10 % thickness over connector metallisation;\n4.\t17 μm copper foil on inner and outer layers;\n5.\tSingle sequence for drilling and plating;\n6.\tSequential lamination.","NOTE\t1\tThe stack-up is laminated once, after which it passes through the lamination process for a second time to simulate sequential construction.\nNOTE\t2\tIt is important to note in Table 9-2, Table 9-3 and Table 9-4 that hole diameters are specified as drill bit diameter, not finished hole diameter.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","9.8.2g","Permission","ECSS-Q-ST-70-60_1390839","In case of project qualification with specific environmental requirements, the thermal cycling may be tailored.","NOTE\t1\tSpecific environmental requirements can include operational temperature below -55 °C or above +85 °C, for instance for detector technology that is exposed to planetary environment. \nNOTE\t2\tIt is not good practice to reduce the temperature range or number of cycles because thermal cycling is not only a simulation of space environment. It also simulates equipment on/off cycles and it is considered a general assessment of PCB robustness.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.2h","Requirement","ECSS-Q-ST-70-60_1390547","For the technological feature dielectric thickness for standard technology. The acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-8. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.3m","Requirement","ECSS-Q-ST-70-60_1390584","For the technological feature smear, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-29.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.3t","Requirement","ECSS-Q-ST-70-60_1390591","For the technological feature rigid-flex interface adhesive voids in coverlay and bond-ply, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-36.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.5f","Requirement","ECSS-Q-ST-70-60_1390647","For the technological feature annular ring for sculptured flex PCB, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-57.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.6.2h","Requirement","ECSS-Q-ST-70-60_1390681","Cracks associated with pad lift shall not reach the hole wall before or after thermal stress.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","10.6.3d","Requirement","ECSS-Q-ST-70-60_1390688","Remaining insulation distance shall be the sum of insulation distances to conductors that are not affected by cracks.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-60C Corr.1","B.2.1.6a","Requirement","ECSS-Q-ST-70-60_1390706","The microsection of coupons for dimensional verification shall be performed for all panels.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","5.1b","Requirement","ECSS-Q-ST-10-09_0350002","Based on the preliminary assessment the supplier’s project PA representative shall take the following actions without delay:\n    1. Provisions for the safety of the personnel and of the equipment.\n    2. Prevention of unauthorized use of the nonconforming items, by marking and, unless otherwise determined by the PA representative, segregation until their disposition.\n    3. Prevention of the recurrence of the nonconformances on similar or identical items under processing or testing at that time.","This can lead to the suspension of manufacturing or testing.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","5.2.2.5a","Requirement","ECSS-Q-ST-10-09_0350027","The supplier shall notify the customer each time a nonconformance is classified as “major” within five working days of their detection.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","5.4.1b","Requirement","ECSS-Q-ST-10-09_0350048","The supplier shall re-submit reworked and repaired items to all planned inspections and tests.","Repair can invoke additional inspection and tests, as defined in the applicable repair procedure.",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","5.4.2d","Requirement","ECSS-Q-ST-10-09_0350055","After close-out, the supplier shall send a copy of the NCR to the customers involved in its processing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","6.2.1c","Requirement","ECSS-Q-ST-10-09_0350076","<<deleted, requirement covered by ECSS-Q-ST-80>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","A.2.1<4>a","Requirement","ECSS-Q-ST-10-09_0350095","The NCR shall contain alpha or numerical identification of updated issues.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","A.2.1<13>a","Requirement","ECSS-Q-ST-10-09_0350105","The NCR shall contain the date and location of the nonconformance observation.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-10-09C Rev. 1","A.2.1<33>a","Requirement","ECSS-Q-ST-10-09_0350126","The NCR shall contain the name of company and person chairing the customer NRB.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-17C","5.2d","Requirement","ECSS-Q-ST-70-17_1380009","The following minimum set of qualification tests shall be performed according to the coating type:\n1.\tfor optical coatings, as specified in Table 5-1,\n2.\tfor TCC coatings, as specified in Table 5-2,\n3.\tfor thick metallic coatings for RF and electrical applications  and corrosion protection coatings, as specified in Table 5-3.","NOTE\tTest methods are defined in clause 6.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-17C","6.1b","Requirement","ECSS-Q-ST-70-17_1380032","During visual inspection no degradation shall be evident compared to the initial inspection.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-17C","6.4b","Requirement","ECSS-Q-ST-70-17_1380053","For the vacuum cycles, the vacuum level shall be < 5 x 10-5 hPa. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-17C","6.4i","Requirement","ECSS-Q-ST-70-17_1380060","The test method and set-up shall be specified.","NOTE\tMethod for thermal cycling testing is defined in ECSS-Q-ST-70-04.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-17C","7.2c","Requirement","ECSS-Q-ST-70-17_1380079","A supplier process audit shall be performed for new suppliers prior to the start of qualification testing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-05C Rev.1","5.1.5.2a","Requirement","ECSS-Q-ST-70-05_0540017","The sample holder in the sample compartment of the infrared spectrometer shall be aligned for obtaining quantitative information.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-05C Rev.1","5.2.3.2b","Requirement","ECSS-Q-ST-70-05_0540024","The window shall then be placed under the IR lamp until the solvent evaporates leaving a thin film of contaminant on the window.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-05C Rev.1","5.4.3.1c","Requirement","ECSS-Q-ST-70-05_0540045","The supplier shall calibrate any measuring equipment to traceable reference standards.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-05C Rev.1","5.4.3.5b","Requirement","ECSS-Q-ST-70-05_0540070","The noise level shall be at least three times less than the signal in order to recognize a signal.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-05C Rev.1","5.5.3c","Requirement","ECSS-Q-ST-70-05_0540091","The supplier shall deliver the review report to all customers within six weeks after the end of the regular review or evaluation testing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.2.2.1d","Requirement","ECSS-Q-ST-70-31_0660015","Coated surfaces shall be shielded from contact by using appropriate bags or sheets.","NOTE \tThe suitable bags are for example plastic bags with desiccators, sheet of tissue-paper, sheet of polyethylene foam.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.2.2.3c","Requirement","ECSS-Q-ST-70-31_0660022","Adhesion test sample shall be prepared and tested according to ECSS-Q-ST-70-13, clause 5.1.2, ISO-2409:2007, or equivalent national standards.","NOTE \tFor silicone’s paint, a tape based on silicon adhesive is used. However the added power of such tape can be out of the ISO specified strength\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.3.1.1a","Requirement","ECSS-Q-ST-70-31_0660043","Surfaces shall be abraded in order to increase the adherence according to coating material manufacturer requirement and agreed with customer.","NOTE \t1\tEmery paper, sand paper, grit blasting can be used as abrasion medium.\nNOTE \t2\tIn certain cases, abrasion is not feasible or can damage the item.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.3.3.2a","Requirement","ECSS-Q-ST-70-31_0660064","Before application of the paint, the primer shall be cured in a clean and dust-free area for duration as defined in the manufacture’s or other paint specific application procedure.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.3.4.1f","Requirement","ECSS-Q-ST-70-31_0660071","Dry nitrogen or clean compressed air shall be used as spray gas.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-31C Rev.1","4.3.6.2c","Requirement","ECSS-Q-ST-70-31_0660092","If the primer needs to be repaired, the same process as the paint shall apply (see technical data sheet).",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.4a","Requirement","ECSS-Q-ST-70-71_1260010","The effect of alloying element depletion at the surface of superalloys in high-temperature oxidizing environments shall be evaluated when sheet is used.","NOTE\tA slight amount of depletion can involve a considerable proportion of the effective cross section of the material.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.8h","Requirement","ECSS-Q-ST-70-71_1260031","Subsequent fusion welding in the vicinity of brazed or soldered joints or other operations with high temperatures that affect the brazed or soldered joint shall not be performed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.11d","Requirement","ECSS-Q-ST-70-71_1260052","Adhesives, coatings and varnishes shall be capable of accommodating dimensional changes resulting from temperature excursions without causing damage to the adhesive bond, or to other parts of the assembly.","NOTE\tElectronic PCBs are example of other parts of the assembly.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.11k","Requirement","ECSS-Q-ST-70-71_1260059","The supplier shall verify that the curing is affecting the whole surface of the bonded area when adhesives need atmospheric moisture as part of the curing process.","NOTE\tThis verification is even more important in case of non-porous or large surfaces. \n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.14a","Requirement","ECSS-Q-ST-70-71_1260079","The selection of the lubricant shall avoid the contamination of the lubricated part.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.17b","Requirement","ECSS-Q-ST-70-71_1260104","Polysulphide materials shall not be used in the space environment.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.17e","Requirement","ECSS-Q-ST-70-71_1260107","Rubbers and elastomers containing plasticisers or extending oils shall not be used under vacuum.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.2.18m","Requirement","ECSS-Q-ST-70-71_1260127","Cellulose and acetate materials in the form of films shall not be used in space applications.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.1f","Requirement","ECSS-Q-ST-70-71_1260152","During the bonding process, the adhesive cure cycle shall be controlled in accordance with an established procedure approved by the customer.","NOTE\tFor guidelines on structural adhesive bonding see ECSS-E-HB-32-21.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.4a","Requirement","ECSS-Q-ST-70-71_1260159","Processes developed for all types of paints shall be implemented and controlled in conformance with requirements from clause 4 of ECSS-Q-ST-70-31.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.6m","Requirement","ECSS-Q-ST-70-71_1260178","The result weld repair process qualification and inspection shall be subject to review by the customer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.6n","Requirement","ECSS-Q-ST-70-71_1260179","Brazing processes shall be evaluated regarding the effect on the parent metal.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.6o","Requirement","ECSS-Q-ST-70-71_1260180","The supplier shall demonstrate that in case the subsequent fusion welding is applied, it is not affecting any brazed joints in the vicinity.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.6p","Requirement","ECSS-Q-ST-70-71_1260181","Brazing operations shall be carried out by trained operators, working with documented and approved brazing procedures.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.7a","Requirement","ECSS-Q-ST-70-71_1260182","Fabrication processes and controls used in crimping of electrical terminations, terminal lugs, splices and two-piece shield termination rings shall conform to the requirements from clause 5 of ECSS-Q-ST-70-26.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.7b","Requirement","ECSS-Q-ST-70-71_1260183","Fabrication processes and controls used in wire wrapped electrical connections shall conform to the requirements from the clause 5 of ECSS-Q-ST-70-30.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.8a","Requirement","ECSS-Q-ST-70-71_1260184","Soldered joints shall not be used for structural applications without the prior approval of the customer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.8b","Requirement","ECSS-Q-ST-70-71_1260185","Fabrication processes and controls used in soldering of electrical connections shall conform to the requirements from clause 5 of ECSS-Q-ST-70-07, from clause 5 to clause 15 of ECSS-Q-ST-70-08 and from clause 5 to clause 16 of ECSS-Q-ST-70-38.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.8c","Requirement","ECSS-Q-ST-70-71_1260186","Repair processes and controls used in soldering of electrical connections shall conform to the requirements of clause 5 of ECSS-Q-ST-70-28.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.8d","Requirement","ECSS-Q-ST-70-71_1260187","The supplier shall demonstrate that when subsequent fusion welding or brazing is applied, it is not affecting any soldered joints in the vicinity.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.1a","Requirement","ECSS-Q-ST-70-71_1260188","All surface treatments process specifications shall include the qualified thickness range.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.1b","Requirement","ECSS-Q-ST-70-71_1260189","Processes and materials shall not degrade the substrate and result in loss of performance or integrity.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.1c","Requirement","ECSS-Q-ST-70-71_1260190","The supplier shall demonstrate that the surface is free from defects and it is not stained or discoloured.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.1d","Requirement","ECSS-Q-ST-70-71_1260191","An assessment shall be performed to demonstrate that the CTE mismatches between coating and substrates, if exist, do not prevent to meet the specified requirements.","NOTE \t1\tSurfaces of materials are often treated for the following reasons:\n·\tTo improve properties, e.g. nitriding, carburising and shot-peening.\n·\tTo increase resistance to an environment, e.g. corrosion, moisture- and diffusion barriers, high-temperature and ATOX.\n·\tTo provide particular characteristics, e.g. thermo-optical properties.\nNOTE \t2\tSome surface treatments are also included in other processes, for example preparation prior to painting and adhesive bonding to improve adhesion. These can include a proprietary “chemical” process such as anodizing or alodining or the application of a primer.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.2a","Requirement","ECSS-Q-ST-70-71_1260192","The supplier shall demonstrate that when anodizing processes are applied to thin foils, the perforation is prevented. ",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.2b","Requirement","ECSS-Q-ST-70-71_1260193","The supplier shall demonstrate that when anodizing processes are applied to thin foils the complete removal of process chemicals in complex parts is ensured.","NOTE\tThin foils include for example honeycomb cores.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.2c","Requirement","ECSS-Q-ST-70-71_1260194","Anodized layers shall be sealed and be continuous when used as the final surface finish of a part.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.2d","Requirement","ECSS-Q-ST-70-71_1260195","Anodized surfaces for pre-treatment of painting shall not be sealed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.2e","Requirement","ECSS-Q-ST-70-71_1260196","Process conditions shall be implemented and controlled.","NOTE \t1\tProcess conditions include for example bath constituents, temperature and time.\nNOTE \t2\tAnodizing is an electrolytic process for thickening and stabilizing the inherent oxide films on metal substrates. Anodizing is widely used on aluminium alloys and can be applied to magnesium and titanium. The anodized layer is electrically non-conductive. \nNOTE \t3\tNot all grades of an alloy can be anodized successfully.\nNOTE \t4\tDepending on the precise process, anodizing can produce:\n·\thard anodized wear resistant and durable surfaces;\n·\tcoloured surfaces (either functional or decorative), e.g. black for optical properties;\n·\tpre-treatment process prior to adhesive bonding or painting.\nNOTE \t5\tSpecifications for aerospace anodizing processes are available (often of American origin), but bath constituents and process conditions tend to vary between organizations.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.3a","Requirement","ECSS-Q-ST-70-71_1260197","Chemical conversion layers shall be continuous when used as the final surface finish of a part.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.9.3b","Requirement","ECSS-Q-ST-70-71_1260198","Control of process conditions shall be implemented and controlled.","NOTE \t1\tProcess conditions include for example bath constituents, temperature and time.\nNOTE \t2\tChemical conversion processes involve the absorption of a protective metal oxide film into an existing oxide film. The resulting surface finish can be electrically conductive or non-conductive.\nNOTE \t3\tNon-metal oxide films may sometimes be used.\nNOTE \t4\tChemical conversion processes include:\n·\t- Chromating (mixed metal-chromium oxide film), providing good corrosion resistance and pre-treatment for subsequently applied organic coatings. \n·\t- Conversion coatings for the replacement of hexavalent chromium are emerging, e.g. trivalent chromium systems.\n·\t- Phosphating, used as a pre-treatment prior to painting on ferrous materials.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10a","Requirement","ECSS-Q-ST-70-71_1260199","Process conditions and environments shall be specified and controlled during all stages of plating.","NOTE\tPlating stages include for example preparation, application, inspection or testing, and storage.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10b","Requirement","ECSS-Q-ST-70-71_1260200","Platings with open porosity shall not be used.","NOTE \t1\tPorous platings fail to provide adequate corrosion protection and can act as sources of contamination.\nNOTE \t2\tPlated layers of less than 1 µm thickness tend to be porous.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10c","Requirement","ECSS-Q-ST-70-71_1260201","An post-plating baking process approved by the customer shall be applied to materials with known or suspected susceptibility to hydrogen embrittlement.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10d","Requirement","ECSS-Q-ST-70-71_1260202","Plating of terminals used in electronic assemblies, shall satisfy the requirements from clause 5 to clause 15 of ECSS-Q-ST-70-08.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10e","Requirement","ECSS-Q-ST-70-71_1260203","In electronic assemblies, processes used for the removal of gold plating shall satisfy the requirements from clause 7.2.3.2 of ECSS-Q-ST-70-08.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.10f","Requirement","ECSS-Q-ST-70-71_1260204","All platings shall be blister tested by heat quench testing into air with a dwell time in the oven allowing to reach the maximum temperature seen in production and verification phases.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.11a","Requirement","ECSS-Q-ST-70-71_1260205","Machining shall not be performed on martensitic steel hardened to ≥1225 MPa UTS.","NOTE \t1\tMachining include for example drilling or grinding.\nNOTE \t2\tNumerous different machining operations are used for aerospace materials. International or national aerospace standards and specifications are normally applied.\nNOTE \t3\tSpecial tools and processes are applied to the machining of composites (laminates and honeycomb panels) to prevent damage to the materials (e.g. delamination, break-out on the backface and distortion of the core) that degrade the material integrity.\nNOTE \t4\tFor guidelines on machining composites, see ECSS-E-HB-32-20.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.11b","Requirement","ECSS-Q-ST-70-71_1260206","When machining is performed, the formation of untempered martensite shall be prevented.","NOTE\tFormation of untempered martensite can be prevented e.g. by the use of carbide tipped tooling.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.11c","Requirement","ECSS-Q-ST-70-71_1260207","The consequences of the effects of the use of EDM machining processes shall be assessed and reflected in any machining specification. ","NOTE\tThe use of EDM machining processes may lead to the formation of re-cast layer on the materials surfaces that has detrimental effects on the fatigue performances.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.11d","Requirement","ECSS-Q-ST-70-71_1260208","Safety equipment in accordance with the specified process shall be provided for operators processing beryllium and beryllium-copper alloys.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.11e","Requirement","ECSS-Q-ST-70-71_1260209","The collection and disposal of dust and debris produced during the processing of beryllium and beryllium-copper alloys shall conform to national or international specifications approved by the customer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.2a","Requirement","ECSS-Q-ST-70-71_1260210","Forging techniques shall be used that produce an internal grain-flow pattern such that the direction of flow is parallel to principal stresses.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.2b","Requirement","ECSS-Q-ST-70-71_1260211","Evaluation of flow patterns, including test data shall be submitted as part of the approval procedure for forged components.","NOTE\tThe mechanical properties are optimum in the direction of material flow during forging.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.3a","Requirement","ECSS-Q-ST-70-71_1260212","Forming processes shall respect the minimum bend radii for the specific alloy and condition.","NOTE\tExample of condition is heat-treatment or temper.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.3b","Requirement","ECSS-Q-ST-70-71_1260213","Annealing processes shall be selected to avoid degradation of the material.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.3c","Requirement","ECSS-Q-ST-70-71_1260214","Hot forming temperatures and soak times shall be selected to avoid segregation effects at grain boundaries or liquation of low melting point alloy constituents, either during heating the material or as a result of localized “over-heating” during forming.","NOTE \t1\tAll forming processes for sheet metals involve plastic deformation of the material. Processing techniques are either conducted “cold”, or “warm or hot”.\nNOTE \t2\tThe amount of deformation possible without fracture is linked to the material ductility. \n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.3d","Requirement","ECSS-Q-ST-70-71_1260215","For materials which harden as a result of cold working normally, an annealing process shall be applied to achieve the final shape without cracking or fracture. ","NOTE \t1\tHigh-strength materials are difficult to form to complex shapes by cold forming, and can be done “warm or hot”.\nNOTE \t2\tForming is often followed by a final heat-treatment to restore the mechanical properties of the finished part.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.4a","Requirement","ECSS-Q-ST-70-71_1260216","Superplastic forming processes shall only be applied to materials meeting the following conditions:\n1.\tmicrostructure: 1 µm to 5 µm grain size and stable at process temperature,\n2.\tplastic deformation in the range of 100 % to 1500 %, without fracture,\n3.\theated to at least 50 % of the melting temperature (in K),\n4.\trelatively low forming stresses,\n5.\tlow deformation rate.","NOTE \t1\tMaterials meeting these conditions are said to behave superplastically.\nNOTE \t2\tCommercial superplastic alloys include those based on aluminium, titanium, copper, nickel, stainless- and carbonsteels.\nNOTE \t3\tDepending on the metal alloy, super plastic forming can be combined with diffusion bonding to create finished parts, such as struts, cylinders and integrally stiffened panels.\nNOTE \t4\tSee ECSS-E-HB-32-20 for superplastic forming processes.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.12.5a","Requirement","ECSS-Q-ST-70-71_1260217","Safety procedures shall be applied for the storage and handling of explosives.","NOTE \t1\tExplosive forming is a rapid process for producing small quantities of large, fairly simply-shaped parts. It is applied to materials retaining acceptable ductility at high plastic deformation rates.\nNOTE \t2\tExplosive forming is also used as a cladding process and for joining dissimilar metals that cannot be joined effectively by any other means.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.13a","Requirement","ECSS-Q-ST-70-71_1260218","Heat treatment of metals and alloys shall conform to national or international specifications for aerospace applications approved by the customer.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.13b","Requirement","ECSS-Q-ST-70-71_1260219","Heat treatment procedures that are not included in any national or international specifications shall be approved by the customer prior to their use.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.13c","Requirement","ECSS-Q-ST-70-71_1260220","Processes shall be selected and controlled to avoid the dezincification of brasses.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.14a","Requirement","ECSS-Q-ST-70-71_1260221","Marking of spacecraft piece parts for identification purposes shall not result in the degradation of any mechanical or surface characteristics.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.14b","Requirement","ECSS-Q-ST-70-71_1260222","Solvents in inks shall not attack substrates.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.14c","Requirement","ECSS-Q-ST-70-71_1260223","Inks shall have outgassing properties in conformance with the requirements from clause 5 of ECSS-Q-ST-70-02.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.14d","Requirement","ECSS-Q-ST-70-71_1260224","Engraving of painted, plated or coated parts shall not be performed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.14e","Requirement","ECSS-Q-ST-70-71_1260225","Stamping resulting in stress-raisers shall not be performed.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.2a","Requirement","ECSS-Q-ST-70-71_1260226","Quality control and inspection procedures of all process related factors influencing the performance and integrity of castings shall be implemented and controlled to all of them.","NOTE\tProcess-related factors influencing the performance and integrity of castings include for example gas bubbles, inclusions and porosity, shrinkage.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.3a","Requirement","ECSS-Q-ST-70-71_1260227","Design of printed circuit board shall conform to the requirements from clause 5 to 15 of ECSS-Q-ST-70-12.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.3b","Requirement","ECSS-Q-ST-70-71_1260228","Procurement of printed circuit boards used for fabrication processes and controls shall conform to the requirements from clause 5 to clause 7 of ECSS-Q-ST-70-11.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.3c","Requirement","ECSS-Q-ST-70-71_1260229","Qualification of printed circuit boards used for fabrication processes and controls shall conform to the requirements from clause 5 to 9 of ECSS-Q-ST-70-10.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.4a","Requirement","ECSS-Q-ST-70-71_1260230","Fabrication processes and controls used in staking and conformal coating of printed circuit boards and electronic assemblies shall conform to the requirements of from clause 5 to clause 15 of ECSS-Q-ST-70-08, from clause 5 of ECSS-Q-ST-70-07 and from clause 5 to clause 16 of ECSS-Q-ST-70-38.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.4b","Requirement","ECSS-Q-ST-70-71_1260231","The repair and modification of printed circuit boards assemblies shall conform to the requirements from clause 4 of ECSS-Q-ST-70-28.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5a","Requirement","ECSS-Q-ST-70-71_1260232","The processes to be used for coaxial cable assembly shall be selected in conformance with clause 5 of ECSS-Q-ST-70-18.","NOTE\tSilver-plated copper strands are the preferred conductors. These are suitable for soldering and crimping.\nThe general requirements for wires and cables assemblies are described by the ESCC standards.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5b","Requirement","ECSS-Q-ST-70-71_1260233","If Nickel plated copper strands are used the supplier shall demonstrate that solderability after ageing is as described by the generic specification.","NOTE\tNickel is magnetic and cannot be used for all applications.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5c","Requirement","ECSS-Q-ST-70-71_1260234","Tin-plated finishes electroplated other than pure tin-coated wires shall be either re-flowed or excluded.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5d","Requirement","ECSS-Q-ST-70-71_1260235","Silver-plated wires shall be procured in conformance with requirements from the ESCC Generic Specification 3901.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5e","Requirement","ECSS-Q-ST-70-71_1260236","The individual wire specification of silver-plated wires shall be applied for requirements other than the ones specified in 4.3.15.5a, b, c and d.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5f","Requirement","ECSS-Q-ST-70-71_1260237","The following shall be assembled or installed in conformance with the requirements from clause 5 to clause 15 of ECSS-Q-ST-70-08:\n1.\telectrical connectors;\n2.\tinterconnecting cables, harness and wiring;\n3.\tsolder splice.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.5g","Requirement","ECSS-Q-ST-70-71_1260238","Solder sleeves shall not be used in flight hardware due to their retention of solder flux and inspection difficulties.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.15.6a","Requirement","ECSS-Q-ST-70-71_1260239","Fabrication processes and controls shall be established for terminations, joining fibre optic cable assemblies and their installation and submitted to the customer for approval.","NOTE\tECSS-Q-TM-70-51 contains guidelines referring to the assembly of fibre optic.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.16a","Requirement","ECSS-Q-ST-70-71_1260240","All NDI processes shall be selected according to aerospace national or international standards, and be submitted to the customer for customer approval.","NOTE\tMany different inspection procedures are employed for spacecraft materials and processes are numerous and varied. They are used at all stages of the manufacturing process and form part of the overall quality assurance plan.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.16b","Requirement","ECSS-Q-ST-70-71_1260241","Inspection procedures shall contain the material, the part, the classification of defects and establish their acceptance and rejection criteria.","NOTE \t1\tThe ability to inspect a part is a critical part of the design development.\nNOTE \t2\tSome inspection procedures can be relatively straightforward, for example visual inspection by unaided eye; whereas others are complex and need equipment that is regularly maintained and calibrated to recognized, approved standards, for example eddy current and ultrasonic.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.16c","Requirement","ECSS-Q-ST-70-71_1260242","Acceptance and rejection criteria shall be defined according to aerospace national or international standards approved by the customer or qualification testing.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70-71C Rev.1","4.3.16d","Requirement","ECSS-Q-ST-70-71_1260243","Inspection equipment shall be maintained and calibrated in conformance with the clause 5.2.6 from ECSS-Q-ST-20.",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-70C Rev.2","4.1.2a","Requirement","ECSS-Q-ST-70_0490001","The supplier shall prepare, maintain and implement a MMPP plan, as part of the overall PA plan in conformance with DRD from Annex A of ECSS-Q-ST-10 and this Standard or as a separate document.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.2b","Requirement","ECSS-Q-ST-70_0490002","The MMPP plan shall be submitted to the customer for approval.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3a","Requirement","ECSS-Q-ST-70_0490003","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3b","Requirement","ECSS-Q-ST-70_0490004","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3c","Requirement","ECSS-Q-ST-70_0490194","The supplier shall appoint a MMPP manager.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3d","Requirement","ECSS-Q-ST-70_0490195","The MMPP Manager shall ensure that the Materials, Mechanical Parts and Processes used to manufacture a spacecraft or a launcher satisfy both the ground and flight functional requirements and constraints of the project.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3e","Requirement","ECSS-Q-ST-70_0490196","To obtain the validation status for materials and qualification status for parts and verification status for processes, the MMPP manager shall present to the customer activities which were performed in conformance with requirement 4.1.3d together with the results obtained.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3f","Requirement","ECSS-Q-ST-70_0490197","The MMPP manager shall organize Materials, Mechanical Parts and Processes Control Board (MPCB) at all suppliers with the task to review and approve the Materials, Mechanical Parts and Processes as specified in the Clauses 5, 6, and 7.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3g","Requirement","ECSS-Q-ST-70_0490198","The MPCB activity shall start not later than at PDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3h","Requirement","ECSS-Q-ST-70_0490199","The MMPP Manager shall agree with the customer on the MPCB’s activities at PDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.1.3i","Requirement","ECSS-Q-ST-70_0490200","Minimum tasks of the MPCB shall be as follows:\n1.\tCoordination of the initiation and approval of RFA’s in conformance with DRD from the Annex D by involving the relevant technical discipline.\n2.\tReview and approval of test programme and related results.\n3.\tReview of preliminary Declared Materials, Mechanical Parts and Processes Lists and of any available evidence to support the approval, by the PDR.\n4.\tReview and approval of Declared Materials, Mechanical Parts and Processes Lists and of the evidence for the approval by the CDR.\n5.\tReview and approval of any change to the approved Declared Materials, Mechanical Parts and Processes Lists. \n6.\tIdentify and mitigate the risks linked to obsolescence of materials, processes, or mechanical parts at all levels of the customer-supplier chain. ","1\tREACH legislation is an example of a source for obsolescence.\n2\tGuidelines for obsolescence management for materials, mechanical parts and processes are provided in ECSS-Q-HB-70-23.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2a","Requirement","ECSS-Q-ST-70_0490005","Each supplier and sub­supplier shall establish, collect, review and deliver the declared materials, mechanical parts and processes lists including all the items intended for use in the flight equipment.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2b","Requirement","ECSS-Q-ST-70_0490006","The lists specified in 4.2.2a shall reflect the current design at the time of issue.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2c","Requirement","ECSS-Q-ST-70_0490007","The lists specified in 4.2.2a shall contain the materials, mechanical parts and processes used in the current design to: \n1.\tdemonstrate compliance with all requirements of the programme;\n2.\tverify the results of equipment supplier activities;\n3.\tcontrol and monitor the status of materials, mechanical parts and processes in conformance with programme milestones.","See Annex F.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2d","Recommendation","ECSS-Q-ST-70_0490269","The following constraints should apply:\n1.\tmaximum use of the materials and processes specified in approved data sources and items already approved on similar projects;\n2.\tuse of project related preferred lists, if available.","For approved data sources see example of ESMDB database in the Annex A of the ECSS-Q-ST-70-71.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2e","Requirement","ECSS-Q-ST-70_0490009","The following constraints shall be assessed: \n1.\trequirements originating from the initial technical specification.\n2.\tprogrammatic project requirements and conditions.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2f","Requirement","ECSS-Q-ST-70_0490010","An analysis of the criticality of preliminary lists specified in the 4.2.2a shall be performed such that, after checking the conformity of the materials, mechanical parts and processes, against all the project requirements, allows them to be classified into three categories:\n1.\tCritical items, subject to evaluation, validation, qualification, or verification programmes.\n2.\tItems that are not critical but which do not conform to one or more project requirements.\n3.\tNon­critical items.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2g","Requirement","ECSS-Q-ST-70_0490011","For items classified as critical in conformance with 4.2.2f.1 a request for approval shall be submitted in conformance with Annex D.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.2h","Recommendation","ECSS-Q-ST-70_0490270","For items classified as not critical but which are not in conformance with one or more project requirements in accordance with 4.2.2f.2 a justified deviation request should be drafted.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3a","Requirement","ECSS-Q-ST-70_0490012","The supplier shall document all materials in the Declared materials list in conformance with Annex A.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3b","Requirement","ECSS-Q-ST-70_0490013","The supplier shall document all mechanical parts in the Declared mechanical parts list in conformance with Annex B.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3c","Requirement","ECSS-Q-ST-70_0490014","The supplier shall document all processes in the Declared process list in conformance with Annex C.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3d","Requirement","ECSS-Q-ST-70_0490015","The supplier shall process the lists of lower level suppliers to ensure exchangeabililty, traceability searchability, sortability, storability and retrievability for that set of lists, before submitting it to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3e","Requirement","ECSS-Q-ST-70_0490016","The lists specified in the requirement 4.2.3a, 4.2.3b and 4.2.3c shall be updated during the course of the project.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3f","Requirement","ECSS-Q-ST-70_0490017","The preliminary lists specified in the requirement 4.2.3a, 4.2.3b and 4.2.3c shall include the items from suppliers’ preliminary needs.","They are used to identify critical items  (available for the PDR).",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3g","Requirement","ECSS-Q-ST-70_0490018","The as­designed lists shall include the items from the baselines various design files, available for CDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3h","Requirement","ECSS-Q-ST-70_0490019","Any change after CDR or QR shall be reflected in the list and shall be in accordance with Figure 4-1 (Part 2).","1\tThe MMPP manager is responsible within the programme to ensure that all the information needed is given and that the approval status is consistent with technical and scheduling objectives and data is exchangeable.\n2 \tWhere no project requirements exist for a separate DMPL, the mechanical parts can be entered into a separate section of the DML\n3\tThe materials of, for example, screws and nuts that are made up of a few materials can be listed in the DMPL. The materials (metals and plastics) of complex parts can be listed in the DML with, for example, outgassing, toxicity, flammability, corrosion and stress corrosion values and reference to the DMPL item.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3i","Requirement","ECSS-Q-ST-70_0490201","The supplier shall establish, collect, review and deliver the declared materials, mechanical parts and processes lists in an electronic format in conformance with Annex A, Annex B, and Annex C.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.3j","Requirement","ECSS-Q-ST-70_0490202","The supplier shall demonstrate that the lists specified in the requirements 4.2.3a, 4.2.3b and 4.2.3c have been formally approved prior to their delivery to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.4a","Requirement","ECSS-Q-ST-70_0490020","The supplier shall perform the following tasks:\n1.\tobtaining the correct and complete lists from lower level suppliers;\n2.\tproviding provisional and, later, definitive approval for each list;\n3.\tsubmitting the project declared lists for approval prior to initiation of the hardware phase, before CDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.4b","Requirement","ECSS-Q-ST-70_0490021","The lists specified in the requirement 4.2.3i by the suppliers shall include all the information described in this Standard.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.4c","Requirement","ECSS-Q-ST-70_0490022","Amendments to the lists specified in the requirement 4.2.3 a, b and c shall be implemented through established change procedures.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.4d","Requirement","ECSS-Q-ST-70_0490023","The following documentation shall be delivered to the customer upon request:\n1.\tRFA with reference and issue in conformance with DRD in Annex D;\n2.\tevaluation reports;\n3.\tdeviation requests.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.2.4e","Requirement","ECSS-Q-ST-70_0490024","The material, mechanical parts or process justification files shall be made available to the customer upon request either on the supplier site, or by any other process agreed by both parties.","For example, by non-disclosure agreement.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.3a","Requirement","ECSS-Q-ST-70_0490025","Mechanical parts, and materials and processes shall satisfy the mission’s functional requirements and constraints.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.3b","Requirement","ECSS-Q-ST-70_0490026","Mechanical parts, and materials and processes shall satisfy both ground environment and flight requirements and constraints.","Examples are:\n·\tGround environment constraints: manufacture, tests, storage, maintenance, transport and integration\n·\tFlight constraints: launch and orbit.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.3c","Requirement","ECSS-Q-ST-70_0490027","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.3d","Requirement","ECSS-Q-ST-70_0490028","The estimated availability of the parts and products obtained from materials and processes used shall be compatible with the space system’s life cycle.","Examples of space system’s life cycle are tests, storage and mission.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.4a","Requirement","ECSS-Q-ST-70_0490029","The supplier shall establish and maintain a contamination and cleanliness control programme including, as a minimum:\n1.\tcleaning procedures, and\n2.\tcleanliness monitoring procedures or methods.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.4b","Requirement","ECSS-Q-ST-70_0490030","The risks of chemical or particle pollution generated by parts, materials or processes used shall be identified and reduced as specified in ECSS-M-ST-80 clause 7.2, in conformance with mission requirements.","Cleanliness or contamination analysis is example of mission requirements.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.4c","Requirement","ECSS-Q-ST-70_0490031","For cleanliness­ or contamination­critical applications, a chemical and particle requirement specification and a specific cleanliness control plan shall be established in conformance with DRDs from Annex A and Annex B of ECSS-Q-ST-70-01.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.5a","Requirement","ECSS-Q-ST-70_0490032","Mechanical parts and materials with hazardous characteristics shall be identified, managed and processed in conformance with requirements from clause 5 to clause 8 of ECSS-Q-ST-40.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.6a","Requirement","ECSS-Q-ST-70_0490033","When optical, mechanical or electrical GSE materials are used in thermal vacuum or interfacing with flight hardware, degradation shall be assessed.","For example, contamination, surface degradation, electro­mechanical and chemical effects.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","4.7a","Requirement","ECSS-Q-ST-70_0490203","For the selection of space materials and processes, ECSS-Q-ST-70-71 shall be applied.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.1a","Requirement","ECSS-Q-ST-70_0490204","Material design data shall be generated for the intended service conditions using test and analysis procedures approved by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.1b","Requirement","ECSS-Q-ST-70_0490205","Material properties shall be compatible with the environments to which they are exposed during terrestrial testing prior to launch, and during the mission.","The requirements of clause 5 apply when the environmental conditions of the mission require their application. The specific requirements, test methods and acceptance or rejection criteria are presented in the ECSS-Q-ST-70 series of documents.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.2a","Requirement","ECSS-Q-ST-70_0490034","Material properties shall be compatible with the thermal environment to which they are exposed.","Examples of thermal environment are also the passage through transition temperatures, e.g. phase transitions, ductile-brittle transition temperatures for metals, glass transition (Tg) for polymer materials, and environmental factors which affect these properties, such as moisture.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.3a","Requirement","ECSS-Q-ST-70_0490035","Materials subject to thermal cycling shall be assessed for their ability to withstand induced thermal stress.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.3b","Requirement","ECSS-Q-ST-70_0490036","The following materials shall be tested in conformance with requirements from clause 5 of ECSS-Q-ST-70-04:\n1.\tMaterials susceptible to thermal vacuum effect.\n2.\tMaterials of unknown characteristics in respect to thermal vacuum.","For a non-exhaustive list of materials specified in the requirement 5.1.3b.1, see ECSS-Q-ST-70-04 Clause 1.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.3c","Requirement","ECSS-Q-ST-70_0490037","Materials subject to thermal cycling except the case specified in the requirement 5.1.3b, shall be tested in conformance with a procedure approved by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.3d","Requirement","ECSS-Q-ST-70_0490206","Thermo optical properties shall be evaluated in conformance with requirement from clause 4 of ECSS-Q-ST-70-09.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.3e","Requirement","ECSS-Q-ST-70_0490207","Directional effects due to manufacturing or processing shall be evaluated via dedicated testing to be agreed with the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.4a","Requirement","ECSS-Q-ST-70_0490038","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.4b","Requirement","ECSS-Q-ST-70_0490039","Outgassing screening tests shall be carried out in conformance with requirements from clause 5 of ECSS-Q-ST-70-02. ","The screening process applied depends on the application",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.4c","Requirement","ECSS-Q-ST-70_0490208","All organic materials for use in space systems shall be evaluated to determine their outgassing characteristics.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.4d","Recommendation","ECSS-Q-ST-70_0490271","The need for retest outgassing characteristics of materials used for an extended period of time at a temperature higher than 50 °C should be mutually agreed with the customer.","When dynamic outgassing tests are required see ECSS-Q-TM-70-52.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.5a","Requirement","ECSS-Q-ST-70_0490040","Spacecraft and associated equipment shall be manufactured from materials and by processes that do not cause hazard to personnel or hardware, either on the ground or in space.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.5b","Requirement","ECSS-Q-ST-70_0490041","Requirements from clause 4 of ECSS-Q-ST-70-29 shall apply for the characterization of offgassing products.","MIL-HDBK-454 test method is not space relevant.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.5c","Requirement","ECSS-Q-ST-70_0490209","For materials for the use in manned compartments of a spacecraft or space segment elements, offgassing and toxicity analysis shall be performed.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.5d","Requirement","ECSS-Q-ST-70_0490210","The levels of offgassing and toxicity specified in the requirement 5.1.5c shall be agreed with the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.6a","Requirement","ECSS-Q-ST-70_0490042","The materials flammability resistance, shall be evaluated in conformance with requirements from the clause 5 of ECSS-Q-ST-70-21 for the most hazardous environment envisaged for their use, and be applicable to:\n1.\tunmanned spacecraft or space segment elements launched by a manned space transportation system when powered on launch, and\n2.\tmanned spacecraft and space segment elements.","See also NASA STD-6001.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.7a","Requirement","ECSS-Q-ST-70_0490043","Materials exposed to radiation shall be assessed in conformance with requirements from clause 5 of ECSS-Q-ST-70-06 to determine their resistance to the radiation dosage expected during the mission.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.7b","Requirement","ECSS-Q-ST-70_0490211","Evaluation of materials resistance to radiation shall include the combined effects of particle radiation and ultraviolet radiation in the normal space environment, along with any mission-specific radiation levels.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.7c","Requirement","ECSS-Q-ST-70_0490212","The effect of bleaching due to vacuum or air recovery shall be evaluated, in case ex-situ measurements are performed.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.7d","Requirement","ECSS-Q-ST-70_0490213","In case synergistic testing is not possible it shall be proven that synergistic effects caused by radiation and temperature are not degrading the materials properties.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.7e","Requirement","ECSS-Q-ST-70_0490214","In case technical limits prevent the synergistic testing approach, it shall be so justified, and the justification for sequential testing shall be provided.","For example when different acceleration factors are required for particle and UV radiation.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.8a","Requirement","ECSS-Q-ST-70_0490044","External surfaces of the spacecraft shall be conductive, interconnected and grounded to the spacecraft structure to avoid the build­up of differential charges in conformance with requirements from clause 6 to clause 10 of ECSS-E-ST-20-06.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.9a","Requirement","ECSS-Q-ST-70_0490045","For all materials that come into contact with atmospheric gases, cleaning fluids or other chemicals, it shall be demonstrated that the degradation of properties during their anticipated service­life does not prevent to meet the performance and integrity requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.9b","Requirement","ECSS-Q-ST-70_0490215","All mechanical parts, assemblies and equipment, including spares, shall be finished to provide protection from corrosion.","This applies equally to fasteners and other fixing devices, such as insert systems.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.10a","Requirement","ECSS-Q-ST-70_0490046","Materials used for structural and load bearing applications (i.e. subject to tensile stress) shall be selected in accordance with requirements of clauses 5.2.1, 5.2.3 and 5.2.4 of ECSS-Q-ST-70-36.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.10b","Requirement","ECSS-Q-ST-70_0490047","Any material not covered by cases specified in requirement 5.1.10a shall be tested in conformance with requirements from clause 5 of ECSS-Q-ST-70-37.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.11a","Requirement","ECSS-Q-ST-70_0490048","Materials within the system exposed to reactive fluids, both directly and as a result of single point failures when failure propagation effects cause hazardous operation of interfacing hardware shall be compatible with that fluid in their application.","Example of reactive fluids are liquid oxygen (LOX) and gaseous oxygen (GOX).",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.11b","Requirement","ECSS-Q-ST-70_0490049","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.11c","Requirement","ECSS-Q-ST-70_0490216","The compatibility of materials which are or can come into contact with LOX or GOX shall be evaluated except the case specified in the requirement 5.1.11d.","See NASA-STD-6001 Tests No. 13 and No. 14.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.11d","Requirement","ECSS-Q-ST-70_0490217","In case no compatibility data are available, tests shall be performed for reactive fluids other than oxygen.","See NASA-STD-6001 Test No. 15.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.12a","Requirement","ECSS-Q-ST-70_0490050","When bimetallic contacts are used, the choice of the pair of metallic materials used shall be agreed with the customer. ","This also includes metal­to­conductive fibre­reinforced materials contacts.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.12b","Requirement","ECSS-Q-ST-70_0490051","Galvanic compatibilities shall be selected in conformance with Table 5-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.12c","Requirement","ECSS-Q-ST-70_0490052","Materials not listed in Table 5-1 shall be evaluated in a flight­simulated configuration using an accelerated environment to be agreed by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.13a","Requirement","ECSS-Q-ST-70_0490053","All materials for use on the external surfaces of spacecraft for use in Low Earth Orbit (LEO) altitudes, between 200 km and 700 km, shall be evaluated for their resistance to atomic oxygen (ATOX).","The flux level varies with altitude, velocity vector and solar activity. Fluence levels vary with the duration of exposure.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.13b","Requirement","ECSS-Q-ST-70_0490054","Test procedures shall be subject to the approval by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.13c","Requirement","ECSS-Q-ST-70_0490218","The effect of ATOX on thermo optical properties including specularity shall be evaluated.","Data related to ATOX are presented in ECSS-E-ST-10-04.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.14a","Requirement","ECSS-Q-ST-70_0490055","The effect of impacts by micrometeoroids and debris on materials shall be reviewed and assessed on a case by case basis.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.14b","Requirement","ECSS-Q-ST-70_0490219","Use of materials shall comply with safety evaluation and assessment results concerning design and application criteria or details.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.14c","Requirement","ECSS-Q-ST-70_0490220","Micrometeoroids and debris analysis and test procedures shall be subject to the approval by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.15a","Requirement","ECSS-Q-ST-70_0490056","Moisture absorption shall be prevented during manufacture and storage of hygroscopic materials. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.16a","Requirement","ECSS-Q-ST-70_0490057","For all solid surfaces in moving contact with other solid surfaces, it shall be demonstrated that the degradation of surface properties over the complete mission does not prevent to meet the performance requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.16b","Requirement","ECSS-Q-ST-70_0490221","For all solid surfaces, moving or in static contact with other solid surfaces, and intended to be separated it shall be demonstrated that the increase in separation force during the physical contact does not exceed the specified limit.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.17a","Requirement","ECSS-Q-ST-70_0490058","Materials shall be selected to ensure that they will meet the material performance requirements during all their specified lifetime. .",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.18a","Requirement","ECSS-Q-ST-70_0490222","Materials selected for manned or fluid systems shall: \n1.\tnot support bacterial or fungus growth,\n2.\tbe sterilizable.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.18b","Requirement","ECSS-Q-ST-70_0490223","The extent of the degradation by the sterilization process shall be determined to define margins for design implementation.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.18c","Requirement","ECSS-Q-ST-70_0490224","The design and qualification of an equipment to be sterilised shall implement the defined margins for sterilisation degradation.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.18d","Requirement","ECSS-Q-ST-70_0490225","The level of bacterial growth and fungus contamination shall be determined on the assembled hardware.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.18e","Requirement","ECSS-Q-ST-70_0490226","Evaluation of organic materials used in the pressurized environment of long-term, manned spacecraft shall be performed prior to selection and verification.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.19a","Requirement","ECSS-Q-ST-70_0490227","The possibility of hydrogen embrittlement occurring during component manufacture or use shall be assessed. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.19b","Requirement","ECSS-Q-ST-70_0490228","The material evaluation specified in 5.1.19a shall be performed including the assessment of a protection and control.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.19c","Requirement","ECSS-Q-ST-70_0490229","Based on the assessment specified in the requirement 5.1.19a and 5.1.19b, protection and control measures shall be implemented to avoid hydrogen embrittlement during both mechanical parts manufacturing and use.","Hydrogen embrittlement can be introduced for example during e.g. plating, welding.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.1.19d","Requirement","ECSS-Q-ST-70_0490230","Mechanical parts subject to fatigue or sustained loading stresses, which are made of material susceptible to hydrogen embrittlement, shall be heat treated after coating.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1a","Requirement","ECSS-Q-ST-70_0490059","Materials shall be chosen as follows:\n1.\tif an identical application in other space programmes similar with respect to environment constraints and lifetime to the proposed application exist, use materials used in such an application;\n2.\totherwise:\n(a)\tif materials exist for which satisfactory evaluation results are obtained on samples representative of the application with margin above the specified ones as regards conditions of use, use such materials;\n(b)\totherwise, use materials included in approved data sources.","For example: ESMDB (see Annex A of ECSS-Q-ST-70-71) ESA and NASA data banks.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1b","Requirement","ECSS-Q-ST-70_0490060","Whether the materials are already validated or remain to be validated, their selection shall ensure that the following criteria are met:\n1.\tcontinuity of supply;\n2.\treproducibility of characteristics;\n3.\tmechanical properties of materials processed according to a specified technique;\n4.\tenvironmental-stability properties under space conditions, together with mission- or application-specific requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1c","Requirement","ECSS-Q-ST-70_0490231","Each critical material shall be validated for the specific application.","Critical material includes the ones of approved data sources.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1d","Requirement","ECSS-Q-ST-70_0490232","Space-proven materials with heritage covering the specific mission requirements shall be selected at the earliest design stage.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1e","Requirement","ECSS-Q-ST-70_0490233","The supplier shall be responsible for the selection of materials that are capable of meeting the requirements of his business agreement.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1f","Requirement","ECSS-Q-ST-70_0490234","The supplier shall be responsible for storing and maintain all materials data in an internal database.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1g","Requirement","ECSS-Q-ST-70_0490235","The access to the data, specified in requirement 5.2.1f, shall be granted to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1h","Requirement","ECSS-Q-ST-70_0490236","To achieve high reliability and good performance, the use of a material shall be restricted to within its maximum qualified range of physical and mechanical properties.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1i","Requirement","ECSS-Q-ST-70_0490237","All test methods and inspection techniques used to verify material characteristics and final products shall conform to standards approved by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.1j","Requirement","ECSS-Q-ST-70_0490238","All test methods and inspection techniques specified in the requirement 5.2.1i shall not be used before approval by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2a","Requirement","ECSS-Q-ST-70_0490061","Pure tin finish with more than 97 % purity shall not be used.","This is due to the possibility of whisker growth and transformation to grey tin powder at low temperatures.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2b","Requirement","ECSS-Q-ST-70_0490062","The incoming inspection of each EEE component batch shall include the verification of the termination composition to avoid assembly of pure tin finish.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2c","Requirement","ECSS-Q-ST-70_0490239","Cadmium and Zinc shall not be used as raw material or surface treatment for flight hardware.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2d","Requirement","ECSS-Q-ST-70_0490240","Cadmium and Zinc shall not be used for ground support equipment exposed to vacuum or when in contact with the flight hardware.","For example during thermal vacuum testing phases on ground.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2e","Requirement","ECSS-Q-ST-70_0490241","The incoming inspection of each non-EEE component batch shall include the verification of the metallic surface treatment to avoid assembly of pure tin, cadmium or zinc finish.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2f","Requirement","ECSS-Q-ST-70_0490242","The materials presented in the following shall not be used: \n1.\tBeryllium oxide\n2.\tMercury and its compounds\n3.\tPolyvinyl chloride (PVC)\n4.\tRadioactive material","This list is not exhaustive.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2g","Requirement","ECSS-Q-ST-70_0490243","Beryllium shall not be used for structures.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.2.2h","Requirement","ECSS-Q-ST-70_0490244","Beryllium shall not be used in applications other than structures, unless:\n1.\tapproved by the customer , and \n2.\tall safety requirements are implemented by the supplier.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.3a","Requirement","ECSS-Q-ST-70_0490063","The supplier shall establish and maintain a declared materials list in conformance with Annex A.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.4.2a","Requirement","ECSS-Q-ST-70_0490064","The supplier shall analyse all the materials contained in his preliminary lists with respect to criticality and in correlation with the risk analysis performed. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.4.2b","Requirement","ECSS-Q-ST-70_0490065","Any material not meeting the project requirements shall be subject to a RFD for customer approval.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.4.2c","Requirement","ECSS-Q-ST-70_0490066","Any critical material shall be subject to a RFA in conformance with Annex D to be submitted to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.4.2d","Requirement","ECSS-Q-ST-70_0490067","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.1a","Requirement","ECSS-Q-ST-70_0490068","If so identified by the criticality analysis, the supplier shall perform an evaluation phase before the validation phase for all critical materials with unknown characteristics (new materials) or with major changes in the use or in the configuration",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.1b","Permission","ECSS-Q-ST-70_0490272","In case of an extension of an existing application, the evaluation specified in requirement 5.5.1a need not be performed if so agreed with the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.1c","Requirement","ECSS-Q-ST-70_0490070","Guarantied characteristics of materials and material supplier inspection methods, together with associated documents, shall be available for review at the supplier’s premises before the start of evaluation or qualification phases.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.2a","Requirement","ECSS-Q-ST-70_0490071","The evaluation specified in 5.5.1a shall assess as a minimum the following:\n1.\tthe limits of use;\n2.\tthe materials physical, chemical or functional characteristics along with their values and tolerances;\n3.\tbehavioural tendencies and degradation processes depending on environmental parameters including sensitivity to pollution;\n4.\tacceptance criteria.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.2b","Requirement","ECSS-Q-ST-70_0490072","When evaluation is performed, the supplier shall provide:\n1.\tan evaluation programme at PDR, according to Figure 4-1, and \n2.       an evaluation report before CDR, according to Figure 4-1 and Table 4-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.3a","Requirement","ECSS-Q-ST-70_0490073","For all critical materials, a validation programme, available at PDR, shall be drawn up by the supplier and then implemented to check or confirm that the materials satisfy the mission requirements with the specified margins to obtain validation status.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.3b","Requirement","ECSS-Q-ST-70_0490074","Validation status shall be decided at CDR in view of the available results obtained written in validation report, and the review of corresponding documentation.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.3c","Requirement","ECSS-Q-ST-70_0490245","The validation programme and report shall be approved by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.4a","Requirement","ECSS-Q-ST-70_0490075","The material shall not receive an approval identification in the declared material list for the project unless the requirements specified in the clauses 5.5.2 and 5.5.3 are satisfied.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.4b","Requirement","ECSS-Q-ST-70_0490076","If approval is not granted, the supplier in charge of the item shall either:\n1.\tselect another material, or\n2.\tpropose a modified evaluation programme and resubmit for approval, or\n3.\tif actions specified in the requirements 5.5.4b.1 and 5.5.4b.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.5.5a","Requirement","ECSS-Q-ST-70_0490077","For materials not conforming to project requirements, whether at the end of criticality analysis or of evaluation and validation tests, the supplier shall submit a request for deviation in conformance with requirements from the clause 5.2.3.5 of ECSS-Q-ST-10-09.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1a","Requirement","ECSS-Q-ST-70_0490078","All materials shall be procured to an internationally or nationally specification approved by the supplier quality system, or an in­house fully configured procurement specification which defines the materials properties, the materials requirements, the test methods, the acceptance criteria for the specific applications, source inspection (if any) and material supplier inspection.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1b","Requirement","ECSS-Q-ST-70_0490079","Where material suppliers do not accept specifications and procurement is by means of a datasheet the supplier shall introduce internal, in­house receipt inspection to ensure that the validation status of the material is maintained during the subsequent procurements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1c","Requirement","ECSS-Q-ST-70_0490080","Materials with long lead times or long procurement delays, versus the project schedule, shall be identified before the formal subsystem PDR. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1d","Requirement","ECSS-Q-ST-70_0490081","Procurement shall be planned, documented and implemented to obtain reliable product assurance provision at CDR. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1e","Requirement","ECSS-Q-ST-70_0490082","Back­up plans shall be prepared and initiated whenever there is evidence of delays or technical problems.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.1f","Requirement","ECSS-Q-ST-70_0490083","The material requirements shall be accepted by the material supplier or manufacturer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.2a","Requirement","ECSS-Q-ST-70_0490084","All materials shall be submitted to an incoming inspection.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.6.2b","Requirement","ECSS-Q-ST-70_0490085","An incoming inspection procedure shall define the inspections and tests to be carried out, particularly for materials that are known to be variable in their final properties.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.1a","Requirement","ECSS-Q-ST-70_0490086","The supplier shall verify that all critical materials are validated before being used in the manufacture of qualification or flight products.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.1b","Requirement","ECSS-Q-ST-70_0490087","Any modification, change of condition or configuration of application shall lead to a re-evaluation in conformance with the process shown in Figure 4-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.2a","Requirement","ECSS-Q-ST-70_0490088","The supplier shall apply the traceability rules specified in the requirements from clause 5.2.5 of ECSS-Q-ST-20 to all materials.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.2b","Requirement","ECSS-Q-ST-70_0490246","Materials shall be identified by a unique reference number, code or a lot number to provide traceability.","The traceability allow to reconstruct the materials history, either individually (individual traceability) or by the manufacturing lot of which it was a part (lot traceability) in case of an incident or nonconformance, or a need for a technical investigation following failure or damage. ",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.3a","Requirement","ECSS-Q-ST-70_0490090","The supplier shall define provisions for packaging, storage and removal from storage for materials.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.3b","Requirement","ECSS-Q-ST-70_0490091","Measurements and inspections used to guarantee the material integrity and monitoring during storage and removal from storage shall be identified.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.4a","Requirement","ECSS-Q-ST-70_0490092","The supplier shall ensure that all materials which have limited­life characteristics have their date of manufacture or date of delivery and shelf­life expiry date identified and clearly marked on each lot or batch.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.4b","Requirement","ECSS-Q-ST-70_0490247","Materials which have exceeded their shelf­life expiry date shall not be re­certified until the physical and chemical characteristics are inspected and the parameters, subject to deterioration, are evaluated for continued acceptability according to the acceptance and rejection criteria in conformance with requirements from the clause 4 of ECSS-Q-ST-70-22.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.5a","Requirement","ECSS-Q-ST-70_0490094","Materials with limited­life after implementation shall be identified and controlled in conformance with requirements from the clause 5 of ECSS-Q-ST-10-04.","1\tPropellant is an example of material with limited-life after implementation\n2\tStorage and mission life are criteria for the assessment and control of those materials.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.6a","Requirement","ECSS-Q-ST-70_0490095","Nonconformances and alerts shall be managed in conformance with requirements from the clause 5 and clause 6 of ECSS-Q-ST-10-09 and clause 5.2 of ECSS-Q-ST-10.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","5.7.7a","Requirement","ECSS-Q-ST-70_0490096","Material safety data sheet or equivalent shall be available for all materials.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.1a","Requirement","ECSS-Q-ST-70_0490097","The supplier shall verify that all materials and processes used in the manufacture of mechanical parts satisfy the mission technical requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.2a","Requirement","ECSS-Q-ST-70_0490098","Mechanical parts shall be chosen from used for an identical application in other space programmes similar with respect to environment constraints and lifetime.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.2b","Requirement","ECSS-Q-ST-70_0490099","Type reduction actions shall be implemented at all levels of the programme.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.2c","Requirement","ECSS-Q-ST-70_0490100","Whether the mechanical parts are already qualified or remain to be qualified, their selection shall ensure that the following criteria are met:\n1.\tdurability of supply;\n2.\treproducibility of characteristics.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.2d","Requirement","ECSS-Q-ST-70_0490248","The supplier shall be responsible for storing and maintain all mechanical parts data in an internal database.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.2e","Requirement","ECSS-Q-ST-70_0490249","The access to the data, specified in requirement 6.2d, shall be granted to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.3a","Requirement","ECSS-Q-ST-70_0490101","The supplier shall establish and maintain a declared mechanical parts list in conformance with Annex B.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.4.2a","Requirement","ECSS-Q-ST-70_0490102","The supplier shall analyse all the mechanical parts contained in their preliminary lists with respect to criticality and in correlation with the risk analyses performed in conformance with requirements from the clause 5 of ECSS-Q-ST-10-04.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.4.2b","Requirement","ECSS-Q-ST-70_0490103","Critical parts shall be identified in the DMPL and included in the critical items list.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.4.2c","Requirement","ECSS-Q-ST-70_0490104","Any critical part shall be the subject of a RFA in conformance with Annex D submitted to customer approval.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.1a","Requirement","ECSS-Q-ST-70_0490105","If so identified by the criticality analysis, the supplier shall perform an evaluation phase before the qualification phase for all critical parts with unknown characteristics or with major changes in the use or in the configuration.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.1b","Permission","ECSS-Q-ST-70_0490273","In case of an extension of an existing application, the evaluation indicated in 6.5.1a need not be performed if so agreed with the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.1c","Requirement","ECSS-Q-ST-70_0490107","Guarantied characteristics of materials and material supplier inspection methods, together with associated documents, shall be available for review at the suppliers premises before the start of evaluation or qualification phases.","Refer to Table 4-1 for an explanation of the steps involved.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.2a","Requirement","ECSS-Q-ST-70_0490108","The evaluation specified in 6.5.1a shall include the following, as a minimum, for each critical part:\n1.\tthe limits of use,\n2.\tthe part’s physical or functional characteristics, along with its values and tolerances,\n3.\tbehavioural tendencies and degradation processes depending on environment parameters, including sensitivity to pollution, and\n4.\tacceptance criteria.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.2b","Requirement","ECSS-Q-ST-70_0490109","When an evaluation is performed the supplier shall provide:\n1.\tan evaluation programme at PDR, and \n2.\tan evaluation report before CDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.2c","Requirement","ECSS-Q-ST-70_0490110","The behaviour of the parameters to be monitored which were also recorded during the evaluation programme tests, shall serve as a reference for the analysis of qualification test results.","Example of such behaviour is variation and change over time.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.3a","Requirement","ECSS-Q-ST-70_0490111","For each critical part a qualification programme shall be drawn up by the supplier of the equipment using the critical part and then implemented to check or confirm whether the parts satisfy mission requirements with the specified margins.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.3b","Requirement","ECSS-Q-ST-70_0490112","Qualification status shall be decided at CDR in view of the available results obtained, written in qualification report, and the reviews of corresponding documentation .",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.3c","Requirement","ECSS-Q-ST-70_0490250","The qualification programme and report shall be submitted to the customer for approval.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.4a","Requirement","ECSS-Q-ST-70_0490113","The mechanical parts shall not receive an approval identification in the declared mechanical parts list for the project unless the requirements from clauses 6.5.2 and 6.5.3 are satisfied.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.4b","Requirement","ECSS-Q-ST-70_0490114","If approval is not granted, the supplier in charge of the item shall either:\n1.\tselect another mechanical part, or\n2.\tpropose a modified evaluation programme and resubmit for approval, or\n3.\tif actions specified in the requirements 6.5.4b.1 and 6.5.4b.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.5.5a","Requirement","ECSS-Q-ST-70_0490115","For mechanical parts not conforming to project requirements, whether at the end of criticality analysis or of evaluation and qualification tests, the supplier shall submit a request for deviation in conformance with requirements from the clause 5.2.3.5 of ECSS-Q-ST-10-09.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.1a","Requirement","ECSS-Q-ST-70_0490116","Mechanical parts with long lead times or procurement delays, versus the project schedule, shall be identified before the subsystem PDR. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.1b","Requirement","ECSS-Q-ST-70_0490117","Procurement shall be planned, documented and implemented to obtain reliable product assurance provision at CDR. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.1c","Requirement","ECSS-Q-ST-70_0490118","Back­up plans shall be prepared and initiated whenever there is evidence of possible delays or technical problems.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.2a","Requirement","ECSS-Q-ST-70_0490119","Each part shall be covered by a procurement specification or a standard approved by the supplier quality system.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.2b","Requirement","ECSS-Q-ST-70_0490120","The procurement specifications shall define the part characteristics, requirements, tests methods, acceptance criteria, lot acceptance testing, source inspection and material supplier inspection.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.2c","Requirement","ECSS-Q-ST-70_0490121","The procurement specifications shall be explicitly accepted by the mechanical part supplier or manufacturer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.3a","Requirement","ECSS-Q-ST-70_0490122","For complex mechanical parts related to a specific project development, each supplier shall define the nature and frequency of their own source inspection points. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.3b","Requirement","ECSS-Q-ST-70_0490123","Source inspection shall be carried out by the customer on the premises of the supplier, mechanical part manufacturer, in conformance with requirements from the clauses 5.4.3 and 5.4.4 of ECSS-Q-ST-20.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.4a","Requirement","ECSS-Q-ST-70_0490124","Each part or batch of mechanical parts shall be submitted to an incoming inspection.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.6.4b","Requirement","ECSS-Q-ST-70_0490125","An incoming inspection procedure shall be established defining the inspections and tests to be carried out.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.1a","Requirement","ECSS-Q-ST-70_0490126","The supplier shall ensure that all critical parts are qualified before being used in the manufacture of qualification or flight products.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.1b","Requirement","ECSS-Q-ST-70_0490127","Any modification, change in condition or configuration of application shall lead to a re-evaluation in conformance with the process shown in Figure 4-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.2a","Requirement","ECSS-Q-ST-70_0490128","The supplier shall apply the traceability rules specified in clause 5.2.5 of ECSS-Q-ST-20 to his mechanical parts.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.2b","Requirement","ECSS-Q-ST-70_0490251","Parts shall be identified by a unique reference number or code and a lot number to provide traceability - where there is an incident or nonconformance, or for the purposes of technical investigations following failure or damage - to reconstruct the mechanical parts history, either individually (individual traceability) or by the manufacturing lot it was part of (lot traceability).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.3a","Requirement","ECSS-Q-ST-70_0490130","The supplier shall define provisions for packaging, storage and removal from storage for mechanical parts.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.3b","Requirement","ECSS-Q-ST-70_0490131","Measurements and inspections used to guarantee the part integrity and monitoring during storage and removal from storage shall be identified.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.4a","Requirement","ECSS-Q-ST-70_0490132","Limited­life mechanical parts after implementation or subject to wear out shall be identified and controlled, including storage and mission life.","Examples of such mechanical parts are mechanisms, pyro initiators and O­rings.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.4b","Requirement","ECSS-Q-ST-70_0490133","Limited­life mechanical parts shall be assessed as candidates to the critical items list in conformance with requirements from clause 5 of ECSS-Q-ST-10-04.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","6.7.5a","Requirement","ECSS-Q-ST-70_0490134","Management of mechanical parts nonconformances and alerts shall be in conformance with requirements from clause 5 to clause 6 of ECSS-Q-ST-10-09 and clause 5.2 of ECSS-Q-ST-10.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.1a","Requirement","ECSS-Q-ST-70_0490135","Each process to be used in the manufacturing or assembly of a product shall be identified by a specification or procedure.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.1b","Requirement","ECSS-Q-ST-70_0490136","Reference shall be made to accept and reject criteria.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.2a","Requirement","ECSS-Q-ST-70_0490137","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3a","Requirement","ECSS-Q-ST-70_0490138","Processes shall be chosen from already verified processes according to the following order of preference and priority:\n1.\tprocesses covered by space agencies or other governmental organization certification for identical conditions of use;\n2.\tprocesses for which satisfactory evaluation and verification results are obtained on samples representative of the application with a sufficient margin as regards conditions of use;\n3.\tprocesses already used by the same supplier for other space programmes in the same conditions of use.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3b","Requirement","ECSS-Q-ST-70_0490139","Whether the processes are already verified or remain to be verified, their selection shall ensure that the following criteria are met:\n1.\treliability;\n2.\tinspectability;\n3.\tre­workability of the process item;\n4.\treproducibility.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3c","Requirement","ECSS-Q-ST-70_0490252","The supplier shall store and maintain all processes data in an internal database.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3d","Requirement","ECSS-Q-ST-70_0490253","The access to the data, from requirement 7.3c, shall be granted to the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3e","Requirement","ECSS-Q-ST-70_0490254","Processes using limited-life materials shall be in conformance with the requirements from clause 4 of ECSS-Q-ST-70-22.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3f","Requirement","ECSS-Q-ST-70_0490255","Operators shall be trained for all processes.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3g","Requirement","ECSS-Q-ST-70_0490256","Operators performing special processes shall be certified in conformance with the requirements of the relevant standard.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3h","Requirement","ECSS-Q-ST-70_0490257","Inspectors shall be trained and certified for all processes.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3i","Requirement","ECSS-Q-ST-70_0490258","Certification shall be reassessed at least every two years.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3j","Requirement","ECSS-Q-ST-70_0490259","All training and certification shall only be performed at a school or by certified instructors in conformance with customer requirements.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3k","Requirement","ECSS-Q-ST-70_0490260","Retraining and recertification of operators shall be applied in the event of a new process, modification to an existing process or a change of the equipment used.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3l","Requirement","ECSS-Q-ST-70_0490261","Retraining and recertification of inspectors shall be applied in the event of a new inspection procedure, modification to an existing inspection procedure or a change of an existing one.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3m","Requirement","ECSS-Q-ST-70_0490262","In the case of a process suspension for four months continuously, retraining and recertification shall be performed.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.3n","Requirement","ECSS-Q-ST-70_0490263","Standards relating to the occupational health of operators working with processes resulting in exposure to vapours, dust or debris shall be implemented and controlled.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.4a","Requirement","ECSS-Q-ST-70_0490140","The supplier shall establish and maintain a declared processes list in conformance with Annex C.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2a","Requirement","ECSS-Q-ST-70_0490141","The supplier shall analyse all the processes contained in their preliminary lists with respect to criticality and in correlation with the risk analyses performed.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2b","Requirement","ECSS-Q-ST-70_0490142","Critical processes shall be identified in the DPL and included in the list of critical items.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2c","Requirement","ECSS-Q-ST-70_0490143","Any critical process shall be the subject of an RFA in conformance with Annex D submitted to customer approval.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2d","Requirement","ECSS-Q-ST-70_0490144","Special processes shall be identified and controlled.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2e","Requirement","ECSS-Q-ST-70_0490145","Process control shall be ensured by means of procedures available for customer review.","Best practice is to implement a statistical process control.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.5.2f","Permission","ECSS-Q-ST-70_0490274","<< deleted >>",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.1a","Requirement","ECSS-Q-ST-70_0490147","If so identified by the criticality analysis, the supplier shall perform an evaluation phase before the verification phase for all critical processes which are new or with major changes in the use or in the configuration. ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.1b","Permission","ECSS-Q-ST-70_0490275","In case of an extension of an existing application, the evaluation specified in requirement 7.6.1a need not be performed if so agreed with the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.1c","Requirement","ECSS-Q-ST-70_0490149","For confidential processes, the supplier shall prove that the process has been verified.","1\tFor example, by presenting a verification certificate from space agencies or other governmental organization responsible to check the applicability of this verification.\n2\tRefer to Table 4-1 for an explanation of the steps involved.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.2a","Requirement","ECSS-Q-ST-70_0490150","The evaluation specified in 7.6.1a shall include the following as a minimum for each critical process:\n1.\tthe limits of use,\n2.\tthe values, determined by test samples or technology samples, of relevant parameters and their tolerances, and\n3.\tacceptance criteria.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.2b","Requirement","ECSS-Q-ST-70_0490151","When an evaluation is performed, the supplier shall provide \n1.\tan evaluation plan at PDR, and\n2.\tan evaluation report before CDR.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.3a","Requirement","ECSS-Q-ST-70_0490152","For each critical process, the supplier shall implement a verification programme.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.3b","Requirement","ECSS-Q-ST-70_0490153","The verification programme shall be defined in conformance with ECSS-E-ST-10-02.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.3c","Requirement","ECSS-Q-ST-70_0490154","The supplier shall ensure that the processes satisfy the mission requirements and that the parameters needed for the product design are defined so as to obtain verification status.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.3d","Requirement","ECSS-Q-ST-70_0490155","Verification status shall be decided at CDR in view of the available results obtained, written in verification report, and the review of corresponding documentation.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.3e","Requirement","ECSS-Q-ST-70_0490264","The verification programme and report shall be approved by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.4a","Requirement","ECSS-Q-ST-70_0490156","A processes shall not receive an approval identification in the declared processes list unless requirements from clauses 7.6.2 and 7.6.3 are satisfied.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.4b","Requirement","ECSS-Q-ST-70_0490265","In case approval specified in the requirement 7.6.4a is not granted, the supplier in charge of the item shall either:\n1.\tselect other processes, or\n2.\tpropose a modified evaluation programme and resubmit for approval, or\n3.\tif actions specified in 7.6.4b.1 and 7.6.4b.2 fail to achieve positive results, initiate a deviation procedure.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.6.5a","Requirement","ECSS-Q-ST-70_0490157","For processes not conforming to project requirements, whether at the end of criticality analysis or of evaluation and verification tests, the supplier shall submit a request for deviation in conformance with requirements from clause 5.2.3.5 of ECSS-Q-ST-10-09.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.1a","Requirement","ECSS-Q-ST-70_0490158","The supplier shall confirm that all critical processes have been verified before being used in the manufacture of qualification or flight products.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.1b","Requirement","ECSS-Q-ST-70_0490159","Any modification, change of condition or configuration of application shall lead to a re-evaluation in conformance with the process.","See Figure 4-1.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.2a","Requirement","ECSS-Q-ST-70_0490160","When a process needs to be re­verified, a request for approval (RFA) in conformance with DRD from Annex D shall be established and a re­verification programme shall be implemented.","Any prolonged stoppage in manufacturing, any major change of the facilities or procedures or any transfer of production to another entity can invalidate partially or completely the initial verification of a process.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.3a","Requirement","ECSS-Q-ST-70_0490161","Before implementation of a process, the supplier shall ensure that personnel are trained in accordance with the training and certification programme specified in 7.3f, 7.3g and 7.3h and that environment, means and documentation are adequate.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.3b","Requirement","ECSS-Q-ST-70_0490162","This verification shall ensure that: \n1.\tmanufacturing and quality control tools associated with the process are adequate, calibrated and properly maintained are used under environmental and cleanliness conditions, in conformance with requirements from clause 4.4,\n2.\tpersonnel is trained and certified in accordance with the training and certification programme specified in 7.3f, 7.3g and 7.3h, and\n3.\tthe processes specifications, manufacturing and inspection procedures and workmanship standards including definition of manufacturing operations and acceptance criteria exist.","1\tPhotographically documented if possible for visual acceptance criteria at the appropriate work and inspection stations.\n2\tFor planning of manufacturing, assembly and integration operation and inspection see ECSS-Q-ST-20.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.4a","Requirement","ECSS-Q-ST-70_0490163","Traceability of processes shall be ensured in conformance with requirements from clause 5.2.5 of ECSS-Q-ST-20.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.5a","Requirement","ECSS-Q-ST-70_0490164","Process nonconformances and alerts shall be processed in conformance with requirements from clause 5 to clause 6 of ECSS-Q-ST-10-09 and clause 5.2.9 of ECSS-Q-ST-10.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.6a","Requirement","ECSS-Q-ST-70_0490165","MIPs shall be defined in conformance with requirements from clause 5.5.8 of ECSS-Q-ST-20.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","7.7.7a","Requirement","ECSS-Q-ST-70_0490166","The supplier shall define provisions for packaging, storage, and removal from storage for products or semi­finished products before and after implementation of processes.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.1<1>a","Requirement","ECSS-Q-ST-70_0490167","The DML shall contain the following statements:\n1.\t“Materials are classified into 20 groups depending on their type or their main use, see Table A-1”.\n2.\t“Primers are classified in the group of their associated component.”\n3.\t“Where no project requirement exists for a separate DMPL, mechanical parts are entered on the DML as a separate group with the corresponding numbers.”",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.1<1>b","Requirement","ECSS-Q-ST-70_0490168","If new groups are created, for a given project, these shall have numbers over 21.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.1<2>a","Requirement","ECSS-Q-ST-70_0490169","The DML shall include the information stated in Figure A-1, where the header information identifies the list as the declared materials list and includes the issue number and date of issue, as follows:\n1.\tItem number (applicable to equipment manufacturer level only)\n(a)\tThis consists of the material group identifier and the user code. It takes the form of:\n<group number>.<identifier within the group>.<running number>.<user code>\nNOTE \tFor example: 11.5.1.KOF.\n(b)\tCharacteristics of the item number are:\n-\tThe user, identified by an agreed user code for the project.\n-\tOne only per material type.\n-\tDoes not change during the life of the materials list (sub­items are permitted when deemed necessary).\n2.\tCommercial identification or standardized designation\n(a)\tEnter the correct and standard designation, such as the trade name plus number.\n(b)\tIf no trade name exists, enter the manufacturer’s name plus number.\n(c)\tFor metal alloys, the Aluminium Association (AA) system is recommended for aluminium alloys, and the American Iron and Steel Institute (AISI) system for steel. For other metals or alloys, the main constituent is entered first except in the case of a traditional name.\nNOTE \tFor example: brass or bronze.\n(d)\tFor each material, as designated in A.2.1<2>a2(a) to(c), use a unique item number. If several lines are used for different applications or processing, add sub­item numbers.\n3.\tChemical nature and product type\n(a)\tFor metallic materials, add the condition as procured if applicable.\nNOTE \tExamples of such conditions are rolled and heat treatment.\n(b)\tWhere a semi­finished product is procured, give the relevant state. \nNOTE \tExamples of such state are form, plate and sheet.\n(c)\tGive the thickness of the material, that can be an important parameter.\nNOTE \tExamples of chemical nature are: epoxy resin, polyurethane adhesive, Ti6Al4V.\n4.\tProcurement information\n(a)\tManufacturer or distributor: name of the manufacturer and name of the distributor if different.\n(b)\tProcurement specification: provide reference to one of the following:\n-\tthe procurement specification with issue, revision and date\n-\ta national or international specification or standard, if this exists, and identifies the source of procurement (if relevant), with issue, revision and date\n-\tdatasheets, in which case indication of issue or date is not applicable.\n5.\tProcessing parameters\nList here a summary of the process parameters applied by the user of the process.\nNOTE \tE.g. mixture proportions, cure temperature, special cleaning agent, surface treatment, thermal treatment and temperature, and reference to specification number.\n6.\tUse and location\n(a)\tUse codes able to define the location of the material with respect to the:\n-\tsubsystem;\n-\tparticular piece of equipment (box or item);\n-\tuse of the equipment, e.g. a structural element, thermal control, electrical insulation.\nNOTE \tIf the CI number is not included in the list header, then a suitable abbreviation of the relevant subsystem is included.\n(b)\tInclude any restrictions that apply to the use of a particular material in the corresponding comment column.\n7.\tEnvironmental code\nThe environmental code is defined using Table A-2.\n8.\tSize code\nThe size code is indicated by an alphanumeric combination, such as A5, V2 or M3, as in Table A-3.\n9.\tValidation references, justification for approval and prime comments and prime approval\n(a)\tMake reference to relevant test data that demonstrates the acceptability of the material under the environmental conditions and the application relevant to the particular project concerned. Specifically, in column 9.1, corrosion (CORR), stress corrosion (SCC), flammability (FLAM), offgassing (OFFG) and outgassing (OUTG) data or report­references are entered.\n(b)\tUse standard abbreviations to summarize the acceptance status of a material for a particular property.\n(c)\tUse the justification for approval (column 9.2) and prime approval (column 9.3) columns for any additional information to obtain customer approval.\n(d)\tStandard abbreviations are used to summarize the acceptability or otherwise of a material for a specific property. These are defined for the project.\n(e)\tSelect the supplier approval status code from Table A-4.\n10.\tCustomer approval status code and comments\n(a)\tSelect this code from Table A-4.\n(b)\tInclude additional comments where appropriate.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.1<2>b","Requirement","ECSS-Q-ST-70_0490266","If heritage is used as justification for approval it shall cover the current hardware configuration and mission profile.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.2a","Requirement","ECSS-Q-ST-70_0490170","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","A.2.2b","Requirement","ECSS-Q-ST-70_0490171","The change record shall include a brief description of the updates which contributed to each issue or revision.","Figure A-1 of this DRD proposes an example of the format and defines the content within the framework of a project or a programme.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.1<1>a","Requirement","ECSS-Q-ST-70_0490172","The DMPL shall contain the following statements:\n“Mechanical parts are classified into 11 groups depending on their type or their main use” (see Table B-1).",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.1<1>b","Requirement","ECSS-Q-ST-70_0490173","If, for a given project it is considered necessary to create new groups, these shall have numbers over 61.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.1<1>c","Recommendation","ECSS-Q-ST-70_0490276","Items that appear in the EEE parts list should not be repeated here.","For example, heaters, some valves, thermostats, relays, transformer coils and solenoids. ",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.1<2>a","Requirement","ECSS-Q-ST-70_0490175","The DMPL shall include the information in Figure B-1, where the header information identifies the list as the declared mechanical parts  list and includes the issue number and date of issue, as follows:\n1.\tItem number (applicable at equipment supplier level only)\n(a)\tThis consists of the mechanical part identifier and the user code. It takes the form of:\n<group number>.<identifier within the group>.<running number>.<user code>\nNOTE \tFor example: 7.2.1.ACSA.\n(b)\tCharacteristics of the item number are:\n-\tIdentify the subcontractor by an agreed user code for the project.\n-\tOne only per mechanical part type. \n-\tDoes not change during the life of the mechanical parts list.\n2.\tCommercial identification\n(a)\tEnter the correct and standard designation, such as trade name plus number. \n(b)\tIf no trade name exists then enter the manufacturers’ name and number.\n3.\tType of part\nDescribe the material and surface treatment (if applicable).\n4.\tProcurement information\n(a)\tManufacturer or distributor: name of the manufacturer and name of the distributor if different.\n(b)\tProcurement specification: provide reference to one of the following:\n-\tthe procurement specification with issue, revision and date\n-\ta national or international specification or standard, if this exists, and identifies the source of procurement (if relevant), with issue, revision and date.\n5.\tElementary function, main characteristics\n(a)\tEnter the function of the mechanical part.\n(b)\tEnter the main characteristics of the mechanical part.\nNOTE \tFor example, number of revolutions per minute for a ball bearing.\n6.\tUse and location\nUse codes able to define the location of the mechanical part with respect to the:\n(a)\tsubsystem;\n(b)\tparticular piece of equipment (box or item);\n(c)\tuse of the equipment.\n7.\tEnvironmental code\nThe environmental code is defined using Table B-2.\n8.\tCriticality\nEnter “C” for critical or “N” for non­critical. If a mechanical part is considered critical, describe the reason for the criticality and methods of control.\n9.\tSupplier reference, prime comments and prime approval status \n(a)\tUse the supplier reference, prime comments and approval columns to enter all additional information that are necessary in order to obtain customer approval.\n(b)\tThis information comprises reference and issue of the RFA or approval, mechanical parts justification file, evaluation reports and deviation requests.\n(c)\tMake reference to the relevant test data that demonstrates acceptability of the mechanical part under the environment conditions and the application relevant to the particular project concerned.\n(d)\tUse standard abbreviations, defined by the customer, to summarize the acceptance status of a mechanical part for a particular property.\n(e)\tIn order to justify the use of a material for flammability resistance, list here the material thickness and height of oxygen share.\n(f)\tSelect the prime approval status code from Table B-3.\n10.\tThe customer approval status code and comments\n(a)\tSelect this code from Table B-3. \n(b)      Include additional comments where appropriate.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.2a","Requirement","ECSS-Q-ST-70_0490176","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","B.2.2b","Requirement","ECSS-Q-ST-70_0490177","This record shall include a brief description of the updates which contributed to each issue or revision.","Figure B-1 of this DRD proposes an example of the format and defines the content within the framework of a project or a programme.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.1<1>a","Requirement","ECSS-Q-ST-70_0490178","The DPL shall contain the following statements:\nProcesses are classified into 17 groups depending on their type or their main use, see Table C-1.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.1<1>b","Requirement","ECSS-Q-ST-70_0490179","If, for a given project it is considered necessary to create new groups, these shall have numbers over 17.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.1<2>a","Requirement","ECSS-Q-ST-70_0490180","The DPL shall include the information in Figure C-1, where the header information identifies the list as the declared processes list and includes the issue number and date of issue, as follows\n1.\tItem number (applicable to equipment supplier level only)\n(a)\tThis consists of the process identifier and the user code. It takes the form of \n<group number>.<identifier within the group>.<running number>.<user code>\nNOTE \tFor example: 1.2.1.SSEX\n(b)\tCharacteristics of the item number are:\n-\tIdentify the subcontractor by an agreed user code for the project.\n-\tOne only per process type. \n-\tDoes not change during the life of the process list.\n2.\tProcess identification\nIndicate the correct and standard identification of the process, e.g. the process name or title: bonding, coating or soldering.\n3.\tSpecification\n(a)\tIdentify the name or abbreviation of the process executor.\n(b)\tMake a reference to the associated procedure, together with the issue, revision and date.\nNOTE \tFor example, national, international, EN, ISO, ECSS or company in­house.\n4.\tProcess description\nEnter here a short description of the process.\n5.\tUse and location\nUse codes able to define the location of the process with respect to the:\n(a)\tsubsystem,\n(b)\tparticular piece of equipment (box or item),\n(c)\tuse of the equipment.\nNOTE \tFor example, a structural element, thermal control, electrical insulation).\n6.\tThis column number is not used.\n7.\tAssociated item numbers\nEnter the associated material list (DML) or mechanical parts list (DMPL) with the process.\n8.\tCriticality\n(a)\tEnter “C” for critical or “N” for non­critical.\n(b)\tIf a process is considered to be critical, Enter the references to the relevant RFA.\n9.\tSupplier reference, prime comments and approval\n(a)\tUse the supplier reference and approval columns to enter all additional information that are necessary to obtain customer approval.\n(b)\tSelect the supplier approval status code from Table C-2.\n(c)\tGive reference to qualification programme performed for critical processes.\n10.\tThe customer approval status code and comments\n(a)\tSelect this code from Table C-2.\n(b)\tInclude additional comments where appropriate.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.1<2>b","Requirement","ECSS-Q-ST-70_0490268","If heritage is used as justification for approval it shall cover the current hardware configuration and mission profile.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.2a","Requirement","ECSS-Q-ST-70_0490181","The change record shall list the successive issues and their release dates since the first formal issue of the document.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","C.2.2b","Requirement","ECSS-Q-ST-70_0490182","This record shall include a brief description of the updates which contributed to each issue or revision.","Figure C-1 of this DRD proposes an example of the format and define the content within the framework of a project or a programme.",{"$nulls":3},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","D.2.1a","Recommendation","ECSS-Q-ST-70_0490277","The RFA should contain the information in Figure D-1 (pages 1 and 2), as follows:\n1.\tThe header information, identifying the document as a request for approval together with the project logo and project name, RFA reference, issue revision and date.\n2.\tOriginator\nOriginator’s name and reference.\n3.\tLocation\nSubsystem and equipment codes.\n4.\tItem description\nBrief description of the item.\n5.\tPMP information\nThe DML, DMPL or DPL item number and list reference.\n6.\tItem status, including the following information:\n(a)\tmanufacturers’ name and qualification reference;\n(b)\tsuppliers’ name and qualification status;\n(c)\tproduct or material specification;\n(d)\tprocurement specification;\n(e)\tprocess or handling specification;\n(f)\tother related process or handling specifications;\n(g)\tverification or qualification specification;\n(h)\treport on verification or qualification.\n7.\tReason for RFA\nEnter the reason for the RFA.\n8.\tApplication and location details\nEnter here the details of the application and exact location of the item.\nGive the reference in the CIL.\n9.\tEvaluation and validation programme\nReference and details of main tests.\n10.\tSubcontractor supplier approval for the first issue of the RFA.\n11.\tCustomer initial decision, to be entered on first issue of the RFA providing:\n(a)\tthe decision concerning the proposed material,\n(b)\tthe requirement to perform tests (deviation request as necessary), and\n(c)\tthe decision concerning the proposed test programme.\n12.\tCustomer’s and final customer’s (if applicable) signature\n13.\tJustification results obtained with reference to the supplier’s validation report and conclusion.\n14.\tSubcontractor supplier approval on RFA final issue.\n15.\tFinal approval status of the RFA by the customer.",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-70C Rev.2","D.2.2a","Requirement","ECSS-Q-ST-70_0490184","The RFA shall be completed by the supplier (parts 1 to 10, 13 and 14) and the customer (parts 11, 12 and 15). ",{"$nulls":4},"active","Product assurance","Level 1"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.2a","Requirement","ECSS-Q-ST-60-14_0470002","The following domains shall be covered and documented by procedures sent to the customer for information, on request:\n1.\tStorage area and storage zone \n2.\tCleanliness\n3.\tESD protection\n4.\tPacking and Packaging\n5.\tHandling\n6.\tQuality assurance.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.3a","Requirement","ECSS-Q-ST-60-14_0470003","It shall be demonstrated that storage areas and storage zones provide such protection against vibration, electromagnetic fields, radiation fields and against light so that possible degradation of organic packaging material is prevented.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.4a","Requirement","ECSS-Q-ST-60-14_0470004","Rules for cleanliness efficiency shall be implemented.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.4b","Requirement","ECSS-Q-ST-60-14_0470005","The working areas and the contained equipment shall be maintained as visually clean with no loose material.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.4c","Requirement","ECSS-Q-ST-60-14_0470006","Access rules shall apply for personnel, materials and equipment.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.4d","Requirement","ECSS-Q-ST-60-14_0470007","Storage areas shall conform to a cleanliness level as defined in ECSS-Q-ST-70-01 clause 5.3.1.4. \n","NOTE \tThis cleanliness level is often called and known as “grey zone”.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.5a","Requirement","ECSS-Q-ST-60-14_0470008","The efficiency of ESD protection measures in storage, handling and testing areas shall be demonstrated.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.6a","Requirement","ECSS-Q-ST-60-14_0470009","EEE parts manufacturers requirements or, by default, ESCC 20600 or IPC/JEDEC J-STD-033D (April 2018) shall apply for packing, packaging and handling.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.1.7a","Requirement","ECSS-Q-ST-60-14_0470010","The storage responsible entity shall establish and document the following:\n1.\tProhibited materials\n2.\tPersonnel access rules\n3.\tProhibited personnel actions\n4.\tMeasures and facilities to segregate and protect components during receiving, inspection, storage and delivery\n5.\tControl measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.2a","Requirement","ECSS-Q-ST-60-14_0470011","Temperature in the immediate vicinity of stored components shall at all times be maintained between a minimum temperature of 17 °C and a maximum temperature of 27 °C.\n","NOTE \tThis is to avoid chemical reactions catalysis when it is too high or electronic reactions on certain technologies when it is too low.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.3a","Requirement","ECSS-Q-ST-60-14_0470012","RH in store cupboards shall be kept in the range 20 % to 65 % of RH.\n","NOTE \tThis is to avoid, when combined with temperature, corrosion phenomena. The lower is the Relative Humidity the greater is the probability for ESD damage.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.3b","Requirement","ECSS-Q-ST-60-14_0470059","EEE parts with MSL > 1 shall be stored, before and after relifing test sequence, in one of the following conditions:\n1.\tNitrogen,\n2.\tDry and ionised air in a range up to 20 % RH maximum,\n1.\tDry packs as specified in IPC/JEDEC J-STD-033D (April 2018).\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.4a","Requirement","ECSS-Q-ST-60-14_0470013","The containers used during storage shall ensure protection against ESD as defined in clause 4.1.6 and against any form of corrosion or contamination.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.4b","Requirement","ECSS-Q-ST-60-14_0470014","Parts shall be stored in containers such that it can be demonstrated that they offer protection against ESD, corrosion and contamination including the contamination induced by the package itself.\n","NOTE \tTheir primary containers can be used as long as they meet this requirement.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","4.2.4c","Requirement","ECSS-Q-ST-60-14_0470015","CCDs and opto-electronic sensors shall be stored in dry air or in neutral ambience, to prevent risks of cover glass pollution and moisture ingress.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","5c","Requirement","ECSS-Q-ST-60-14_0470060","The maximum lifetime requirements of the EEE parts manufacturers shall be taken into account.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","5d","Requirement","ECSS-Q-ST-60-14_0470016","In absence of EEE manufacturer's lifetime limitation and when required, relifing shall be performed between T1 and T2 according to the timing parameters given in Table 5‑1.\n","NOTE \t1\tRelife can be anticipated before T1, provided dT remains applicable.\nNOTE \t2\tFor parts not planned to be mounted and to be kept in stock, relifing is not mandatory.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","5e","Recommendation","ECSS-Q-ST-60-14_0470057","In case of parts procured through an external procurement entity, the customer should require the supplier to state the minimum period of validity of parts, w.r.t. T1 or T2, after delivery.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","5f","Requirement","ECSS-Q-ST-60-14_0470061","When started, all relifing tests as described in Table 6‑1 and Table 7‑1 shall be completed in a maximum period of six weeks.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","5g","Requirement","ECSS-Q-ST-60-14_0470062","First of all, the maximum lifetime requirements of the EEE parts manufacturers shall be taken into account.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1a","Requirement","ECSS-Q-ST-60-14_0470018","For relifing, the following tests, as specified in Table 6‑1 shall be performed: \n1.\tExternal Visual Inspection \n2.\tElectrical measurements \n3.\tSeal test \n4.\tSpecific test\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1b","Requirement","ECSS-Q-ST-60-14_0470019","Component families not covered in Table 6‑1 shall be subject to special procedures to be defined by the program.\n","NOTE \tThe relifing procedure can be applied on a sub-lot containing only the quantity of components immediately needed for production.  In this case, the relifing date-code is applicable only to parts actually tested.  The time limits specified in Table 5‑1 remain applicable for the residual sub-lot.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1c","Requirement","ECSS-Q-ST-60-14_0470020","When sampling is specified in Table 6‑1, it shall be performed in accordance with AQL 0,65 % level II according to ANSI ASQ Z1.4-2003 Revision 2008.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1d","Requirement","ECSS-Q-ST-60-14_0470021","The specifications and methods to be used during relifing shall be those that were in effect for the initial procurement or, if demonstrated that they are not applicable, the most recent updated issues.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1e","Requirement","ECSS-Q-ST-60-14_0470022","Seal test shall be performed on components made with a hermetic cavity package in conformance with the applicable procurement specification.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1f","Requirement","ECSS-Q-ST-60-14_0470023","For ceramic chip or moulded capacitors, electrical measurement shall be done after 4 hours of stabilisation at 125 °C for Type II ceramic.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1g","Requirement","ECSS-Q-ST-60-14_0470024","Multi-chips (stacked) capacitors shall be submitted to 100% visual inspection and electrical testing.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1h","Requirement","ECSS-Q-ST-60-14_0470025","For all type of solid tantalum capacitors, the following specific tests shall be performed before the parametrical measurement:\n1.\tApply 9 discharges and 8 charges with a cycle time of 2 seconds and under nominal voltage and monitor the current during both charge and discharge tests to detect short circuit,\n2.\tPerform a burn-in test for a duration or 96 hours at rated voltage at 85 °C.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1i","Requirement","ECSS-Q-ST-60-14_0470063","For all type of non-solid tantalum capacitors, the following specific test shall be performed before the parametrical measurement: \n1.\tPerform a burn-in test for a duration or 96 hours at rated voltage at 85 °C.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1j","Requirement","ECSS-Q-ST-60-14_0470026","For film capacitors using the polycarbonate technology, a DPA test shall be performed on three pieces, including:\n1.\texternal visual inspection,\n2.\tsealing test after insulate sleeve removal,\n3.\tmicrosection on two pieces, and\n4.\tdecaping on third part.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1k","Requirement","ECSS-Q-ST-60-14_0470027","For programmed parts, the total duration, including storage and mission, shall not exceed data retention duration given by the manufacturer.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1l","Permission","ECSS-Q-ST-60-14_0470058","For VLSI, hybrids and CCD, when electrical test is not practicable because of test program or product complexity, the validation may be transferred to use step such as functional tests or programming stages.\n","NOTE \tFor example, VLSI can be ASIC, FPGA, MMIC, DSP, microprocessors, microcontrollers.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1m","Requirement","ECSS-Q-ST-60-14_0470029","For electromagnetic relays of latching and non-latching type, 10 switching shall be run before electrical measurements.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1n","Requirement","ECSS-Q-ST-60-14_0470030","For low frequency and radio-frequency wires and cables, the following shall be done:\n1.\tinspect at least 0,5 m, and\n2.\tremove 0,2 m of the insulating material.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1o","Requirement","ECSS-Q-ST-60-14_0470031","Electrical test shall be optional for cavity hermetically sealed qualified parts when the qualification level is in line with the quality level defined by the applicable Tables 7-1, Table 7-2 or Table 7-3 of ECSS-Q-ST-60.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1p","Requirement","ECSS-Q-ST-60-14_0470064","For cable assemblies, electrical test shall be limited to insulation resistance test.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.1q","Requirement","ECSS-Q-ST-60-14_0470065","When relifed, commercial components shall be tested as defined in Table 6‑1 providing in addition, the following:\n1.\tthe availability of endurance test results on the flight lot,\n2.\tthe availability of humidity test results on the flight lot as per ECSS-Q-ST-60-13, in case of non-hermetic package sensitive to humidity,\n3.\tthe availability of a report of DPA performed on 3 pieces for each lot of commercial components in the frame of the relifing procedure.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.3a","Requirement","ECSS-Q-ST-60-14_0470032","A subset of DC parameters as given in the table of room temperature electrical measurements of the relevant procurement specification, ESCC or equivalent, shall be selected, submitted for customer approval on request and then measured.\n","NOTE \t1\tIt is important to pay attention to the test and set up procedures which can have changed since the initial date code.\nNOTE \t2\tAdditional burn-in and drift calculation to be performed only when specified in Table 6‑1.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.4a","Requirement","ECSS-Q-ST-60-14_0470033","In case of doubt or anomaly regarding any surface of the leads, one part shall be sampled in order to make a solderability test according to the applicable test method. \n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.4b","Requirement","ECSS-Q-ST-60-14_0470034","The solderability test results shall be recorded in the relifing report.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.4c","Requirement","ECSS-Q-ST-60-14_0470035","The part tested for solderability shall be considered destroyed.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.4d","Requirement","ECSS-Q-ST-60-14_0470066","External Visual Inspection shall be done in accordance with applicable procurement specifications.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.5a","Requirement","ECSS-Q-ST-60-14_0470036","The sealing tests shall be recorded as \"pass\" where the results meet the requirements of the original procurement specification\n","NOTE \tSealing tests include fine leaks or gross leaks or both, depending on the applicable specification.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.1.5b","Requirement","ECSS-Q-ST-60-14_0470037","The measurement values of leaks on non-conforming components shall be recorded in the relifing report.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2a","Requirement","ECSS-Q-ST-60-14_0470038","ECSS-Q-ST-10-09 shall apply for the handling and processing of nonconformances.\n","NOTE \tThe processing of nonconformances is identical for both relifing and normal procurement procedures. \n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2b","Requirement","ECSS-Q-ST-60-14_0470039","Any components not satisfying at least one of the requirements included in this standard shall be considered as not conform.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2c","Requirement","ECSS-Q-ST-60-14_0470040","When performing the sampling test, as per  Table 6‑1, any batch of components failing the sampling rule defined in requirement 6.1.1c shall be considered as not conform. \n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2d","Requirement","ECSS-Q-ST-60-14_0470041","<<deleted>>\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2e","Requirement","ECSS-Q-ST-60-14_0470042","In the case specified in 6.2c, the test shall be repeated on a 100% basis on the whole lot and the causes of the nonconformance investigated and recorded in the relifing report.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.2f","Requirement","ECSS-Q-ST-60-14_0470043","In case of 100% test, as per Table 6‑1, any batch of components shall be declared as  not conform when failing the following requirement:\n(a)\tlot size < 100 parts\t: 0 defect allowed\n(b)\tlot size > 100 parts\t: 1 defect allowed\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.3a","Requirement","ECSS-Q-ST-60-14_0470044","The relifing date code shall correspond to the week code of the first test performed on the lot. \n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.3b","Requirement","ECSS-Q-ST-60-14_0470045","This date code shall be assigned independent of the report conclusions.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.3c","Requirement","ECSS-Q-ST-60-14_0470046","The relifing date code shall not be marked on the component and no other additional marking added.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.4a","Requirement","ECSS-Q-ST-60-14_0470047","When relifing a component, a relifing report shall be established and sent, on request, to the customer for information.\n","NOTE \tGuidelines of a Relifing report are given in Annex C.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.5a","Requirement","ECSS-Q-ST-60-14_0470048","Once a batch is accepted, supported by a relifing report giving an “acceptable” decision or as a result of NCR processing, the original Certificate of Conformity shall be annotated with the relifing date code.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.5b","Requirement","ECSS-Q-ST-60-14_0470049","The Certificate of Conformity shall be delivered with the components.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.5c","Requirement","ECSS-Q-ST-60-14_0470050","Discarded batches shall be processed internally by the relevant reject system of the supplier.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","6.5d","Requirement","ECSS-Q-ST-60-14_0470067","The relifing NCR, if any, signed and dated by the supplier, shall be delivered with the components.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1a","Requirement","ECSS-Q-ST-60-14_0470068","For relifing, the following tests, as specified in Table 7‑1 shall be performed: \n1.\tExternal Visual Inspection\n2.\tElectrical measurements\n3.\tSpecific test\n","NOTE \tThe relifing procedure can be applied on a sub-lot containing only the quantity of components immediately needed for production. In this case, the relifing date-code is applicable only to parts actually tested. The time limits specified in Table 5‑1 remain applicable for the residual sub-lot.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1b","Requirement","ECSS-Q-ST-60-14_0470069","When sampling is specified in Table 7‑1, it shall be performed in accordance with AQL 0,65 % level II according to ANSI ASQ Z1.4.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1c","Requirement","ECSS-Q-ST-60-14_0470070","The relifing requirements defined in Table 7‑1 shall apply to Class 3 programmes.\n","NOTE \tComponents that are not listed in the Table 7‑1 are not subject to relifing.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1d","Requirement","ECSS-Q-ST-60-14_0470071","The specifications and methods to be used during relifing shall be those that were in effect for the initial procurement or, if demonstrated that they are not applicable, the most recent updated issues.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1e","Requirement","ECSS-Q-ST-60-14_0470072","For all type of solid tantalum capacitors, the following specific tests shall be performed before the parametrical measurement: \n1.\tApply 9 discharges and 8 charges with a cycle time of 2 seconds and under nominal voltage and monitor the current during both charge and discharge tests to detect short circuit. \n2.\tPerform a burn-in test for a duration of 96 hours, at rated voltage, at 85 °C.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1f","Requirement","ECSS-Q-ST-60-14_0470073","For all type of non-solid tantalum capacitors, the following specific tests shall be performed before the parametrical measurement: \n1.\tPerform a burn-in test for a duration of 96 hours, at rated voltage, at 85 °C.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1g","Permission","ECSS-Q-ST-60-14_0470074","For hybrids and commercial active parts, when electrical test is not practicable because of test program or product complexity, the validation may be transferred to use step such as functional test or programming stage.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.1h","Requirement","ECSS-Q-ST-60-14_0470075","When relifed, commercial components shall be tested as defined in Table 7‑1, providing in addition the following:\n1.\tthe availability of lifetest test results on the flight lot,\n2.\tthe availability of humidity test results on the flight lot as per ECSS-Q-ST-60-13, in the case of non-hermetic package sensitive to humidity,\n3.\ta DPA is performed on 3 pieces for each lot of commercial components in the frame of the relifing procedure.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.2a","Requirement","ECSS-Q-ST-60-14_0470077","A subset of DC parameters, as given in the Table of room temperature electrical measurements of the relevant procurement specification, ESCC or equivalent, shall be selected, submitted to customer’s approval and then measured.\n","NOTE \t1\tIt is important to pay attention to the test and set up procedures which can have changed since the initial date code.\nNOTE \t2\tAdditional burn-in to be performed only when specified inTable 7‑1.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.3a","Requirement","ECSS-Q-ST-60-14_0470078","In case of doubt or anomaly regarding any surface of the leads, one part shall be sampled in order to make a solderability test according to the applicable test method.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.3b","Requirement","ECSS-Q-ST-60-14_0470079","The solderability test results shall be recorded in the relifing report.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.3c","Requirement","ECSS-Q-ST-60-14_0470080","The part tested for solderability shall be considered destroyed.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.1.3d","Requirement","ECSS-Q-ST-60-14_0470081","In case of doubt or anomaly in the integrity of the glass sealing, parts shall be submitted to seal test according to the applicable test method.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.2a","Requirement","ECSS-Q-ST-60-14_0470082","ECSS-Q-ST-10-09 shall apply for the handling and processing of nonconformances.\n","NOTE \tThe processing of nonconformances is identical for both relifing and normal procurement procedures.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.2b","Requirement","ECSS-Q-ST-60-14_0470083","Any components that are not in compliance  at least with one of the requirements of ECSS-Q-ST-10-09 shall be declared as not conform.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.2c","Requirement","ECSS-Q-ST-60-14_0470084","When performing the sampling test, as per Table 7‑1, any batch of components failing the sampling rule defined in requirement 7.1.1b shall be considered as not conform.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.2d","Requirement","ECSS-Q-ST-60-14_0470085","In the case specified in 7.2c, the test shall be repeated on a 100 % basis on the whole lot and the causes of the nonconformance investigated and recorded in the relifing report.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.2e","Requirement","ECSS-Q-ST-60-14_0470086","In case of 100 % test, as per Table 7‑1, any batch of components shall be declared as not conform when failing the following “pass” conditions:\n1.\tlot size < 100 parts: 0 defect allowed\n2.\tlot size > 100 parts: 1 defect allowed\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.3a","Requirement","ECSS-Q-ST-60-14_0470087","The relifing date code shall correspond to the week code of the last test performed on the lot.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.3b","Requirement","ECSS-Q-ST-60-14_0470088","The relifing date code shall be assigned independent of the report conclusions.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.3c","Requirement","ECSS-Q-ST-60-14_0470089","The relifing date code shall not be marked on the component and no other additional marking added.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.4a","Requirement","ECSS-Q-ST-60-14_0470090","When relifing a component, a relifing report shall be established and sent, on request, to the customer for information.\n","NOTE \tGuidelines of an Relifing report are given in Annex C.\n",{"$nulls":3},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.5a","Requirement","ECSS-Q-ST-60-14_0470091","Once a batch is accepted, supported by a relifing report giving an “acceptable” decision or as a result of NCR processing, the original Certificate of Conformity shall be annotated with the relifing date code.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.5b","Requirement","ECSS-Q-ST-60-14_0470092","The Certificate of Conformity shall be attached with the components during their delivery.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.5c","Requirement","ECSS-Q-ST-60-14_0470093","Discarded batches shall be processed internally by the relevant reject system of the supplier.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","7.5d","Requirement","ECSS-Q-ST-60-14_0470094","The relifing NCR, if any, signed and dated by the supplier, shall be delivered with the components.\n",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","A.2.1a","Requirement","ECSS-Q-ST-60-14_0470051","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","A.2.1b","Requirement","ECSS-Q-ST-60-14_0470052","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","A.2.1c","Requirement","ECSS-Q-ST-60-14_0470053","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","A.2.1d","Requirement","ECSS-Q-ST-60-14_0470054","<<deleted>>",{"$nulls":4},"active","Product assurance","Level 2"]
["ECSS-S-ST-00C Rev.1","9.2a","Requirement","ECSS-S-ST-00_1000001","The customer shall select which ECSS Standards to make applicable and to use to establish the project/product requirements, including use of ECSS-S-ST-00-01 for terms and definitions.\n",{"$nulls":4},"active","System","Level 1"]
["ECSS-S-ST-00C Rev.1","9.2b","Requirement","ECSS-S-ST-00_1000002","The customer shall define, as part of the project requirements documentation (PRD), the set of requirements tailored from ECSS documents to the project specificities which are made applicable.\n",{"$nulls":4},"active","System","Level 1"]
["ECSS-S-ST-00C Rev.1","9.2c","Requirement","ECSS-S-ST-00_1000003","The customer shall produce, as part of the PRD, a documentation identifying the ECSS requirements applicable to the project.\n","NOTE \tAn “ECSS applicable requirements matrix” (EARM) is a recommended method for this component of the PRD.\n",{"$nulls":3},"active","System","Level 1"]
["ECSS-S-ST-00C Rev.1","9.2d","Requirement","ECSS-S-ST-00_1000004","The documentation identifying the requirements applicable to the project shall include following data (e.g. EARM):\n1.\tThe complete list of ECSS standards either fully or partially applicable to the project/product, including any standard (ECSS or not) made applicable via the chain of normative references;\n2.\tFor each partially applicable standard, the status of each requirement:\napplicable without modification\napplicable with modification\nnot applicable\n3.\tThe complete list of additional requirements\n4.\tFor modified and additional requirements, their complete formulation \n",{"$nulls":4},"active","System","Level 1"]
["ECSS-S-ST-00C Rev.1","9.3a","Requirement","ECSS-S-ST-00_1000005","The supplier shall demonstrate compliance with the PRD requirements.\n","NOTE \tAn “ECSS compliance matrix” (ECM) is a recommended method to document the demonstration of this compliance. The ECM is part of the project compliance matrix, addressing compliance to the applicable ECSS requirements (e.g. EARM).\n",{"$nulls":3},"active","System","Level 1"]
["ECSS-S-ST-00C Rev.1","9.3b","Requirement","ECSS-S-ST-00_1000006","The documentation identifying the compliance to ECSS requirements applicable to the project (e.g. the ECM) shall include following data:\n1.\tThe complete list of ECSS requirements applicable to the project (e.g. in the EARM).\n2.\tFor each requirement, the actual indication of compliance. When deviation is identified the justification is provided.\n",{"$nulls":4},"active","System","Level 1"]
["ECSS-U-ST-20C","5.1a","Requirement","ECSS-U-ST-20_1430001","The PPAA shall provide to the supplier planetary protection related obligations of relevant external authorities.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1b","Requirement","ECSS-U-ST-20_1430002","The supplier shall prepare a preliminary Planetary Protection Requirements document in conformance with the DRD in Annex A during the Phase A and no later than the PRR.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1c","Requirement","ECSS-U-ST-20_1430003","For missions that target or encounter multiple Solar system bodies, the preliminary Planetary Protection Requirements document shall include requirements for all the protected Solar system bodies.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1d","Requirement","ECSS-U-ST-20_1430004","The Planetary Protection Requirements document shall be subject to approval by the PPAA and released at the latest at SRR.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1e","Requirement","ECSS-U-ST-20_1430005","The delivery of hardware and services to a third-party mission with planetary protection constraints shall be subject to approval by the PPAA.\n","NOTE \tThe customer of the mission lead of the third-part mission bears the overall planetary protection responsibility at mission level, including assigning, monitoring, reviewing and approving planetary protection categories and associated requirements.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1f","Requirement","ECSS-U-ST-20_1430006","Impact of significant changes in the mission concept on the planetary protection requirements and implementation approach shall be assessed by the supplier and are subject to approval by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.1g","Requirement","ECSS-U-ST-20_1430007","The PPAA, or its designated entity, shall conduct independent verification assays on flight hardware and controlled environments, including launch site, during the course of the project at times and intervals planned and agreed with the supplier.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.2.1a","Requirement","ECSS-U-ST-20_1430008","Except as specified in 5.3.2.1d, all flight hardware subject to planetary protection constraints shall be assembled and maintained until and including launch in ISO class 8 cleanrooms “in operation”, or better, as specified in ECSS-Q-ST-70-01.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.2.2a","Requirement","ECSS-U-ST-20_1430009","A probability of impact analysis on protected Solar system bodies shall be performed and a report delivered for customer and PPAA review.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.2.2b","Requirement","ECSS-U-ST-20_1430010","The probability of impact analysis specified in 5.2.2a shall include:\n1.\tSingle and multiple pass analysis;\n2.\tHardware, software and operational reliability;\n3.\tMeteoroid impacts and effects on spacecraft reliability;\nMeteoroid model (e.g., IMEM 1.1) and parameters (fluence, directionality, velocity, density and margins) as defined in the project applicable environmental specifications\nDamage equations in IADC-WD-00-03 for the damage assessment\n4.\tSpacecraft state including location, and velocity vector;\n5.\tManoeuvre and planet and satellite ephemeris uncertainty;\n6.\tStochastic variability of the atmospheric density with the amplitude of the Solar cycle estimated for the mission and sun epoch.\n","NOTE \t1\tDifferent meteoroid models are used depending on the mission profile; dedicated models are currently developed for the Jovian system.\nNOTE \t2\tRequirements that need a probability of impact analysis to demonstrate compliance are described in 5.3.2.1d, 5.3.2.1e.1, and 5.3.3.1b.4.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.2.3a","Requirement","ECSS-U-ST-20_1430011","Except where numerical requirements are otherwise specified in this document, the probability of contaminating a Solar system body with viable terrestrial organisms shall be ≤ 1x10-3 over a period of 50 years after the arrival of the mission at the protected Solar system body.\n","NOTE \tDescription how compliance to this requirement will be demonstrated needs to be described in the Planetary Protection Plan DRD in B.2.1a.3.(e).\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.1a","Requirement","ECSS-U-ST-20_1430012","An organic materials inventory of bulk constituents present in quantities above the limit agreed with the PPAA shall be provided by the project in conformance with DRD in Annex H.\n","NOTE \tThis also applies to missions not going to the Moon but having a final disposition that would end up on the Moon.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.1a","Requirement","ECSS-U-ST-20_1430013","An organic materials inventory of bulk constituents present on the spacecraft in quantities ≥1 kg shall be provided by the supplier in conformance with DRD in Annex H.\n","NOTE \tThis requirement is not applicable in case requirement 5.3.2.1e.1 is met.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.1b","Requirement","ECSS-U-ST-20_1430014","A 50 gram sample for each organic material used on the spacecraft in quantities ≥25 kg shall be provided by the supplier and stored by the customer under controlled conditions for 50 years after launch.\n","NOTE \tThis requirement is not applicable in case requirement  5.3.2.1e.1 is met.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.1c","Requirement","ECSS-U-ST-20_1430015","Compliance to all bioburden requirements shall be verified pre-launch.\n","NOTE \tThis verification is usually done on last physical access of the flight hardware or hardware elements, i.e., at delivery of flight hardware to next level contractor, delivery to launch site, and at the launch site prior to fairing closure.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.1d","Requirement","ECSS-U-ST-20_1430016","The probability of impact on Mars by any element not assembled and maintained in at least ISO class 8 conditions shall be ≤ 1x10-4 for the first 50 years after launch for nominal and off-nominal flight conditions.\n","NOTE \tExamples are upper stages.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.1e","Requirement","ECSS-U-ST-20_1430017","One of the following conditions shall be met:\n1.\tThe probability of impact on Mars by any part of a spacecraft assembled and maintained in ISO class 8 conditions, or better, is ≤ 1x10-2 for the first 20 years after launch, and ≤ 5x10-2 for the time period from 20 to 50 years after launch for nominal and off-nominal flight conditions.\n2.\tThe total bioburden of the spacecraft on Mars, including surface, mated, and encapsulated bioburden, is ≤ 5x105 bacterial spores.\n","NOTE \tThis requirement is also applicable for fly-by and gravity assist manoeuvres.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2a","Requirement","ECSS-U-ST-20_1430018","The bioburden of the landed system on Mars shall be ≤ 3x105 bacterial spores on exposed internal and external surfaces.\n","NOTE \tAttention – for bioburden allocations to hardware and payload suppliers take into account re-contamination during different on-ground phases (e.g., testing at sub-system and system level, launch).\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2b","Requirement","ECSS-U-ST-20_1430019","The average bioburden of the landed system on Mars shall be ≤ 300 bacterial spores/m2 on exposed internal and external surfaces.\n","NOTE \t1\tAttention – for bioburden allocations to hardware and payload suppliers take into account re-contamination during different on ground phases (e.g., testing at sub-system and system level, launch).\nNOTE \t2\tAttention – for large spacecraft systems the average bioburden to meet requirement 5.3.2.2.2a needs to be much lower than 300 bacterial spore/m2.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2c","Requirement","ECSS-U-ST-20_1430020","The supplier shall provide an analysis or assessment whether the spacecraft during nominal and off-nominal conditions has the potential to modify the local martian environment in a way that can create a Mars special region.\n","NOTE \tSuch an analysis or assessment is in particular important for spacecraft using radioisotope heat sources targeting areas with surface or sub-surface water ice.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2d","Requirement","ECSS-U-ST-20_1430021","Planned 3-sigma pre-launch landing ellipses shall be evaluated and documented on a case-by-case basis as part of the landing site selection process to determine whether the mission can land or come within contamination range of areas or volumes meeting the parameter definition for Mars Special Regions or impinge on already described features that can be treated as Mars Special Regions. \n","NOTE \tThis means at least no areas or volumes meeting the parameter definition for Mars Special Regions or already described features that can be treated as Mars Special Regions can be within the 3-sigma landing ellipse.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2e","Requirement","ECSS-U-ST-20_1430022","The evaluations specified in 5.3.2.2.2c and 5.3.2.2.2d shall be based on the latest scientific evidence and include an assessment of the extent to which the temperature and water activity values specified for Mars Special Regions are separated in time. \n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.2f","Requirement","ECSS-U-ST-20_1430023","The evaluation specified in 5.3.2.2.2d shall be updated during the mission whenever new evidence indicates that the landing ellipse and the operational environment contain, or are in contamination range of areas or volumes meeting the parameter definition for Mars Special Regions.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.3a","Requirement","ECSS-U-ST-20_1430024","For surface mission with life detection one of the following conditions shall be met:\n1.\tThe bioburden of the surface system on Mars is ≤ 30 bacterial spores on exposed internal and external surfaces, or at a contamination level driven by the nature and sensitivity of the particular life-detection investigations.\n2.\tThe average bioburden of the subsystems that are involved in the acquisition, delivery, and analysis of samples used for life-detection investigations is either:\n(a)\t≤ 0,03 bacterial spores/m2, or\n(b)\tat a contamination level driven by the nature and sensitivity of the particular life-detection investigations.\n","NOTE \tThe contamination level driven by the particular life-detection investigation needs to be described in the Planetary Protection Plan DRR, Annex B.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.3b","Requirement","ECSS-U-ST-20_1430025","The specific contamination level driven by the nature and sensitivity of the particular life-detection investigation described in 5.3.2.2.3a.1 and 5.3.2.2.3a.2(b) shall be subject to review and approval by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.3c","Requirement","ECSS-U-ST-20_1430026","Recontamination prevention of the subsystems specified in 5.3.2.2.3a.2 and the samples to be analysed shall be in place until the end of the life-detection investigations.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.4a","Requirement","ECSS-U-ST-20_1430027","If a Mars special region is within the 3-sigma landing ellipse, the bioburden of the entire surface system on Mars shall be ≤ 30 bacterial spores on exposed internal and external surfaces.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.4b","Requirement","ECSS-U-ST-20_1430028","If a Mars special region is accessed through horizontal or vertical mobility, one of the following conditions shall be met:\n1.\tThe bioburden of the entire surface system on Mars is ≤ 30 bacterial spores on exposed internal and external surfaces.\n2.\tThe subsystems which directly contact the Mars special region are sterilized to levels specified in 5.3.2.2.4b.1, and a method of preventing their recontamination prior to accessing the Mars special region is in place.\n","NOTE \tExample of accessing Mars special regions are by roving (horizontal mobility) or by drilling (vertical mobility).\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.2.4c","Requirement","ECSS-U-ST-20_1430029","If an off-nominal condition can cause a high probability of inadvertent biological contamination of a Mars special region by the spacecraft the bioburden shall be the following:\n1.\tThe bioburden of the entire surface system on Mars is ≤ 30 bacterial spores on exposed internal and external surfaces, and \n2.\tThe total surface, mated, and encapsulated bioburden level on Mars is ≤ 30 + 1,5 x 104 bacterial spores.\n","NOTE \tExample for off-nominal condition is a hard landing.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3a","Requirement","ECSS-U-ST-20_1430030","Requirements in clause 5.3.2.2.3 shall be applied to the outbound leg of a Mars sample return mission.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3b","Requirement","ECSS-U-ST-20_1430031","The severity of potential consequences of releasing unsterilized material from Mars and flight hardware that has been exposed to unsterilized material from Mars into the terrestrial environment shall be categorised as catastrophic in accordance with ECSS-Q-ST-40.\n","NOTE \tThe categorization of this severity level is not because a catastrophic consequence is expected but only following the precautionary principle due to the large number of unknowns.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3c","Requirement","ECSS-U-ST-20_1430032","Safety critical functions as defined in 3.2.19 shall be treated as severity function criticality level 1 in accordance with ECSS-Q-ST-40.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3d","Requirement","ECSS-U-ST-20_1430033","The probability that a single unsterilized martian particle of ≥ 0,01 μm in diameter is released into the terrestrial environment shall be ≤ 1x10-6 for the first 100 years after launch from Mars.\n","NOTE \t1\tRational for this requirement is to “break the chain of contact” between Mars and Earth.\nNOTE \t2\tSource and context for numerical values in [5].\nNOTE \t3\tThe term ‘particle’ includes material from Mars and flight hardware exposed to material from Mars.\nNOTE \t4\tIf the size requirement of 0,01 μm cannot be met without decreasing the overall level of assurance for the non-release of such a particle, the release of a single unsterilised particle of up to 0,05 μm can be considered as a potentially tolerable systems-level adjustment, assuming that it has been demonstrated that this size is the lowest achievable at a reasonable cost (BAT approach) and it has been independently reviewed.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3e","Requirement","ECSS-U-ST-20_1430034","A quantitative PRA shall be conducted as part of evaluating the risk of releasing unsterilized material from Mars and flight hardware that has been exposed to unsterilized material from Mars into the terrestrial environment.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.2.3f","Requirement","ECSS-U-ST-20_1430035","No unsterilised portion of the materials returned from Mars shall be released from containment unless approved by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.1a","Requirement","ECSS-U-ST-20_1430036","The probability of inadvertent contamination of a subsurface ocean by viable terrestrial organisms shall be ≤ 1 x 10-4 per mission.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.1b","Requirement","ECSS-U-ST-20_1430037","The calculation of the probability specified in 5.3.3.1a of inadvertent contamination shall address the following factors, at a minimum:\n1.\tBioburden at launch;\n2.\tCruise survival for bioburden;\n3.\tBioburden survival in the respective radiation environment;\n4.\tProbability of landing on Solar system body;\n5.\tThe mechanisms and timescales of transport to the subsurface;\n6.\tBioburden survival and proliferation before, during, and after subsurface transfer.\n","NOTE \tMethods of bioburden reduction reflect the type of environments found on Europa or Enceladus, focusing on terrestrial organisms most likely to survive on Europa or Enceladus, such with cold, desiccation and radiation tolerance. \n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.1c","Requirement","ECSS-U-ST-20_1430038","When computing the calculation of requirement 5.3.3.1b the estimate for poorly known parameters shall be subject to approval by the customer and the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.2.2a","Requirement","ECSS-U-ST-20_1430039","Requirements in clause 5.3.2.2.3, shall be applied to the outbound leg of a sample return mission.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.2.2b","Requirement","ECSS-U-ST-20_1430040","The severity of potential consequences of releasing unsterilized material from Europa or Enceladus and flight hardware that were exposed to unsterilized material from Europa or Enceladus into the terrestrial environment shall be categorised as catastrophic in accordance with ECSS-Q-ST-40.\n","NOTE \tThe categorization of this severity level is not because a catastrophic consequence is expected but only following the precautionary principle due to the large number of unknowns.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.2.2c","Requirement","ECSS-U-ST-20_1430041","Safety critical functions as defined in 3.2.19 shall be treated as severity function criticality level 1 in accordance with ECSS-Q-ST-40.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.3.2.2d","Requirement","ECSS-U-ST-20_1430042","No unsterilised portion of the materials returned from Europa or Enceladus shall be released from containment unless approved by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.1a","Requirement","ECSS-U-ST-20_1430043","Categorization of missions to small Solar system bodies shall be made on a case-by-case basis.\n","NOTE \tThe small Solar system bodies (SB) not elsewhere discussed in this document represent a large class of objects. Most missions to SB are classified as Category I or Category II missions for forward contamination, and Category V, unrestricted Earth return, for backward contamination.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.1b","Requirement","ECSS-U-ST-20_1430044","The mission shall be categorized as “restricted Earth return” if the answer to all the following six questions is \"no\" or “uncertain”, otherwise the mission is categorized as “unrestricted”:\n1.\tDoes scientific evidence indicate that there was never liquid water in or on the target body?\n2.\tDoes scientific evidence indicate that metabolically useful energy sources were never present?\n3.\tDoes scientific evidence indicate that there was never sufficient organic matter or CO2 or carbonates and an appropriate source of reducing equivalents in or on the target body to support life?\n4.\tDoes scientific evidence indicate that subsequent to the disappearance of liquid water, the target body has been subjected to extreme temperatures >160 °C?\n5.\tDoes scientific evidence indicate that there is or was sufficient radiation for sterilization of terrestrial life forms?\n6.\tDoes scientific evidence indicate that there has been a natural influx to Earth, via meteorites, of material equivalent to a sample returned from the target body?\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.1c","Requirement","ECSS-U-ST-20_1430045","If a mission is categorized as “restricted Earth return” in accordance with 5.3.4.1b, procedures shall be applied to the mission as specified in requirements from clause 5.3.4.2\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.2.2a","Requirement","ECSS-U-ST-20_1430046","Category IVb requirements in clause 5.3.2.2.3, shall be applied to the outbound leg of a sample return mission.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.2.2b","Requirement","ECSS-U-ST-20_1430047","The severity of potential consequences of releasing unsterilized material from specific small solar system bodies and flight hardware that has been exposed to unsterilized material from specific small solar system bodies into the terrestrial environment shall be categorised as catastrophic in accordance with ECSS-Q-ST-40.\n","NOTE \tThe categorization of this severity level is not because a catastrophic consequence is expected but only following the precautionary principle due to the large number of unknowns..\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.2.2c","Requirement","ECSS-U-ST-20_1430048","Safety critical functions as defined in 3.2.19 shall be treated as severity function criticality level 1 in accordance with ECSS-Q-ST-40.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.3.4.2.2d","Requirement","ECSS-U-ST-20_1430049","No unsterilised portion of the materials returned from Mars shall be released from containment unless approved by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.1a","Requirement","ECSS-U-ST-20_1430050","Requirements from clause 5 of ECSS-Q-ST-70-58 shall be applied for bioburden controlled environments.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2a","Requirement","ECSS-U-ST-20_1430051","Bioburden assessment on flight hardware shall be performed, using procedures \"Swab assay 1 (standard swab assay)\" or \"Wipe assay 1 (standard wipe assay) \"as per procedures D.1 and E.1 from Annex D and Annex E of ECSS-Q-ST-70-55.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2b","Requirement","ECSS-U-ST-20_1430052","If direct assays are not possible, estimation of the flight hardware bioburden using the highest number in the respective category of Table 5‑1 shall be used.\n","NOTE \tThe encapsulated bioburden values in Table 5‑1 cannot be used for ALM produced hardware.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2c","Requirement","ECSS-U-ST-20_1430054","Use of assay procedures not described in Annex D, Annex E, Annex F and Annex G of ECSS-Q-ST-70-55 shall be approved by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2d","Requirement","ECSS-U-ST-20_1430055","The number of samples to evaluate the bioburden for the flight hardware shall be agreed with the PPAA and meet the following conditions:\n1.\tFive swabs for each surface area on flight hardware of 0,1 m2;\n2.\tA proportionate number, but at least one swab, for each surface area on flight hardware smaller than 0,1 m2;\n3.\tOne wipe for each surface area on flight hardware in the size range of 1 m2;\n4.\tTwo wipes for each individual surface area on flight hardware per 10 m2.\n","NOTE \tAlthough the sampling plan is specific to the size and geometry of the sampled hardware, sampling at least 20 % of the surface area is a reasonable guideline. To reduce the conservatism in the overall bioburden calculations it is better to sample larger surface areas.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2e","Requirement","ECSS-U-ST-20_1430056","The methods for calculation surface bioburden and bioburden densities shall be agreed with PPAA. \n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.2f","Requirement","ECSS-U-ST-20_1430057","Bioburden prior to the application of a bioburden reduction procedure shall be established by using procedures specified in requirements 5.4.2a or 5.4.2b.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.3a","Requirement","ECSS-U-ST-20_1430058","Biodiversity assessment on flight hardware and bioburden controlled environment(s) shall be performed using procedures D.3-D.6 for Swab assays and procedures E.3-E.6 for Wipe assays as per Annex D and Annex E of ECSS-Q-ST-70-55.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.4a","Requirement","ECSS-U-ST-20_1430059","Dry heat microbial reduction shall be performed in compliance with requirements from clause 5 of ECSS-Q-ST-70-57.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.4b","Requirement","ECSS-U-ST-20_1430060","Hydrogen peroxide microbial reduction shall be performed in compliance with requirements from clause 5 of ECSS-Q-ST-70-56.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.4c","Requirement","ECSS-U-ST-20_1430061","Use of other bioburden reduction procedures shall be approved by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.4.4d","Requirement","ECSS-U-ST-20_1430062","Evaluation of material and hardware compatibility with bioburden reduction procedures shall be performed in compliance with requirements from clause 5 of ECSS-Q-ST-70-53.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.5a","Requirement","ECSS-U-ST-20_1430063","Planetary protection documentation shall be provided according to the matrix in Table 5‑2.\n","NOTE \t1\tTable 5‑2 can be tailored to the respective project.\nNOTE \t2\tDocumenting the implementation of planetary protection requirements is not limited to the dedicated planetary protection documents but needs to be reflected in the affected project documentation, e.g., management plan, quality plan, AIV and AIT plan, VCD.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.5b","Requirement","ECSS-U-ST-20_1430064","The supplier shall support the PPAA, for the preparation of the customer level planetary protection report of a mission.\n","NOTE \t1\tThe report is delivered no later than nine months after launch to the President of COSPAR and the chair of the COSPAR panel on planetary protection.\nNOTE \t2\tContent of the customer level planetary protection report to COSPAR is described in the COSPAR Planetary Protection Policy [2].\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.6a","Requirement","ECSS-U-ST-20_1430066","Planetary protection implementation activities and applicable planetary protection documentation specified in Table 5‑2, including any documentation to support conclusions of analysis, shall be reviewed during regular reviews to which PPAA participates.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.6b","Requirement","ECSS-U-ST-20_1430067","Planetary protection reviews shall be held for Earth return missions to authorize the different segments of the return phase:\n1.\tSubsequent to sample collection and prior to a manoeuvre to enter a Earth return trajectory;\n2.\tPrior to commitment for Earth entry.\n","NOTE \t1\tThe objective of these reviews is to demonstrate that the mission continues to meet the planetary protection requirements in general, and Earth safety in particular.\nNOTE \t2\tThe planetary protection reviews can be part of regular project reviews.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.7a","Requirement","ECSS-U-ST-20_1430068","ECSS-Q-ST-10-09 shall be applied for nonconformances and waivers.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.7b","Requirement","ECSS-U-ST-20_1430069","All nonconformance related to planetary protection shall be specified as major nonconformance.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.7c","Requirement","ECSS-U-ST-20_1430070","The disposition of nonconformances related to planetary protection requirements shall be subject to approval by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","5.7d","Requirement","ECSS-U-ST-20_1430071","The approval of waivers related to planetary protection requirements shall be subject to approval by the PPAA.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","A.2.1a","Requirement","ECSS-U-ST-20_1430072","The planetary protection requirements document shall include at least the following items:\n1.\tMission description\n(a)\tScientific objectives and payload description\n(b)\tMission type fly-by, orbiter, lander, Earth return\n(c)\tDescription of mission phases\n(d)\tDescription of launch vehicle and launch site\n(e)\tIdentification of targeted and encountered Solar system bodies\n(f)\tIdentification and use of nuclear heat and power sources\n(g)\tIdentification and use of aerobraking and aerocapture manoeuvres\n(h)\tDescription of entry, descent and landing phases\n(i)\tDescription of intended landing site and expected landing accuracy\n(j)\tIntended final disposition of all launched hardware\n(k)\tDescription of international cooperation\n2.\tPlanetary protection category\n3.\tPlanetary protection management requirements, tailored ECSS-U-ST-20\n4.\tTechnical planetary protection requirements, tailored ECSS-U-ST-20\n5.\tPlanetary protection methods and procedures, tailored ECSS-U-ST-20\n6.\tPlanetary protection documentation and reviews, tailored ECSS-U-ST-20\n","NOTE \tPlanetary protection requirements for the payload are usually described in the payload interface requirements.\n",{"$nulls":3},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","A.2.2a","Permission","ECSS-U-ST-20_1430073","The Mission description, specified in A.2.1a.1, may be covered by a reference to another project document.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","B.2.1a","Requirement","ECSS-U-ST-20_1430074","The planetary protection plan shall include the following items:\n1.\tMission description.\n2.\tAssessment of the consequences to implement the planetary protection requirements with respect to design, development, schedule and operations.\n3.\tGeneral implementation approach:\n(a)\tPlanetary protection management and organisation.\n(b)\tDescription of bioburden control approach for all major flight hardware elements, including payload and launch recontamination.\n(c)\tDescription of bioburden allocations with identified margins and uncertainties for all major flight hardware elements.\n(d)\tDescription of bioburden control approach and/or contamination control approach for life-detection investigation, in accordance with ECSS-U-ST-20 requirement 5.3.2.2.3a.\n(e)\tDescription of probability of impact analysis, in accordance with ECSS-U-ST-20 requirements 5.2.2a, 5.2.2b, 5.3.2.1d, 5.3.2.1e including: \n(1)\tImpact analysis for launcher and spacecraft elements against target bodies identified in the “planetary protection requirements” document, with analysis supporting the conclusions providing evidence that the selected approach is feasible for the specific mission; \n(1)\tIf probability of impact approach is not possible or selected, break-up, burn-up and general atmospheric entry heating analysis providing evidence that the selected approach is feasible for the specific mission.\n(f)\tDescription of probability of contamination analysis, in accordance with ECSS-U-ST-20 requirements 5.2.3a, 5.3.2.2.2c, d, e, f, 5.3.2.2.3c and 5.3.3.2.2a.\n(g)\tDescription for methods and procedures to be used, in accordance with ECSS-U-ST-20 requirements in clause 5.4.\n(h)\tDescription of planned requests for using methods, procedures or values not described in this standard, in accordance with ECSS-U-ST-20 requirements in clause 5.7.\n4.\tPlanetary protection documentation and reviews, in accordance with ECSS-U-ST-20 requirements in clauses 5.5 and 5.6.\n5.\tIdentify planetary protection activities and events in the project schedule.\n6.\tCompliance matrix against the planetary protection requirements.\n7.\tAnalysis and conclusions of consequences for planned non-conformances or waivers.\n8.\tVerification matrix against the planetary protection requirements.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","B.2.2a","Permission","ECSS-U-ST-20_1430075","The Mission description, as per B.2.1a.1. may be covered by a reference to another project document.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","B.2.2b","Permission","ECSS-U-ST-20_1430076","The Assessment of the consequences, as per B.2.1a.2. may summarize the consequences with references to other project documentation for detailed descriptions.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","B.2.2c","Permission","ECSS-U-ST-20_1430077","The compliance matrix, as per B.2.1a.6. may be included in a project level compliance and verification matrix.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","B.2.2d","Permission","ECSS-U-ST-20_1430078","The Verification matrix as per B.2.1a.8. may be included in a project level compliance and verification matrix.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","C.2.1a","Requirement","ECSS-U-ST-20_1430079","The planetary protection implementation plan shall include the following items:\n1.\tFlight system description\n(a)\tHardware description\n(1)\tSystem and sub-system description, including payload\n(2)\tPlanetary protection description vs. subsystem names\n(b)\tCriteria for exposed surfaces and planetary protection accountable volumes\n(c)\tMission planetary protection issues as they are intended to be implemented, accounting for the following data: \n(1)\tProbability of impact analysis, in accordance with ECSS-U-ST-20 requirements 5.2.2a, 5.2.2b, 5.3.2.1d, 5.3.2.1e; \n(2)\tProbability of contamination analysis in accordance with ECSS-U-ST-20 requirements 5.2.3a, 5.3.3.2.2a;\n(3)\tSpacecraft induced special regions, in accordance with ECSS-U-ST-20 requirement 5.3.2.2.2c; \n(4)\tLanding site selection; \n(5)\tDraft organic material inventory in accordance with ECSS-U-ST-20 requirements 5.3.1a, 5.3.2.1a.\n2.\tDescription of Facilities\n(a)\tFormal system including \n(1)\tRisk assessment;\n(2)\tAlerts and action levels;\n(3)\tControl approach.\n(b)\tCommissioning\n(c)\tOperation\n3.\tBioburden control plan for the flight system\n(a)\tBioburden allocation including:\n(1)\tExposed surface bioburden allocation; \n(2)\tTotal bioburden allocation;\n(3)\tHardware exceptions.\n(b)\tSampling and Assay plan including:\n(1)\tFraction of exposed surfaces sampled;\n(2)\tNumber of samples; \n(3)\tSampling site selection;\n(4)\tSampling schedule.\n(c)\tStatistical treatment of the assay results including:\n(1)\tCase for total spore count greater than one;\n(2)\tCase for total spore count of zero or one;\n(3)\tCase for treatment of bulk assay;\n(4)\tBasis for bioburden density standard deviation;\n(5)\tAssay results acceptance guidelines.\n(d)\tBioburden assessment, in accordance with ECSS-U-ST-20 requirements 5.4.1a, and requirements from clause 5.4.2 including: \n(1)\tCalculation of surface bioburden density and number of spores from assay data;\n(2)\tSurface bioburden density and number of spores without assay data;\n(3)\tSurface bioburden density and number of spores for hardware treated by a bioburden reduction procedures;\n(4)\tEncapsulated bioburden density and number of spores with assay data;\n(5)\tEncapsulated bioburden density and number of spores without assay data.\n(e)\tBiodiversity assessment, in accordance with ECSS-U-ST-20 requirement 5.4.3a.\n4.\tBioburden reduction plan for the flight system, in accordance with ECSS-U-ST-20 requirements in clause 5.4.4\n(a)\tSpacecraft hardware subject to bioburden reduction processes;\n(b)\tProcess analysis;\n(c)\tProcess verification and control;\n(d)\tRecontamination prevention approach.\n5.\tGeneral implementation approach for the flight system\n(a)\tPre-AIV, AIT and launch operations including: \n(1)\tGeneral approach at hardware manufacturing sites;\n(2)\tGeneral approach at Customer, supplier and instrument provider site.\n(b)\tAIV, AIT and launch operations including: \n(1)\tAcceptance criteria; \n(2)\tGeneral approach at Customer and supplier and payload provider site; \n(3)\tGeneral approach at test site; \n(4)\tGeneral approach at launch site.\n(c)\tInside surface of the launch vehicle fairing, launch vehicle air conditioning, and white room air conditioning.\n(d)\tUpper stage and propulsion module.\n6.\tUpdated list of the foreseen waivers and NCRs and the associated impact analysis.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","D.2.1a","Requirement","ECSS-U-ST-20_1430080","The pre-launch planetary protection report shall include the following items:\n1.\tDeviation from planetary protection requirements and plan;\n2.\tDeviation from the planetary protection implementation plan;\n3.\tResults of contamination control measures, including raw and processed data of bioburden assays for the entire product tree;\n4.\tUpdate of probability of impact analysis, in accordance with ECSS-U-ST-20 requirements 5.2.2a, 5.2.2b, 5.3.2.1d, 5.3.2.1e;\n5.\tUpdate for probability of contamination analysis in accordance with ECSS-U-ST-20 requirements 5.2.3a, 5.3.3.2.2a;\n6.\tOrganic materials inventory, in accordance with ECSS-U-ST-20 requirements 5.3.1a, 5.3.2.1a;\n7.\tConclusions of the report.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","E.2.1a","Requirement","ECSS-U-ST-20_1430081","The post-launch planetary protection report shall include the following items:\n1.\tGround processing affecting bioburden control;\n2.\tLast verification assay results;\n3.\tLaunch events affecting bioburden control;\n4.\tPost Launch effects within the deployment and in orbit commissioning timeframe;\n5.\tConclusions of the report.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","F.2.1a","Requirement","ECSS-U-ST-20_1430082","The extended mission planetary protection report shall include the following items:\n1.\tDeviation from planetary protection requirements and plan;\n2.\tDeviation from the planetary protection implementation plan;\n3.\tUpdate of probability of impact analysis, in accordance with ECSS-U-ST-20 requirements 5.2.2a, 5.2.2b, 5.3.2.1d, 5.3.2.1e;\n4.\tUpdate for probability of contamination analysis, in accordance with ECSS-U-ST-20 requirements 5.2.3a, 5.3.3.2.2a;\n5.\tConclusions of the report.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","G.2.1a","Requirement","ECSS-U-ST-20_1430083","The end-of-mission planetary protection report shall include the following items:\n1.\tDisposition and condition of all launched flight hardware including the launcher upper stage, either in space describing the orbital parameters or for landed or impacting elements by position on the target body;\n2.\tDeviation from planetary protection requirements and plan;\n3.\tDeviation from the planetary protection implementation plan;\n4.\tUpdate of probability of impact analysis in accordance with ECSS-U-ST-20 requirements 5.2.2a, 5.2.2b, 5.3.2.1d, 5.3.2.1e;\n5.\tUpdate for probability of contamination analysis, in accordance with ECSS-U-ST-20 requirements 5.2.3a, 5.3.3.2.2a;\n6.\tConclusions of the report.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","H.2.1a","Requirement","ECSS-U-ST-20_1430084","The organic material inventory shall include the following for each organic material present above a specified limit agreed with PPAA:\n1.\tIdentity;\n2.\tChemical composition;\n3.\tUsage, with respect to product tree;\n4.\tMass estimate using the mass codes specified in ECSS-Q-ST-70-01;\n5.\tRating and reference for outgassing for each item using ECSS-Q-ST-70-01;\n6.\tSupplier for each item.\n",{"$nulls":4},"active","Sustainability","Level 1"]
["ECSS-U-ST-20C","H.2.1b","Requirement","ECSS-U-ST-20_1430085","For missions to the Moon, including fly-by-gravity assist, a description of the products released by the propulsion and life-support system, as applicable, into the lunar environment shall be provided, including:\n1.\tA quantitative and qualitative description of the major chemical species, and\n2.\tAn indication of the minor chemical species and quantity.\n",{"$nulls":4},"active","Sustainability","Level 1"]

{"sheet":"Statistic Active Standards","index":1,"n_rows":51,"n_cols":14,"rows_kept":51}
["Statistics from ECSS DOORS database v0.8 (October 2020)"]
[]
["The following data shows the number of Requirments, Recommendations and Persmissions of the ACTIVE ECSS Standards"]
["ECSS Discipline","(All)",null,"ECSS Discipline","(All)",null,"ECSS Discipline","(All)"]
["Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 2"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["Permission",668,null,"Permission",108,null,"Permission",560]
["Recommendation",843,null,"Recommendation",131,null,"Recommendation",712]
["Requirement",27976,null,"Requirement",5848,null,"Requirement",22128]
["Grand Total",29487,null,"Grand Total",6087,null,"Grand Total",23400]
[]
[]
[]
["Number of Requirements, Recommendations and Permissions split per ECSS Discipline and Level"]
[]
["ECSS Discipline","Engineering",null,"ECSS Discipline","Management",null,"ECSS Discipline","Product Assurance",null,"ECSS Discipline","Sustainability",null,"ECSS Discipline","System"]
["Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["Permission",337,null,"Permission",15,null,"Permission",311,null,"Permission",5,null,"Requirement",6]
["Recommendation",534,null,"Recommendation",14,null,"Recommendation",295,null,"Requirement",78,null,"Grand Total",6]
["Requirement",17996,null,"Requirement",558,null,"Requirement",9338,null,"Grand Total",83]
["Grand Total",18867,null,"Grand Total",587,null,"Grand Total",9944]
[]
["Level 1 Standards only"]
[]
["ECSS Discipline","Engineering",null,"ECSS Discipline","Management",null,"ECSS Discipline","Product Assurance",null,"ECSS Discipline","Sustainability",null,"ECSS Discipline","System"]
["Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 1"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["Permission",37,null,"Permission",15,null,"Permission",51,null,"Permission",5,null,"Requirement",6]
["Recommendation",111,null,"Recommendation",14,null,"Recommendation",6,null,"Requirement",78,null,"Grand Total",6]
["Requirement",3502,null,"Requirement",504,null,"Requirement",1758,null,"Grand Total",83]
["Grand Total",3650,null,"Grand Total",533,null,"Grand Total",1815]
[]
[]
["Level 2 Standards only"]
[]
["ECSS Discipline","Engineering",null,"ECSS Discipline","Management",null,"ECSS Discipline","Product Assurance",null,"ECSS Discipline","Sustainability",null,"ECSS Discipline","System"]
["Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 2",null,"Level 1 or Level 2 Standard","Level 2",null,"Level 1 or Level 2 Standard","Level 2",null,"Level 1 or Level 2 Standard","Level 2"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["Permission",37,null,"Requirement",54,null,"Permission",260,null,"Grand Total",null,null,"Grand Total"]
["Recommendation",111,null,"Grand Total",54,null,"Recommendation",289]
["Requirement",3502,{"$nulls":4},"Requirement",7580]
["Grand Total",3650,{"$nulls":4},"Grand Total",8129]

{"sheet":"Statistics per Standard","index":2,"n_rows":242,"n_cols":14,"rows_kept":242}
["Number of Requirements, Recommendations and Permissions per Active ECSS Standard"]
[]
["ECSS Discipline","(All)",null,"ECSS Discipline","(All)",null,"ECSS Discipline","(All)"]
["Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","Level 1",null,"Level 1 or Level 2 Standard","Level 2"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["Permission",668,null,"Permission",108,null,"Permission",560]
["Recommendation",843,null,"Recommendation",131,null,"Recommendation",712]
["Requirement",27976,null,"Requirement",5848,null,"Requirement",22128]
["Grand Total",29487,null,"Grand Total",6087,null,"Grand Total",23400]
[]
[]
[]
["Number of Requirements, Recommendations and Permissions split per ECSS Discipline and Level"]
[]
["ECSS Discipline","Engineering",null,"ECSS Discipline","Management",null,"ECSS Discipline","Product Assurance",null,"ECSS Discipline","Sustainability",null,"ECSS Discipline","System"]
["Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)"]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
[]
["Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type",null,"Row Labels","Count of Type"]
["ECSS-E-ST-10-02C Rev.1",192,null,"ECSS-M-ST-10-01C",54,null,"ECSS-Q-ST-10-04C",62,null,"ECSS-U-ST-20C",83,null,"ECSS-S-ST-00C Rev.1",6]
["Permission",1,null,"Requirement",54,null,"Requirement",62,null,"Permission",5,null,"Requirement",6]
["Recommendation",1,null,"ECSS-M-ST-10C Rev. 1",99,null,"ECSS-Q-ST-10-09C Rev. 1",142,null,"Requirement",78,null,"Grand Total",6]
["Requirement",190,null,"Permission",6,null,"Permission",1,null,"Grand Total",83]
["ECSS-E-ST-10-03C",438,null,"Requirement",93,null,"Recommendation",6]
["Permission",7,null,"ECSS-M-ST-40C Rev. 1",237,null,"Requirement",135]
["Recommendation",8,null,"Permission",2,null,"ECSS-Q-ST-10C Rev.1",71]
["Requirement",423,null,"Recommendation",1,null,"Permission",4]
["ECSS-E-ST-10-04C Rev.1",139,null,"Requirement",234,null,"Requirement",67]
["Permission",17,null,"ECSS-M-ST-60C",131,null,"ECSS-Q-ST-20-07C",183]
["Recommendation",4,null,"Permission",3,null,"Recommendation",1]
["Requirement",118,null,"Recommendation",6,null,"Requirement",182]
["ECSS-E-ST-10-06C",54,null,"Requirement",122,null,"ECSS-Q-ST-20-08C",140]
["Recommendation",6,null,"ECSS-M-ST-80C",66,null,"Recommendation",3]
["Requirement",48,null,"Permission",4,null,"Requirement",137]
["ECSS-E-ST-10-09C",92,null,"Recommendation",7,null,"ECSS-Q-ST-20-10C",139]
["Recommendation",5,null,"Requirement",55,null,"Requirement",139]
["Requirement",87,null,"Grand Total",587,null,"ECSS-Q-ST-20C Rev.2",239]
["ECSS-E-ST-10-11C",197,{"$nulls":4},"Permission",3]
["Requirement",197,{"$nulls":4},"Recommendation",1]
["ECSS-E-ST-10-12C",149,{"$nulls":4},"Requirement",235]
["Permission",6,{"$nulls":4},"ECSS-Q-ST-30-02C",181]
["Requirement",143,{"$nulls":4},"Permission",1]
["ECSS-E-ST-10-24C",76,{"$nulls":4},"Requirement",180]
["Permission",4,{"$nulls":4},"ECSS-Q-ST-30-09C",45]
["Requirement",72,{"$nulls":4},"Requirement",45]
["ECSS-E-ST-10C Rev.1",400,{"$nulls":4},"ECSS-Q-ST-30-11C Rev.1",133]
["Permission",2,{"$nulls":4},"Permission",2]
["Recommendation",2,{"$nulls":4},"Recommendation",14]
["Requirement",396,{"$nulls":4},"Requirement",117]
["ECSS-E-ST-20-01C",220,{"$nulls":4},"ECSS-Q-ST-30C Rev.1",144]
["Permission",20,{"$nulls":4},"Permission",8]
["Recommendation",3,{"$nulls":4},"Requirement",136]
["Requirement",197,{"$nulls":4},"ECSS-Q-ST-40-02C",11]
["ECSS-E-ST-20-06C Rev.1",172,{"$nulls":4},"Requirement",11]
["Permission",13,{"$nulls":4},"ECSS-Q-ST-40-12C",7]
["Recommendation",3,{"$nulls":4},"Requirement",7]
["Requirement",156,{"$nulls":4},"ECSS-Q-ST-40C Rev.1",328]
["ECSS-E-ST-20-07C Rev. 1",233,{"$nulls":4},"Permission",2]
["Permission",5,{"$nulls":4},"Requirement",326]
["Recommendation",2,{"$nulls":4},"ECSS-Q-ST-60-02C",196]
["Requirement",226,{"$nulls":4},"Permission",3]
["ECSS-E-ST-20-08C Rev. 1",1020,{"$nulls":4},"Recommendation",1]
["Permission",12,{"$nulls":4},"Requirement",192]
["Recommendation",26,{"$nulls":4},"ECSS-Q-ST-60-05C Rev. 1",221]
["Requirement",982,{"$nulls":4},"Permission",23]
["ECSS-E-ST-20-20C",124,{"$nulls":4},"Recommendation",1]
["Recommendation",10,{"$nulls":4},"Requirement",197]
["Requirement",114,{"$nulls":4},"ECSS-Q-ST-60-12C",218]
["ECSS-E-ST-20-21C",80,{"$nulls":4},"Permission",10]
["Permission",2,{"$nulls":4},"Recommendation",6]
["Recommendation",17,{"$nulls":4},"Requirement",202]
["Requirement",61,{"$nulls":4},"ECSS-Q-ST-60-13C",460]
["ECSS-E-ST-20C Rev.1",394,{"$nulls":4},"Permission",19]
["Permission",2,{"$nulls":4},"Requirement",441]
["Recommendation",21,{"$nulls":4},"ECSS-Q-ST-60-14C Rev.1 Corr.1",88]
["Requirement",371,{"$nulls":4},"Permission",2]
["ECSS-E-ST-31-02C Rev.1",272,{"$nulls":4},"Recommendation",1]
["Recommendation",1,{"$nulls":4},"Requirement",85]
["Requirement",271,{"$nulls":4},"ECSS-Q-ST-60-15C",105]
["ECSS-E-ST-31-04C",22,{"$nulls":4},"Permission",1]
["Permission",3,{"$nulls":4},"Recommendation",1]
["Recommendation",3,{"$nulls":4},"Requirement",103]
["Requirement",16,{"$nulls":4},"ECSS-Q-ST-60C Rev. 2",463]
["ECSS-E-ST-31C",232,{"$nulls":4},"Permission",30]
["Permission",1,{"$nulls":4},"Requirement",433]
["Requirement",231,{"$nulls":4},"ECSS-Q-ST-70-01C",253]
["ECSS-E-ST-32-01C Rev. 1",308,{"$nulls":4},"Recommendation",5]
["Permission",15,{"$nulls":4},"Requirement",248]
["Recommendation",2,{"$nulls":4},"ECSS-Q-ST-70-02C",152]
["Requirement",291,{"$nulls":4},"Recommendation",4]
["ECSS-E-ST-32-02C Rev. 1",418,{"$nulls":4},"Requirement",148]
["Permission",32,{"$nulls":4},"ECSS-Q-ST-70-03C",64]
["Requirement",386,{"$nulls":4},"Requirement",64]
["ECSS-E-ST-32-03C",45,{"$nulls":4},"ECSS-Q-ST-70-04C",58]
["Recommendation",2,{"$nulls":4},"Requirement",58]
["Requirement",43,{"$nulls":4},"ECSS-Q-ST-70-05C Rev.1",98]
["ECSS-E-ST-32-08C Rev. 1",77,{"$nulls":4},"Recommendation",1]
["Recommendation",1,{"$nulls":4},"Requirement",97]
["Requirement",76,{"$nulls":4},"ECSS-Q-ST-70-06C",80]
["ECSS-E-ST-32-10C Rev.2 Corr.1",28,{"$nulls":4},"Requirement",80]
["Requirement",28,{"$nulls":4},"ECSS-Q-ST-70-07C",84]
["ECSS-E-ST-32-11C",128,{"$nulls":4},"Requirement",84]
["Recommendation",9,{"$nulls":4},"ECSS-Q-ST-70-08C",513]
["Requirement",119,{"$nulls":4},"Permission",30]
["ECSS-E-ST-32C Rev. 1",750,{"$nulls":4},"Requirement",483]
["Permission",9,{"$nulls":4},"ECSS-Q-ST-70-09C",41]
["Recommendation",27,{"$nulls":4},"Requirement",41]
["Requirement",714,{"$nulls":4},"ECSS-Q-ST-70-12C",501]
["ECSS-E-ST-33-01C Rev.2",442,{"$nulls":4},"Permission",56]
["Permission",2,{"$nulls":4},"Recommendation",93]
["Recommendation",24,{"$nulls":4},"Requirement",352]
["Requirement",416,{"$nulls":4},"ECSS-Q-ST-70-13C Rev. 1",74]
["ECSS-E-ST-33-11C Rev.1",396,{"$nulls":4},"Permission",1]
["Permission",5,{"$nulls":4},"Recommendation",3]
["Recommendation",9,{"$nulls":4},"Requirement",70]
["Requirement",382,{"$nulls":4},"ECSS-Q-ST-70-14C",72]
["ECSS-E-ST-34C",229,{"$nulls":4},"Permission",5]
["Recommendation",1,{"$nulls":4},"Recommendation",1]
["Requirement",228,{"$nulls":4},"Requirement",66]
["ECSS-E-ST-35-01C",349,{"$nulls":4},"ECSS-Q-ST-70-17C",82]
["Permission",1,{"$nulls":4},"Permission",4]
["Recommendation",12,{"$nulls":4},"Requirement",78]
["Requirement",336,{"$nulls":4},"ECSS-Q-ST-70-18C",207]
["ECSS-E-ST-35-02C",166,{"$nulls":4},"Permission",3]
["Permission",3,{"$nulls":4},"Recommendation",6]
["Recommendation",6,{"$nulls":4},"Requirement",198]
["Requirement",157,{"$nulls":4},"ECSS-Q-ST-70-20C",34]
["ECSS-E-ST-35-03C",321,{"$nulls":4},"Permission",1]
["Recommendation",1,{"$nulls":4},"Requirement",33]
["Requirement",320,{"$nulls":4},"ECSS-Q-ST-70-21C",147]
["ECSS-E-ST-35-06C Rev.2",374,{"$nulls":4},"Permission",1]
["Permission",6,{"$nulls":4},"Recommendation",7]
["Recommendation",13,{"$nulls":4},"Requirement",139]
["Requirement",355,{"$nulls":4},"ECSS-Q-ST-70-22C",28]
["ECSS-E-ST-35-10C",179,{"$nulls":4},"Requirement",28]
["Permission",6,{"$nulls":4},"ECSS-Q-ST-70-26C Rev.1 Corr.1",213]
["Recommendation",2,{"$nulls":4},"Permission",4]
["Requirement",171,{"$nulls":4},"Recommendation",2]
["ECSS-E-ST-35C Rev. 1",403,{"$nulls":4},"Requirement",207]
["Recommendation",8,{"$nulls":4},"ECSS-Q-ST-70-28C",123]
["Requirement",395,{"$nulls":4},"Recommendation",28]
["ECSS-E-ST-40-07C",534,{"$nulls":4},"Requirement",95]
["Permission",2,{"$nulls":4},"ECSS-Q-ST-70-29C",67]
["Recommendation",1,{"$nulls":4},"Recommendation",1]
["Requirement",531,{"$nulls":4},"Requirement",66]
["ECSS-E-ST-40C",662,{"$nulls":4},"ECSS-Q-ST-70-30C",184]
["Permission",14,{"$nulls":4},"Recommendation",1]
["Recommendation",37,{"$nulls":4},"Requirement",183]
["Requirement",611,{"$nulls":4},"ECSS-Q-ST-70-31C Rev.1",107]
["ECSS-E-ST-50-01C",50,{"$nulls":4},"Permission",5]
["Permission",3,{"$nulls":4},"Requirement",102]
["Recommendation",2,{"$nulls":4},"ECSS-Q-ST-70-36C",55]
["Requirement",45,{"$nulls":4},"Permission",1]
["ECSS-E-ST-50-02C",91,{"$nulls":4},"Requirement",54]
["Permission",4,{"$nulls":4},"ECSS-Q-ST-70-37C",71]
["Recommendation",6,{"$nulls":4},"Recommendation",1]
["Requirement",81,{"$nulls":4},"Requirement",70]
["ECSS-E-ST-50-03C",135,{"$nulls":4},"ECSS-Q-ST-70-38C Rev.1 Corr.1",477]
["Permission",8,{"$nulls":4},"Permission",18]
["Requirement",127,{"$nulls":4},"Recommendation",5]
["ECSS-E-ST-50-04C",260,{"$nulls":4},"Requirement",454]
["Permission",9,{"$nulls":4},"ECSS-Q-ST-70-39C",236]
["Recommendation",4,{"$nulls":4},"Permission",6]
["Requirement",247,{"$nulls":4},"Recommendation",4]
["ECSS-E-ST-50-05C Rev. 2",242,{"$nulls":4},"Requirement",226]
["Permission",3,{"$nulls":4},"ECSS-Q-ST-70-45C",98]
["Recommendation",24,{"$nulls":4},"Recommendation",1]
["Requirement",215,{"$nulls":4},"Requirement",97]
["ECSS-E-ST-50-11C",1171,{"$nulls":4},"ECSS-Q-ST-70-46C Rev. 1",147]
["Permission",43,{"$nulls":4},"Requirement",147]
["Recommendation",46,{"$nulls":4},"ECSS-Q-ST-70-50C",219]
["Requirement",1082,{"$nulls":4},"Permission",1]
["ECSS-E-ST-50-12C Rev.1",534,{"$nulls":4},"Recommendation",21]
["Permission",11,{"$nulls":4},"Requirement",197]
["Recommendation",38,{"$nulls":4},"ECSS-Q-ST-70-53C",55]
["Requirement",485,{"$nulls":4},"Requirement",55]
["ECSS-E-ST-50-13C",180,{"$nulls":4},"ECSS-Q-ST-70-54C",54]
["Permission",9,{"$nulls":4},"Recommendation",2]
["Recommendation",3,{"$nulls":4},"Requirement",52]
["Requirement",168,{"$nulls":4},"ECSS-Q-ST-70-55C",36]
["ECSS-E-ST-50-14C",137,{"$nulls":4},"Permission",1]
["Permission",7,{"$nulls":4},"Requirement",35]
["Recommendation",8,{"$nulls":4},"ECSS-Q-ST-70-56C",43]
["Requirement",122,{"$nulls":4},"Requirement",43]
["ECSS-E-ST-50-15C",233,{"$nulls":4},"ECSS-Q-ST-70-57C",37]
["Permission",7,{"$nulls":4},"Requirement",37]
["Recommendation",9,{"$nulls":4},"ECSS-Q-ST-70-58C",70]
["Requirement",217,{"$nulls":4},"Recommendation",2]
["ECSS-E-ST-50-51C",14,{"$nulls":4},"Requirement",68]
["Permission",2,{"$nulls":4},"ECSS-Q-ST-70-60C Corr.1",773]
["Requirement",12,{"$nulls":4},"Permission",61]
["ECSS-E-ST-50-52C",360,{"$nulls":4},"Recommendation",65]
["Permission",9,{"$nulls":4},"Requirement",647]
["Recommendation",60,{"$nulls":4},"ECSS-Q-ST-70-71C Rev.1",245]
["Requirement",291,{"$nulls":4},"Recommendation",2]
["ECSS-E-ST-50-53C",51,{"$nulls":4},"Requirement",243]
["Permission",2,{"$nulls":4},"ECSS-Q-ST-70C Rev.2",257]
["Recommendation",2,{"$nulls":4},"Permission",4]
["Requirement",47,{"$nulls":4},"Recommendation",5]
["ECSS-E-ST-50C",221,{"$nulls":4},"Requirement",248]
["Permission",1,{"$nulls":4},"ECSS-Q-ST-80C Rev.1",313]
["Recommendation",12,{"$nulls":4},"Requirement",313]
["Requirement",208,{"$nulls":4},"Grand Total",9944]
["ECSS-E-ST-60-10C",39]
["Recommendation",4]
["Requirement",35]
["ECSS-E-ST-60-20C Rev. 2",189]
["Permission",3]
["Recommendation",6]
["Requirement",180]
["ECSS-E-ST-60-21C",235]
["Permission",4]
["Recommendation",2]
["Requirement",229]
["ECSS-E-ST-60-30C",141]
["Recommendation",2]
["Requirement",139]
["ECSS-E-ST-70-01C",140]
["Recommendation",1]
["Requirement",139]
["ECSS-E-ST-70-11C",348]
["Permission",1]
["Recommendation",17]
["Requirement",330]
["ECSS-E-ST-70-31C",186]
["Recommendation",6]
["Requirement",180]
["ECSS-E-ST-70-32C",51]
["Permission",12]
["Recommendation",11]
["Requirement",28]
["ECSS-E-ST-70-41C",3185]
["Permission",1]
["Recommendation",1]
["Requirement",3183]
["ECSS-E-ST-70C",359]
["Permission",8]
["Recommendation",3]
["Requirement",348]
["Grand Total",18867]

{"sheet":"Number of Active Modules","index":3,"n_rows":69,"n_cols":14,"rows_kept":69}
["Number of modules of Active ECSS Standards per Discipline contained in ECSS DOORS databe v0.8 (October 2020)"]
[]
["Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active",null,"Active or superseded ECSS","active"]
["ECSS Discipline","Engineering",null,"ECSS Discipline","Management",null,"ECSS Discipline","Product Assurance",null,"ECSS Discipline","Sustainability",null,"ECSS Discipline","System"]
["Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)",null,"Level 1 or Level 2 Standard","(All)"]
["Total of 61 DOORS modules",null,null,"Total of 5 DOORS modules",null,null,"Total of 60 DOORS modules",null,null,"Total of 1 DOORS modules",null,null,"Total of 1 DOORS modules"]
["Row Labels",null,null,"Row Labels",null,null,"Row Labels",null,null,"Row Labels",null,null,"Row Labels"]
["ECSS-E-ST-10-02C Rev.1",1,null,"ECSS-M-ST-10-01C",1,null,"ECSS-Q-ST-10-04C",1,null,"ECSS-U-ST-20C",1,null,"ECSS-S-ST-00C Rev.1",1]
["ECSS-E-ST-10-03C",2,null,"ECSS-M-ST-10C Rev. 1",2,null,"ECSS-Q-ST-10-09C Rev. 1",2,null,"Grand Total",null,null,"Grand Total"]
["ECSS-E-ST-10-04C Rev.1",3,null,"ECSS-M-ST-40C Rev. 1",3,null,"ECSS-Q-ST-10C Rev.1",3]
["ECSS-E-ST-10-06C",4,null,"ECSS-M-ST-60C",4,null,"ECSS-Q-ST-20-07C",4]
["ECSS-E-ST-10-09C",5,null,"ECSS-M-ST-80C",5,null,"ECSS-Q-ST-20-08C",5]
["ECSS-E-ST-10-11C",6,null,"Grand Total",null,null,"ECSS-Q-ST-20-10C",6]
["ECSS-E-ST-10-12C",7,{"$nulls":4},"ECSS-Q-ST-20C Rev.2",7]
["ECSS-E-ST-10-24C",8,{"$nulls":4},"ECSS-Q-ST-30-02C",8]
["ECSS-E-ST-10C Rev.1",9,{"$nulls":4},"ECSS-Q-ST-30-09C",9]
["ECSS-E-ST-20-01C",10,{"$nulls":4},"ECSS-Q-ST-30-11C Rev.1",10]
["ECSS-E-ST-20-06C Rev.1",11,{"$nulls":4},"ECSS-Q-ST-30C Rev.1",11]
["ECSS-E-ST-20-07C Rev. 1",12,{"$nulls":4},"ECSS-Q-ST-40-02C",12]
["ECSS-E-ST-20-08C Rev. 1",13,{"$nulls":4},"ECSS-Q-ST-40-12C",13]
["ECSS-E-ST-20-20C",14,{"$nulls":4},"ECSS-Q-ST-40C Rev.1",14]
["ECSS-E-ST-20-21C",15,{"$nulls":4},"ECSS-Q-ST-60-02C",15]
["ECSS-E-ST-20C Rev.1",16,{"$nulls":4},"ECSS-Q-ST-60-05C Rev. 1",16]
["ECSS-E-ST-31-02C Rev.1",17,{"$nulls":4},"ECSS-Q-ST-60-12C",17]
["ECSS-E-ST-31-04C",18,{"$nulls":4},"ECSS-Q-ST-60-13C",18]
["ECSS-E-ST-31C",19,{"$nulls":4},"ECSS-Q-ST-60-14C Rev.1 Corr.1",19]
["ECSS-E-ST-32-01C Rev. 1",20,{"$nulls":4},"ECSS-Q-ST-60-15C",20]
["ECSS-E-ST-32-02C Rev. 1",21,{"$nulls":4},"ECSS-Q-ST-60C Rev. 2",21]
["ECSS-E-ST-32-03C",22,{"$nulls":4},"ECSS-Q-ST-70-01C",22]
["ECSS-E-ST-32-08C Rev. 1",23,{"$nulls":4},"ECSS-Q-ST-70-02C",23]
["ECSS-E-ST-32-10C Rev.2 Corr.1",24,{"$nulls":4},"ECSS-Q-ST-70-03C",24]
["ECSS-E-ST-32-11C",25,{"$nulls":4},"ECSS-Q-ST-70-04C",25]
["ECSS-E-ST-32C Rev. 1",26,{"$nulls":4},"ECSS-Q-ST-70-05C Rev.1",26]
["ECSS-E-ST-33-01C Rev.2",27,{"$nulls":4},"ECSS-Q-ST-70-06C",27]
["ECSS-E-ST-33-11C Rev.1",28,{"$nulls":4},"ECSS-Q-ST-70-07C",28]
["ECSS-E-ST-34C",29,{"$nulls":4},"ECSS-Q-ST-70-08C",29]
["ECSS-E-ST-35-01C",30,{"$nulls":4},"ECSS-Q-ST-70-09C",30]
["ECSS-E-ST-35-02C",31,{"$nulls":4},"ECSS-Q-ST-70-12C",31]
["ECSS-E-ST-35-03C",32,{"$nulls":4},"ECSS-Q-ST-70-13C Rev. 1",32]
["ECSS-E-ST-35-06C Rev.2",33,{"$nulls":4},"ECSS-Q-ST-70-14C",33]
["ECSS-E-ST-35-10C",34,{"$nulls":4},"ECSS-Q-ST-70-17C",34]
["ECSS-E-ST-35C Rev. 1",35,{"$nulls":4},"ECSS-Q-ST-70-18C",35]
["ECSS-E-ST-40-07C",36,{"$nulls":4},"ECSS-Q-ST-70-20C",36]
["ECSS-E-ST-40C",37,{"$nulls":4},"ECSS-Q-ST-70-21C",37]
["ECSS-E-ST-50-01C",38,{"$nulls":4},"ECSS-Q-ST-70-22C",38]
["ECSS-E-ST-50-02C",39,{"$nulls":4},"ECSS-Q-ST-70-26C Rev.1 Corr.1",39]
["ECSS-E-ST-50-03C",40,{"$nulls":4},"ECSS-Q-ST-70-28C",40]
["ECSS-E-ST-50-04C",41,{"$nulls":4},"ECSS-Q-ST-70-29C",41]
["ECSS-E-ST-50-05C Rev. 2",42,{"$nulls":4},"ECSS-Q-ST-70-30C",42]
["ECSS-E-ST-50-11C",43,{"$nulls":4},"ECSS-Q-ST-70-31C Rev.1",43]
["ECSS-E-ST-50-12C Rev.1",44,{"$nulls":4},"ECSS-Q-ST-70-36C",44]
["ECSS-E-ST-50-13C",45,{"$nulls":4},"ECSS-Q-ST-70-37C",45]
["ECSS-E-ST-50-14C",46,{"$nulls":4},"ECSS-Q-ST-70-38C Rev.1 Corr.1",46]
["ECSS-E-ST-50-15C",47,{"$nulls":4},"ECSS-Q-ST-70-39C",47]
["ECSS-E-ST-50-51C",48,{"$nulls":4},"ECSS-Q-ST-70-45C",48]
["ECSS-E-ST-50-52C",49,{"$nulls":4},"ECSS-Q-ST-70-46C Rev. 1",49]
["ECSS-E-ST-50-53C",50,{"$nulls":4},"ECSS-Q-ST-70-50C",50]
["ECSS-E-ST-50C",51,{"$nulls":4},"ECSS-Q-ST-70-53C",51]
["ECSS-E-ST-60-10C",52,{"$nulls":4},"ECSS-Q-ST-70-54C",52]
["ECSS-E-ST-60-20C Rev. 2",53,{"$nulls":4},"ECSS-Q-ST-70-55C",53]
["ECSS-E-ST-60-21C",54,{"$nulls":4},"ECSS-Q-ST-70-56C",54]
["ECSS-E-ST-60-30C",55,{"$nulls":4},"ECSS-Q-ST-70-57C",55]
["ECSS-E-ST-70-01C",56,{"$nulls":4},"ECSS-Q-ST-70-58C",56]
["ECSS-E-ST-70-11C",57,{"$nulls":4},"ECSS-Q-ST-70-60C Corr.1",57]
["ECSS-E-ST-70-31C",58,{"$nulls":4},"ECSS-Q-ST-70-71C Rev.1",58]
["ECSS-E-ST-70-32C",59,{"$nulls":4},"ECSS-Q-ST-70C Rev.2",59]
["ECSS-E-ST-70-41C",60,{"$nulls":4},"ECSS-Q-ST-80C Rev.1",60]
["ECSS-E-ST-70C",61,{"$nulls":4},"Grand Total"]
["Grand Total"]