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["ECSS Source Reference","DOORS Project","ECSS Req. Identifier","Type","IE PUID","RCM Version","ECSS Change Status","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)"]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","4a","Requirement","ECSS-Q-ST-30-11_0140001",1,"Created","The user of this Standard shall verify that the ordered assurance level of procured components is compatible with the intended application."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2a","Requirement","ECSS-Q-ST-30-11_0140002",1,"Created","Derating shall be applied in consideration of temperature limits recommended."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2b","Requirement","ECSS-Q-ST-30-11_0140003",1,"Created","The derating requirements of this Standard shall not be used as a justification to upgrade the quality level of components."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2c","Requirement","ECSS-Q-ST-30-11_0140004",1,"Created","The derating requirements shall be taken into account at the beginning of the design cycle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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2d","Requirement","ECSS-Q-ST-30-11_0140005",1,"Created","Component families and groups excluded in this Standard are due to the lack of experimental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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2e","Requirement","ECSS-Q-ST-30-11_0140006",1,"Created","Components may be excluded from this Standard if they are used for short durations of less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. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2f","Requirement","ECSS-Q-ST-30-11_0140007",1,"Created","In the same way, during a test (e.g. qualification and EMC), derating requirements are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. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2g","Requirement","ECSS-Q-ST-30-11_0140008",1,"Created","Derating shall be applied on normal operating conditions and not on the fault condition. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.3.2h","Requirement","ECSS-Q-ST-30-11_0140009",1,"Created","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)."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.4.2a","Requirement","ECSS-Q-ST-30-11_0140010",1,"Created","If ratings are provided for transients or surge conditions, the same derating figures as for steady-state equivalent parameters shall be used."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.4.2b","Requirement","ECSS-Q-ST-30-11_0140011",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.4.2c","Requirement","ECSS-Q-ST-30-11_0140012",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.4.2d","Requirement","ECSS-Q-ST-30-11_0140013",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-30-11_0140014",1,"Created","For hybrids, individual components shall be in conformance with their respective derating rules."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.2.1a","Requirement","ECSS-Q-ST-30-11_0140015",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.2.1b","Permission","ECSS-Q-ST-30-11_0140079",1,"Created","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. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.2.1c","Recommendation","ECSS-Q-ST-30-11_0140080",1,"Created","Physical limitation for type II: maximum surge dV/dt approximate to 100 V/ms. This should be verified with the manufacturer."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.2.1d","Recommendation","ECSS-Q-ST-30-11_0140081",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1a","Requirement","ECSS-Q-ST-30-11_0140019",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1b","Requirement","ECSS-Q-ST-30-11_0140020",1,"Created","100 % surge current screening shall be applied for all surface mounted capacitors types."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1c","Requirement","ECSS-Q-ST-30-11_0140021",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1d","Requirement","ECSS-Q-ST-30-11_0140022",1,"Created","Reverse voltage shall not exceed 75 % of the manufacturer’s specified maximum value for the reverse voltage."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1e","Requirement","ECSS-Q-ST-30-11_0140023",1,"Created","Ripple power shall never exceed 50 % of the manufacturer’s specified maximum value."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.3.1f","Recommendation","ECSS-Q-ST-30-11_0140082",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.4.1a","Requirement","ECSS-Q-ST-30-11_0140025",1,"Created","Reverse voltage shall not exceed 75 % of the manufacturer’s specified maximum value for the reverse voltage."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.4.1b","Requirement","ECSS-Q-ST-30-11_0140026",1,"Created","Manufacturer’s ratings for ripple power or current shall never be exceeded. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.4.1c","Recommendation","ECSS-Q-ST-30-11_0140083",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.5.1a","Requirement","ECSS-Q-ST-30-11_0140028",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.5.1b","Requirement","ECSS-Q-ST-30-11_0140029",1,"Created","For other films, clearing recommendations from manufacturers shall be followed."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.5.1c","Recommendation","ECSS-Q-ST-30-11_0140084",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.6.1a","Recommendation","ECSS-Q-ST-30-11_0140085",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.7.1a","Recommendation","ECSS-Q-ST-30-11_0140086",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.8.1a","Recommendation","ECSS-Q-ST-30-11_0140087",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.9.1a","Recommendation","ECSS-Q-ST-30-11_0140088",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.10.1a","Recommendation","ECSS-Q-ST-30-11_0140089",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.11.1a","Requirement","ECSS-Q-ST-30-11_0140036",1,"Created","For power connectors, power and return lines shall be separated by at least one unassigned contact to reduce the short-circuit risk."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.11.1b","Requirement","ECSS-Q-ST-30-11_0140037",1,"Created","Connector savers shall be used during testing of equipment to minimize number of mating and demating cycles."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.11.1c","Requirement","ECSS-Q-ST-30-11_0140038",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.11.1d","Requirement","ECSS-Q-ST-30-11_0140039",1,"Created","The connector and its constituent parts shall be from the same manufacturer."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.12.1a","Requirement","ECSS-Q-ST-30-11_0140040",1,"Created","Connector savers shall be used during testing of equipment to minimize number of mating and demating cycles."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.14.1a","Requirement","ECSS-Q-ST-30-11_0140041",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.15.1a","Requirement","ECSS-Q-ST-30-11_0140042",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.17.1a","Requirement","ECSS-Q-ST-30-11_0140043",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.17.1b","Requirement","ECSS-Q-ST-30-11_0140044",1,"Created","The largest fuse rating compatible with the source capability shall be used."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.17.1c","Requirement","ECSS-Q-ST-30-11_0140045",1,"Created","The power supply shall be capable of delivering three times the specified fuse rated current in order to obtain short fusing times."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.18.1a","Requirement","ECSS-Q-ST-30-11_0140046",1,"Created","For custom-made inductors and transformers, the maximum rated temperature shall be evaluated taking into consideration the temperature characteristics of the materials used."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.19.1a","Requirement","ECSS-Q-ST-30-11_0140047",1,"Created","Some devices can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.20.1a","Requirement","ECSS-Q-ST-30-11_0140048",1,"Created","Some devices can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.21.1a","Requirement","ECSS-Q-ST-30-11_0140049",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.21.1b","Requirement","ECSS-Q-ST-30-11_0140050",1,"Created","Additional margins can be applied for radiation effects."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.22.1a","Requirement","ECSS-Q-ST-30-11_0140051",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.23.1a","Requirement","ECSS-Q-ST-30-11_0140052",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.23.2a","Requirement","ECSS-Q-ST-30-11_0140053",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.23.2b","Requirement","ECSS-Q-ST-30-11_0140054",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.24.1a","Requirement","ECSS-Q-ST-30-11_0140055",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.24.1b","Requirement","ECSS-Q-ST-30-11_0140056",1,"Created","Some integrated circuits can be radiation sensitive: this shall be recorded and approved in accordance with ECSS-Q-ST-60."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1a","Requirement","ECSS-Q-ST-30-11_0140057",1,"Created","The coil supply voltage shall be within the specified voltage range or between the specified rated and the maximum coil voltage."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1b","Requirement","ECSS-Q-ST-30-11_0140058",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1c","Requirement","ECSS-Q-ST-30-11_0140059",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1d","Requirement","ECSS-Q-ST-30-11_0140060",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1e","Requirement","ECSS-Q-ST-30-11_0140061",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1f","Requirement","ECSS-Q-ST-30-11_0140062",1,"Created","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. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.25.1g","Requirement","ECSS-Q-ST-30-11_0140063",1,"Created","Suppression diodes shall not be used inside relays. "]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.26.1.1a","Requirement","ECSS-Q-ST-30-11_0140064",1,"Created","The mentioned temperatures cited below refer to case temperatures."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.26.1.9a","Requirement","ECSS-Q-ST-30-11_0140065",1,"Created","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"]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.26.1.10a","Requirement","ECSS-Q-ST-30-11_0140066",1,"Created","If ratings are provided for transient or surge condition, the same derating figures as for steady-state equivalent parameters shall be used."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.26.1.10b","Requirement","ECSS-Q-ST-30-11_0140067",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.26.2a","Requirement","ECSS-Q-ST-30-11_0140068",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.28.1a","Requirement","ECSS-Q-ST-30-11_0140069",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.29.1a","Requirement","ECSS-Q-ST-30-11_0140070",1,"Created","Only SEE radiation characterized MOSFETs shall be used in space applications."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.29.1b","Requirement","ECSS-Q-ST-30-11_0140071",1,"Created","The user shall consider power cycling when this is critical to his application."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.30.1a","Requirement","ECSS-Q-ST-30-11_0140072",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.31.1a","Requirement","ECSS-Q-ST-30-11_0140073",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.33.1a","Requirement","ECSS-Q-ST-30-11_0140074",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.33.1b","Requirement","ECSS-Q-ST-30-11_0140075",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.33.1c","Requirement","ECSS-Q-ST-30-11_0140076",1,"Created","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."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.34.1a","Requirement","ECSS-Q-ST-30-11_0140077",1,"Created","For connectorized components, connector savers shall be used during testing of equipment to minimize number of mating and demating cycles."]
["ECSS-Q-ST-30-11C","ECSS - Superseded v0.9","6.36a","Requirement","ECSS-Q-ST-30-11_0140078",1,"Created","For hybrids, individual components shall be in conformance with their respective derating rules."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.1a","Requirement","ECSS-Q-ST-70-13_0610001",1,"Created","The supplier shall identify, manage and process materials and parts with hazardous characteristics according to ECSS-Q-ST-40."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.1b","Requirement","ECSS-Q-ST-70-13_0610002",1,"Created","The supplier shall keep the health and safety precautions according to the supplier’s national safety regulations."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1a","Requirement","ECSS-Q-ST-70-13_0610003",1,"Created","The supplier shall prepare the material samples according to the process specifications or manufacturer’s data."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1b","Requirement","ECSS-Q-ST-70-13_0610004",1,"Created","The material samples shall be representative of batch variance."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1c","Requirement","ECSS-Q-ST-70-13_0610005",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1d","Requirement","ECSS-Q-ST-70-13_0610006",1,"Created","The sample for testing shall have clean flat surfaces which do not overlap the sample holder described in clause 5.1.4."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1e","Requirement","ECSS-Q-ST-70-13_0610007",1,"Created","The width of the test sample surface face shall be at least equal to the width of the tape used in the test procedure."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1f","Requirement","ECSS-Q-ST-70-13_0610008",1,"Created","The nominal tape width shall be 20 mm."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1g","Requirement","ECSS-Q-ST-70-13_0610009",1,"Created","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.."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1h","Requirement","ECSS-Q-ST-70-13_0610010",1,"Created","The supplier shall test at least ten test samples."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1i","Requirement","ECSS-Q-ST-70-13_0610011",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1j","Requirement","ECSS-Q-ST-70-13_0610012",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.1k","Requirement","ECSS-Q-ST-70-13_0610013",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.2a","Requirement","ECSS-Q-ST-70-13_0610014",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.2b","Requirement","ECSS-Q-ST-70-13_0610015",1,"Created","The supplier shall not carry out further cleaning or other treatments."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.3a","Requirement","ECSS-Q-ST-70-13_0610016",1,"Created","The supplier shall handle the samples only with clean nylon or lint-free gloves."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.3b","Requirement","ECSS-Q-ST-70-13_0610017",1,"Created","The supplier shall store the samples in a controlled area, with an ambient temperature of (22 ± 3) °C and relative humidity of (55 ± 10) %."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.3c","Requirement","ECSS-Q-ST-70-13_0610018",1,"Created","The supplier shall shield coated surfaces from contact by using polyethylene or polypropylene bags or sheets."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.3d","Requirement","ECSS-Q-ST-70-13_0610019",1,"Created","The supplier shall avoid physical damage by packing the polyethylene or polypropylene-wrapped workpieces in clean, dust- and lint-free material."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.3e","Requirement","ECSS-Q-ST-70-13_0610020",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.4.1a","Requirement","ECSS-Q-ST-70-13_0610021",1,"Created","The supplier shall identify materials submitted for testing in conformance to annex A of ECSS-Q-ST-70-02."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.2.4.2a","Requirement","ECSS-Q-ST-70-13_0610022",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.3.1a","Requirement","ECSS-Q-ST-70-13_0610023",1,"Created","The work area shall be clean and free of dust."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.3.1b","Requirement","ECSS-Q-ST-70-13_0610024",1,"Created","The supplier shall filter the air used for ventilation to prevent contamination of the sample."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.3.2a","Requirement","ECSS-Q-ST-70-13_0610025",1,"Created","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"]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.1a","Requirement","ECSS-Q-ST-70-13_0610026",1,"Created","The supplier shall use the equipment as detailed in clauses 5.1.4.2 and 5.1.4.3."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.2a","Requirement","ECSS-Q-ST-70-13_0610027",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.2b","Requirement","ECSS-Q-ST-70-13_0610028",1,"Created","The machine shall have a fixed or essentially stationary member supporting a load cell and the tape holder."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.2c","Requirement","ECSS-Q-ST-70-13_0610029",1,"Created","A movable member shall carry the sample holder."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.2d","Requirement","ECSS-Q-ST-70-13_0610030",1,"Created","The applied compressive and tensile loads, as measured and recorded, shall be accurate within 1 percent of the load."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.2e","Requirement","ECSS-Q-ST-70-13_0610031",1,"Created","The rate of travel of the sample holder shall be at a nominal rate of 0,2 cm/min."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.3a","Recommendation","ECSS-Q-ST-70-13_0610074",1,"Created","The tape holder should be of a design similar to that depicted in Figure 5-1."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.3b","Requirement","ECSS-Q-ST-70-13_0610033",1,"Created","The part shall be screwed into the fixed member of the testing machine or be located firmly on it."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.3c","Requirement","ECSS-Q-ST-70-13_0610034",1,"Created","The supplier shall clamp a length of pressure-sensitive tape from one tape holder over the rubber block to the other tape holder."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.3d","Requirement","ECSS-Q-ST-70-13_0610035",1,"Created","The surface of the pressure-sensitive tape in contact with the flat surface of the rubber block shall be 4 cm2 ± 5 %."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.4a","Requirement","ECSS-Q-ST-70-13_0610036",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.4b","Requirement","ECSS-Q-ST-70-13_0610037",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.1.4.5a","Requirement","ECSS-Q-ST-70-13_0610038",1,"Created","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 %."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.1.1a","Requirement","ECSS-Q-ST-70-13_0610039",1,"Created","The supplier shall locate the test sample on the sample holder in conformance with the requirements stated in clause 5.1.4.3."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.1.1b","Requirement","ECSS-Q-ST-70-13_0610040",1,"Created","If an adhesive bond is used between the sample and the sample support, this shall in no way interfere with the area under test."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.1.1c","Requirement","ECSS-Q-ST-70-13_0610041",1,"Created","The supplier shall ensure that there is no physical or chemical interaction between any adhesive employed during sample preparation and the sample materials."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.1.2a","Requirement","ECSS-Q-ST-70-13_0610042",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.2a","Recommendation","ECSS-Q-ST-70-13_0610076",1,"Created","The supplier should run the peel and pull-off test as described in Annex B."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.2b","Requirement","ECSS-Q-ST-70-13_0610044",1,"Created","If the supplier uses a different procedure, the supplier shall submit it for customer approval."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.2.3a","Requirement","ECSS-Q-ST-70-13_0610045",1,"Created","The supplier shall apply the conditions specified in clause 5.1.2.3 unless other post test disposal instructions are given."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3a","Requirement","ECSS-Q-ST-70-13_0610046",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3b","Requirement","ECSS-Q-ST-70-13_0610047",1,"Created","The supplier shall examine samples in detail, which have been disturbed during the test sequence."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3c","Requirement","ECSS-Q-ST-70-13_0610048",1,"Created","The supplier shall carry out a visual examination for sample defects at ×7 magnification."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3d","Recommendation","ECSS-Q-ST-70-13_0610077",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3e","Requirement","ECSS-Q-ST-70-13_0610050",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3f","Requirement","ECSS-Q-ST-70-13_0610051",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3g","Requirement","ECSS-Q-ST-70-13_0610052",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3h","Requirement","ECSS-Q-ST-70-13_0610053",1,"Created","The supplier shall agree with the customer on the granularity level of failure analysis to be performed on failed samples, prior to the test."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.3i","Requirement","ECSS-Q-ST-70-13_0610054",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.1a","Requirement","ECSS-Q-ST-70-13_0610055",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.2a","Requirement","ECSS-Q-ST-70-13_0610056",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.3a","Requirement","ECSS-Q-ST-70-13_0610057",1,"Created","The supplier shall use only measuring equipment calibrated to traceable reference standard."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.3b","Requirement","ECSS-Q-ST-70-13_0610058",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.3c","Requirement","ECSS-Q-ST-70-13_0610059",1,"Created","The supplier shall notify the customer of the nonconformance details."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","5.4.4a","Requirement","ECSS-Q-ST-70-13_0610060",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1a","Requirement","ECSS-Q-ST-70-13_0610061",1,"Created","The test result sheet shall contain the trade names of the materials under test."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1b","Requirement","ECSS-Q-ST-70-13_0610062",1,"Created","The test result sheet shall contain the batch numbers of the materials under test."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1c","Requirement","ECSS-Q-ST-70-13_0610063",1,"Created","The test result sheet shall contain name of manufacturer or supplier through whom the purchase was made."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1d","Requirement","ECSS-Q-ST-70-13_0610064",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1e","Requirement","ECSS-Q-ST-70-13_0610065",1,"Created","The test result sheet shall contain details of the testing room environment conditions and test equipment."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1f","Requirement","ECSS-Q-ST-70-13_0610066",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1g","Requirement","ECSS-Q-ST-70-13_0610067",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1h","Requirement","ECSS-Q-ST-70-13_0610068",1,"Created","The test result sheet shall contain the number of sample tests."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1i","Requirement","ECSS-Q-ST-70-13_0610069",1,"Created","The test result sheet shall contain the results of the values obtained for peel or pull-off strength."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1j","Requirement","ECSS-Q-ST-70-13_0610070",1,"Created","The test result sheet shall contain the peel strength indicated by the manufacturer of the pressure-sensitive tape used."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1k","Requirement","ECSS-Q-ST-70-13_0610071",1,"Created","The test result sheet shall contain the results of any failure analysis carried out according to clause 5.3."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1l","Requirement","ECSS-Q-ST-70-13_0610072",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9","A.2.1m","Requirement","ECSS-Q-ST-70-13_0610073",1,"Created","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."]
["ECSS-Q-ST-70-13C","ECSS - Superseded v0.9",null,"Permission","ECSS-Q-ST-70-13_0610078",1,"Created","The supplier may use the template given in Figure A-1."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.1a","Requirement","ECSS-Q-ST-60_0480001",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.2.1a","Requirement","ECSS-Q-ST-60_0480002",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.2.1b","Requirement","ECSS-Q-ST-60_0480003",1,"Created","The supplier’s organization shall comply with all the requirements of ECSS-M-ST-10."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.2.2a","Requirement","ECSS-Q-ST-60_0480004",1,"Created","The supplier shall prepare a Component Control Plan (CCP) in conformance with its DRD in Annex A."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.2.2b","Permission","ECSS-Q-ST-60_0480446",1,"Created","The CCP may be part of the overall project PA plan."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.2.2c","Requirement","ECSS-Q-ST-60_0480006",1,"Created","The supplier shall submit the CCP to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.3a","Requirement","ECSS-Q-ST-60_0480007",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.3b","Requirement","ECSS-Q-ST-60_0480008",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.3c","Permission","ECSS-Q-ST-60_0480447",1,"Created","Other pertinent experts from the customer or suppliers may also participate, on request."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.3d","Requirement","ECSS-Q-ST-60_0480010",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4a","Requirement","ECSS-Q-ST-60_0480011",1,"Created","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4b","Requirement","ECSS-Q-ST-60_0480012",1,"Created","This list shall be kept under configuration control (issue and identification of changes). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4c","Requirement","ECSS-Q-ST-60_0480013",1,"Created","The DCL shall be issued as a minimum at PDR and CDR (as designed) and at flight hardware delivery (as built)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4d","Requirement","ECSS-Q-ST-60_0480014",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4e","Requirement","ECSS-Q-ST-60_0480015",1,"Created","The “as design” DCL shall be sent to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4f","Requirement","ECSS-Q-ST-60_0480016",1,"Created","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4g","Requirement","ECSS-Q-ST-60_0480017",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.4h","Requirement","ECSS-Q-ST-60_0480018",1,"Created","The content of the DCL shall be in conformance with its DRD in Annex B."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.5a","Requirement","ECSS-Q-ST-60_0480019",1,"Created","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.1.5b","Requirement","ECSS-Q-ST-60_0480020",1,"Created","Flight hardware connectors interfaces to GSE shall be protected by connector savers."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.1a","Requirement","ECSS-Q-ST-60_0480021",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1a","Requirement","ECSS-Q-ST-60_0480022",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1b","Requirement","ECSS-Q-ST-60_0480023",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1c","Requirement","ECSS-Q-ST-60_0480024",1,"Created","Preference shall be given to components which necessitate the least evaluation or qualification effort. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1d","Requirement","ECSS-Q-ST-60_0480025",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1e","Requirement","ECSS-Q-ST-60_0480026",1,"Created","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.1f","Requirement","ECSS-Q-ST-60_0480027",1,"Created","The supplier shall implement a type reduction activity."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2a","Requirement","ECSS-Q-ST-60_0480028",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2b","Requirement","ECSS-Q-ST-60_0480029",1,"Created","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2c","Requirement","ECSS-Q-ST-60_0480030",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2d","Requirement","ECSS-Q-ST-60_0480031",1,"Created","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,"]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2e","Requirement","ECSS-Q-ST-60_0480032",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2f","Permission","ECSS-Q-ST-60_0480448",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2g","Requirement","ECSS-Q-ST-60_0480034",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.2h","Requirement","ECSS-Q-ST-60_0480035",1,"Created","The use of pure tin (inside or outside the part) shall be declared in the PAD."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.3a","Requirement","ECSS-Q-ST-60_0480036",1,"Created","Parts shall be chosen from the EPPL part I."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.3b","Requirement","ECSS-Q-ST-60_0480037",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.3c","Requirement","ECSS-Q-ST-60_0480038",1,"Created","Parts subject to export restrictions or regulations shall not be preferred. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4a","Requirement","ECSS-Q-ST-60_0480039",1,"Created","The radiation requirements for EEE components are project specific."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4b","Requirement","ECSS-Q-ST-60_0480040",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4c","Requirement","ECSS-Q-ST-60_0480041",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4d","Requirement","ECSS-Q-ST-60_0480042",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4e","Requirement","ECSS-Q-ST-60_0480043",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4f","Requirement","ECSS-Q-ST-60_0480044",1,"Created","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4g","Requirement","ECSS-Q-ST-60_0480045",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4h","Requirement","ECSS-Q-ST-60_0480046",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.4i","Requirement","ECSS-Q-ST-60_0480047",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.5a","Requirement","ECSS-Q-ST-60_0480048",1,"Created","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.2.5b","Requirement","ECSS-Q-ST-60_0480049",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1a","Requirement","ECSS-Q-ST-60_0480050",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1b","Requirement","ECSS-Q-ST-60_0480051",1,"Created","The supplier shall plan and carry out the evaluation."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1c","Requirement","ECSS-Q-ST-60_0480052",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1d","Requirement","ECSS-Q-ST-60_0480053",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1e","Requirement","ECSS-Q-ST-60_0480054",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1f","Requirement","ECSS-Q-ST-60_0480055",1,"Created","Omission of any of these elements, or the introduction of alternative activities, shall be justified."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1g","Requirement","ECSS-Q-ST-60_0480056",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1h","Requirement","ECSS-Q-ST-60_0480057",1,"Created","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1i","Requirement","ECSS-Q-ST-60_0480058",1,"Created","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.1j","Requirement","ECSS-Q-ST-60_0480059",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.2.2a","Requirement","ECSS-Q-ST-60_0480060",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.2.2b","Requirement","ECSS-Q-ST-60_0480061",1,"Created","The complete manufacturer assessment, including the survey report and the associated corrective actions, shall be part of the evaluation report."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.3a","Requirement","ECSS-Q-ST-60_0480062",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.3b","Requirement","ECSS-Q-ST-60_0480063",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.3c","Requirement","ECSS-Q-ST-60_0480064",1,"Created","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.4a","Requirement","ECSS-Q-ST-60_0480065",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.3.4b","Requirement","ECSS-Q-ST-60_0480066",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.4a","Requirement","ECSS-Q-ST-60_0480067",1,"Created","The supplier shall document the procedure for approval of each component type intended for use in flight products. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.4b","Requirement","ECSS-Q-ST-60_0480068",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.4c","Requirement","ECSS-Q-ST-60_0480069",1,"Created","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.4d","Requirement","ECSS-Q-ST-60_0480070",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.2.4e","Requirement","ECSS-Q-ST-60_0480071",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1a","Requirement","ECSS-Q-ST-60_0480072",1,"Created","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1b","Requirement","ECSS-Q-ST-60_0480073",1,"Created","Class 1 components shall meet the quality levels ands supplementary conditions specified in Table 7-1."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1c","Requirement","ECSS-Q-ST-60_0480074",1,"Created","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1d","Requirement","ECSS-Q-ST-60_0480075",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1e","Requirement","ECSS-Q-ST-60_0480076",1,"Created","The supplier shall ensure the compatibility of the change with its application."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1f","Requirement","ECSS-Q-ST-60_0480077",1,"Created","The change shall be submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.1g","Requirement","ECSS-Q-ST-60_0480078",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2a","Requirement","ECSS-Q-ST-60_0480079",1,"Created","The supplier shall procure EEE components according to controlled specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2b","Requirement","ECSS-Q-ST-60_0480080",1,"Created","International specifications systems, recognized as suitable for space applications (e.g. ESCC, MIL), shall be used by the supplier. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2c","Requirement","ECSS-Q-ST-60_0480081",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2d","Requirement","ECSS-Q-ST-60_0480082",1,"Created","The content of any new specification shall be in conformance with Annex C."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2e","Requirement","ECSS-Q-ST-60_0480083",1,"Created","The use of any new specification shall be submitted to the customer for approval through the approval process (see clause 4.2.4) "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2f","Requirement","ECSS-Q-ST-60_0480084",1,"Created","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.2g","Requirement","ECSS-Q-ST-60_0480085",1,"Created","The supplier shall keep each procurement specification under configuration control."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.3a","Requirement","ECSS-Q-ST-60_0480086",1,"Created","All components to be incorporated into flight standard hardware shall be subjected to screening. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.3b","Requirement","ECSS-Q-ST-60_0480087",1,"Created","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.3c","Requirement","ECSS-Q-ST-60_0480088",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.3d","Requirement","ECSS-Q-ST-60_0480089",1,"Created","The applicable quality levels defined in Table 7-1 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.3e","Requirement","ECSS-Q-ST-60_0480090",1,"Created","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.4a","Requirement","ECSS-Q-ST-60_0480091",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.4b","Requirement","ECSS-Q-ST-60_0480092",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.4c","Requirement","ECSS-Q-ST-60_0480093",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.5a","Requirement","ECSS-Q-ST-60_0480094",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.5b","Requirement","ECSS-Q-ST-60_0480095",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.6a","Requirement","ECSS-Q-ST-60_0480096",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.6b","Requirement","ECSS-Q-ST-60_0480097",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.6c","Permission","ECSS-Q-ST-60_0480449",1,"Created","The buy-off may be replaced by an incoming inspection at the procurement entity's facilities."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.6d","Requirement","ECSS-Q-ST-60_0480099",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.7a","Requirement","ECSS-Q-ST-60_0480100",1,"Created","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.7b","Requirement","ECSS-Q-ST-60_0480101",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.7c","Requirement","ECSS-Q-ST-60_0480102",1,"Created","The incoming inspection shall be documented by a procedure to be sent, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.7d","Requirement","ECSS-Q-ST-60_0480103",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.7e","Requirement","ECSS-Q-ST-60_0480104",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.8a","Requirement","ECSS-Q-ST-60_0480105",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.8b","Requirement","ECSS-Q-ST-60_0480106",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.8c","Requirement","ECSS-Q-ST-60_0480107",1,"Created","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 4.2.4."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.8d","Requirement","ECSS-Q-ST-60_0480108",1,"Created","The results of RVT shall be documented by a report. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.8e","Requirement","ECSS-Q-ST-60_0480109",1,"Created","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9a","Requirement","ECSS-Q-ST-60_0480110",1,"Created","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)"]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9b","Requirement","ECSS-Q-ST-60_0480111",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9c","Requirement","ECSS-Q-ST-60_0480112",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9d","Requirement","ECSS-Q-ST-60_0480113",1,"Created","The DPA sample size may be reduced in some cases which shall be submitted to the customer for approval through the PAD process."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9e","Requirement","ECSS-Q-ST-60_0480114",1,"Created","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9f","Requirement","ECSS-Q-ST-60_0480115",1,"Created","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9g","Permission","ECSS-Q-ST-60_0480450",1,"Created","Independent laboratories may perform DPA when approved by the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9h","Permission","ECSS-Q-ST-60_0480451",1,"Created","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9i","Requirement","ECSS-Q-ST-60_0480118",1,"Created","For health and safety reasons, any test producing beryllium oxide dust shall be omitted."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.9j","Requirement","ECSS-Q-ST-60_0480119",1,"Created","The results of DPA shall be documented by a report sent to the customer, on request, for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.10a","Permission","ECSS-Q-ST-60_0480452",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.10b","Requirement","ECSS-Q-ST-60_0480121",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.11a","Requirement","ECSS-Q-ST-60_0480122",1,"Created","The manufacturer’s CoC shall be delivered to the parts procurer. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.11b","Requirement","ECSS-Q-ST-60_0480123",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.3.11c","Requirement","ECSS-Q-ST-60_0480124",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.4a","Requirement","ECSS-Q-ST-60_0480125",1,"Created","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.4b","Requirement","ECSS-Q-ST-60_0480126",1,"Created","The procedures shall be applicable at any facility dealing with components for flight application."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.4c","Requirement","ECSS-Q-ST-60_0480127",1,"Created","On request, handling and storage procedures shall be sent to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.4d","Requirement","ECSS-Q-ST-60_0480128",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.1a","Requirement","ECSS-Q-ST-60_0480129",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.2a","Requirement","ECSS-Q-ST-60_0480130",1,"Created","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.2b","Requirement","ECSS-Q-ST-60_0480131",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.2c","Requirement","ECSS-Q-ST-60_0480132",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.2d","Requirement","ECSS-Q-ST-60_0480133",1,"Created","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.3a","Requirement","ECSS-Q-ST-60_0480134",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.3b","Requirement","ECSS-Q-ST-60_0480135",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.3c","Requirement","ECSS-Q-ST-60_0480136",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.4a","Requirement","ECSS-Q-ST-60_0480137",1,"Created","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.4b","Requirement","ECSS-Q-ST-60_0480138",1,"Created","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.4c","Requirement","ECSS-Q-ST-60_0480139",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.4d","Requirement","ECSS-Q-ST-60_0480140",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.4e","Requirement","ECSS-Q-ST-60_0480141",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.5a","Requirement","ECSS-Q-ST-60_0480142",1,"Created","If tests are performed by sampling, the sampled parts shall be selected so that they are representative of the lot distribution. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.5.5b","Requirement","ECSS-Q-ST-60_0480143",1,"Created","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.1a","Requirement","ECSS-Q-ST-60_0480144",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.2a","Requirement","ECSS-Q-ST-60_0480145",1,"Created","ECSS-Q-ST-60-02 shall apply for the design development."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.3a","Requirement","ECSS-Q-ST-60_0480146",1,"Created","ECSS-Q-ST-60-05 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4a","Requirement","ECSS-Q-ST-60_0480147",1,"Created","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4b","Requirement","ECSS-Q-ST-60_0480148",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4c","Permission","ECSS-Q-ST-60_0480453",1,"Created","The programming process and the acceptance of the programmed parts may be part of PCB, for customer approval, if not indicated in the PAD."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4d","Requirement","ECSS-Q-ST-60_0480150",1,"Created","One time programmable components shall be submitted to a post-programming sequence. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4e","Requirement","ECSS-Q-ST-60_0480151",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4f","Requirement","ECSS-Q-ST-60_0480152",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4g","Requirement","ECSS-Q-ST-60_0480153",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.4h","Permission","ECSS-Q-ST-60_0480454",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.6.5a","Requirement","ECSS-Q-ST-60_0480155",1,"Created","ECSS-Q-ST-60-12 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","4.7a","Requirement","ECSS-Q-ST-60_0480156",1,"Created","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.1a","Requirement","ECSS-Q-ST-60_0480157",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.2.1a","Requirement","ECSS-Q-ST-60_0480158",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.2.2a","Requirement","ECSS-Q-ST-60_0480159",1,"Created","The supplier shall prepare a compliance matrix to the clauses of this standard. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.2.2b","Requirement","ECSS-Q-ST-60_0480160",1,"Created","The supplier shall submit his compliance matrix to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.3a","Requirement","ECSS-Q-ST-60_0480161",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.3b","Requirement","ECSS-Q-ST-60_0480162",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.3c","Permission","ECSS-Q-ST-60_0480455",1,"Created","Other pertinent experts from the customer or suppliers may also participate, on request."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.3d","Requirement","ECSS-Q-ST-60_0480164",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4a","Requirement","ECSS-Q-ST-60_0480165",1,"Created","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4b","Requirement","ECSS-Q-ST-60_0480166",1,"Created","This list shall be kept under configuration control (issue and identification of changes). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4c","Requirement","ECSS-Q-ST-60_0480167",1,"Created","The DCL shall be issued as a minimum at PDR and CDR (as designed) and at flight hardware delivery (as built)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4d","Requirement","ECSS-Q-ST-60_0480168",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4e","Requirement","ECSS-Q-ST-60_0480169",1,"Created","The “as design” DCL shall be sent to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4f","Requirement","ECSS-Q-ST-60_0480170",1,"Created","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4g","Requirement","ECSS-Q-ST-60_0480171",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.4h","Requirement","ECSS-Q-ST-60_0480172",1,"Created","The content of the DCL shall be in conformance with its DRD in Annex B."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.5a","Requirement","ECSS-Q-ST-60_0480173",1,"Created","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.1.5b","Requirement","ECSS-Q-ST-60_0480174",1,"Created","Flight hardware connectors interfaces to GSE shall be protected by connector savers."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-60_0480175",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.1a","Requirement","ECSS-Q-ST-60_0480176",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.1b","Requirement","ECSS-Q-ST-60_0480177",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.1c","Requirement","ECSS-Q-ST-60_0480178",1,"Created","Preference shall be given to components which necessitate the least evaluation or qualification effort. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.1d","Requirement","ECSS-Q-ST-60_0480179",1,"Created","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2a","Requirement","ECSS-Q-ST-60_0480180",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2b","Requirement","ECSS-Q-ST-60_0480181",1,"Created","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2c","Requirement","ECSS-Q-ST-60_0480182",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2d","Requirement","ECSS-Q-ST-60_0480183",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2e","Requirement","ECSS-Q-ST-60_0480184",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2f","Permission","ECSS-Q-ST-60_0480456",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2g","Requirement","ECSS-Q-ST-60_0480186",1,"Created","As per 5.2.2.2e., the justification of the use of pure tin shall be presented during a PCB for customer’s approval,"]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.2h","Requirement","ECSS-Q-ST-60_0480187",1,"Created","The use of pure tin (inside or outside the part) shall be declared in the PAD."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3a","Requirement","ECSS-Q-ST-60_0480188",1,"Created","The radiation requirements for EEE components are project specific."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3b","Requirement","ECSS-Q-ST-60_0480189",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3c","Requirement","ECSS-Q-ST-60_0480190",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3d","Requirement","ECSS-Q-ST-60_0480191",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3e","Requirement","ECSS-Q-ST-60_0480192",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3f","Requirement","ECSS-Q-ST-60_0480193",1,"Created","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3g","Requirement","ECSS-Q-ST-60_0480194",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3h","Requirement","ECSS-Q-ST-60_0480195",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.3i","Requirement","ECSS-Q-ST-60_0480196",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.4a","Requirement","ECSS-Q-ST-60_0480197",1,"Created","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.2.4b","Requirement","ECSS-Q-ST-60_0480198",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1a","Requirement","ECSS-Q-ST-60_0480199",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1b","Requirement","ECSS-Q-ST-60_0480200",1,"Created","The supplier shall plan and carry out the evaluation."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1c","Requirement","ECSS-Q-ST-60_0480201",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1d","Requirement","ECSS-Q-ST-60_0480202",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1e","Requirement","ECSS-Q-ST-60_0480203",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1f","Requirement","ECSS-Q-ST-60_0480204",1,"Created","Omission of any of these elements, or the introduction of alternative activities, shall be justified."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1g","Requirement","ECSS-Q-ST-60_0480205",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1h","Requirement","ECSS-Q-ST-60_0480206",1,"Created","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1i","Requirement","ECSS-Q-ST-60_0480207",1,"Created","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.1j","Requirement","ECSS-Q-ST-60_0480208",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.2a","Requirement","ECSS-Q-ST-60_0480209",1,"Created","A component manufacturer assessment is not required. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.3a","Requirement","ECSS-Q-ST-60_0480210",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.3b","Requirement","ECSS-Q-ST-60_0480211",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.3c","Requirement","ECSS-Q-ST-60_0480212",1,"Created","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.4a","Requirement","ECSS-Q-ST-60_0480213",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.3.4b","Requirement","ECSS-Q-ST-60_0480214",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.4a","Requirement","ECSS-Q-ST-60_0480215",1,"Created","The supplier shall document the procedure for approval of each component type intended for use in flight products. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.4b","Requirement","ECSS-Q-ST-60_0480216",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.4c","Requirement","ECSS-Q-ST-60_0480217",1,"Created","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.4d","Requirement","ECSS-Q-ST-60_0480218",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.2.4e","Requirement","ECSS-Q-ST-60_0480219",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1a","Requirement","ECSS-Q-ST-60_0480220",1,"Created","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1b","Requirement","ECSS-Q-ST-60_0480221",1,"Created","Class 2 components shall meet the quality levels and supplementary conditions specified in Table 7-2."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1c","Requirement","ECSS-Q-ST-60_0480222",1,"Created","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1d","Requirement","ECSS-Q-ST-60_0480223",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1e","Requirement","ECSS-Q-ST-60_0480224",1,"Created","The supplier shall ensure the compatibility of the change with its application."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1f","Requirement","ECSS-Q-ST-60_0480225",1,"Created","The change shall be submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.1g","Requirement","ECSS-Q-ST-60_0480226",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2a","Requirement","ECSS-Q-ST-60_0480227",1,"Created","The supplier shall procure EEE components according to controlled specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2b","Requirement","ECSS-Q-ST-60_0480228",1,"Created","International specifications systems, new specifications or manufacturer’s datasheets under configuration shall be used by the supplier. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2c","Requirement","ECSS-Q-ST-60_0480229",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2d","Requirement","ECSS-Q-ST-60_0480230",1,"Created","The content of any new specification shall be in conformance with Annex C."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2e","Requirement","ECSS-Q-ST-60_0480231",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2f","Requirement","ECSS-Q-ST-60_0480232",1,"Created","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.2g","Requirement","ECSS-Q-ST-60_0480233",1,"Created","The supplier shall keep each procurement specification or manufacturer’s datasheet under configuration control. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.3a","Requirement","ECSS-Q-ST-60_0480234",1,"Created","All components to be incorporated into flight standard hardware shall be subjected to screening. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.3b","Requirement","ECSS-Q-ST-60_0480235",1,"Created","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.3c","Requirement","ECSS-Q-ST-60_0480236",1,"Created","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.."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.3d","Requirement","ECSS-Q-ST-60_0480237",1,"Created","The applicable quality levels defined in Table 7-2 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.3e","Requirement","ECSS-Q-ST-60_0480238",1,"Created","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s review. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.4a","Requirement","ECSS-Q-ST-60_0480239",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.4b","Requirement","ECSS-Q-ST-60_0480240",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.5a","Requirement","ECSS-Q-ST-60_0480241",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.5b","Permission","ECSS-Q-ST-60_0480457",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.6a","Requirement","ECSS-Q-ST-60_0480243",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.6b","Requirement","ECSS-Q-ST-60_0480244",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.6c","Permission","ECSS-Q-ST-60_0480458",1,"Created","The buy-off may be replaced by an incoming inspection at the procurement entity's facilities; "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.6d","Requirement","ECSS-Q-ST-60_0480246",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.7a","Requirement","ECSS-Q-ST-60_0480247",1,"Created","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.7b","Requirement","ECSS-Q-ST-60_0480248",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.7c","Requirement","ECSS-Q-ST-60_0480249",1,"Created","The incoming inspection shall be documented by a procedure to be presented, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.7d","Requirement","ECSS-Q-ST-60_0480250",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.7e","Requirement","ECSS-Q-ST-60_0480251",1,"Created","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"]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.8a","Requirement","ECSS-Q-ST-60_0480252",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.8b","Requirement","ECSS-Q-ST-60_0480253",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.8c","Requirement","ECSS-Q-ST-60_0480254",1,"Created","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 5.2.4. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.8d","Requirement","ECSS-Q-ST-60_0480255",1,"Created","The results of RVT shall be documented by a report. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.8e","Requirement","ECSS-Q-ST-60_0480256",1,"Created","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9a","Requirement","ECSS-Q-ST-60_0480257",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9b","Requirement","ECSS-Q-ST-60_0480258",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9c","Requirement","ECSS-Q-ST-60_0480259",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9d","Requirement","ECSS-Q-ST-60_0480260",1,"Created","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9e","Requirement","ECSS-Q-ST-60_0480261",1,"Created","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9f","Permission","ECSS-Q-ST-60_0480459",1,"Created","Independent laboratories may perform DPA when approved by the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9g","Permission","ECSS-Q-ST-60_0480460",1,"Created","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9h","Requirement","ECSS-Q-ST-60_0480264",1,"Created","For health and safety reasons, any test producing beryllium oxide dust shall be omitted."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.9i","Requirement","ECSS-Q-ST-60_0480265",1,"Created","The results of DPA shall be documented by a report sent to the customer, on request, for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.10a","Permission","ECSS-Q-ST-60_0480461",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.10b","Requirement","ECSS-Q-ST-60_0480267",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.11a","Requirement","ECSS-Q-ST-60_0480268",1,"Created","The manufacturer’s CoC shall be delivered to the parts procurer. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.11b","Requirement","ECSS-Q-ST-60_0480269",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.3.11c","Requirement","ECSS-Q-ST-60_0480270",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.4a","Requirement","ECSS-Q-ST-60_0480271",1,"Created","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.4b","Requirement","ECSS-Q-ST-60_0480272",1,"Created","The procedures shall be applicable at any facility dealing with components for flight application."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.4c","Requirement","ECSS-Q-ST-60_0480273",1,"Created","On request, handling and storage procedures shall be sent to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.4d","Requirement","ECSS-Q-ST-60_0480274",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-Q-ST-60_0480275",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-60_0480276",1,"Created","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.2b","Requirement","ECSS-Q-ST-60_0480277",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.2c","Requirement","ECSS-Q-ST-60_0480278",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.2d","Requirement","ECSS-Q-ST-60_0480279",1,"Created","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.3a","Requirement","ECSS-Q-ST-60_0480280",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.3b","Requirement","ECSS-Q-ST-60_0480281",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.4a","Requirement","ECSS-Q-ST-60_0480282",1,"Created","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.4b","Requirement","ECSS-Q-ST-60_0480283",1,"Created","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.4c","Requirement","ECSS-Q-ST-60_0480284",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.4d","Requirement","ECSS-Q-ST-60_0480285",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.4e","Requirement","ECSS-Q-ST-60_0480286",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.5.5a","Requirement","ECSS-Q-ST-60_0480287",1,"Created","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.1a","Requirement","ECSS-Q-ST-60_0480288",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.2a","Requirement","ECSS-Q-ST-60_0480289",1,"Created","ECSS-Q-ST-60-02 shall apply for the design development. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.3a","Requirement","ECSS-Q-ST-60_0480290",1,"Created","ECSS-Q-ST-60-05 shall apply. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4a","Requirement","ECSS-Q-ST-60_0480291",1,"Created","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4b","Requirement","ECSS-Q-ST-60_0480292",1,"Created","The PAD shall allow traceability to the information related to the procurement of blank parts, the programming and the acceptance of the programmed parts."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4c","Permission","ECSS-Q-ST-60_0480462",1,"Created","The programming and the acceptance of the programmed parts may be part of PCB, for customer approval, if not indicated in the PAD."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4d","Requirement","ECSS-Q-ST-60_0480294",1,"Created","One time programmable components shall be submitted to a post-programming sequence. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4e","Requirement","ECSS-Q-ST-60_0480295",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4f","Requirement","ECSS-Q-ST-60_0480296",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4g","Requirement","ECSS-Q-ST-60_0480297",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.4h","Permission","ECSS-Q-ST-60_0480463",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.6.5a","Requirement","ECSS-Q-ST-60_0480299",1,"Created","ECSS-Q-ST-60-12 shall apply. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","5.7a","Requirement","ECSS-Q-ST-60_0480300",1,"Created","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.1a","Requirement","ECSS-Q-ST-60_0480301",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.2.1a","Requirement","ECSS-Q-ST-60_0480302",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.2.2a","Requirement","ECSS-Q-ST-60_0480303",1,"Created","The supplier shall prepare a compliance matrix to the clauses of this standard. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.2.2b","Requirement","ECSS-Q-ST-60_0480304",1,"Created","The supplier shall submit his compliance matrix to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.3a","Requirement","ECSS-Q-ST-60_0480305",1,"Created","A PCB is not required."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4a","Requirement","ECSS-Q-ST-60_0480306",1,"Created","For each equipment, its supplier shall issue a DCL in an editable electronic format, identifying all component types needed. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4b","Requirement","ECSS-Q-ST-60_0480307",1,"Created","The DCL shall be kept under configuration control (issue and identification of changes). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4c","Requirement","ECSS-Q-ST-60_0480308",1,"Created","The DCL shall be issued as a minimum at PDR and CDR (as designed) ."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4d","Requirement","ECSS-Q-ST-60_0480309",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4e","Requirement","ECSS-Q-ST-60_0480310",1,"Created","The “as design” DCL shall be sent to the customer for approval. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4f","Requirement","ECSS-Q-ST-60_0480311",1,"Created","Any change of parts during equipment manufacturing (e.g. type and manufacturer) shall be handled through RFWs submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.4g","Requirement","ECSS-Q-ST-60_0480312",1,"Created","The content of the DCL shall be in conformance with the DRD in Annex B."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.5a","Requirement","ECSS-Q-ST-60_0480313",1,"Created","EEE components used in GSE, which are physically and directly interfacing to flight hardware, shall meet the requirements of this document."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.1.5b","Requirement","ECSS-Q-ST-60_0480314",1,"Created","Flight hardware connectors interfaces to GSE shall be protected by connector savers."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.1a","Requirement","ECSS-Q-ST-60_0480315",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.1a","Requirement","ECSS-Q-ST-60_0480316",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.1b","Requirement","ECSS-Q-ST-60_0480317",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.1c","Requirement","ECSS-Q-ST-60_0480318",1,"Created","Preference shall be given to components which necessitate the least evaluation or qualification effort. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.1d","Requirement","ECSS-Q-ST-60_0480319",1,"Created","When selecting items, the supplier shall check the current data, applicability of the basis of qualification, problem notifications and alerts, and adequacy of specifications. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2a","Requirement","ECSS-Q-ST-60_0480320",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2b","Requirement","ECSS-Q-ST-60_0480321",1,"Created","The supplier shall evaluate the robustness of selected EEE components against the stresses induced by the assembly techniques to be employed."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2c","Requirement","ECSS-Q-ST-60_0480322",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2d","Requirement","ECSS-Q-ST-60_0480323",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2e","Requirement","ECSS-Q-ST-60_0480324",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2f","Permission","ECSS-Q-ST-60_0480464",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2g","Requirement","ECSS-Q-ST-60_0480326",1,"Created","As per 6.2.2.2e, the justification of the use of pure tin shall be presented during a PCB for customer’s approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.2h","Requirement","ECSS-Q-ST-60_0480327",1,"Created","The use of pure tin (inside or outside the part) shall be declared in the PAD."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.3a","Requirement","ECSS-Q-ST-60_0480328",1,"Created","Reference documents for the selection of components are not prescribed."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4a","Requirement","ECSS-Q-ST-60_0480329",1,"Created","The radiation requirements for EEE components are project specific."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4b","Requirement","ECSS-Q-ST-60_0480330",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4c","Requirement","ECSS-Q-ST-60_0480331",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4d","Requirement","ECSS-Q-ST-60_0480332",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4e","Requirement","ECSS-Q-ST-60_0480333",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4f","Requirement","ECSS-Q-ST-60_0480334",1,"Created","The supplier shall identify components which are not compliant with the radiation requirements as critical radiation sensitive components. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4g","Requirement","ECSS-Q-ST-60_0480335",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4h","Requirement","ECSS-Q-ST-60_0480336",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.4i","Requirement","ECSS-Q-ST-60_0480337",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.5a","Requirement","ECSS-Q-ST-60_0480338",1,"Created","The supplier shall implement derating rules for components used in his designs in accordance with the requirements of ECSS-Q-ST-30-11."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.2.5b","Requirement","ECSS-Q-ST-60_0480339",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1a","Requirement","ECSS-Q-ST-60_0480340",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1b","Requirement","ECSS-Q-ST-60_0480341",1,"Created","The supplier shall plan and carry out the evaluation."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1c","Requirement","ECSS-Q-ST-60_0480342",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1d","Requirement","ECSS-Q-ST-60_0480343",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1e","Requirement","ECSS-Q-ST-60_0480344",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1f","Requirement","ECSS-Q-ST-60_0480345",1,"Created","Omission of any of these elements, or the introduction of alternative activities, shall be justified."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1g","Requirement","ECSS-Q-ST-60_0480346",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1h","Requirement","ECSS-Q-ST-60_0480347",1,"Created","For programmable devices, the representativeness shall include the programming hardware tools and the compatibility of the software."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1i","Requirement","ECSS-Q-ST-60_0480348",1,"Created","The supplier shall review the evaluation results to determine their impact on the content of the procurement specification which shall be amended as necessary."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1j","Requirement","ECSS-Q-ST-60_0480349",1,"Created","The supplier shall summarize the evaluation results in the evaluation report and sent it to the customer for approval."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.1k","Requirement","ECSS-Q-ST-60_0480350",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.2a","Requirement","ECSS-Q-ST-60_0480351",1,"Created","A component manufacturer assessment is not required. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.3a","Requirement","ECSS-Q-ST-60_0480352",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.3b","Requirement","ECSS-Q-ST-60_0480353",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.3c","Requirement","ECSS-Q-ST-60_0480354",1,"Created","The findings of the analysis shall be contained within a Constructional Analysis Report and shall be included in the Evaluation Report."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.4a","Requirement","ECSS-Q-ST-60_0480355",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.3.4b","Requirement","ECSS-Q-ST-60_0480356",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.4a","Requirement","ECSS-Q-ST-60_0480357",1,"Created","The supplier shall document the procedure for approval of each component type intended for use in flight products. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.4b","Requirement","ECSS-Q-ST-60_0480358",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.4c","Requirement","ECSS-Q-ST-60_0480359",1,"Created","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.4d","Requirement","ECSS-Q-ST-60_0480360",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.2.4e","Requirement","ECSS-Q-ST-60_0480361",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.1a","Requirement","ECSS-Q-ST-60_0480362",1,"Created","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.1b","Requirement","ECSS-Q-ST-60_0480363",1,"Created","Class 3 components shall meet the quality levels and supplementary conditions specified in Table 7-3."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.1c","Requirement","ECSS-Q-ST-60_0480364",1,"Created","The supplier shall be responsible for manufacturer surveillance and control throughout the procurement programme."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.1d","Requirement","ECSS-Q-ST-60_0480365",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2a","Requirement","ECSS-Q-ST-60_0480366",1,"Created","The supplier shall procure EEE components according to controlled specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2b","Requirement","ECSS-Q-ST-60_0480367",1,"Created","International specifications systems, new specifications or manufacturer’s datasheets under configuration shall be used by the supplier. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2c","Requirement","ECSS-Q-ST-60_0480368",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2d","Requirement","ECSS-Q-ST-60_0480369",1,"Created","The content of any new specification shall be in conformance with the procurement specification DRD in Annex C."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2e","Requirement","ECSS-Q-ST-60_0480370",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2f","Requirement","ECSS-Q-ST-60_0480371",1,"Created","Upon request, any new procurement specification prepared in the frame of the project, shall be delivered to the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.2g","Requirement","ECSS-Q-ST-60_0480372",1,"Created","The supplier shall keep each procurement specification or manufacturer’s datasheet under configuration control."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.3a","Requirement","ECSS-Q-ST-60_0480373",1,"Created","All components to be incorporated into flight standard hardware shall be subjected to screening."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.3b","Requirement","ECSS-Q-ST-60_0480374",1,"Created","The screening test requirements shall be so designed that accumulated stress does not jeopardize component reliability. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.3c","Requirement","ECSS-Q-ST-60_0480375",1,"Created","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 ."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.3d","Requirement","ECSS-Q-ST-60_0480376",1,"Created","The applicable quality levels defined in Table 7-3 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.3e","Requirement","ECSS-Q-ST-60_0480377",1,"Created","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s review. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.4a","Requirement","ECSS-Q-ST-60_0480378",1,"Created","A customer precap is not required."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.5a","Requirement","ECSS-Q-ST-60_0480379",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.5b","Requirement","ECSS-Q-ST-60_0480380",1,"Created","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)"]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.6a","Requirement","ECSS-Q-ST-60_0480381",1,"Created","A buy-off is not required."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.7a","Requirement","ECSS-Q-ST-60_0480382",1,"Created","The procurement entity shall perform incoming inspection at his premises on all components to verify conformance with the purchase order requirements."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.7b","Requirement","ECSS-Q-ST-60_0480383",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.7c","Requirement","ECSS-Q-ST-60_0480384",1,"Created","The incoming inspection shall be documented by a procedure to be presented, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.7d","Requirement","ECSS-Q-ST-60_0480385",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.7e","Requirement","ECSS-Q-ST-60_0480386",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.8a","Requirement","ECSS-Q-ST-60_0480387",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.8b","Requirement","ECSS-Q-ST-60_0480388",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.8c","Requirement","ECSS-Q-ST-60_0480389",1,"Created","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 6.2.4."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.8d","Requirement","ECSS-Q-ST-60_0480390",1,"Created","The results of RVT shall be documented by a report. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.8e","Requirement","ECSS-Q-ST-60_0480391",1,"Created","When RVT is performed in the frame of the project, the supplier shall send the related report to the customer for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9a","Requirement","ECSS-Q-ST-60_0480392",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9b","Requirement","ECSS-Q-ST-60_0480393",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9c","Requirement","ECSS-Q-ST-60_0480394",1,"Created","The DPA sample size may be reduced in some cases which shall be submitted to the customer for approval through the PAD process."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9d","Requirement","ECSS-Q-ST-60_0480395",1,"Created","The DPA process shall be documented by a procedure to be sent, on request, to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9e","Requirement","ECSS-Q-ST-60_0480396",1,"Created","The supplier shall verify that the outcome of the DPA is satisfactory prior to the installation of the components into flight hardware."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9f","Permission","ECSS-Q-ST-60_0480465",1,"Created","Independent laboratories may perform DPA when approved by the customer."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9g","Permission","ECSS-Q-ST-60_0480466",1,"Created","DPA may be performed by the manufacturer if witnessed by the supplier (or approved representative)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9h","Requirement","ECSS-Q-ST-60_0480399",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9i","Requirement","ECSS-Q-ST-60_0480400",1,"Created","For health and safety reasons, any test producing beryllium oxide dust shall be omitted."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.9j","Requirement","ECSS-Q-ST-60_0480401",1,"Created","The results of DPA shall be documented by a report sent to the customer, on request, for information."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.10a","Permission","ECSS-Q-ST-60_0480467",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.10b","Requirement","ECSS-Q-ST-60_0480403",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.11a","Requirement","ECSS-Q-ST-60_0480404",1,"Created","The manufacturer’s CoC shall be delivered to the parts procurer. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.11b","Requirement","ECSS-Q-ST-60_0480405",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.3.11c","Requirement","ECSS-Q-ST-60_0480406",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.4a","Requirement","ECSS-Q-ST-60_0480407",1,"Created","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.4b","Requirement","ECSS-Q-ST-60_0480408",1,"Created","The procedures shall be applicable at any facility dealing with components for flight application."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.4c","Requirement","ECSS-Q-ST-60_0480409",1,"Created","On request, these procedures shall be sent to the customer for review."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.4d","Requirement","ECSS-Q-ST-60_0480410",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.1a","Requirement","ECSS-Q-ST-60_0480411",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.2a","Requirement","ECSS-Q-ST-60_0480412",1,"Created","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-20."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.2b","Requirement","ECSS-Q-ST-60_0480413",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.2c","Requirement","ECSS-Q-ST-60_0480414",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.2d","Requirement","ECSS-Q-ST-60_0480415",1,"Created","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.3a","Requirement","ECSS-Q-ST-60_0480416",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.3b","Requirement","ECSS-Q-ST-60_0480417",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.4a","Requirement","ECSS-Q-ST-60_0480418",1,"Created","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.4b","Requirement","ECSS-Q-ST-60_0480419",1,"Created","The traceability shall be maintained through incoming, storage, and installation at the procurer and user of the component in accordance with programme PA requirements. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.4c","Requirement","ECSS-Q-ST-60_0480420",1,"Created","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). "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.4d","Requirement","ECSS-Q-ST-60_0480421",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.4e","Requirement","ECSS-Q-ST-60_0480422",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.5.5a","Requirement","ECSS-Q-ST-60_0480423",1,"Created","For radiation tests, the set of test samples used shall be a representative distribution for the wafer lot. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.1a","Requirement","ECSS-Q-ST-60_0480424",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.2a","Requirement","ECSS-Q-ST-60_0480425",1,"Created","ECSS-Q-60-02 shall apply for the design development."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.3a","Requirement","ECSS-Q-ST-60_0480426",1,"Created","ECSS-Q-ST-60-05 shall apply."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4a","Requirement","ECSS-Q-ST-60_0480427",1,"Created","For FPGA, ECSS-Q-ST-60-02, shall apply for the design development. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4b","Requirement","ECSS-Q-ST-60_0480428",1,"Created","The PAD shall allow traceability to the information related to the procurement of blank parts, the programming and the acceptance of the programmed parts."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4c","Permission","ECSS-Q-ST-60_0480468",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4d","Requirement","ECSS-Q-ST-60_0480430",1,"Created","One time programmable components shall be submitted to a post-programming sequence. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4e","Requirement","ECSS-Q-ST-60_0480431",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4f","Requirement","ECSS-Q-ST-60_0480432",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4g","Requirement","ECSS-Q-ST-60_0480433",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.4h","Permission","ECSS-Q-ST-60_0480469",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.6.5a","Requirement","ECSS-Q-ST-60_0480435",1,"Created","ECSS-Q-ST-60-12 shall apply. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","6.7a","Requirement","ECSS-Q-ST-60_0480436",1,"Created","Any result from inspection or control shall be documented (including, precap, lot acceptance, buy-off, incoming, relifing and complementary tests)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","A.2.1a","Requirement","ECSS-Q-ST-60_0480437",1,"Created","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. "]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","A.2.2a","Permission","ECSS-Q-ST-60_0480470",1,"Created","In conformance with 4.2.2.1b the CCP may be part of the overall project PA plan."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","B.2.1a","Requirement","ECSS-Q-ST-60_0480439",1,"Created","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)."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","C.2.1a","Requirement","ECSS-Q-ST-60_0480440",1,"Created","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."]
["ECSS-Q-ST-60C Rev. 1","ECSS - Superseded v0.9","D.2a","Requirement","ECSS-Q-ST-60_0480441",1,"Created","The information given in Table D-1 shall be provided."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.1a","Requirement","ECSS-Q-ST-20_0380001",1,"Created","The supplier shall prepare, maintain and implement a QA plan in conformance with the DRD in Annex A."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.1b","Requirement","ECSS-Q-ST-20_0380002",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.2a","Requirement","ECSS-Q-ST-20_0380003",1,"Created","The supplier shall establish a documented training programme for the personnel whose performance determines or affects product quality."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.2b","Requirement","ECSS-Q-ST-20_0380004",1,"Created","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”."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.2c","Requirement","ECSS-Q-ST-20_0380005",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.1.2d","Requirement","ECSS-Q-ST-20_0380006",1,"Created","The supplier shall maintain records of the training."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-20_0380007",1,"Created","The supplier shall implement Critical-items control in conformance with ECSS-Q-ST-10-04."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.2a","Requirement","ECSS-Q-ST-20_0380008",1,"Created","The supplier shall implement a nonconformance control system in conformance with ECSS-Q-ST-10-09."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.3a","Requirement","ECSS-Q-ST-20_0380009",1,"Created","The supplier shall manage alerts in conformance with ECSS-Q-ST-10, clause 5.2.9."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4a","Requirement","ECSS-Q-ST-20_0380010",1,"Created","The supplier shall establish and maintain a documented stamp control system to ensure the correct and legitimate use of all fabrication and inspection stamps."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4b","Requirement","ECSS-Q-ST-20_0380011",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4c","Requirement","ECSS-Q-ST-20_0380012",1,"Created","The use of stamps shall be restricted to authorized personnel as identified in the stamp control system."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4d","Requirement","ECSS-Q-ST-20_0380013",1,"Created","Stamps shall be traceable to individuals responsible for their use."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4e","Requirement","ECSS-Q-ST-20_0380014",1,"Created","Stamps shall be applied directly to parts and materials, when specified by engineering drawings and specifications, and associated documents, records, labels."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4f","Requirement","ECSS-Q-ST-20_0380015",1,"Created","Stamping materials and methods shall be compatible with the articles and their use."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.4g","Permission","ECSS-Q-ST-20_0380225",1,"Created","Signatures instead of stamps may be used provided that similar traceability and responsibility records are maintained and available."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.5a","Requirement","ECSS-Q-ST-20_0380017",1,"Created","The supplier shall ensure that a bidirectional and unequivocal relationship between parts, materials or products and associated documentation or records is established and maintained."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.5b","Requirement","ECSS-Q-ST-20_0380018",1,"Created","The supplier shall be capable to trace data, personnel and equipment related to procurement, manufacturing, inspection, test, assembly, integration and operations activities."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.5c","Requirement","ECSS-Q-ST-20_0380019",1,"Created","The supplier shall be capable to trace backward the locations of materials, parts, sub-assemblies."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.5d","Requirement","ECSS-Q-ST-20_0380020",1,"Created","The supplier shall be capable to trace forward the locations of materials from raw stock."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.5e","Requirement","ECSS-Q-ST-20_0380021",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6a","Requirement","ECSS-Q-ST-20_0380022",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6b","Requirement","ECSS-Q-ST-20_0380023",1,"Created","The supplier shall use equipment in a manner which ensures that measurement uncertainty is known and is consistent with the specified measurement capability."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6c","Requirement","ECSS-Q-ST-20_0380024",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6d","Requirement","ECSS-Q-ST-20_0380025",1,"Created","The supplier shall record the basis for the calculation of the cumulative errors as specified in requirement 5.2.6c."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6e","Requirement","ECSS-Q-ST-20_0380026",1,"Created","The supplier shall select inspection, measuring and test equipment in conformance with the required measurement accuracy and precision."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6f","Requirement","ECSS-Q-ST-20_0380027",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6g","Requirement","ECSS-Q-ST-20_0380028",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6h","Requirement","ECSS-Q-ST-20_0380029",1,"Created","The supplier shall ensure that the inspection, measuring and test equipment is capable of the specified accuracy and precision."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6i","Requirement","ECSS-Q-ST-20_0380030",1,"Created","The supplier shall identify inspection, measuring and test equipment with a suitable indicator or approved identification record to show the calibration status."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6j","Requirement","ECSS-Q-ST-20_0380031",1,"Created","The supplier shall maintain calibration records for inspection, measuring and test equipment."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6k","Requirement","ECSS-Q-ST-20_0380032",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6l","Requirement","ECSS-Q-ST-20_0380033",1,"Created","The supplier shall ensure that the environmental conditions are suitable for the calibrations, inspections, measurements and tests being carried out."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6m","Requirement","ECSS-Q-ST-20_0380034",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6n","Requirement","ECSS-Q-ST-20_0380035",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6o","Requirement","ECSS-Q-ST-20_0380036",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6p","Requirement","ECSS-Q-ST-20_0380037",1,"Created","The supplier shall establish the extent and frequency of such checks and shall maintain records as evidence of control."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.6q","Requirement","ECSS-Q-ST-20_0380038",1,"Created","The supplier shall make the measurement design data available to the customer upon request."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.1a","Requirement","ECSS-Q-ST-20_0380039",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.2a","Requirement","ECSS-Q-ST-20_0380040",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.2b","Requirement","ECSS-Q-ST-20_0380041",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.2c","Requirement","ECSS-Q-ST-20_0380042",1,"Created","Each segregated area shall be identified and labelled for its intended use."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.2d","Requirement","ECSS-Q-ST-20_0380043",1,"Created","The supplier shall maintain control over acceptance into and withdrawal from storage areas."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.2e","Requirement","ECSS-Q-ST-20_0380044",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.7.3a","Requirement","ECSS-Q-ST-20_0380045",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.8.1a","Requirement","ECSS-Q-ST-20_0380046",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.8.1b","Requirement","ECSS-Q-ST-20_0380047",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.8.1c","Requirement","ECSS-Q-ST-20_0380048",1,"Created","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. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.8.2a","Requirement","ECSS-Q-ST-20_0380049",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.2.8.2b","Requirement","ECSS-Q-ST-20_0380050",1,"Created","The supplier shall maintain records of the sampling tests, together with the identification of the characteristics to which sampling is applied."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.1.1a","Requirement","ECSS-Q-ST-20_0380051",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.1.2a","Requirement","ECSS-Q-ST-20_0380052",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.1.3a","Requirement","ECSS-Q-ST-20_0380053",1,"Created","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)."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.1.4a","Requirement","ECSS-Q-ST-20_0380054",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.1a","Requirement","ECSS-Q-ST-20_0380055",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.1b","Requirement","ECSS-Q-ST-20_0380056",1,"Created","The supplier shall ensure that top-down requirement allocations and bottom-up requirement verifications are complete and consistent."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.1c","Requirement","ECSS-Q-ST-20_0380057",1,"Created","The supplier shall ensure that a system for tracking requirements and verification of results is established and maintained during the whole project life cycle."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.1d","Requirement","ECSS-Q-ST-20_0380058",1,"Created","The supplier shall ensure that verification methods are adequate and consistent with the type and criticality of the requirements."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.1e","Requirement","ECSS-Q-ST-20_0380059",1,"Created","The supplier shall ensure that appropriate reference to the verification documentation is recorded and status updated at project reviews up to final acceptance."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.2a","Requirement","ECSS-Q-ST-20_0380060",1,"Created","The supplier shall ensure that the objectives of the analysis are defined in relation with the development logic defined in the verification plan."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.2b","Requirement","ECSS-Q-ST-20_0380061",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.3a","Requirement","ECSS-Q-ST-20_0380062",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.1a","Requirement","ECSS-Q-ST-20_0380063",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.1b","Requirement","ECSS-Q-ST-20_0380064",1,"Created","The supplier QA shall review and approve the qualification plan."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.1c","Requirement","ECSS-Q-ST-20_0380065",1,"Created","The supplier QA shall review and approve the qualification results."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.2a","Requirement","ECSS-Q-ST-20_0380066",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.2b","Requirement","ECSS-Q-ST-20_0380067",1,"Created","Any difference in definition with respect to the reference product and any difference in the required qualification tests shall be identified."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.2c","Requirement","ECSS-Q-ST-20_0380068",1,"Created","The need for complementary qualification tests shall be analysed and the decision justified and submitted to the customer for approval."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.2d","Requirement","ECSS-Q-ST-20_0380069",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.3a","Requirement","ECSS-Q-ST-20_0380070",1,"Created","The product used for qualification testing shall be produced in accordance with a full and clearly identified manufacturing and inspection file. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.3b","Requirement","ECSS-Q-ST-20_0380071",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.4a","Requirement","ECSS-Q-ST-20_0380072",1,"Created","The supplier shall report the qualification status in conformance with the “Qualification status list” DRD as defined in ECSS-Q-ST-10."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.4.5a","Requirement","ECSS-Q-ST-20_0380073",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.3.2.5a","Requirement","ECSS-Q-ST-20_0380074",1,"Created","The supplier shall ensure that all design changes and modifications are identified, documented, reviewed and approved before their implementation."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.1.1a","Requirement","ECSS-Q-ST-20_0380075",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.1.2a","Requirement","ECSS-Q-ST-20_0380076",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.1.2b","Requirement","ECSS-Q-ST-20_0380077",1,"Created","The supplier shall document and maintain on file results of supplier selection process."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.1.3a","Requirement","ECSS-Q-ST-20_0380078",1,"Created","The supplier shall establish and maintain records of all procurement sources involved in business agreement performance."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.1.3b","Requirement","ECSS-Q-ST-20_0380079",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.2a","Requirement","ECSS-Q-ST-20_0380080",1,"Created","The supplier shall ensure that supplies are identified and that all applicable requirements are defined in the procurement documents."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.2b","Requirement","ECSS-Q-ST-20_0380081",1,"Created","The supplier shall ensure that requirements to those contained in lower tier procurement documents are traceable."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.2c","Requirement","ECSS-Q-ST-20_0380082",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.2d","Requirement","ECSS-Q-ST-20_0380083",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.3a","Requirement","ECSS-Q-ST-20_0380084",1,"Created","The supplier shall exercise surveillance over all the activities carried out by lower level suppliers during business agreement performance."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.3b","Requirement","ECSS-Q-ST-20_0380085",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.3c","Requirement","ECSS-Q-ST-20_0380086",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.3d","Requirement","ECSS-Q-ST-20_0380087",1,"Created","The supplier shall ensure that each of his suppliers implements surveillance on their lower level suppliers, in accordance with the same criteria."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.3e","Permission","ECSS-Q-ST-20_0380226",1,"Created","Surveillance may be delegated by the customer to third parties."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.1a","Requirement","ECSS-Q-ST-20_0380089",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.1b","Requirement","ECSS-Q-ST-20_0380090",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.1c","Requirement","ECSS-Q-ST-20_0380091",1,"Created","Receiving inspectors shall have available the procurement documents, specifications, drawings and any other document relevant to incoming supplies as required in the procurement documents."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.2a","Requirement","ECSS-Q-ST-20_0380092",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.3a","Requirement","ECSS-Q-ST-20_0380093",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.4.4.4a","Requirement","ECSS-Q-ST-20_0380094",1,"Created","The supplier shall maintain receiving inspection records to ensure traceability and the availability of historical data to monitor supplier performance and quality trends."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-Q-ST-20_0380095",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1b","Requirement","ECSS-Q-ST-20_0380096",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1c","Requirement","ECSS-Q-ST-20_0380097",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1d","Requirement","ECSS-Q-ST-20_0380098",1,"Created","The supplier shall issue and maintain manufacturing, assembly and integration documents in accordance with established and formal procedures."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1e","Requirement","ECSS-Q-ST-20_0380099",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1f","Requirement","ECSS-Q-ST-20_0380100",1,"Created","Only “first off” shop travellers shall be reviewed unless subsequent travellers incorporate a significant change of inspection requirements or order of events."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.1g","Requirement","ECSS-Q-ST-20_0380101",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-20_0380102",1,"Created","The supplier shall perform an internal review of the readiness for manufacturing, prior to starting the manufacture of the first flight-standard product."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.2b","Requirement","ECSS-Q-ST-20_0380103",1,"Created","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"]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.1a","Requirement","ECSS-Q-ST-20_0380104",1,"Created","The supplier shall monitor all processes used for manufacturing, assembly and integration, and enforce all applicable process requirements."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.1b","Requirement","ECSS-Q-ST-20_0380105",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.1c","Requirement","ECSS-Q-ST-20_0380106",1,"Created","Process specifications shall include QA provisions, methods for inspection and test, number of samples, accept or reject criteria."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.1d","Requirement","ECSS-Q-ST-20_0380107",1,"Created","Process witness samples shall be stored in controlled conditions."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.2a","Requirement","ECSS-Q-ST-20_0380108",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.3.3a","Recommendation","ECSS-Q-ST-20_0380227",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.4a","Requirement","ECSS-Q-ST-20_0380110",1,"Created","The supplier shall employ workmanship standards throughout all phases of manufacturing, assembly and integration, to ensure acceptable and consistent workmanship quality levels."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.4b","Requirement","ECSS-Q-ST-20_0380111",1,"Created","Workmanship standards shall identify acceptance or rejection criteria."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.4c","Requirement","ECSS-Q-ST-20_0380112",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.5a","Requirement","ECSS-Q-ST-20_0380113",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.5b","Requirement","ECSS-Q-ST-20_0380114",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.5c","Requirement","ECSS-Q-ST-20_0380115",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1a","Requirement","ECSS-Q-ST-20_0380116",1,"Created","The supplier shall make provisions for accountability, identification and maintenance of manufacture, assembly and integration tooling."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1b","Requirement","ECSS-Q-ST-20_0380117",1,"Created","Manufacture, assembly and integration tooling shall be checked for its dimensional accuracy, regarding the product drawings, and correct function."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1c","Requirement","ECSS-Q-ST-20_0380118",1,"Created","The QA organization shall approve tooling prior to use."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1d","Requirement","ECSS-Q-ST-20_0380119",1,"Created","The approval shall be stamped in conformance with 5.2.4, and recorded."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1e","Requirement","ECSS-Q-ST-20_0380120",1,"Created","Tools shall be checked for accuracy during the production life at adequate intervals."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1f","Requirement","ECSS-Q-ST-20_0380121",1,"Created","Tools shall be submitted to re-approval following modification."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1g","Requirement","ECSS-Q-ST-20_0380122",1,"Created","Tools shall be properly stored to prevent misuse, damage and deterioration."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1h","Requirement","ECSS-Q-ST-20_0380123",1,"Created","Unnecessary tools shall be removed from working areas."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.1i","Requirement","ECSS-Q-ST-20_0380124",1,"Created","Records shall be kept of all manufacturing equipment. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.2a","Requirement","ECSS-Q-ST-20_0380125",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.6.2b","Requirement","ECSS-Q-ST-20_0380126",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.1a","Requirement","ECSS-Q-ST-20_0380127",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.2a","Requirement","ECSS-Q-ST-20_0380128",1,"Created","Contamination-sensitive items shall be cleaned, controlled and maintained to the required cleanliness levels."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.2b","Requirement","ECSS-Q-ST-20_0380129",1,"Created","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. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.3a","Requirement","ECSS-Q-ST-20_0380130",1,"Created","The supplier shall develop detailed methods for attaining the cleanliness levels specified for the hardware."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.4a","Requirement","ECSS-Q-ST-20_0380131",1,"Created","Contamination shall be minimized by operating in clean working areas and by proper handling, preservation, packaging and storage."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.4b","Requirement","ECSS-Q-ST-20_0380132",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.4c","Requirement","ECSS-Q-ST-20_0380133",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.7.5a","Requirement","ECSS-Q-ST-20_0380134",1,"Created","Fabrication, assembly and integration of contamination sensitive items shall be conducted in facilities that provide cleanliness levels compatible with the specified product cleanliness."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8a","Requirement","ECSS-Q-ST-20_0380135",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8b","Requirement","ECSS-Q-ST-20_0380136",1,"Created","All identified critical characteristics shall be inspected as defined in the critical-item control programme."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8c","Requirement","ECSS-Q-ST-20_0380137",1,"Created","Self-inspection by the operators performing the associated manufacturing, assembly and integration activities shall not be considered sufficient for critical characteristics."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8d","Requirement","ECSS-Q-ST-20_0380138",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8e","Requirement","ECSS-Q-ST-20_0380139",1,"Created","MIPs shall be agreed with the customer."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8f","Requirement","ECSS-Q-ST-20_0380140",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8g","Requirement","ECSS-Q-ST-20_0380141",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8h","Requirement","ECSS-Q-ST-20_0380142",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.8i","Requirement","ECSS-Q-ST-20_0380143",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.1a","Requirement","ECSS-Q-ST-20_0380144",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.1b","Requirement","ECSS-Q-ST-20_0380145",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.1c","Requirement","ECSS-Q-ST-20_0380146",1,"Created","The supplier shall establish and maintain records of temporary installations and removals."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.1d","Requirement","ECSS-Q-ST-20_0380147",1,"Created","Temporarily installed items shall be accounted for to prevent their being incorporated in the final flight configuration."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.2a","Requirement","ECSS-Q-ST-20_0380148",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.2b","Requirement","ECSS-Q-ST-20_0380149",1,"Created","Equipment logbooks shall start with the first qualification or acceptance test after assembly."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.2c","Requirement","ECSS-Q-ST-20_0380150",1,"Created","Subsystem and system logbooks shall follow-on from the individual equipment logbooks to form a full record."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.2d","Requirement","ECSS-Q-ST-20_0380151",1,"Created","The logbook shall accompany the hardware whenever it is placed in the custody of another organization"]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.9.2e","Requirement","ECSS-Q-ST-20_0380152",1,"Created","The receiving organization shall maintain the logbook up-to-date."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.5.10a","Requirement","ECSS-Q-ST-20_0380153",1,"Created","The supplier shall establish and maintain manufacturing, assembly and integration records to provide all manufacturing, assembly, integration and inspection data required for traceability."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.1a","Requirement","ECSS-Q-ST-20_0380154",1,"Created","The supplier shall ensure that test facilities, either internal or external, conform to specified requirements."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.2a","Requirement","ECSS-Q-ST-20_0380155",1,"Created","The supplier shall ensure that computer-aided testing techniques and data are validated prior to use and controlled during their use in testing."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.2b","Requirement","ECSS-Q-ST-20_0380156",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.2c","Requirement","ECSS-Q-ST-20_0380157",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.3.1a","Requirement","ECSS-Q-ST-20_0380158",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.3.1b","Requirement","ECSS-Q-ST-20_0380159",1,"Created","The QA organization shall review and approve test procedures."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.3.2a","Requirement","ECSS-Q-ST-20_0380160",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.3.2b","Requirement","ECSS-Q-ST-20_0380161",1,"Created","The QA organization shall review and approve test reports."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4a","Requirement","ECSS-Q-ST-20_0380162",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4b","Requirement","ECSS-Q-ST-20_0380163",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4c","Requirement","ECSS-Q-ST-20_0380164",1,"Created","All testing activities related to critical characteristics as identified in the critical-items control programme shall be certified."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4d","Requirement","ECSS-Q-ST-20_0380165",1,"Created","Self-certification by the operators performing the test activities shall not be considered sufficient for critical characteristics."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4e","Requirement","ECSS-Q-ST-20_0380166",1,"Created","Testing activities or results to be subject to QA certification shall be identified as such in the relevant test procedure."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4f","Requirement","ECSS-Q-ST-20_0380167",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.4g","Requirement","ECSS-Q-ST-20_0380168",1,"Created","Where safety of personnel or damage to items or associated test equipment is possible, QA personnel shall have the authority to stop the test."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.5a","Requirement","ECSS-Q-ST-20_0380169",1,"Created","The supplier shall ensure that formal reviews are performed before and after major portions of qualification or acceptance tests."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.6.5b","Requirement","ECSS-Q-ST-20_0380170",1,"Created","The QA organization shall be represented in the formal boards established for the review of readiness for testing and testing accomplishment."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.1a","Requirement","ECSS-Q-ST-20_0380171",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.1b","Requirement","ECSS-Q-ST-20_0380172",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.2a","Requirement","ECSS-Q-ST-20_0380173",1,"Created","The supplier shall provide an EIDP for each deliverable end item in conformance with the DRD in Annex B."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.2b","Requirement","ECSS-Q-ST-20_0380174",1,"Created","The EIDP shall constitute the basis for formal acceptance reviews."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.2c","Requirement","ECSS-Q-ST-20_0380175",1,"Created","EIDPs shall be maintained and integrated into higher level EIDPs during subsystem or system integration and testing. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3a","Requirement","ECSS-Q-ST-20_0380176",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3b","Requirement","ECSS-Q-ST-20_0380177",1,"Created","The DRB functions at system level shall be fulfilled by the final acceptance review and chaired by the customer."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3c","Requirement","ECSS-Q-ST-20_0380178",1,"Created","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)."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3d","Requirement","ECSS-Q-ST-20_0380179",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3e","Requirement","ECSS-Q-ST-20_0380180",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3f","Requirement","ECSS-Q-ST-20_0380181",1,"Created","Delivery shall only be authorized by the unanimous agreement of the DRB members."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.3g","Requirement","ECSS-Q-ST-20_0380182",1,"Created","For the delivery a certificate of conformity, in conformance with Annex D, shall be made available and signed by the supplier."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.4.1a","Requirement","ECSS-Q-ST-20_0380183",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.4.2a","Requirement","ECSS-Q-ST-20_0380184",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.5.1a","Requirement","ECSS-Q-ST-20_0380185",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.5.1b","Requirement","ECSS-Q-ST-20_0380186",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.7.5.2a","Requirement","ECSS-Q-ST-20_0380187",1,"Created","The supplier shall make provisions for the prevention of damage to items during transportation."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.1.1.1a","Requirement","ECSS-Q-ST-20_0380188",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.1.1.1b","Requirement","ECSS-Q-ST-20_0380189",1,"Created","The supplier shall ensure that development risks are identified and appropriate back-up solutions are identified."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.1.1.1c","Requirement","ECSS-Q-ST-20_0380190",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.2a","Requirement","ECSS-Q-ST-20_0380191",1,"Created","The supplier shall ensure that GSE is configuration controlled."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.3.1a","Requirement","ECSS-Q-ST-20_0380192",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.3.1b","Requirement","ECSS-Q-ST-20_0380193",1,"Created","Procurement documents shall identify validation and receiving inspection requirements, and conform to the requirements in clause 5.4.2."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.3.2a","Recommendation","ECSS-Q-ST-20_0380228",1,"Created","The supplier and his lower level suppliers should not deviate from their standard practices when these are already documented and recognized for similar items."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.4.1a","Requirement","ECSS-Q-ST-20_0380195",1,"Created","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)."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.5a","Requirement","ECSS-Q-ST-20_0380196",1,"Created","Acceptance shall be achieved through a formal review process \n    NOTE Review process is defined in ECSS-M-ST-10-01."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.5b","Requirement","ECSS-Q-ST-20_0380197",1,"Created","The acceptance process shall include:\n    1. acceptance plan,\n    2. inspection and test procedures, and\n    3. inspection and test reports."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.5c","Permission","ECSS-Q-ST-20_0380229",1,"Created","Acceptance may be achieved through a simple inspection process if agreed between customer and supplier."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.6a","Requirement","ECSS-Q-ST-20_0380199",1,"Created","The supplier shall propose GSE elements for which acceptance is granted by a delivery board and agree these with his customer."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.6b","Requirement","ECSS-Q-ST-20_0380200",1,"Created","The delivery board shall include QA representatives from the supplier and the customer."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.7a","Requirement","ECSS-Q-ST-20_0380201",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.8a","Requirement","ECSS-Q-ST-20_0380202",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.9a","Requirement","ECSS-Q-ST-20_0380203",1,"Created","The supplier shall ensure that maintenance activities are planned."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","5.8.9b","Requirement","ECSS-Q-ST-20_0380204",1,"Created","The supplier shall ensure that maintenance demonstration is performed in order to prove that maintainability requirements are satisfied in the real operational environment."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-20_0380205",1,"Created","The Quality Assurance Plan shall introduce the purpose, objective and the reason prompting its preparation "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<2>a","Requirement","ECSS-Q-ST-20_0380206",1,"Created","The Quality Assurance Plan shall list the applicable and reference documents in support of the generation of the document."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<3>a","Requirement","ECSS-Q-ST-20_0380207",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<4>a","Requirement","ECSS-Q-ST-20_0380208",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<5>a","Requirement","ECSS-Q-ST-20_0380209",1,"Created","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"]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<6>a","Requirement","ECSS-Q-ST-20_0380210",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<7>a","Requirement","ECSS-Q-ST-20_0380211",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.1<8>a","Requirement","ECSS-Q-ST-20_0380212",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","A.2.2a","Permission","ECSS-Q-ST-20_0380230",1,"Created","The response to this DRD may be combined with the response to the product assurance plan, as defined in ECSS-Q-ST-10."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","B.2.1a","Requirement","ECSS-Q-ST-20_0380214",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1a","Requirement","ECSS-Q-ST-20_0380215",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1b","Requirement","ECSS-Q-ST-20_0380216",1,"Created","The logbook shall contain the “hardware configuration and traceability” table, which reports all the identification references of single elements composing the CI. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1c","Requirement","ECSS-Q-ST-20_0380217",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1d","Requirement","ECSS-Q-ST-20_0380218",1,"Created","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"]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1e","Requirement","ECSS-Q-ST-20_0380219",1,"Created","The logbook shall contain the summary list of nonconformances with relevant identification references, issue date, closure dates, and status."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1f","Requirement","ECSS-Q-ST-20_0380220",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1g","Requirement","ECSS-Q-ST-20_0380221",1,"Created","The logbook shall contain the records of total operating hours for each limited-life element identified in the test procedures."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1h","Requirement","ECSS-Q-ST-20_0380222",1,"Created","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. "]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","C.2.1i","Requirement","ECSS-Q-ST-20_0380223",1,"Created","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."]
["ECSS-Q-ST-20C","ECSS - Superseded v0.9","D.2.1a","Requirement","ECSS-Q-ST-20_0380224",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.1.2a","Requirement","ECSS-Q-ST-70_0490001",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.1.2b","Requirement","ECSS-Q-ST-70_0490002",1,"Created","The MMPP plan shall be submitted to the customer for approval."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.1.3a","Requirement","ECSS-Q-ST-70_0490003",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.1.3b","Requirement","ECSS-Q-ST-70_0490004",1,"Created","The MMPP manager shall organize technical review meetings with his suppliers at all levels."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2a","Requirement","ECSS-Q-ST-70_0490005",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2b","Requirement","ECSS-Q-ST-70_0490006",1,"Created","The lists shall reflect the current design at the time of issue."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2c","Requirement","ECSS-Q-ST-70_0490007",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2d","Recommendation","ECSS-Q-ST-70_0490194",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2e","Requirement","ECSS-Q-ST-70_0490009",1,"Created","The following constraints shall be taken into account: \n    1. requirements originating from the initial technical specification;\n    2. programmatic project requirements and conditions;"]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2f","Requirement","ECSS-Q-ST-70_0490010",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.2g","Requirement","ECSS-Q-ST-70_0490011",1,"Created","For critical items a request for approval shall be submitted in conformance with Annex D."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3a","Requirement","ECSS-Q-ST-70_0490012",1,"Created","The supplier shall document all materials in the Declared materials list in conformance with Annex A."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3b","Requirement","ECSS-Q-ST-70_0490013",1,"Created","The supplier shall document all mechanical parts in the Declared mechanical parts list in conformance with Annex B."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3c","Requirement","ECSS-Q-ST-70_0490014",1,"Created","The supplier shall document all processes in the Declared process list in conformance with Annex C."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3d","Requirement","ECSS-Q-ST-70_0490015",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3e","Requirement","ECSS-Q-ST-70_0490016",1,"Created","These lists shall be updated during the course of the project."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3f","Requirement","ECSS-Q-ST-70_0490017",1,"Created","The preliminary lists shall include the items from suppliers’ preliminary needs.\n    NOTE They are used to identify critical items (available for the PDR)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3g","Requirement","ECSS-Q-ST-70_0490018",1,"Created","The as-designed lists shall include the items from the baselines various design files (available for the CDR)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.3h","Requirement","ECSS-Q-ST-70_0490019",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.4a","Requirement","ECSS-Q-ST-70_0490020",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.4b","Requirement","ECSS-Q-ST-70_0490021",1,"Created","The lists established by the suppliers shall include all the information described in this Standard."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.4c","Requirement","ECSS-Q-ST-70_0490022",1,"Created","Amendments to the lists shall be implemented only through established change procedures."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.4d","Requirement","ECSS-Q-ST-70_0490023",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.2.4e","Requirement","ECSS-Q-ST-70_0490024",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.3a","Requirement","ECSS-Q-ST-70_0490025",1,"Created","Parts and materials shall satisfy the mission’s functional constraints."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.3b","Requirement","ECSS-Q-ST-70_0490026",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.3c","Requirement","ECSS-Q-ST-70_0490027",1,"Created","The technical criteria from clause 5.1 shall be taken into account, according to the mission."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.3d","Requirement","ECSS-Q-ST-70_0490028",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.4a","Requirement","ECSS-Q-ST-70_0490029",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.4b","Requirement","ECSS-Q-ST-70_0490030",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.4c","Requirement","ECSS-Q-ST-70_0490031",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.5a","Requirement","ECSS-Q-ST-70_0490032",1,"Created","Parts and materials with hazardous characteristics shall be identified, managed and processed in conformance with ECSS-Q-ST-40."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","4.6a","Requirement","ECSS-Q-ST-70_0490033",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.2a","Requirement","ECSS-Q-ST-70_0490034",1,"Created","Material properties shall be compatible with the thermal environment to which they are exposed."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.3a","Requirement","ECSS-Q-ST-70_0490035",1,"Created","Materials subject to thermal cycling shall be assessed for their ability to withstand induced thermal stress."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.3b","Requirement","ECSS-Q-ST-70_0490036",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.3c","Requirement","ECSS-Q-ST-70_0490037",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.4a","Requirement","ECSS-Q-ST-70_0490038",1,"Created","Materials selection shall be made in conformance with ECSS-Q-ST-70-71."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.4b","Requirement","ECSS-Q-ST-70_0490039",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.5a","Requirement","ECSS-Q-ST-70_0490040",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.5b","Requirement","ECSS-Q-ST-70_0490041",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.6a","Requirement","ECSS-Q-ST-70_0490042",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.7a","Requirement","ECSS-Q-ST-70_0490043",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.8a","Requirement","ECSS-Q-ST-70_0490044",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.9a","Requirement","ECSS-Q-ST-70_0490045",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.10a","Requirement","ECSS-Q-ST-70_0490046",1,"Created","Materials used for structural and load-bearing applications (subject to tensile stress) shall be chosen in conformance with ECSS-Q-ST-70-36."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.10b","Requirement","ECSS-Q-ST-70_0490047",1,"Created","Any material not covered by standard ECSS-Q-ST-70-36 shall be tested in conformance with ECSS-Q-ST-70-37."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.11a","Requirement","ECSS-Q-ST-70_0490048",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.11b","Requirement","ECSS-Q-ST-70_0490049",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.12a","Requirement","ECSS-Q-ST-70_0490050",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.12b","Requirement","ECSS-Q-ST-70_0490051",1,"Created","Galvanic compatibilities shall be selected in conformance with Table 5-1."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.12c","Requirement","ECSS-Q-ST-70_0490052",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.13a","Requirement","ECSS-Q-ST-70_0490053",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.13b","Requirement","ECSS-Q-ST-70_0490054",1,"Created","Test procedures shall be subject to the approval of the customer."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.14a","Requirement","ECSS-Q-ST-70_0490055",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.15a","Requirement","ECSS-Q-ST-70_0490056",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.16a","Requirement","ECSS-Q-ST-70_0490057",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.1.17a","Requirement","ECSS-Q-ST-70_0490058",1,"Created","Materials shall be selected to ensure sufficient life with respect to the intended application."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-70_0490059",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-Q-ST-70_0490060",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.2.2a","Requirement","ECSS-Q-ST-70_0490061",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.2.2b","Requirement","ECSS-Q-ST-70_0490062",1,"Created","The incoming inspection of each component batch shall include the verification of the termination composition (to avoid assembly of pure tin finish)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.3a","Requirement","ECSS-Q-ST-70_0490063",1,"Created","The supplier shall establish and maintain a declared materials list in conformance with Annex A."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.4.2a","Requirement","ECSS-Q-ST-70_0490064",1,"Created","The supplier shall analyse all the materials contained in his preliminary lists with respect to criticality and in correlation with the risk analysis performed. "]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.4.2b","Requirement","ECSS-Q-ST-70_0490065",1,"Created","Any material not meeting the project requirements shall be subject to a RFD to be submitted to the next customer."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.4.2c","Requirement","ECSS-Q-ST-70_0490066",1,"Created","Any critical material shall be subject to a RFA to be submitted to the customer."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.4.2d","Requirement","ECSS-Q-ST-70_0490067",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-Q-ST-70_0490068",1,"Created","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"]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.1b","Permission","ECSS-Q-ST-70_0490195",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.1c","Requirement","ECSS-Q-ST-70_0490070",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-70_0490071",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.2b","Requirement","ECSS-Q-ST-70_0490072",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.3a","Requirement","ECSS-Q-ST-70_0490073",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.3b","Requirement","ECSS-Q-ST-70_0490074",1,"Created","Validation status shall depend on the results obtained (validation report) and the review of corresponding documentation (available at CDR)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.4a","Requirement","ECSS-Q-ST-70_0490075",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.4b","Requirement","ECSS-Q-ST-70_0490076",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.5.5a","Requirement","ECSS-Q-ST-70_0490077",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1a","Requirement","ECSS-Q-ST-70_0490078",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1b","Requirement","ECSS-Q-ST-70_0490079",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1c","Requirement","ECSS-Q-ST-70_0490080",1,"Created","Materials with long lead times or long procurement delays (versus the project schedule) shall be identified before the formal subsystem PDR. "]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1d","Requirement","ECSS-Q-ST-70_0490081",1,"Created","Procurement shall be thoroughly planned, documented and implemented in a timely manner to obtain reliable product assurance provision at CDR. "]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1e","Requirement","ECSS-Q-ST-70_0490082",1,"Created","Back-up plans shall be prepared and initiated whenever there is evidence of delays or technical problems."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.1f","Requirement","ECSS-Q-ST-70_0490083",1,"Created","The material requirements shall be explicitly accepted by the material supplier or manufacturer."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.2a","Requirement","ECSS-Q-ST-70_0490084",1,"Created","All materials shall be submitted to an incoming inspection."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.6.2b","Requirement","ECSS-Q-ST-70_0490085",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.1a","Requirement","ECSS-Q-ST-70_0490086",1,"Created","The supplier shall verify that all critical materials are validated before being used in the manufacture of qualification or flight products."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.1b","Requirement","ECSS-Q-ST-70_0490087",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.2a","Requirement","ECSS-Q-ST-70_0490088",1,"Created","The supplier shall apply the traceability rules defined in ECSS-Q-ST-20 to all materials."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.2b","Recommendation","ECSS-Q-ST-70_0490196",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.3a","Requirement","ECSS-Q-ST-70_0490090",1,"Created","The supplier shall define provisions for packaging, storage and removal from storage for materials."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.3b","Requirement","ECSS-Q-ST-70_0490091",1,"Created","Measurements and inspections used to guarantee the material integrity and monitoring during storage and removal from storage shall be identified."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.4a","Requirement","ECSS-Q-ST-70_0490092",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.4b","Permission","ECSS-Q-ST-70_0490197",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.5a","Requirement","ECSS-Q-ST-70_0490094",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.6a","Requirement","ECSS-Q-ST-70_0490095",1,"Created","Nonconformances and alerts shall be managed in conformance with ECSS-Q-ST-10."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","5.7.7a","Requirement","ECSS-Q-ST-70_0490096",1,"Created","Material safety data sheet or equivalent shall be available for all materials."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.1a","Requirement","ECSS-Q-ST-70_0490097",1,"Created","The supplier shall verify that all materials and processes used in the manufacture of parts satisfy the mission technical requirements."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.2a","Requirement","ECSS-Q-ST-70_0490098",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.2b","Requirement","ECSS-Q-ST-70_0490099",1,"Created","Type reduction actions shall be implemented at all levels of the programme."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.2c","Requirement","ECSS-Q-ST-70_0490100",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.3a","Requirement","ECSS-Q-ST-70_0490101",1,"Created","The supplier shall establish and maintain a declared mechanical parts list in conformance with Annex B."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.4.2a","Requirement","ECSS-Q-ST-70_0490102",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.4.2b","Requirement","ECSS-Q-ST-70_0490103",1,"Created","Critical parts shall be identified in the DMPL and included in the critical items list."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.4.2c","Requirement","ECSS-Q-ST-70_0490104",1,"Created","Any critical part shall be the subject of a RFA."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.1a","Requirement","ECSS-Q-ST-70_0490105",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.1b","Permission","ECSS-Q-ST-70_0490198",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.1c","Requirement","ECSS-Q-ST-70_0490107",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.2a","Requirement","ECSS-Q-ST-70_0490108",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.2b","Requirement","ECSS-Q-ST-70_0490109",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.2c","Requirement","ECSS-Q-ST-70_0490110",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.3a","Requirement","ECSS-Q-ST-70_0490111",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.3b","Requirement","ECSS-Q-ST-70_0490112",1,"Created","Qualification status shall depend on the results obtained (qualification report) and the reviews of corresponding documentation (available at CDR)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.4a","Requirement","ECSS-Q-ST-70_0490113",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.4b","Requirement","ECSS-Q-ST-70_0490114",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.5.5a","Requirement","ECSS-Q-ST-70_0490115",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.1a","Requirement","ECSS-Q-ST-70_0490116",1,"Created","Mechanical parts with long lead times or procurement delays (versus the project schedule) shall be identified before the subsystem PDR."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.1b","Requirement","ECSS-Q-ST-70_0490117",1,"Created","Procurement shall be planned, documented and implemented in a timely manner to obtain reliable product assurance provision at CDR."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.1c","Requirement","ECSS-Q-ST-70_0490118",1,"Created","Back-up plans shall be prepared and initiated whenever there is evidence of possible delays or technical problems."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.2a","Requirement","ECSS-Q-ST-70_0490119",1,"Created","Each part shall be covered by a procurement specification or a standard."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.2b","Requirement","ECSS-Q-ST-70_0490120",1,"Created","The procurement specifications shall define the part characteristics, requirements, tests methods, acceptance criteria, lot acceptance testing, source inspection (if any) and material supplier inspection."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.2c","Requirement","ECSS-Q-ST-70_0490121",1,"Created","The procurement specifications shall be explicitly accepted by the part supplier or manufacturer."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.3a","Requirement","ECSS-Q-ST-70_0490122",1,"Created","For complex parts related to a specific project development, each supplier shall define the nature and frequency of their own source inspection points. "]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.3b","Requirement","ECSS-Q-ST-70_0490123",1,"Created","Source inspection shall be carried out by the customer on the premises of the supplier (part manufacturer) in conformance with ECSS-Q-ST-20."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.4a","Requirement","ECSS-Q-ST-70_0490124",1,"Created","Each part or batch of parts shall be submitted to an incoming inspection."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.6.4b","Requirement","ECSS-Q-ST-70_0490125",1,"Created","An incoming inspection procedure shall be established defining the inspections and tests to be carried out."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.1a","Requirement","ECSS-Q-ST-70_0490126",1,"Created","The supplier shall ensure that all critical parts are qualified before being used in the manufacture of qualification or flight products."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.1b","Requirement","ECSS-Q-ST-70_0490127",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.2a","Requirement","ECSS-Q-ST-70_0490128",1,"Created","The supplier shall apply the traceability rules defined in ECSS-Q-ST-20 to his parts."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.2b","Recommendation","ECSS-Q-ST-70_0490199",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.3a","Requirement","ECSS-Q-ST-70_0490130",1,"Created","The supplier shall define provisions for packaging, storage and removal from storage for parts."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.3b","Requirement","ECSS-Q-ST-70_0490131",1,"Created","Measurements and inspections used to guarantee the part integrity and monitoring during storage and removal from storage shall be identified."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.4a","Requirement","ECSS-Q-ST-70_0490132",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.4b","Requirement","ECSS-Q-ST-70_0490133",1,"Created","Limited-life parts shall be assessed as candidates to the critical items list in conformance with ECSS-Q-ST-10-04."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","6.7.5a","Requirement","ECSS-Q-ST-70_0490134",1,"Created","Management of nonconformances and alerts shall be in conformance with ECSS-Q-ST-10."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.1a","Requirement","ECSS-Q-ST-70_0490135",1,"Created","Each process to be used in the manufacturing or assembly of a product shall be identified by a specification or procedure."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.1b","Requirement","ECSS-Q-ST-70_0490136",1,"Created","Reference shall be made to accept and reject criteria."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.2a","Requirement","ECSS-Q-ST-70_0490137",1,"Created","The supplier shall verify that the materials and the mechanical parts used during the implementation of processes satisfy the requirements of this Standard."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.3a","Requirement","ECSS-Q-ST-70_0490138",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.3b","Requirement","ECSS-Q-ST-70_0490139",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.4a","Requirement","ECSS-Q-ST-70_0490140",1,"Created","The supplier shall establish and maintain a declared processes list in conformance with Annex C."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2a","Requirement","ECSS-Q-ST-70_0490141",1,"Created","The supplier shall analyse all the processes contained in their preliminary lists with respect to criticality and in correlation with the risk analyses performed."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2b","Requirement","ECSS-Q-ST-70_0490142",1,"Created","Critical processes shall be identified in the DPL and included in the list of critical items."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2c","Requirement","ECSS-Q-ST-70_0490143",1,"Created","Any critical process shall be the subject of an RFA."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2d","Requirement","ECSS-Q-ST-70_0490144",1,"Created","Special processes shall be identified and controlled."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2e","Requirement","ECSS-Q-ST-70_0490145",1,"Created","Process control shall be ensured by means of procedures or personnel certification or inline process control."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.5.2f","Permission","ECSS-Q-ST-70_0490200",1,"Created","Whenever feasible a statistical process may be carried out."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.1a","Requirement","ECSS-Q-ST-70_0490147",1,"Created","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. "]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.1b","Permission","ECSS-Q-ST-70_0490201",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.1c","Requirement","ECSS-Q-ST-70_0490149",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.2a","Requirement","ECSS-Q-ST-70_0490150",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.2b","Requirement","ECSS-Q-ST-70_0490151",1,"Created","When an evaluation is performed, the supplier shall provide \n    1. an evaluation plan at PDR and\n    2. an evaluation report before CDR."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.3a","Requirement","ECSS-Q-ST-70_0490152",1,"Created","For each critical process, the supplier shall implement a verification programme."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.3b","Requirement","ECSS-Q-ST-70_0490153",1,"Created","The verification programme shall be defined in conformance with existing ECSS or national agency standards of verification."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.3c","Requirement","ECSS-Q-ST-70_0490154",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.3d","Requirement","ECSS-Q-ST-70_0490155",1,"Created","Verification status shall depend on the results obtained (verification report) and the review of corresponding documentation (available at CDR)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.4a","Requirement","ECSS-Q-ST-70_0490156",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.6.5a","Requirement","ECSS-Q-ST-70_0490157",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.1a","Requirement","ECSS-Q-ST-70_0490158",1,"Created","The supplier shall confirm that all critical processes have been verified before being used in the manufacture of qualification or flight products."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.1b","Requirement","ECSS-Q-ST-70_0490159",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.2a","Requirement","ECSS-Q-ST-70_0490160",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.3a","Requirement","ECSS-Q-ST-70_0490161",1,"Created","Before implementation of a process, the supplier shall ensure that personnel are trained and that environment, means and documentation are adequate."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.3b","Requirement","ECSS-Q-ST-70_0490162",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.4a","Requirement","ECSS-Q-ST-70_0490163",1,"Created","Traceability of processes shall be ensured in conformance with ECSS-Q-ST-20."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.5a","Requirement","ECSS-Q-ST-70_0490164",1,"Created","Nonconformances and alerts shall be processed in conformance with ECSS-Q-ST-10."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.6a","Requirement","ECSS-Q-ST-70_0490165",1,"Created","MIPs shall be defined in conformance with ECSS-Q-ST-20."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","7.7.7a","Requirement","ECSS-Q-ST-70_0490166",1,"Created","The supplier shall define provisions for packaging, storage, and removal from storage for products or semi-finished products before and after implementation of processes."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-70_0490167",1,"Created","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.”"]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","A.2.1<1>b","Requirement","ECSS-Q-ST-70_0490168",1,"Created","If new groups are created, for a given project, these shall have numbers over 21."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","A.2.1<2>a","Requirement","ECSS-Q-ST-70_0490169",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","A.2.2a","Requirement","ECSS-Q-ST-70_0490170",1,"Created","The change record shall list the successive issues and their release dates since the first formal issue of the document."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","A.2.2b","Requirement","ECSS-Q-ST-70_0490171",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.1<1>a","Requirement","ECSS-Q-ST-70_0490172",1,"Created","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)."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.1<1>b","Requirement","ECSS-Q-ST-70_0490173",1,"Created","If, for a given project it is considered necessary to create new groups, these shall have numbers over 61."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.1<1>c","Recommendation","ECSS-Q-ST-70_0490202",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.1<2>a","Requirement","ECSS-Q-ST-70_0490175",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.2a","Requirement","ECSS-Q-ST-70_0490176",1,"Created","The change record shall list the successive issues and their release dates since the first formal issue of the document."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","B.2.2b","Requirement","ECSS-Q-ST-70_0490177",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","C.2.1<1>a","Requirement","ECSS-Q-ST-70_0490178",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","C.2.1<1>b","Requirement","ECSS-Q-ST-70_0490179",1,"Created","If, for a given project it is considered necessary to create new groups, these shall have numbers over 17."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","C.2.1<2>a","Requirement","ECSS-Q-ST-70_0490180",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","C.2.2a","Requirement","ECSS-Q-ST-70_0490181",1,"Created","The change record shall list the successive issues and their release dates since the first formal issue of the document."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","C.2.2b","Requirement","ECSS-Q-ST-70_0490182",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","D.2.1a","Recommendation","ECSS-Q-ST-70_0490203",1,"Created","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."]
["ECSS-Q-ST-70C","ECSS - Superseded v0.9","D.2.2a","Requirement","ECSS-Q-ST-70_0490184",1,"Created","The RFA shall be completed by the supplier (parts 1 to 10, 13 and 14) and the customer (parts 11 12 and 15)."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.1a","Requirement","ECSS-Q-ST-10_0360001",1,"Created","The supplier shall identify the personnel responsible for implementing and performing PA management and other PA disciplines."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.1b","Requirement","ECSS-Q-ST-10_0360002",1,"Created","The supplier shall assign a project PA manager reporting to the project manager and having unimpeded access to higher management."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.1c","Requirement","ECSS-Q-ST-10_0360003",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.1d","Requirement","ECSS-Q-ST-10_0360004",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.2a","Requirement","ECSS-Q-ST-10_0360005",1,"Created","The supplier shall define and document the responsibility, the authority and the interrelation of personnel who manage, perform and verify work affecting product assurance."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.2b","Requirement","ECSS-Q-ST-10_0360006",1,"Created","The supplier shall define and document the responsibilities and the interfaces of the PA functions, either external or internal, involved in a project."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.2c","Requirement","ECSS-Q-ST-10_0360007",1,"Created","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"]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.3a","Requirement","ECSS-Q-ST-10_0360008",1,"Created","The supplier shall identify the PA resources needed to implement the PA programme."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.3b","Requirement","ECSS-Q-ST-10_0360009",1,"Created","The supplier shall provide resources capable to perform the PA tasks identified in the PA programme."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.1.3c","Requirement","ECSS-Q-ST-10_0360010",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.2a","Requirement","ECSS-Q-ST-10_0360011",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.2b","Requirement","ECSS-Q-ST-10_0360012",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.2c","Requirement","ECSS-Q-ST-10_0360013",1,"Created","The PA manager shall interface with the customer regarding all Product Assurance matters."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.2d","Requirement","ECSS-Q-ST-10_0360014",1,"Created","The PA manager shall interface with lower-tier suppliers regarding all Product Assurance matters."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.3a","Requirement","ECSS-Q-ST-10_0360015",1,"Created","The supplier shall prepare, maintain and implement a plan of the PA activities in accordance with the customer PA requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.3b","Requirement","ECSS-Q-ST-10_0360016",1,"Created","The Product Assurance plan shall be prepared in conformance with DRD in Annex A."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.1.3c","Requirement","ECSS-Q-ST-10_0360017",1,"Created","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"]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-10_0360018",1,"Created","The PA manager shall ensure that PA disciplines are organized at the beginning of the project according to customer contractual requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-Q-ST-10_0360019",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1c","Requirement","ECSS-Q-ST-10_0360020",1,"Created","The PA manager shall ensure that the PA disciplines perform the tasks described in the PA Plan in line with the project schedule."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1d","Requirement","ECSS-Q-ST-10_0360021",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1e","Requirement","ECSS-Q-ST-10_0360022",1,"Created","The PA manager shall ensure the application of processes defined in applicable project plans and documents. "]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1f","Requirement","ECSS-Q-ST-10_0360023",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1g","Requirement","ECSS-Q-ST-10_0360024",1,"Created","The PA manager shall ensure that PA contributions to verification are defined and provided."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1h","Requirement","ECSS-Q-ST-10_0360025",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1i","Requirement","ECSS-Q-ST-10_0360026",1,"Created","The PA manager shall ensure that the qualification programme is implemented and the qualification results are recorded, evaluated and documented."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1j","Requirement","ECSS-Q-ST-10_0360027",1,"Created","The PA manager shall ensure that a Qualification Status List of the programme items is maintained in conformance with Annex B."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1k","Requirement","ECSS-Q-ST-10_0360028",1,"Created","The PA manager shall review and approve the achieved qualification status."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.1l","Requirement","ECSS-Q-ST-10_0360029",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.2a","Requirement","ECSS-Q-ST-10_0360030",1,"Created","The supplier shall report on the status and progress of the product assurance program implementation."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.2b","Requirement","ECSS-Q-ST-10_0360031",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.2c","Permission","ECSS-Q-ST-10_0360066",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.3a","Requirement","ECSS-Q-ST-10_0360033",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.3b","Requirement","ECSS-Q-ST-10_0360034",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.3c","Requirement","ECSS-Q-ST-10_0360035",1,"Created","In addition to the planned audits, extra audits shall be performed when necessary to overcome failure, consistent poor quality, or other problems. "]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.3d","Requirement","ECSS-Q-ST-10_0360036",1,"Created","The supplier shall plan and perform audits using established and maintained procedures."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.4a","Requirement","ECSS-Q-ST-10_0360037",1,"Created","The supplier shall establish a critical items control programme in conformance with ECSS-Q-ST-10-04."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.4b","Requirement","ECSS-Q-ST-10_0360038",1,"Created","The PA manager shall identify and evaluate critical items in support of the overall project risk management activities."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.4c","Requirement","ECSS-Q-ST-10_0360039",1,"Created","The PA manager shall ensure that a critical item control programme is implemented to eliminate or mitigate associated risks."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.5a","Requirement","ECSS-Q-ST-10_0360040",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.5b","Requirement","ECSS-Q-ST-10_0360041",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.5c","Requirement","ECSS-Q-ST-10_0360042",1,"Created","The PA manager shall ensure that obsolete documents and data retained for legal or knowledge preservation purposes are identified as such."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.5d","Requirement","ECSS-Q-ST-10_0360043",1,"Created","The PA manager shall identify the project documents requiring approval including those requiring approval by PA."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.6a","Requirement","ECSS-Q-ST-10_0360044",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.7a","Requirement","ECSS-Q-ST-10_0360045",1,"Created","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"]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.7b","Requirement","ECSS-Q-ST-10_0360046",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.8a","Requirement","ECSS-Q-ST-10_0360047",1,"Created","The supplier shall establish and maintain a nonconformance control system in conformance with ECSS-Q-ST-10-09."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.9a","Requirement","ECSS-Q-ST-10_0360048",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.9b","Requirement","ECSS-Q-ST-10_0360049",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.9c","Requirement","ECSS-Q-ST-10_0360050",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","5.2.9d","Requirement","ECSS-Q-ST-10_0360051",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-10_0360052",1,"Created","The PAP shall introduce the purpose, objective and the reason prompting its preparation.\n    NOTE For example: programme or project reference and phase."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<2>a","Requirement","ECSS-Q-ST-10_0360053",1,"Created","The PAP shall list the applicable and reference documents in support of the generation of the document."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<3.1>a","Requirement","ECSS-Q-ST-10_0360054",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<3.2>a","Requirement","ECSS-Q-ST-10_0360055",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<4>a","Requirement","ECSS-Q-ST-10_0360056",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable quality assurance requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<5>a","Requirement","ECSS-Q-ST-10_0360057",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable dependability requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<6>a","Requirement","ECSS-Q-ST-10_0360058",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable safety requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<7>a","Requirement","ECSS-Q-ST-10_0360059",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable EEE Component requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<8>a","Requirement","ECSS-Q-ST-10_0360060",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable Material and Processes requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<9>a","Requirement","ECSS-Q-ST-10_0360061",1,"Created","The PAP shall describe the activities, processes and procedures to be applied by the supplier to fulfil the applicable Software product assurance requirements."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.1<10>a","Requirement","ECSS-Q-ST-10_0360062",1,"Created","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."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.2a","Permission","ECSS-Q-ST-10_0360067",1,"Created","The response to this DRD may be combined with the response to the project management plan, as defined in ECSS-M-ST-10."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","A.2.2b","Permission","ECSS-Q-ST-10_0360068",1,"Created","The response to this DRD may be performed by reference to separate discipline plans addressing some of the above clauses of this DRD."]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","B.2.1a","Requirement","ECSS-Q-ST-10_0360065",1,"Created","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"]
["ECSS-Q-ST-10C","ECSS - Superseded v0.9","B.2.2a","Permission","ECSS-Q-ST-10_0360069",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.1a","Requirement","ECSS-Q-ST-30_0410001",1,"Created","The dependability assurance shall be implemented by means of a systematic process for specifying requirements for dependability and demonstrating that these requirements are achieved. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.1b","Requirement","ECSS-Q-ST-30_0410002",1,"Created","The dependability assurance process shall be in conformance with the dependability assurance programme plan for the project."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.2a","Requirement","ECSS-Q-ST-30_0410003",1,"Created","The supplier shall coordinate, implement and integrate the dependability programme management with the PA programme management."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3a","Requirement","ECSS-Q-ST-30_0410004",1,"Created","The supplier shall develop, maintain and implement a dependability plan for all project phases in conformance with the DRD in Annex C."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3b","Requirement","ECSS-Q-ST-30_0410005",1,"Created","The plan shall address the applicable requirements of this document.\n    ","NOTE The plan can be included in the PA programme plan."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3c","Requirement","ECSS-Q-ST-30_0410006",1,"Created","The extent that dependability assurance is applied shall take account of the severity (as defined in Table 5-1) of the consequences of failures."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3d","Requirement","ECSS-Q-ST-30_0410007",1,"Created","The establishment and implementation of the dependability programme plan shall be considered in conjunction with the safety aspects of the programme. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3e","Requirement","ECSS-Q-ST-30_0410008",1,"Created","The Supplier shall ensure that any potential conflict between dependability and safety requirements are managed. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.3f","Requirement","ECSS-Q-ST-30_0410009",1,"Created","Responsibilities for carrying out all dependability tasks within each phase of the lifecycle shall be defined."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.4a","Requirement","ECSS-Q-ST-30_0410010",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.4b","Requirement","ECSS-Q-ST-30_0410011",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.4c","Requirement","ECSS-Q-ST-30_0410012",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.5a","Requirement","ECSS-Q-ST-30_0410013",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.5b","Requirement","ECSS-Q-ST-30_0410014",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.5c","Requirement","ECSS-Q-ST-30_0410015",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.5d","Requirement","ECSS-Q-ST-30_0410016",1,"Created","The dependability aspects shall be considered during the entire verification process for dependability critical items until closeout."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.6a","Requirement","ECSS-Q-ST-30_0410017",1,"Created","The supplier shall ensure that all dependability data for a design review are presented to the customer in accordance with the project review schedule. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.6b","Requirement","ECSS-Q-ST-30_0410018",1,"Created","All dependability data submitted shall indicate the design baseline and shall be coherent with all other supporting technical documentation."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.6c","Requirement","ECSS-Q-ST-30_0410019",1,"Created","All design changes shall be assessed for their impact on dependability and a reassessment of the dependability shall be performed"]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.7a","Requirement","ECSS-Q-ST-30_0410020",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.8a","Requirement","ECSS-Q-ST-30_0410021",1,"Created","The supplier shall report dependability progress to the customer as part of product assurance activities in conformance with ECSS-Q-ST-10."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","4.9a","Requirement","ECSS-Q-ST-30_0410022",1,"Created","The supplier shall maintain all data used for the dependability programme."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.1a","Requirement","ECSS-Q-ST-30_0410023",1,"Created","Dependability shall be integrated as part of the design process. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.1b","Requirement","ECSS-Q-ST-30_0410024",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.1c","Requirement","ECSS-Q-ST-30_0410025",1,"Created","Manufacture, assembly, integration, test and operations shall not degrade dependability attributes introduced into the design."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.2a","Requirement","ECSS-Q-ST-30_0410026",1,"Created","The dependability requirement specification shall be part of the overall project requirements."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.2b","Requirement","ECSS-Q-ST-30_0410027",1,"Created","Dependability requirements shall be apportioned, in a top-down process, to establish dependability requirements for lower level elements. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.2c","Requirement","ECSS-Q-ST-30_0410028",1,"Created","Dependability requirements shall be applied during the preparation and review of design and test specifications. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.2d","Requirement","ECSS-Q-ST-30_0410029",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.1a","Requirement","ECSS-Q-ST-30_0410030",1,"Created","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…). "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.1b","Requirement","ECSS-Q-ST-30_0410031",1,"Created","The success criteria (sometimes referred to as “mission success criteria”) shall be defined at each level to be analysed. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.2a","Requirement","ECSS-Q-ST-30_0410032",1,"Created","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). "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.2b","Requirement","ECSS-Q-ST-30_0410033",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.2c","Requirement","ECSS-Q-ST-30_0410034",1,"Created","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"]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.2d","Requirement","ECSS-Q-ST-30_0410035",1,"Created","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)."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.2e","Requirement","ECSS-Q-ST-30_0410036",1,"Created","An understanding to these criteria identified in table 1 shall be agreed between customer and supplier."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.3a","Requirement","ECSS-Q-ST-30_0410037",1,"Created","Failure tolerance requirements shall be defined in the performance specifications."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.3b","Requirement","ECSS-Q-ST-30_0410038",1,"Created","The verification of the failure tolerance shall address all failure modes whose severity of consequence is classified as catastrophic, critical and major."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.4a","Requirement","ECSS-Q-ST-30_0410039",1,"Created","The supplier shall confirm that reliability is built into the design using fault tolerance and design margins. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.4b","Requirement","ECSS-Q-ST-30_0410040",1,"Created","The supplier shall analyse the failure characteristics of systems in order to identify areas of design weakness and propose corrective solutions. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.3.4c","Requirement","ECSS-Q-ST-30_0410041",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.4a","Requirement","ECSS-Q-ST-30_0410042",1,"Created","During the preliminary design phase, the contractor shall classify functions, operations and products in accordance with their criticality level."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.4b","Requirement","ECSS-Q-ST-30_0410043",1,"Created","Classification shall be approved by the customer."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.4c","Requirement","ECSS-Q-ST-30_0410044",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.4d","Requirement","ECSS-Q-ST-30_0410045",1,"Created","The criticality of a product (hardware and software) shall be identified at the highest criticality of the functions associated to that product."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.4e","Requirement","ECSS-Q-ST-30_0410046",1,"Created","The classification shall be used to focus efforts on the most critical areas during the project phases."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.5a","Requirement","ECSS-Q-ST-30_0410047",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.5b","Requirement","ECSS-Q-ST-30_0410048",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.6a","Requirement","ECSS-Q-ST-30_0410049",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.6b","Requirement","ECSS-Q-ST-30_0410050",1,"Created","Procedures for operations shall be analysed to identify and assess the risks associated with operations, sequences and situations that can affect dependability performance."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.6c","Requirement","ECSS-Q-ST-30_0410051",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.7a","Requirement","ECSS-Q-ST-30_0410052",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.7b","Requirement","ECSS-Q-ST-30_0410053",1,"Created","All recommendations from 5.7a shall be justified, documented and tracked."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.7c","Requirement","ECSS-Q-ST-30_0410054",1,"Created","Formal evidence of acceptance or rejection of the recommendation by the supplier’s management shall be provided."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","5.7d","Requirement","ECSS-Q-ST-30_0410055",1,"Created","An accepted dependability recommendation shall be implemented into the relevant corresponding documentation .\n    ","NOTE Example of corresponding documentation are: design documents, and operation manuals."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.1a","Requirement","ECSS-Q-ST-30_0410056",1,"Created","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)."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.1b","Requirement","ECSS-Q-ST-30_0410057",1,"Created","Preliminary identification and classification of undesirable events shall be determined from analysis of criteria for mission success, during conceptual and preliminary design phases. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.1c","Requirement","ECSS-Q-ST-30_0410058",1,"Created","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). "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.1d","Requirement","ECSS-Q-ST-30_0410059",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.1e","Requirement","ECSS-Q-ST-30_0410060",1,"Created","Identification and classification of undesirable events shall be finalised after assessment of failure scenarios (see clause 6.2)."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.2a","Requirement","ECSS-Q-ST-30_0410061",1,"Created","The supplier shall analyse the possible scenarios leading to the occurrence of undesirable events, "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.2b","Requirement","ECSS-Q-ST-30_0410062",1,"Created","The supplier shall identify failure modes, failure origins and causes, detailed failure effects leading to undesirable events."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.3a","Requirement","ECSS-Q-ST-30_0410063",1,"Created","Dependability analyses shall be performed on all space projects throughout the project life cycle to support the tasks and requirements specified in clause 5."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.3b","Requirement","ECSS-Q-ST-30_0410064",1,"Created","Dependability analyses shall be performed initially to contribute to the definition of the conceptual design and the system requirements. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.3c","Requirement","ECSS-Q-ST-30_0410065",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.3d","Requirement","ECSS-Q-ST-30_0410066",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.3e","Requirement","ECSS-Q-ST-30_0410067",1,"Created","The results of dependability analyses shall be incorporated into the design justification file in order to support improvements to the design."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.1a","Requirement","ECSS-Q-ST-30_0410068",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.1b","Requirement","ECSS-Q-ST-30_0410069",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.1c","Requirement","ECSS-Q-ST-30_0410070",1,"Created","A set of analyses selected from clauses 6.4.2 to 6.4.4 shall be defined as part of the contract requirement."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.1a","Requirement","ECSS-Q-ST-30_0410071",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.1b","Requirement","ECSS-Q-ST-30_0410072",1,"Created","The reliability data sources and methods used in reliability predictions shall be as specified by the customer. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.1c","Requirement","ECSS-Q-ST-30_0410073",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.1d","Requirement","ECSS-Q-ST-30_0410074",1,"Created","Reliability models shall be prepared to support predictions and FMEA/FMECA. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2a","Requirement","ECSS-Q-ST-30_0410075",1,"Created","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). "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2b","Requirement","ECSS-Q-ST-30_0410076",1,"Created","All potential failure modes shall be identified and classified according to the severity (FMEA) or criticality (FMECA) of their consequences."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2c","Requirement","ECSS-Q-ST-30_0410077",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2d","Requirement","ECSS-Q-ST-30_0410078",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2e","Requirement","ECSS-Q-ST-30_0410079",1,"Created","Provisions for failure detection and recovery actions shall be identified as part of the FMEA/FMECA."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2f","Requirement","ECSS-Q-ST-30_0410080",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.2g","Requirement","ECSS-Q-ST-30_0410081",1,"Created","As part of the FMEA/FMECA, potential failure propagation shall be assessed.\n    ","NOTE For FMEA/FMECA refer to ECSS-Q-ST-30-02."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.3a","Requirement","ECSS-Q-ST-30_0410082",1,"Created","HSIA shall be performed to ensure that the software reacts in an acceptable way to hardware failure. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.3b","Requirement","ECSS-Q-ST-30_0410083",1,"Created","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)."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.4a","Requirement","ECSS-Q-ST-30_0410084",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.5a","Requirement","ECSS-Q-ST-30_0410085",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.6a","Requirement","ECSS-Q-ST-30_0410086",1,"Created","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                                                 "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.7a","Requirement","ECSS-Q-ST-30_0410087",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.7b","Requirement","ECSS-Q-ST-30_0410088",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.7c","Requirement","ECSS-Q-ST-30_0410089",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.8a","Requirement","ECSS-Q-ST-30_0410090",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.8b","Requirement","ECSS-Q-ST-30_0410091",1,"Created","Part stress analyses shall be performed at part level to verify that the derating rules have been implemented."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.9a","Requirement","ECSS-Q-ST-30_0410092",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.2.10a","Requirement","ECSS-Q-ST-30_0410093",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.3a","Requirement","ECSS-Q-ST-30_0410094",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.3b","Requirement","ECSS-Q-ST-30_0410095",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.3c","Requirement","ECSS-Q-ST-30_0410096",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.3d","Requirement","ECSS-Q-ST-30_0410097",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.4a","Requirement","ECSS-Q-ST-30_0410098",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.4b","Requirement","ECSS-Q-ST-30_0410099",1,"Created","The supplier shall perform an analysis of outages in order to supply input data for availability analysis. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.4c","Requirement","ECSS-Q-ST-30_0410100",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.4d","Requirement","ECSS-Q-ST-30_0410101",1,"Created","The means of outage detection and the recovery methods shall be identified in the analysis."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.4.4e","Requirement","ECSS-Q-ST-30_0410102",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5a","Requirement","ECSS-Q-ST-30_0410103",1,"Created","The Dependability critical items identified by the dependability analyses shall be documented in conformance with ECSS-Q-ST-10-04."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5b","Requirement","ECSS-Q-ST-30_0410104",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5c","Requirement","ECSS-Q-ST-30_0410105",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5d","Requirement","ECSS-Q-ST-30_0410106",1,"Created","All items that have failure consequences classified as catastrophic shall be included in the dependability critical items list."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5e","Requirement","ECSS-Q-ST-30_0410107",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","6.5f","Requirement","ECSS-Q-ST-30_0410108",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","7.1a","Requirement","ECSS-Q-ST-30_0410109",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","7.2a","Requirement","ECSS-Q-ST-30_0410110",1,"Created","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)."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","7.3a","Requirement","ECSS-Q-ST-30_0410111",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","7.3b","Requirement","ECSS-Q-ST-30_0410112",1,"Created","“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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","7.4a","Requirement","ECSS-Q-ST-30_0410113",1,"Created","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. "]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","C.7a","Requirement","ECSS-Q-ST-30_0410114",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","D.7a","Requirement","ECSS-Q-ST-30_0410115",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","E.7a","Requirement","ECSS-Q-ST-30_0410116",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","F.7a","Requirement","ECSS-Q-ST-30_0410117",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","G.7a","Requirement","ECSS-Q-ST-30_0410118",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","H.7a","Requirement","ECSS-Q-ST-30_0410119",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","I.7a","Requirement","ECSS-Q-ST-30_0410120",1,"Created","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."]
["ECSS-Q-ST-30C","ECSS - Superseded v0.9","J.7a","Requirement","ECSS-Q-ST-30_0410121",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.1a","Requirement","ECSS-Q-ST-40_0440001",1,"Created","The supplier shall establish and maintain a safety programme to assure conformance with project safety policy and requirements."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.1b","Requirement","ECSS-Q-ST-40_0440002",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.2a","Requirement","ECSS-Q-ST-40_0440003",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.2b","Requirement","ECSS-Q-ST-40_0440004",1,"Created","The supplier shall cover, in his safety programme plan, the safety tasks for the project phases in conformance with 5.7.1."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.3a","Requirement","ECSS-Q-ST-40_0440005",1,"Created","The supplier shall comply with all applicable national or international safety regulations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.3b","Requirement","ECSS-Q-ST-40_0440006",1,"Created","The launch site safety regulations and rules shall be applied."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.3c","Requirement","ECSS-Q-ST-40_0440007",1,"Created","The implementation of safety requirements shall not be compromised by other requirements.\n    NOTE For example: security requirements."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.1a","Requirement","ECSS-Q-ST-40_0440008",1,"Created","Each supplier shall appoint a safety manager who has appropriate training or experience."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.1b","Requirement","ECSS-Q-ST-40_0440009",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.2.1a","Requirement","ECSS-Q-ST-40_0440010",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.2.2a","Requirement","ECSS-Q-ST-40_0440011",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.3a","Requirement","ECSS-Q-ST-40_0440012",1,"Created","The supplier shall perform safety audits or reviews to verify compliance to project safety policy and requirements."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.3b","Requirement","ECSS-Q-ST-40_0440013",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.3c","Requirement","ECSS-Q-ST-40_0440014",1,"Created","The customer shall be informed of the audit schedule."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.4a","Requirement","ECSS-Q-ST-40_0440015",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.5a","Requirement","ECSS-Q-ST-40_0440016",1,"Created","The safety manager (or a designated representative) shall have concluded the review of, and approved, any hazardous operation before it is executed."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.6a","Requirement","ECSS-Q-ST-40_0440017",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.6b","Requirement","ECSS-Q-ST-40_0440018",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.4.7a","Requirement","ECSS-Q-ST-40_0440019",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.5a","Requirement","ECSS-Q-ST-40_0440020",1,"Created","The safety risk identification, reduction and control shall be part of the project's risk management process as specified in ECSS-M-ST-80."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.5b","Requirement","ECSS-Q-ST-40_0440021",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.5c","Requirement","ECSS-Q-ST-40_0440022",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.6a","Requirement","ECSS-Q-ST-40_0440023",1,"Created","The safety critical items shall be part of the project's overall critical items control programme as specified in ECSS-Q-ST-10-04."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.1a","Requirement","ECSS-Q-ST-40_0440024",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.1b","Requirement","ECSS-Q-ST-40_0440025",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.2a","Requirement","ECSS-Q-ST-40_0440026",1,"Created","Safety analysis shall support trade-off analyses in arriving at the concept that has acceptable safety risk considering the project and mission constraints. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.2b","Requirement","ECSS-Q-ST-40_0440027",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.2c","Requirement","ECSS-Q-ST-40_0440028",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.3a","Requirement","ECSS-Q-ST-40_0440029",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.3b","Requirement","ECSS-Q-ST-40_0440030",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.3c","Requirement","ECSS-Q-ST-40_0440031",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.4a","Requirement","ECSS-Q-ST-40_0440032",1,"Created","Safety analysis shall support detailed design, production, qualification, testing."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.4b","Requirement","ECSS-Q-ST-40_0440033",1,"Created","Safety analysis shall also support operational safety optimization, safety requirements implementation evaluation, risk reduction verification, and hazard and risk acceptance."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.4c","Requirement","ECSS-Q-ST-40_0440034",1,"Created","Analysis of operations shall also support the identification of emergency and contingency response planning and training requirements, and the development of procedures."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.4d","Requirement","ECSS-Q-ST-40_0440035",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.5a","Requirement","ECSS-Q-ST-40_0440036",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.5b","Requirement","ECSS-Q-ST-40_0440037",1,"Created","The analysis shall also support the evaluation of operational anomalies for impact to safety, and the continued evaluation of risk trends."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.5c","Requirement","ECSS-Q-ST-40_0440038",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.6a","Requirement","ECSS-Q-ST-40_0440039",1,"Created","Safety analysis shall evaluate all disposal operations and associated hazards. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.6b","Requirement","ECSS-Q-ST-40_0440040",1,"Created","Disposal solutions shall be identified which meet the project's safety requirements."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.1.6c","Requirement","ECSS-Q-ST-40_0440041",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.2a","Requirement","ECSS-Q-ST-40_0440042",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.2b","Requirement","ECSS-Q-ST-40_0440043",1,"Created","The relevant customer and supplier specialists shall attend the meetings."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.3a","Requirement","ECSS-Q-ST-40_0440044",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.3b","Requirement","ECSS-Q-ST-40_0440045",1,"Created","The supplier shall support safety reviews by the customer and the relevant safety approval authority, as specified in the relevant review plans. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.3c","Requirement","ECSS-Q-ST-40_0440046",1,"Created","Each supplier participating in a safety review shall prepare, and submit for review, the safety data package."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.7.3d","Requirement","ECSS-Q-ST-40_0440047",1,"Created","Safety reviews shall be performed, and the review objectives achieved, in conformance with clause 5.7.1."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.8a","Requirement","ECSS-Q-ST-40_0440048",1,"Created","The supplier shall provide a statement of safety compliance to demonstrate that the space system elements conform to stated safety requirements. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.8b","Requirement","ECSS-Q-ST-40_0440049",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.8c","Requirement","ECSS-Q-ST-40_0440050",1,"Created","The project shall provide to the safety approval authority all safety-related information for their acceptance of the statement of safety compliance."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.1a","Requirement","ECSS-Q-ST-40_0440051",1,"Created","Safety training shall be part of the overall training in accordance with ECSS-Q-ST-20."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.1b","Requirement","ECSS-Q-ST-40_0440052",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.2a","Requirement","ECSS-Q-ST-40_0440053",1,"Created","The supplier shall identify the need for product specific safety training and implement the corresponding safety training programme for all relevant parties. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.2b","Requirement","ECSS-Q-ST-40_0440054",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.2c","Requirement","ECSS-Q-ST-40_0440055",1,"Created","The supplier shall support the implementation of the customer's training programme for the flight operations crew or mission control personnel."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.3a","Requirement","ECSS-Q-ST-40_0440056",1,"Created","All personnel accessing the area where the product is processed shall participate previously in the general safety awareness briefing."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.4a","Requirement","ECSS-Q-ST-40_0440057",1,"Created","The supplier shall provide basic technical training to all project engineering and safety personnel working with hazardous products."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.9.5a","Requirement","ECSS-Q-ST-40_0440058",1,"Created","The supplier shall maintain records of personnel having received safety training in accordance with ECSS-Q-ST-20."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10a","Requirement","ECSS-Q-ST-40_0440059",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10b","Requirement","ECSS-Q-ST-40_0440060",1,"Created","The supplier shall support - at request - project related accident and incident investigations that occur outside of the supplier’s control or facility."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10c","Requirement","ECSS-Q-ST-40_0440061",1,"Created","The supplier shall coordinate the investigation activities in cooperation with other supplier functional departments and lower tier suppliers."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10d","Requirement","ECSS-Q-ST-40_0440062",1,"Created","The accident or incident investigation report shall be formally closed by the supplier upon approval by the customer."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10e","Requirement","ECSS-Q-ST-40_0440063",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.10f","Requirement","ECSS-Q-ST-40_0440064",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.1a","Requirement","ECSS-Q-ST-40_0440065",1,"Created","The supplier shall maintain, as part of the project documentation, all safety-related data to support reviews and safety compliance demonstration."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.1b","Requirement","ECSS-Q-ST-40_0440066",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2a","Requirement","ECSS-Q-ST-40_0440067",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2b","Requirement","ECSS-Q-ST-40_0440068",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2c","Requirement","ECSS-Q-ST-40_0440069",1,"Created","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). "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2d","Requirement","ECSS-Q-ST-40_0440070",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2e","Requirement","ECSS-Q-ST-40_0440071",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.2f","Requirement","ECSS-Q-ST-40_0440072",1,"Created","All safety data shall be traceable from the safety data package and available for review."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.1a","Requirement","ECSS-Q-ST-40_0440073",1,"Created","Safety requirements that cannot be met shall be identified as specified in ECSS-M-ST-40."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.1b","Requirement","ECSS-Q-ST-40_0440074",1,"Created","A request for deviation or waiver shall be generated and tracked according to the requirements of ECSS-M-ST-40. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.2a","Requirement","ECSS-Q-ST-40_0440075",1,"Created","All RFD/RFW shall be assessed in order to identify those which impact safety. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.2b","Requirement","ECSS-Q-ST-40_0440076",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.3a","Requirement","ECSS-Q-ST-40_0440077",1,"Created","Safety deviations and waivers shall be subject to safety approval authority acceptance."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.3.4a","Requirement","ECSS-Q-ST-40_0440078",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.4a","Requirement","ECSS-Q-ST-40_0440079",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.4b","Requirement","ECSS-Q-ST-40_0440080",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","5.11.5a","Requirement","ECSS-Q-ST-40_0440081",1,"Created","The safety critical items identified by the safety analysis shall be documented in accordance with ECSS-Q-ST-10-04."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.2a","Requirement","ECSS-Q-ST-40_0440082",1,"Created","Safety requirements shall be identified and traced from the system level into the design and then allocated to the lower levels."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.2b","Requirement","ECSS-Q-ST-40_0440083",1,"Created","When specified by the project, the identified safety requirements shall be justified in the design and presented in an appropriate document."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.2a","Requirement","ECSS-Q-ST-40_0440084",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.1a","Requirement","ECSS-Q-ST-40_0440085",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.2a","Requirement","ECSS-Q-ST-40_0440086",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.3a","Requirement","ECSS-Q-ST-40_0440087",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.1a","Requirement","ECSS-Q-ST-40_0440088",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.1b","Requirement","ECSS-Q-ST-40_0440089",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.2a","Requirement","ECSS-Q-ST-40_0440090",1,"Created","Failure tolerance is the basic safety requirement that shall be used to control most hazards. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.2b","Requirement","ECSS-Q-ST-40_0440091",1,"Created","The design shall tolerate a minimum number of credible failures and/or operator errors determined by the hazard consequence."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.2c","Requirement","ECSS-Q-ST-40_0440092",1,"Created","The supplier shall establish the list of failures to be considered as \"non credible\" for customer approval as early as possible in development."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.3a","Requirement","ECSS-Q-ST-40_0440093",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.4a","Requirement","ECSS-Q-ST-40_0440094",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.4b","Requirement","ECSS-Q-ST-40_0440095",1,"Created","The safety devices, specified in 6.3.3.4.4a, shall not be dependant on human performance."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.4c","Recommendation","ECSS-Q-ST-40_0440320",1,"Created","Use of software in automatic safety devices should be avoided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.4d","Requirement","ECSS-Q-ST-40_0440097",1,"Created","If software is used in automatic safety devices, justification shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.5a","Requirement","ECSS-Q-ST-40_0440098",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.5b","Requirement","ECSS-Q-ST-40_0440099",1,"Created","This shall be coupled with emergency controls of corrective action for operators to safe or shut down the affected subsystem."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.6a","Requirement","ECSS-Q-ST-40_0440100",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.6b","Requirement","ECSS-Q-ST-40_0440101",1,"Created","Special procedures shall be verified by test and appropriate training be provided for personnel."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.6c","Requirement","ECSS-Q-ST-40_0440102",1,"Created","Hazard detection shall be implemented if alternative means cannot be used."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.3.4.6d","Requirement","ECSS-Q-ST-40_0440103",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.4a","Requirement","ECSS-Q-ST-40_0440104",1,"Created","The system design shall meet the safety requirements under the worst-case natural and induced environments defined for the project."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.4b","Requirement","ECSS-Q-ST-40_0440105",1,"Created","Design and performance margins shall be established and applied for worst-case combinations of induced and natural environments and operating characteristics."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.5a","Requirement","ECSS-Q-ST-40_0440106",1,"Created","Loss, malfunctioning, and sudden restoration of external services shall be defined as an input to the development phase."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.5b","Requirement","ECSS-Q-ST-40_0440107",1,"Created","The system design shall be defined so that catastrophic or critical consequences are not induced by loss, malfunctioning, and sudden restoration of external services."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6a","Requirement","ECSS-Q-ST-40_0440108",1,"Created","Safety monitoring, display, alarm and safing capabilities shall be incorporated for manned space systems."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6b","Requirement","ECSS-Q-ST-40_0440109",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6c","Requirement","ECSS-Q-ST-40_0440110",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6d","Requirement","ECSS-Q-ST-40_0440111",1,"Created","The performance of these functions shall be verifiable during flight and ground operational phases."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6e","Requirement","ECSS-Q-ST-40_0440112",1,"Created","The emergency, caution and warning function shall detect and notify the crew and system operators of emergency, warning and caution situations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6f","Requirement","ECSS-Q-ST-40_0440113",1,"Created","Safing functions and capabilities shall be included that provide for the containment or control of emergency, warning and caution situations. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6g","Requirement","ECSS-Q-ST-40_0440114",1,"Created","Provisions shall be included for the monitoring of safing function execution. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6h","Requirement","ECSS-Q-ST-40_0440115",1,"Created","Dedicated safing functions shall be provided for emergency situations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6i","Requirement","ECSS-Q-ST-40_0440116",1,"Created","Control of warning and caution situations shall be acceptable by system reconfiguration or by dedicated safing functions."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6j","Requirement","ECSS-Q-ST-40_0440117",1,"Created","A single failure shall not cause loss of the emergency and warning function."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6k","Requirement","ECSS-Q-ST-40_0440118",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6l","Requirement","ECSS-Q-ST-40_0440119",1,"Created","A single failure shall not cause loss of the emergency and warning functions together with the monitored functions. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6m","Requirement","ECSS-Q-ST-40_0440120",1,"Created","Emergency, warning and caution data, out of limit annunciation and safing commands shall be given priority over other data processing and command functions."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6n","Requirement","ECSS-Q-ST-40_0440121",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6o","Requirement","ECSS-Q-ST-40_0440122",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.6p","Requirement","ECSS-Q-ST-40_0440123",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.7a","Requirement","ECSS-Q-ST-40_0440124",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.8a","Requirement","ECSS-Q-ST-40_0440125",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.9a","Requirement","ECSS-Q-ST-40_0440126",1,"Created","Biological contamination (including organic-constituents) resulting from the introduction of extraterrestrial matter shall be avoided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.9b","Requirement","ECSS-Q-ST-40_0440127",1,"Created","The introduction of extraterrestrial matter shall not affect the environmental conditions on Earth."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.9c","Requirement","ECSS-Q-ST-40_0440128",1,"Created","Extraterrestrial matter shall be treated as hazardous substances until proven otherwise."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.9d","Requirement","ECSS-Q-ST-40_0440129",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.9e","Requirement","ECSS-Q-ST-40_0440130",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10a","Requirement","ECSS-Q-ST-40_0440131",1,"Created","A mission abort capability shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10b","Requirement","ECSS-Q-ST-40_0440132",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10c","Requirement","ECSS-Q-ST-40_0440133",1,"Created","Escape and rescue functions shall be provided. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10d","Requirement","ECSS-Q-ST-40_0440134",1,"Created","The capability to reconfigure the system to restore the functional capability of safety critical functions in case of failures or accidents shall be provided. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10e","Requirement","ECSS-Q-ST-40_0440135",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.10f","Requirement","ECSS-Q-ST-40_0440136",1,"Created","The space system shall provide an on-board medical facility and the capability for handling a permanently impaired or deceased crewmember."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.3.11a","Requirement","ECSS-Q-ST-40_0440137",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1a","Requirement","ECSS-Q-ST-40_0440138",1,"Created","The severity of potential consequences of identified hazardous events shall be categorized as shown in Table 6-1."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1b","Requirement","ECSS-Q-ST-40_0440139",1,"Created","An understanding of the criteria defined in Table 6-1 shall be agreed between customer and supplier."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1c","Requirement","ECSS-Q-ST-40_0440140",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1d","Requirement","ECSS-Q-ST-40_0440141",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1e","Requirement","ECSS-Q-ST-40_0440142",1,"Created","For international programmes, a coherent set of consequence severity shall be established for joint operational phases."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1f","Requirement","ECSS-Q-ST-40_0440143",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1g","Requirement","ECSS-Q-ST-40_0440144",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.1h","Requirement","ECSS-Q-ST-40_0440145",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.1a","Requirement","ECSS-Q-ST-40_0440146",1,"Created","Failure tolerance shall be the basic safety requirement used to control hazards."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.1b","Requirement","ECSS-Q-ST-40_0440147",1,"Created","No single system failure or single operator error shall have critical or catastrophic consequences. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.1c","Requirement","ECSS-Q-ST-40_0440148",1,"Created","No combination of two independent system failures or operator errors shall have catastrophic consequences."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.1d","Requirement","ECSS-Q-ST-40_0440149",1,"Created","Safety inhibits shall be independent, verifiable, stable and stay in a safe position even in case of energy failure."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.1e","Requirement","ECSS-Q-ST-40_0440150",1,"Created","Multiple failures, which result from common-cause or common-mode failure mechanisms, shall be analysed as single failures for determining failure tolerance."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.2a","Requirement","ECSS-Q-ST-40_0440151",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.2b","Requirement","ECSS-Q-ST-40_0440152",1,"Created","The capability shall be provided to the flight crew and mission control to override automatic safing and redundancy switch-over."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.2c","Requirement","ECSS-Q-ST-40_0440153",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.2.3a","Requirement","ECSS-Q-ST-40_0440154",1,"Created","Hardware failures or software errors shall not cause additional failures with hazardous effects or propagate to cause the hazardous operation of interfacing hardware."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.1a","Requirement","ECSS-Q-ST-40_0440155",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.2a","Requirement","ECSS-Q-ST-40_0440156",1,"Created","Structural safety factors shall be defined and applied in accordance with ECSS-E-ST-32-10 or higher safety factor where applicable."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.2b","Requirement","ECSS-Q-ST-40_0440157",1,"Created","Safety margins shall be based on worst credible combinations of environmental conditions."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.3a","Requirement","ECSS-Q-ST-40_0440158",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.3b","Requirement","ECSS-Q-ST-40_0440159",1,"Created","For unmanned systems, only pressure vessels shall be designed in accordance with ECSS-E-ST-32-01, when required by launch site safety authority."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.4a","Requirement","ECSS-Q-ST-40_0440160",1,"Created","Materials shall be selected and controlled in accordance with ECSS-Q-ST-70."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.4b","Requirement","ECSS-Q-ST-40_0440161",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.3.4c","Requirement","ECSS-Q-ST-40_0440162",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.4a","Requirement","ECSS-Q-ST-40_0440163",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.4.4b","Requirement","ECSS-Q-ST-40_0440164",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.1a","Requirement","ECSS-Q-ST-40_0440165",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.1b","Requirement","ECSS-Q-ST-40_0440166",1,"Created","Identification shall be done without taking into account hazards controls to be or already implemented."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.2a","Requirement","ECSS-Q-ST-40_0440167",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.3a","Requirement","ECSS-Q-ST-40_0440168",1,"Created","The system shall provide failure tolerance and redundancy status information of safety-critical functions."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.3b","Requirement","ECSS-Q-ST-40_0440169",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.4a","Requirement","ECSS-Q-ST-40_0440170",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.5a","Requirement","ECSS-Q-ST-40_0440171",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.1a","Requirement","ECSS-Q-ST-40_0440172",1,"Created","Safety aspects associated with the software function shall be an integral part of the overall system safety efforts and not be assessed in isolation."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.1b","Requirement","ECSS-Q-ST-40_0440173",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.2a","Requirement","ECSS-Q-ST-40_0440174",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.3a","Requirement","ECSS-Q-ST-40_0440175",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.4a","Requirement","ECSS-Q-ST-40_0440176",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.4b","Requirement","ECSS-Q-ST-40_0440177",1,"Created","Safety-critical software shall be analysed for the identification and verification of adequate software controls and inhibits and validated accordingly. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.5.6.4c","Requirement","ECSS-Q-ST-40_0440178",1,"Created","The level of required software product assurance effort shall be determined in accordance with the criticality of the software component."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1a","Requirement","ECSS-Q-ST-40_0440179",1,"Created","Safety involvement in the operational phase shall be planned."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1b","Requirement","ECSS-Q-ST-40_0440180",1,"Created","Responsibilities, rules and contingency procedures shall be established prior to operation for hazardous “limit” conditions that can occur during ground and in-flight operations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1c","Requirement","ECSS-Q-ST-40_0440181",1,"Created","Operating ranges and performance limits for safe operation shall be established and specified."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1d","Requirement","ECSS-Q-ST-40_0440182",1,"Created","The design shall not require continuous active control by personnel in order to stay within the established operating ranges and performance limits."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1e","Requirement","ECSS-Q-ST-40_0440183",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.1f","Requirement","ECSS-Q-ST-40_0440184",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.1a","Requirement","ECSS-Q-ST-40_0440185",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.2a","Requirement","ECSS-Q-ST-40_0440186",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.3a","Requirement","ECSS-Q-ST-40_0440187",1,"Created","Flight rules shall be prepared for each mission that outline pre-planned decisions in case of off-nominal situations and consistent with safety requirements."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.4a","Requirement","ECSS-Q-ST-40_0440188",1,"Created","Hazardous commanding control shall ensure that all hazardous commands are identified."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.4b","Requirement","ECSS-Q-ST-40_0440189",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.4c","Requirement","ECSS-Q-ST-40_0440190",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.4d","Requirement","ECSS-Q-ST-40_0440191",1,"Created",".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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.5a","Requirement","ECSS-Q-ST-40_0440192",1,"Created","Mission operation change control shall ensure that all changes, which are desired or become necessary during mission, are reviewed for safety impact."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.5b","Requirement","ECSS-Q-ST-40_0440193",1,"Created","Mission operation change control shall ensure that the responsible safety approval authority approves all operational change requests with safety impact."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.6a","Requirement","ECSS-Q-ST-40_0440194",1,"Created","Safety status parameters shall be identified."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.6b","Requirement","ECSS-Q-ST-40_0440195",1,"Created","Safety status parameters shall be monitored."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.6c","Requirement","ECSS-Q-ST-40_0440196",1,"Created","Deviation from specified limits shall be managed."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.7a","Requirement","ECSS-Q-ST-40_0440197",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.7b","Requirement","ECSS-Q-ST-40_0440198",1,"Created","The launch vehicle and spent stage trajectories shall be monitored to determine vehicle, stage or debris impact points."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.2.7c","Requirement","ECSS-Q-ST-40_0440199",1,"Created","Residual propellants contained in spent or aborted suborbital stages shall be safely dispersed."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.1a","Requirement","ECSS-Q-ST-40_0440200",1,"Created","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,"]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.2a","Requirement","ECSS-Q-ST-40_0440201",1,"Created","The supplier shall establish procedures to perform safety readiness reviews and inspections prior to the performance of any applicable operation."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.3a","Requirement","ECSS-Q-ST-40_0440202",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.4a","Requirement","ECSS-Q-ST-40_0440203",1,"Created","Hazardous operations shall be monitored for conforming to safety requirements and procedures, and for the possible development of unforeseen hazardous situations. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.4b","Requirement","ECSS-Q-ST-40_0440204",1,"Created","Where necessary, contingency and emergency plans or procedures shall be established and verified prior to the commencement of the operation. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.4c","Requirement","ECSS-Q-ST-40_0440205",1,"Created","The safety manager or safety relevant authority shall have the authority to stop any operation that does not conform to safety requirements. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.5a","Requirement","ECSS-Q-ST-40_0440206",1,"Created","Launch, landing, turn-around and mission operations shall be subject to hazard analysis."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.5b","Requirement","ECSS-Q-ST-40_0440207",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.6a","Requirement","ECSS-Q-ST-40_0440208",1,"Created","All Ground support equipment (GSE) shall be subjected to hazard analysis."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.6b","Requirement","ECSS-Q-ST-40_0440209",1,"Created","All GSE shall conform to the ‘Essential Health & Safety Requirements’ of all applicable EU ‘New Approach directives’. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.6c","Requirement","ECSS-Q-ST-40_0440210",1,"Created","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’."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","6.6.3.6d","Requirement","ECSS-Q-ST-40_0440211",1,"Created","Conformance to any other product related directives shall be demonstrated.\n    NOTE Further guidance is given in Annex G."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.2a","Requirement","ECSS-Q-ST-40_0440212",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.2b","Requirement","ECSS-Q-ST-40_0440213",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.2c","Requirement","ECSS-Q-ST-40_0440214",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.2d","Requirement","ECSS-Q-ST-40_0440215",1,"Created","Analysis shall always be made with reference to a defined configuration baseline as defined by ECSS-M-ST-40."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.1a","Requirement","ECSS-Q-ST-40_0440216",1,"Created","The supplier shall respond to and comply with the applicable safety requirements for the project."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.2a","Requirement","ECSS-Q-ST-40_0440217",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.3a","Requirement","ECSS-Q-ST-40_0440218",1,"Created","The supplier shall define the safety requirements for the various functions of the system."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.4a","Requirement","ECSS-Q-ST-40_0440219",1,"Created","The supplier shall define the safety requirements associated with the various subsystems and lower levels."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.5a","Requirement","ECSS-Q-ST-40_0440220",1,"Created","The supplier shall justify to the customer the proposed allocation of safety requirements at the latest at the end of the detailed definition phase."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.3.6a","Requirement","ECSS-Q-ST-40_0440221",1,"Created","The supplier shall ensure that the function and subsystem safety requirements are included in the relevant functional and subsystem specification."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.4a","Requirement","ECSS-Q-ST-40_0440222",1,"Created","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"]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.1a","Requirement","ECSS-Q-ST-40_0440223",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2a","Requirement","ECSS-Q-ST-40_0440224",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2b","Requirement","ECSS-Q-ST-40_0440225",1,"Created","Hazard analysis shall support the hazard reduction process."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2c","Requirement","ECSS-Q-ST-40_0440226",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2d","Requirement","ECSS-Q-ST-40_0440227",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2e","Requirement","ECSS-Q-ST-40_0440228",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.2f","Requirement","ECSS-Q-ST-40_0440229",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.3a","Requirement","ECSS-Q-ST-40_0440230",1,"Created","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)                                                     "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.3b","Requirement","ECSS-Q-ST-40_0440231",1,"Created","Safety risk assessment shall be started early in the design process and performed in progressive steps during the implementation of the safety programme. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.1a","Requirement","ECSS-Q-ST-40_0440232",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.1b","Requirement","ECSS-Q-ST-40_0440233",1,"Created","Supporting analyses shall be agreed with all relevant parties."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.2a","Requirement","ECSS-Q-ST-40_0440234",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.2b","Requirement","ECSS-Q-ST-40_0440235",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.2c","Requirement","ECSS-Q-ST-40_0440236",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.3a","Requirement","ECSS-Q-ST-40_0440237",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.3b","Requirement","ECSS-Q-ST-40_0440238",1,"Created","The caution and warning analysis shall utilize the results of the warning time and hazards analyses as appropriate."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.1a","Requirement","ECSS-Q-ST-40_0440239",1,"Created","Multiple failures, which result from common-cause or common-mode failure mechanisms, shall be analysed as single failures for determining failure tolerance. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.2a","Requirement","ECSS-Q-ST-40_0440240",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.3a","Requirement","ECSS-Q-ST-40_0440241",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.3b","Requirement","ECSS-Q-ST-40_0440242",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.4a","Requirement","ECSS-Q-ST-40_0440243",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.4b","Requirement","ECSS-Q-ST-40_0440244",1,"Created","The common-mode analysis shall be coordinated with the FMEA/FMECA."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.4.5a","Requirement","ECSS-Q-ST-40_0440245",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.5a","Requirement","ECSS-Q-ST-40_0440246",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.5b","Requirement","ECSS-Q-ST-40_0440247",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.6a","Requirement","ECSS-Q-ST-40_0440248",1,"Created","Whenever safety analyses identify operator errors as a cause of catastrophic or critical hazards, a dedicated analysis shall be carried out."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.6b","Requirement","ECSS-Q-ST-40_0440249",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.6c","Requirement","ECSS-Q-ST-40_0440250",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.7a","Requirement","ECSS-Q-ST-40_0440251",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.8a","Requirement","ECSS-Q-ST-40_0440252",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","7.5.4.8b","Requirement","ECSS-Q-ST-40_0440253",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.1a","Requirement","ECSS-Q-ST-40_0440254",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.1b","Requirement","ECSS-Q-ST-40_0440255",1,"Created","For common techniques for verification of design features used to control hazards, the requirements of ECSS-E-ST-10 shall apply. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.1c","Requirement","ECSS-Q-ST-40_0440256",1,"Created","To successfully complete the safety process, positive feedback shall be provided on completion results for all verification items associated with a given hazard."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.1a","Requirement","ECSS-Q-ST-40_0440257",1,"Created","The supplier shall establish a hazard reporting system for tracking the status of all identified hazards."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.1b","Requirement","ECSS-Q-ST-40_0440258",1,"Created","The system shall be applied for all hazards with potentially catastrophic or critical consequences."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.1c","Requirement","ECSS-Q-ST-40_0440259",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.1d","Requirement","ECSS-Q-ST-40_0440260",1,"Created","If verification cannot be completed, the supplier shall establish a Safety Verification Tracking Log (SVTL) (refer to clause 8.5.1a.)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.2a","Requirement","ECSS-Q-ST-40_0440261",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.2.3a","Requirement","ECSS-Q-ST-40_0440262",1,"Created","All hazard documentation shall be formally issued for each safety review and major project review, as specified in clause 5.11). "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.1a","Requirement","ECSS-Q-ST-40_0440263",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.1b","Requirement","ECSS-Q-ST-40_0440264",1,"Created","Verification planning shall commence in an integrated manner upon selection of the control method."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.2a","Requirement","ECSS-Q-ST-40_0440265",1,"Created","Safety verification methods shall include alternatively or in combination review of design, analysis, inspection and test."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.2b","Requirement","ECSS-Q-ST-40_0440266",1,"Created","For all safety verifications traceability shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.3a","Requirement","ECSS-Q-ST-40_0440267",1,"Created","All relevant technical safety and engineering analyses performed or updated with analysis in respect to the as-built configuration shall be used for verification. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.3b","Requirement","ECSS-Q-ST-40_0440268",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.1a","Requirement","ECSS-Q-ST-40_0440269",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2a","Requirement","ECSS-Q-ST-40_0440270",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2b","Requirement","ECSS-Q-ST-40_0440271",1,"Created","Launch preparation inspections shall be entered into the launch base procedure. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2c","Requirement","ECSS-Q-ST-40_0440272",1,"Created","The closeout shall be given by the approved launch authority procedure."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2d","Requirement","ECSS-Q-ST-40_0440273",1,"Created","Late access procedures shall be the subject of training and be performed by qualified personnel. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2e","Requirement","ECSS-Q-ST-40_0440274",1,"Created","Training for flight crew and mission operation teams shall be performed, including specific safety briefing, training and mission simulation. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.2f","Requirement","ECSS-Q-ST-40_0440275",1,"Created","Close-out shall be by safety-approved procedure, documented training session and simulations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.4.3a","Requirement","ECSS-Q-ST-40_0440276",1,"Created","Inflight inspections shall be entered into flight procedures and operation manuals."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.5a","Requirement","ECSS-Q-ST-40_0440277",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.3.5b","Requirement","ECSS-Q-ST-40_0440278",1,"Created","The results of safety verification shall be submitted for approval to the relevant safety approval authority."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.1a","Requirement","ECSS-Q-ST-40_0440279",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.1b","Requirement","ECSS-Q-ST-40_0440280",1,"Created","The tests shall include the demonstration of nominal, contingency and emergency operational modes."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.2a","Requirement","ECSS-Q-ST-40_0440281",1,"Created","The safety-critical characteristics of all safety-critical functions shall be qualified by test."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.2b","Requirement","ECSS-Q-ST-40_0440282",1,"Created","Safety-critical function qualification testing shall include the determination of performance margins considering worst case combinations of induced and natural environments and operating conditions. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.2c","Requirement","ECSS-Q-ST-40_0440283",1,"Created","Qualification “by similarity” shall not be applied except after customer approval on a case-by-case basis. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.3a","Requirement","ECSS-Q-ST-40_0440284",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.4a","Requirement","ECSS-Q-ST-40_0440285",1,"Created","Verification of unique safety required design or operational characteristics shall form part of the development, qualification or acceptance testing programmes as appropriate. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.5a","Requirement","ECSS-Q-ST-40_0440286",1,"Created","Where full-scale testing is not performed, equivalent safety verification method based on technically representative hardware or models shall be justified, approved and performed. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.4.5b","Requirement","ECSS-Q-ST-40_0440287",1,"Created","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)."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.5.1a","Requirement","ECSS-Q-ST-40_0440288",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.5.1b","Requirement","ECSS-Q-ST-40_0440289",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.5.1c","Requirement","ECSS-Q-ST-40_0440290",1,"Created","If the safety verification constrains any ground operations, the safety manager shall give notification to the safety review panel."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.5.2a","Requirement","ECSS-Q-ST-40_0440291",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","8.6a","Requirement","ECSS-Q-ST-40_0440292",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.1<1>a","Requirement","ECSS-Q-ST-40_0440293",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.1<1>b","Requirement","ECSS-Q-ST-40_0440294",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.1<2>a","Requirement","ECSS-Q-ST-40_0440295",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.1<3>a","Requirement","ECSS-Q-ST-40_0440296",1,"Created","The plan shall describe how safety-related activities and requirements are defined for and controlled at suppliers’ and lower tier suppliers’ premises."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.1<4>a","Requirement","ECSS-Q-ST-40_0440297",1,"Created","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. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","B.2.2a","Permission","ECSS-Q-ST-40_0440321",1,"Created","The safety programme plan may be incorporated within the Product Assurance Plan when agreed between the relevant parties."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<1>a","Requirement","ECSS-Q-ST-40_0440299",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<2>a","Requirement","ECSS-Q-ST-40_0440300",1,"Created","For each verification item to be tracked a unique identifier shall be used."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<2>b","Requirement","ECSS-Q-ST-40_0440301",1,"Created","The SVTL shall use the designations assigned by the safety manager."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<3>a","Requirement","ECSS-Q-ST-40_0440302",1,"Created","The identification number of the hazard report containing the verification item shall be indicated."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<4>a","Requirement","ECSS-Q-ST-40_0440303",1,"Created","The verification method or the verification means shall be transferred from the hazard report including the procedures by number and title."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<5>a","Requirement","ECSS-Q-ST-40_0440304",1,"Created","The input of “yes” or “no” shall indicate whether this safety verification constrains any ground operations."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<5>b","Requirement","ECSS-Q-ST-40_0440305",1,"Created","If “yes” for flight tracking log: an attachment shall be provided that identifies which ground operation is constrained."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<5>c","Requirement","ECSS-Q-ST-40_0440306",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<6>a","Requirement","ECSS-Q-ST-40_0440307",1,"Created","The input of \"yes\" or \"no\" shall indicate whether the verification has to be performed independently (in accordance with 8.4.5b). "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<7>a","Requirement","ECSS-Q-ST-40_0440308",1,"Created","The planned date for the completion of the verification shall be indicated."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<8>a","Requirement","ECSS-Q-ST-40_0440309",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","C.2.1<8>b","Permission","ECSS-Q-ST-40_0440322",1,"Created","Any appropriate information or remarks may be added."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<1>a","Requirement","ECSS-Q-ST-40_0440311",1,"Created","Title - The title of the safety analysis report shall identify the applicable project. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<1>b","Requirement","ECSS-Q-ST-40_0440312",1,"Created","Title page - A title page shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<1>c","Requirement","ECSS-Q-ST-40_0440313",1,"Created","Contents - A contents list shall be provided. "]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<1>d","Requirement","ECSS-Q-ST-40_0440314",1,"Created","Foreword - A foreword shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<1>e","Requirement","ECSS-Q-ST-40_0440315",1,"Created","Introduction - An introduction shall be provided."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<2>a","Requirement","ECSS-Q-ST-40_0440316",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<2>b","Requirement","ECSS-Q-ST-40_0440317",1,"Created","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."]
["ECSS-Q-ST-40C","ECSS - Superseded v0.9","D.2.1<2>c","Requirement","ECSS-Q-ST-40_0440318",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.2a","Requirement","ECSS-Q-ST-70-26_0130001",1,"Created","The supplier shall provide cleaning services for production facilities of high reliability crimping."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.2b","Requirement","ECSS-Q-ST-70-26_0130002",1,"Created","The areas, in which crimping is carried out, shall be maintained in an orderly fashion."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.2c","Requirement","ECSS-Q-ST-70-26_0130003",1,"Created","Loose material that can cause contamination of the crimped connection shall be removed. \n    NOTE For example: Dirt, dust, oils and clipped wires."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.2d","Requirement","ECSS-Q-ST-70-26_0130004",1,"Created","Furniture shall be kept to a minimum in the work areas and be arranged to allow easy and thorough cleaning of the floor."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.2e","Requirement","ECSS-Q-ST-70-26_0130005",1,"Created","Working surfaces shall be covered with an easily cleaned hard top or have a replaceable surface of clean, non-corrosive silicone-free paper."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.3a","Requirement","ECSS-Q-ST-70-26_0130006",1,"Created","The crimping area shall have a controlled environment, which limits entry of contamination. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.3b","Requirement","ECSS-Q-ST-70-26_0130007",1,"Created","The area shall be continuously controlled as follows:\n    1. room temperature:(22 ± 3) °C;\n    2. relative humidity: (55 ± 10) %."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.3c","Requirement","ECSS-Q-ST-70-26_0130008",1,"Created","The workstations shall not be exposed to draughts."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.3d","Requirement","ECSS-Q-ST-70-26_0130009",1,"Created","Fresh air shall be supplied to the room through a filtering system with positive pressure difference with regard to adjacent rooms."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.3e","Requirement","ECSS-Q-ST-70-26_0130010",1,"Created","The exhaust air shall be suitably restricted."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.4a","Requirement","ECSS-Q-ST-70-26_0130011",1,"Created","The supplier shall ensure adequate illumination conditions of the crimp workstations."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.4b","Requirement","ECSS-Q-ST-70-26_0130012",1,"Created","The light intensity shall be 1 080 lux on the work surface. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.1.4c","Requirement","ECSS-Q-ST-70-26_0130013",1,"Created","90 % of the work area shall be shadowless and without severe reflections."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1a","Requirement","ECSS-Q-ST-70-26_0130014",1,"Created","The supplier shall provide the tooling necessary for continued high quality crimping."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1b","Requirement","ECSS-Q-ST-70-26_0130015",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1c","Requirement","ECSS-Q-ST-70-26_0130016",1,"Created","Tools shall be marked to show the size and type of termination for which it is calibrated."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1d","Requirement","ECSS-Q-ST-70-26_0130017",1,"Created","Tool calibration shall be verified once each shift in conformance with the clause 5.5.5 requirements."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1e","Requirement","ECSS-Q-ST-70-26_0130018",1,"Created","Proper operation of the integral ratcheting mechanism or the positive stops on pneumatic tools shall be verified as defined in clause 5.5.6."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1f","Requirement","ECSS-Q-ST-70-26_0130019",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1g","Requirement","ECSS-Q-ST-70-26_0130020",1,"Created","If the tool settings seals are broken, the tool shall be returned immediately for recalibration."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.1h","Requirement","ECSS-Q-ST-70-26_0130021",1,"Created","Tools used in the crimping operation shall be clean; excess lubricants shall be removed before crimping starts."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.2a","Requirement","ECSS-Q-ST-70-26_0130022",1,"Created","The supplier shall provide the tooling necessary to avoid damage to the conductor."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.2b","Requirement","ECSS-Q-ST-70-26_0130023",1,"Created","The selection of thermal or precision cutting devices, manual or automatic power-driven, shall provide protection of the conductor strands. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.2c","Requirement","ECSS-Q-ST-70-26_0130024",1,"Created","Wire stretching by use of mechanical strippers shall be avoided."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.2d","Requirement","ECSS-Q-ST-70-26_0130025",1,"Created","The conductor shall not be twisted, ringed, nicked, cut or scored by stripping operation."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.2e","Requirement","ECSS-Q-ST-70-26_0130026",1,"Created","Both thermal and mechanical stripping tools shall be calibrated periodically on sample evaluation during a production run."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.3a","Requirement","ECSS-Q-ST-70-26_0130027",1,"Created","The supplier shall provide the tooling necessary for precision wire trimming and cutting."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.3b","Requirement","ECSS-Q-ST-70-26_0130028",1,"Created","The cutter used for trimming conductor wire shall shear sharply and consistently produce a clean, flat, smooth-cut surface along the entire cutting edge. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.3c","Requirement","ECSS-Q-ST-70-26_0130029",1,"Created","Twisting action during cutting operation shall be avoided. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.3d","Requirement","ECSS-Q-ST-70-26_0130030",1,"Created","Smooth, long-nose pliers or tweezers shall be used for attaching or removing conductor wire."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.3e","Requirement","ECSS-Q-ST-70-26_0130031",1,"Created","The cutting edges of pliers shall be regularly checked for damage and maintained in a sharp condition."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.1.2.4a","Requirement","ECSS-Q-ST-70-26_0130032",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-70-26_0130033",1,"Created","The supplier shall visually examine wire, terminal and connector contacts for cleanliness, absence of oil films and freedom from tarnish or corrosion before assembly."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-Q-ST-70-26_0130034",1,"Created","The supplier shall perform cleaning of the work pieces in conformance with ECSS-Q-ST-70-08. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1c","Requirement","ECSS-Q-ST-70-26_0130035",1,"Created","Further cleaning or other treatment shall not be carried out."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1d","Requirement","ECSS-Q-ST-70-26_0130036",1,"Created","The supplier shall handle work pieces with clean lint free gloves or finger cots."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1e","Requirement","ECSS-Q-ST-70-26_0130037",1,"Created","Before a crimping activity, tools at the operator’s station shall be verified to conform to those selected in accordance with the applicable PID."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1f","Requirement","ECSS-Q-ST-70-26_0130038",1,"Created","All conductor strands shall be inserted cleanly into the barrel without any buckling. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1g","Requirement","ECSS-Q-ST-70-26_0130039",1,"Created","Strands shall not be left outside or cut back to reduce the conductor diameter to fit an undersized barrel. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1h","Requirement","ECSS-Q-ST-70-26_0130040",1,"Created","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"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1i","Requirement","ECSS-Q-ST-70-26_0130041",1,"Created","The supplier shall take provisions to avoid degradation of the silver plated wire caused by tarnish during storage. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.1j","Requirement","ECSS-Q-ST-70-26_0130042",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2a","Requirement","ECSS-Q-ST-70-26_0130043",1,"Created","The supplier shall use silver plated copper multi stranded wire and braided shield cable in crimp type connectors. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2b","Requirement","ECSS-Q-ST-70-26_0130044",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2c","Requirement","ECSS-Q-ST-70-26_0130045",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2d","Requirement","ECSS-Q-ST-70-26_0130046",1,"Created","The supplier shall use space-qualified components having gold plated terminals in conformance with ECSS-Q-ST-60."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2e","Requirement","ECSS-Q-ST-70-26_0130047",1,"Created","Specific terminals such as ferrules, splices and lugs shall be purchased to MIL or SAE-AS-7928 specifications. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2f","Requirement","ECSS-Q-ST-70-26_0130048",1,"Created","When gold plating is not available the finish shall be in conformance with ECSS-Q-ST-70-71."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.2g","Requirement","ECSS-Q-ST-70-26_0130049",1,"Created","Cadmium, chromate-coated cadmium and non-fused tin-plating shall not be used."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.3a","Requirement","ECSS-Q-ST-70-26_0130050",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.3b","Requirement","ECSS-Q-ST-70-26_0130051",1,"Created","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"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.3c","Requirement","ECSS-Q-ST-70-26_0130052",1,"Created","The results of the review shall be documented in a PID in conformance with DRD of ECSS-Q-ST-70-38."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4a","Requirement","ECSS-Q-ST-70-26_0130053",1,"Created","The supplier shall give preference to the selection of single wire interconnections."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4b","Requirement","ECSS-Q-ST-70-26_0130054",1,"Created","The supplier shall not use strands of wire doubled backed to increase the conductor diameter."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4c","Requirement","ECSS-Q-ST-70-26_0130055",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4d","Requirement","ECSS-Q-ST-70-26_0130056",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4e","Requirement","ECSS-Q-ST-70-26_0130057",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.4f","Requirement","ECSS-Q-ST-70-26_0130058",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5a","Requirement","ECSS-Q-ST-70-26_0130059",1,"Created","Requirements of this clause shall be applied when single wire crimping cannot be used."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5b","Requirement","ECSS-Q-ST-70-26_0130060",1,"Created","The maximum number of wires in one crimp barrel shall be two."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5c","Requirement","ECSS-Q-ST-70-26_0130061",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5d","Requirement","ECSS-Q-ST-70-26_0130062",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5e","Requirement","ECSS-Q-ST-70-26_0130063",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.5f","Requirement","ECSS-Q-ST-70-26_0130064",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.6a","Requirement","ECSS-Q-ST-70-26_0130065",1,"Created","The shielded wires on coaxial cables shall be braided."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.6b","Requirement","ECSS-Q-ST-70-26_0130066",1,"Created","Axial strength measurements shall be performed only on the shield after removal of the core dielectric."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.6c","Requirement","ECSS-Q-ST-70-26_0130067",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7a","Requirement","ECSS-Q-ST-70-26_0130068",1,"Created","Tools specified by the manufacturer of the terminals shall be used."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7b","Requirement","ECSS-Q-ST-70-26_0130069",1,"Created","The maximum number of wires shall be ten."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7c","Requirement","ECSS-Q-ST-70-26_0130070",1,"Created","Seven wires maximum shall be on the same side."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7d","Requirement","ECSS-Q-ST-70-26_0130071",1,"Created","All conductors shall be of the same material and within a size range of 4 wire gauges on the same side."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7e","Requirement","ECSS-Q-ST-70-26_0130072",1,"Created","All conductors shall be positioned parallel in the terminal before crimping."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7f","Requirement","ECSS-Q-ST-70-26_0130073",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7g","Requirement","ECSS-Q-ST-70-26_0130074",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.2.7h","Requirement","ECSS-Q-ST-70-26_0130075",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.1a","Requirement","ECSS-Q-ST-70-26_0130076",1,"Created","Requirement of this clause shall be applied to crimp configurations that are not specified in clauses 5.2.4 to 5.2.7"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.1b","Requirement","ECSS-Q-ST-70-26_0130077",1,"Created","The supplier shall document the data of successful process qualification in the PID format to ensure continued high quality of production performance."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.1c","Requirement","ECSS-Q-ST-70-26_0130078",1,"Created","An approved PID and additional relevant data from a previous project shall be presented to substantiate a RFA."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.2a","Requirement","ECSS-Q-ST-70-26_0130079",1,"Created","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"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.2b","Requirement","ECSS-Q-ST-70-26_0130080",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.2c","Requirement","ECSS-Q-ST-70-26_0130081",1,"Created","Test data shall be recorded for PID justification."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.3.3a","Requirement","ECSS-Q-ST-70-26_0130082",1,"Created","The supplier shall seal and mark calibrated tools in conformance with clause 5.5.6.3 requirements."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.1a","Requirement","ECSS-Q-ST-70-26_0130083",1,"Created","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). "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.1b","Requirement","ECSS-Q-ST-70-26_0130084",1,"Created","Test samples shall meet the requirements of clause 5.5.4.1. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.1c","Requirement","ECSS-Q-ST-70-26_0130085",1,"Created","Records of all results shall be tabulated in conformance with 5.5.7. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.2a","Requirement","ECSS-Q-ST-70-26_0130086",1,"Created","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). "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.2b","Requirement","ECSS-Q-ST-70-26_0130087",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.2c","Requirement","ECSS-Q-ST-70-26_0130088",1,"Created","The voltage drop of the contact crimp joint shall not exceed the value specified in Table 5-2 for each wire tested."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.1a","Requirement","ECSS-Q-ST-70-26_0130089",1,"Created","The supplier shall use a tensile testing device with characteristics in conformance with Table 5-1. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.1b","Requirement","ECSS-Q-ST-70-26_0130090",1,"Created","The connections shall be loaded until failure occurs. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.1c","Requirement","ECSS-Q-ST-70-26_0130091",1,"Created","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”. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.1d","Requirement","ECSS-Q-ST-70-26_0130092",1,"Created","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"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.2a","Requirement","ECSS-Q-ST-70-26_0130093",1,"Created","The required axial strength shall be 75 % of the wire strength."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.2b","Requirement","ECSS-Q-ST-70-26_0130094",1,"Created","Axial strength for copper and copper-alloy wires having either silver-, tin- or nickel-plated finishes shall be as specified in Table 5-3."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.3.3a","Requirement","ECSS-Q-ST-70-26_0130095",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4a","Requirement","ECSS-Q-ST-70-26_0130096",1,"Created","The supplier shall employ a certified laboratory to perform the metallographic tests described below."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4b","Requirement","ECSS-Q-ST-70-26_0130097",1,"Created","The customer shall approve the certification status of the laboratory."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4c","Requirement","ECSS-Q-ST-70-26_0130098",1,"Created","The joint to be sectioned shall be mounted in a low exotherm resin capable of being moulded without the application of external pressure. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4d","Requirement","ECSS-Q-ST-70-26_0130099",1,"Created","The joint shall be oriented that the wire is perpendicular to the polishing surface. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4e","Requirement","ECSS-Q-ST-70-26_0130100",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4f","Requirement","ECSS-Q-ST-70-26_0130101",1,"Created","This section shall then be polished with successively finer grades of diamond paste down to 1 µm. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4g","Requirement","ECSS-Q-ST-70-26_0130102",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4h","Requirement","ECSS-Q-ST-70-26_0130103",1,"Created","The section shall be examined in both as-polished and etched states using a metallographic microscope at a magnification up to ´400."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.4.4i","Requirement","ECSS-Q-ST-70-26_0130104",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-Q-ST-70-26_0130105",1,"Created","The supplier shall install a Quality Assurance (QA) function in conformance with the requirements as defined in ECSS-Q-ST-20. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.1b","Requirement","ECSS-Q-ST-70-26_0130106",1,"Created","The quality control process shall be as specified in Figure 5-7."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.1a","Requirement","ECSS-Q-ST-70-26_0130107",1,"Created","The supplier shall employ trained and competent personnel for all crimping operations. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.1b","Requirement","ECSS-Q-ST-70-26_0130108",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.2a","Requirement","ECSS-Q-ST-70-26_0130109",1,"Created","Trained personnel, performing crimping operations, shall be certified according to a customer approved process "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.2b","Requirement","ECSS-Q-ST-70-26_0130110",1,"Created","The certification of personnel shall be based upon objective evidence of crimp quality, resulting from test and inspection of the crimped joints. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.2c","Requirement","ECSS-Q-ST-70-26_0130111",1,"Created","Operators or inspectors shall be re-certified in cases of repeatedly unacceptable quality levels and changes in crimping techniques, parameters or required skills."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.2d","Requirement","ECSS-Q-ST-70-26_0130112",1,"Created","The supplier shall perform training and certification at a school authorized by the customer."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.2.3a","Requirement","ECSS-Q-ST-70-26_0130113",1,"Created","The supplier shall maintain records of the training and certification status of crimping operators and inspection personnel."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.3a","Requirement","ECSS-Q-ST-70-26_0130114",1,"Created","The supplier shall prepare standards consisting of satisfactory work samples (in conformance with the Figure 5-8 and Figure 5-9)"]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.3b","Requirement","ECSS-Q-ST-70-26_0130115",1,"Created","The supplier shall have readily available visual aids, which clearly illustrate the quality characteristics of all crimped connections utilized. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.3c","Requirement","ECSS-Q-ST-70-26_0130116",1,"Created","Defects such as those listed in clause 5.5.4.2 and shown in Figure 5-8 shall be included as examples."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.3d","Requirement","ECSS-Q-ST-70-26_0130117",1,"Created","The operator shall discard production crimps which in his judgement are defective."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.3e","Requirement","ECSS-Q-ST-70-26_0130118",1,"Created","Defective test samples shall not be discarded."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.1a","Requirement","ECSS-Q-ST-70-26_0130119",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.1b","Requirement","ECSS-Q-ST-70-26_0130120",1,"Created","Damaged wires where the base material is exposed shall not be used. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.1c","Requirement","ECSS-Q-ST-70-26_0130121",1,"Created","Contacts and terminal barrels that show evidence of the presence of tarnish, corrosion or physical damage, including bent contacts, shall not be used."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.1d","Requirement","ECSS-Q-ST-70-26_0130122",1,"Created","Inspection shall verify that wire size and type, the contact and terminal are as specified in the drawing or control document."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.2a","Requirement","ECSS-Q-ST-70-26_0130123",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.2b","Requirement","ECSS-Q-ST-70-26_0130124",1,"Created","The inspector shall not physically disturb parts and conductor leads to aid inspection. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.2c","Requirement","ECSS-Q-ST-70-26_0130125",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.4.2d","Requirement","ECSS-Q-ST-70-26_0130126",1,"Created","Failure to meet the acceptance criteria of 5.5.4.2c shall be cause for rejection."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5a","Requirement","ECSS-Q-ST-70-26_0130127",1,"Created","Each operator shall prepare four samples at the beginning of a shift or before a series of crimping operations."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5b","Requirement","ECSS-Q-ST-70-26_0130128",1,"Created","At the end of the operation four further samples shall be crimped. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5c","Requirement","ECSS-Q-ST-70-26_0130129",1,"Created","Alternatively the supplier shall keep a logbook for each tool. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5d","Requirement","ECSS-Q-ST-70-26_0130130",1,"Created","The logbook shall show the quantity of parts crimped since each calibration and since each go/no-go operation. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5e","Requirement","ECSS-Q-ST-70-26_0130131",1,"Created","Four samples shall be crimped after each 100 crimping operations have been performed."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5f","Requirement","ECSS-Q-ST-70-26_0130132",1,"Created","A tool shall be changed whenever a wire size or contact size is changed. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5g","Requirement","ECSS-Q-ST-70-26_0130133",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5h","Requirement","ECSS-Q-ST-70-26_0130134",1,"Created","In each case, the operator shall submit three samples to the tensile strength test detailed in clause 5.4.3. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5i","Requirement","ECSS-Q-ST-70-26_0130135",1,"Created","The fourth sample shall be retained for reference and traceability purposes (in conformance with clause 5.5.6.2 requirements)."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.5j","Requirement","ECSS-Q-ST-70-26_0130136",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.1a","Requirement","ECSS-Q-ST-70-26_0130137",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.1b","Requirement","ECSS-Q-ST-70-26_0130138",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.1c","Requirement","ECSS-Q-ST-70-26_0130139",1,"Created","The QA organization of the supplier shall notify the customer of the nonconformance details."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.1d","Requirement","ECSS-Q-ST-70-26_0130140",1,"Created","The supplier’s calibration procedure shall include the requirements specified in this clause for tool calibration."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.2a","Requirement","ECSS-Q-ST-70-26_0130141",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.2b","Requirement","ECSS-Q-ST-70-26_0130142",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.2c","Requirement","ECSS-Q-ST-70-26_0130143",1,"Created","After satisfactory calibration the tool status shall be documented in a “tool calibration sheet” to ensure tool traceability."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.2d","Requirement","ECSS-Q-ST-70-26_0130144",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.2e","Requirement","ECSS-Q-ST-70-26_0130145",1,"Created","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)."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.3a","Requirement","ECSS-Q-ST-70-26_0130146",1,"Created","The supplier shall provide sealing for calibrated crimping tools to ensure against unauthorized alteration of adjustment settings. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.3b","Requirement","ECSS-Q-ST-70-26_0130147",1,"Created","A wire and lead seal method shall be used if the tool has provisions for it; "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.3c","Requirement","ECSS-Q-ST-70-26_0130148",1,"Created","Alternatively, the tool shall be sealed by a non-reusable decal seal, which, if the calibrated setting is altered, is visibly damaged. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.3d","Requirement","ECSS-Q-ST-70-26_0130149",1,"Created","Seals shall be placed on all external adjustment points of the tool."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.4a","Requirement","ECSS-Q-ST-70-26_0130150",1,"Created","Tools that are out of calibration shall be returned to the tool facility for readjustment and calibration. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.6.4b","Requirement","ECSS-Q-ST-70-26_0130151",1,"Created","Tools that are worn or damaged shall be identified as rejected and removed from the fabrication area."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.7a","Requirement","ECSS-Q-ST-70-26_0130152",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.7b","Requirement","ECSS-Q-ST-70-26_0130153",1,"Created","Quality records and logbooks shall be retained for at least ten years "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.7c","Requirement","ECSS-Q-ST-70-26_0130154",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.8a","Requirement","ECSS-Q-ST-70-26_0130155",1,"Created","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. "]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.5.8b","Requirement","ECSS-Q-ST-70-26_0130156",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.6a","Requirement","ECSS-Q-ST-70-26_0130157",1,"Created","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."]
["ECSS-Q-ST-70-26C","ECSS - Superseded v0.9","5.6b","Requirement","ECSS-Q-ST-70-26_0130158",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.1a","Requirement","ECSS-Q-ST-80_0720001",1,"Created","The supplier shall ensure that an organizational structure is defined for software development, and that individuals have defined tasks and responsibilities."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.2.1a","Requirement","ECSS-Q-ST-80_0720002",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.2.2a","Requirement","ECSS-Q-ST-80_0720003",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.2.3a","Requirement","ECSS-Q-ST-80_0720004",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.3.1a","Requirement","ECSS-Q-ST-80_0720005",1,"Created","The supplier shall provide adequate resources to perform the required software product assurance tasks.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; SRR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.3.2a","Requirement","ECSS-Q-ST-80_0720006",1,"Created","Reviews and audits of processes and of products shall be carried out by personnel not directly involved in the work being performed."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.4.1a","Requirement","ECSS-Q-ST-80_0720007",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.4.2a","Requirement","ECSS-Q-ST-80_0720008",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.5.1a","Requirement","ECSS-Q-ST-80_0720009",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.5.2a","Requirement","ECSS-Q-ST-80_0720010",1,"Created","The supplier shall maintain training records.\n","EXPECTED OUTPUT: Records of training and experience [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.5.3a","Requirement","ECSS-Q-ST-80_0720011",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.1.5.4a","Requirement","ECSS-Q-ST-80_0720012",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.1a","Requirement","ECSS-Q-ST-80_0720013",1,"Created","The supplier shall develop a software product assurance plan in response to the software product assurance requirements in conformance with DRD in annex B."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.1b","Requirement","ECSS-Q-ST-80_0720014",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.2a","Requirement","ECSS-Q-ST-80_0720015",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.3a","Requirement","ECSS-Q-ST-80_0720016",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.4a","Requirement","ECSS-Q-ST-80_0720017",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.5a","Requirement","ECSS-Q-ST-80_0720018",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.1.5b","Requirement","ECSS-Q-ST-80_0720019",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.2.1a","Requirement","ECSS-Q-ST-80_0720020",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.2.2a","Requirement","ECSS-Q-ST-80_0720021",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.2.3a","Requirement","ECSS-Q-ST-80_0720022",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.3a","Requirement","ECSS-Q-ST-80_0720023",1,"Created","For software audits, ECSS-Q-ST-10 clause 5.2.3 shall apply.\n","EXPECTED OUTPUT: Audit plan and schedule [PAF, -; SRR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.4a","Requirement","ECSS-Q-ST-80_0720024",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.5.1a","Requirement","ECSS-Q-ST-80_0720025",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.5.2a","Requirement","ECSS-Q-ST-80_0720026",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.5.3a","Requirement","ECSS-Q-ST-80_0720027",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.5.4a","Requirement","ECSS-Q-ST-80_0720028",1,"Created","The supplier shall ensure the correct application of problem reporting procedures."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.6.1a","Requirement","ECSS-Q-ST-80_0720029",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.6.1b","Requirement","ECSS-Q-ST-80_0720030",1,"Created","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]"]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.6.2a","Requirement","ECSS-Q-ST-80_0720031",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.7.1a","Requirement","ECSS-Q-ST-80_0720032",1,"Created","Quality models shall be used to specify the software quality requirements.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.2.7.2a","Requirement","ECSS-Q-ST-80_0720033",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.3.1a","Requirement","ECSS-Q-ST-80_0720034",1,"Created","Risk management for software shall be performed by cross-reference to the project risk policy, as specified in ECSS-M-ST-80."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.3.2.1a","Requirement","ECSS-Q-ST-80_0720035",1,"Created","For critical item control, ECSS-Q-ST-10-04 shall apply."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.3.2.2a","Requirement","ECSS-Q-ST-80_0720036",1,"Created","The supplier shall identify the characteristics of the software items that qualify them for inclusion in the Critical Item List."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.1.1a","Requirement","ECSS-Q-ST-80_0720037",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.1.2a","Requirement","ECSS-Q-ST-80_0720038",1,"Created","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; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.2.1a","Requirement","ECSS-Q-ST-80_0720039",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.2.2a","Requirement","ECSS-Q-ST-80_0720040",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.3.1a","Requirement","ECSS-Q-ST-80_0720041",1,"Created","The supplier shall monitor the next lower level suppliers’ conformance to the product assurance requirements. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.3.2a","Requirement","ECSS-Q-ST-80_0720042",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.3.3a","Requirement","ECSS-Q-ST-80_0720043",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.3.4a","Requirement","ECSS-Q-ST-80_0720044",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.4.4a","Requirement","ECSS-Q-ST-80_0720045",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-Q-ST-80_0720046",1,"Created","For procurement documents, ECSS-Q-ST-20 clause 5.4.2 shall apply."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-80_0720047",1,"Created","The choice of procured software shall be described and submitted for customer review.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; SRR, PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.3a","Requirement","ECSS-Q-ST-80_0720048",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.4a","Requirement","ECSS-Q-ST-80_0720049",1,"Created","All the procured software shall be identified and registered by configuration management."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.5a","Requirement","ECSS-Q-ST-80_0720050",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.5.6a","Requirement","ECSS-Q-ST-80_0720051",1,"Created","Exportability constraints shall be identified."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.1.1a","Requirement","ECSS-Q-ST-80_0720052",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.1.2a","Requirement","ECSS-Q-ST-80_0720053",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.1.3a","Requirement","ECSS-Q-ST-80_0720054",1,"Created","The correct use of methods and tools shall be verified and reported. \n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.2.1a","Requirement","ECSS-Q-ST-80_0720055",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.2.2a","Requirement","ECSS-Q-ST-80_0720056",1,"Created","The suitability of the software development environment shall be justified.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; SRR, PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.6.2.3a","Requirement","ECSS-Q-ST-80_0720057",1,"Created","The availability of the software development environment to developers and other users shall be verified before the start of each development phase."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.1a","Requirement","ECSS-Q-ST-80_0720058",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.2.1a","Requirement","ECSS-Q-ST-80_0720059",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.2.2a","Requirement","ECSS-Q-ST-80_0720060",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.2.3a","Requirement","ECSS-Q-ST-80_0720061",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.2.4a","Requirement","ECSS-Q-ST-80_0720062",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.3.1a","Requirement","ECSS-Q-ST-80_0720063",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.3.1b","Requirement","ECSS-Q-ST-80_0720064",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.3.2a","Requirement","ECSS-Q-ST-80_0720065",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","5.7.3.3a","Requirement","ECSS-Q-ST-80_0720066",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.1a","Requirement","ECSS-Q-ST-80_0720067",1,"Created","The software development life cycle shall be defined or referenced in the software product assurance plan."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.1b","Requirement","ECSS-Q-ST-80_0720068",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.2a","Requirement","ECSS-Q-ST-80_0720069",1,"Created","In the definition of the life cycle and associated milestones and documents, the quality objectives shall be used."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.3a","Requirement","ECSS-Q-ST-80_0720070",1,"Created","The software life cycle shall be reviewed against the contractual software engineering and product assurance requirements. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.4a","Requirement","ECSS-Q-ST-80_0720071",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.1.5a","Requirement","ECSS-Q-ST-80_0720072",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.1a","Requirement","ECSS-Q-ST-80_0720073",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.2a","Requirement","ECSS-Q-ST-80_0720074",1,"Created","All plans shall be finalized before the start of the related activities.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.3a","Requirement","ECSS-Q-ST-80_0720075",1,"Created","All plans shall be updated for each milestone to reflect any changes during development.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.4a","Requirement","ECSS-Q-ST-80_0720076",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.5a","Requirement","ECSS-Q-ST-80_0720077",1,"Created","Each plan shall be reviewed against the relevant contractual requirements. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.6a","Requirement","ECSS-Q-ST-80_0720078",1,"Created","Procedures and project standards shall address all types of software products included in the project.\n","EXPECTED OUTPUT: Procedures and standards [PAF, -; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.7a","Requirement","ECSS-Q-ST-80_0720079",1,"Created","All procedures and project standards shall be finalized before starting the related activities.\n","EXPECTED OUTPUT: Procedures and standards [PAF, -; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.8a","Requirement","ECSS-Q-ST-80_0720080",1,"Created","Each procedure or standard shall be reviewed against the relevant plans and contractual requirements."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.1.9a","Requirement","ECSS-Q-ST-80_0720081",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.1a","Requirement","ECSS-Q-ST-80_0720082",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.2a","Requirement","ECSS-Q-ST-80_0720083",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.3a","Requirement","ECSS-Q-ST-80_0720084",1,"Created","The supplier shall identify the methods and techniques for the software dependability and safety analysis to be performed at technical specification and design level."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.3b","Requirement","ECSS-Q-ST-80_0720085",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.4a","Requirement","ECSS-Q-ST-80_0720086",1,"Created","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)."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.5a","Requirement","ECSS-Q-ST-80_0720087",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.6a","Requirement","ECSS-Q-ST-80_0720088",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.7a","Requirement","ECSS-Q-ST-80_0720089",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.8a","Requirement","ECSS-Q-ST-80_0720090",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.2.9a","Requirement","ECSS-Q-ST-80_0720091",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.1a","Requirement","ECSS-Q-ST-80_0720092",1,"Created","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). "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.1b","Requirement","ECSS-Q-ST-80_0720093",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.2a","Requirement","ECSS-Q-ST-80_0720094",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.3a","Requirement","ECSS-Q-ST-80_0720095",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.4a","Requirement","ECSS-Q-ST-80_0720096",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.5a","Requirement","ECSS-Q-ST-80_0720097",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.6a","Requirement","ECSS-Q-ST-80_0720098",1,"Created","Identified unreachable code shall be removed and the need for re-verification and re-validation shall be analysed. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.7a","Requirement","ECSS-Q-ST-80_0720099",1,"Created","Unit and integration testing shall be (re-)executed on non-instrumented code."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.3.8a","Requirement","ECSS-Q-ST-80_0720100",1,"Created","Validation testing shall be (re-)executed on non-instrumented code."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.1a","Requirement","ECSS-Q-ST-80_0720101",1,"Created","ECSS-M-ST-40 shall be applied for software configuration management, complemented by the following requirements."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.2a","Requirement","ECSS-Q-ST-80_0720102",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.3a","Requirement","ECSS-Q-ST-80_0720103",1,"Created","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; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.4a","Requirement","ECSS-Q-ST-80_0720104",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.5a","Requirement","ECSS-Q-ST-80_0720105",1,"Created","Any components of the code generation tool that are customizable by the user shall be put under configuration control."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.5b","Requirement","ECSS-Q-ST-80_0720106",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.6a","Requirement","ECSS-Q-ST-80_0720107",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.7a","Requirement","ECSS-Q-ST-80_0720108",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.8a","Requirement","ECSS-Q-ST-80_0720109",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.9a","Requirement","ECSS-Q-ST-80_0720110",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.10a","Requirement","ECSS-Q-ST-80_0720111",1,"Created","The checksum value shall be provided in the software configuration file with each software delivery.\n","EXPECTED OUTPUT: Software configuration file [DDF, SCF; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.4.11a","Requirement","ECSS-Q-ST-80_0720112",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.5.1a","Requirement","ECSS-Q-ST-80_0720113",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.5.2a","Requirement","ECSS-Q-ST-80_0720114",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.5.3a","Requirement","ECSS-Q-ST-80_0720115",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.5.4a","Requirement","ECSS-Q-ST-80_0720116",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.5.5a","Requirement","ECSS-Q-ST-80_0720117",1,"Created","Metrics reports shall be included in the software product assurance reports.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.1a","Requirement","ECSS-Q-ST-80_0720118",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.2a","Requirement","ECSS-Q-ST-80_0720119",1,"Created","The outputs of each development activity shall be verified for conformance against pre-defined criteria."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.2b","Requirement","ECSS-Q-ST-80_0720120",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.3a","Requirement","ECSS-Q-ST-80_0720121",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.4a","Requirement","ECSS-Q-ST-80_0720122",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.5a","Requirement","ECSS-Q-ST-80_0720123",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.6a","Requirement","ECSS-Q-ST-80_0720124",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.7a","Requirement","ECSS-Q-ST-80_0720125",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.8a","Requirement","ECSS-Q-ST-80_0720126",1,"Created","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. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.9a","Requirement","ECSS-Q-ST-80_0720127",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.10a","Requirement","ECSS-Q-ST-80_0720128",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.11a","Requirement","ECSS-Q-ST-80_0720129",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.12a","Requirement","ECSS-Q-ST-80_0720130",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.13a","Requirement","ECSS-Q-ST-80_0720131",1,"Created","Independent software verification shall be performed by a third party."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.6.13b","Requirement","ECSS-Q-ST-80_0720132",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.2a","Requirement","ECSS-Q-ST-80_0720133",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.3a","Requirement","ECSS-Q-ST-80_0720134",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.4a","Requirement","ECSS-Q-ST-80_0720135",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.5a","Requirement","ECSS-Q-ST-80_0720136",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.6a","Requirement","ECSS-Q-ST-80_0720137",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.7a","Requirement","ECSS-Q-ST-80_0720138",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.8a","Requirement","ECSS-Q-ST-80_0720139",1,"Created","Reverse engineering techniques shall be applied to generate missing documentation and to reach the required verification and validation coverage."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.8b","Requirement","ECSS-Q-ST-80_0720140",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.9a","Requirement","ECSS-Q-ST-80_0720141",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.10a","Requirement","ECSS-Q-ST-80_0720142",1,"Created","All the reused software shall be kept under configuration control."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.7.11a","Requirement","ECSS-Q-ST-80_0720143",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.1a","Requirement","ECSS-Q-ST-80_0720144",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.2a","Requirement","ECSS-Q-ST-80_0720145",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.3a","Requirement","ECSS-Q-ST-80_0720146",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.4a","Requirement","ECSS-Q-ST-80_0720147",1,"Created","Modelling standards for automatic code generation tools shall be defined and applied.\n","EXPECTED OUTPUT: Modelling standards [PAF, -; SRR, PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.5a","Requirement","ECSS-Q-ST-80_0720148",1,"Created","Adherence to modelling standards shall be verified.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.6a","Requirement","ECSS-Q-ST-80_0720149",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.2.8.7a","Requirement","ECSS-Q-ST-80_0720150",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.1.1a","Requirement","ECSS-Q-ST-80_0720151",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.1.2a","Requirement","ECSS-Q-ST-80_0720152",1,"Created","The requirements baseline shall be subject to documentation control and configuration management as part of the development documentation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.1.3a","Requirement","ECSS-Q-ST-80_0720153",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.2.1a","Requirement","ECSS-Q-ST-80_0720154",1,"Created","The requirements baseline shall be analyzed to fully and unambiguously define the software requirements in the technical specification."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.2.2a","Requirement","ECSS-Q-ST-80_0720155",1,"Created","The technical specification shall be subject to documentation control and configuration management as part of the development documentation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.2.3a","Requirement","ECSS-Q-ST-80_0720156",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.2.4a","Requirement","ECSS-Q-ST-80_0720157",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.2.5a","Requirement","ECSS-Q-ST-80_0720158",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.1a","Requirement","ECSS-Q-ST-80_0720159",1,"Created","The design definition file shall be subject to documentation control and configuration management. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.2a","Requirement","ECSS-Q-ST-80_0720160",1,"Created","Mandatory and advisory design standards shall be defined and applied.\n","EXPECTED OUTPUT: Design standards [PAF, -; SRR, PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.3a","Requirement","ECSS-Q-ST-80_0720161",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.4a","Requirement","ECSS-Q-ST-80_0720162",1,"Created","Adherence to design standards shall be verified.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.5a","Requirement","ECSS-Q-ST-80_0720163",1,"Created","The supplier shall define means, criteria and tools to ensure that the complexity and modularity of the design meet the quality requirements."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.5b","Requirement","ECSS-Q-ST-80_0720164",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.6a","Requirement","ECSS-Q-ST-80_0720165",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.3.7a","Requirement","ECSS-Q-ST-80_0720166",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.1a","Requirement","ECSS-Q-ST-80_0720167",1,"Created","Coding standards (including consistent naming conventions and adequate commentary rules) shall be specified and observed.\n","EXPECTED OUTPUT: Coding standards [PAF, -; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.2a","Requirement","ECSS-Q-ST-80_0720168",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.3a","Requirement","ECSS-Q-ST-80_0720169",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.4a","Requirement","ECSS-Q-ST-80_0720170",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.5a","Requirement","ECSS-Q-ST-80_0720171",1,"Created","Use of low-level programming languages shall be justified.\n","EXPECTED OUTPUT: Software development plan [MGT, SDP; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.6a","Requirement","ECSS-Q-ST-80_0720172",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.6b","Requirement","ECSS-Q-ST-80_0720173",1,"Created","The code evaluation shall be performed in parallel with the coding process, in order to provide feedback to the software programmers."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.7a","Requirement","ECSS-Q-ST-80_0720174",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.4.8a","Requirement","ECSS-Q-ST-80_0720175",1,"Created","The code shall be put under configuration control immediately after successful unit testing."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.1a","Requirement","ECSS-Q-ST-80_0720176",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.2a","Requirement","ECSS-Q-ST-80_0720177",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.3a","Requirement","ECSS-Q-ST-80_0720178",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.4a","Requirement","ECSS-Q-ST-80_0720179",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.5a","Requirement","ECSS-Q-ST-80_0720180",1,"Created","Test coverage shall be checked with respect to the stated goals.\n","EXPECTED OUTPUT: Software product assurance reports [PAF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.5b","Requirement","ECSS-Q-ST-80_0720181",1,"Created","Feedback from the results of test coverage evaluation shall be continuously provided to the software developers."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.6a","Requirement","ECSS-Q-ST-80_0720182",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.7a","Requirement","ECSS-Q-ST-80_0720183",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.8a","Requirement","ECSS-Q-ST-80_0720184",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.9a","Requirement","ECSS-Q-ST-80_0720185",1,"Created","Provisions shall be made to allow witnessing of tests by the customer."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.10a","Requirement","ECSS-Q-ST-80_0720186",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.11a","Requirement","ECSS-Q-ST-80_0720187",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.12a","Requirement","ECSS-Q-ST-80_0720188",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.13a","Requirement","ECSS-Q-ST-80_0720189",1,"Created","The supplier shall confirm in writing that the tests are successfully completed.\n","EXPECTED OUTPUT: Testing and validation reports [DJF, -; CDR, QR, AR, ORR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.14a","Requirement","ECSS-Q-ST-80_0720190",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.15a","Requirement","ECSS-Q-ST-80_0720191",1,"Created","Areas affected by any modification shall be identified and re-tested (regression testing)."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.16a","Requirement","ECSS-Q-ST-80_0720192",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.17a","Requirement","ECSS-Q-ST-80_0720193",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.18a","Requirement","ECSS-Q-ST-80_0720194",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.19a","Requirement","ECSS-Q-ST-80_0720195",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.20a","Requirement","ECSS-Q-ST-80_0720196",1,"Created","Validation of the flight software against the requirement baseline on the flight equipment model shall be performed on a software version without any patch. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.21a","Requirement","ECSS-Q-ST-80_0720197",1,"Created","The supplier shall review the test documentation to ensure that it is up to date and organized to facilitate its reuse for maintenance."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.22a","Requirement","ECSS-Q-ST-80_0720198",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.23a","Requirement","ECSS-Q-ST-80_0720199",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.24a","Requirement","ECSS-Q-ST-80_0720200",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.25a","Requirement","ECSS-Q-ST-80_0720201",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.26a","Requirement","ECSS-Q-ST-80_0720202",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.27a","Requirement","ECSS-Q-ST-80_0720203",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.28a","Requirement","ECSS-Q-ST-80_0720204",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.29a","Requirement","ECSS-Q-ST-80_0720205",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.30a","Requirement","ECSS-Q-ST-80_0720206",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.31a","Requirement","ECSS-Q-ST-80_0720207",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.5.32a","Requirement","ECSS-Q-ST-80_0720208",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.1a","Requirement","ECSS-Q-ST-80_0720209",1,"Created","The roles, responsibilities and obligations of the supplier and customer during installation shall be established.\n","EXPECTED OUTPUT: Installation procedure [DDF, SCF; AR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.2a","Requirement","ECSS-Q-ST-80_0720210",1,"Created","The installation shall be performed in accordance with the installation procedure."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.3a","Requirement","ECSS-Q-ST-80_0720211",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.4a","Requirement","ECSS-Q-ST-80_0720212",1,"Created","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)."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.5a","Requirement","ECSS-Q-ST-80_0720213",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.6a","Requirement","ECSS-Q-ST-80_0720214",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.7a","Requirement","ECSS-Q-ST-80_0720215",1,"Created","Any discovered problems shall be documented in nonconformance reports.\n","EXPECTED OUTPUT: Nonconformance reports [DJF, -; AR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.8a","Requirement","ECSS-Q-ST-80_0720216",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.6.9a","Requirement","ECSS-Q-ST-80_0720217",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.7.1a","Requirement","ECSS-Q-ST-80_0720218",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.7.2a","Requirement","ECSS-Q-ST-80_0720219",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.7.3a","Requirement","ECSS-Q-ST-80_0720220",1,"Created","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]"]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.1a","Requirement","ECSS-Q-ST-80_0720221",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.2a","Requirement","ECSS-Q-ST-80_0720222",1,"Created","The maintenance organization shall specify the assurance, verification and validation activities applicable to maintenance interventions.\n","EXPECTED OUTPUT: Maintenance plan [MF, -; QR, AR, ORR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.3a","Requirement","ECSS-Q-ST-80_0720223",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.4a","Requirement","ECSS-Q-ST-80_0720224",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.5a","Requirement","ECSS-Q-ST-80_0720225",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.6a","Requirement","ECSS-Q-ST-80_0720226",1,"Created","All maintenance activities shall be logged in predefined formats and retained. \n","EXPECTED OUTPUT: Maintenance records [MF, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","6.3.8.7a","Requirement","ECSS-Q-ST-80_0720227",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.1a","Requirement","ECSS-Q-ST-80_0720228",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.2a","Requirement","ECSS-Q-ST-80_0720229",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.3a","Requirement","ECSS-Q-ST-80_0720230",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.4a","Requirement","ECSS-Q-ST-80_0720231",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.5a","Requirement","ECSS-Q-ST-80_0720232",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.6a","Requirement","ECSS-Q-ST-80_0720233",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.7a","Requirement","ECSS-Q-ST-80_0720234",1,"Created","Numerical accuracy shall be estimated and verified.\n","EXPECTED OUTPUT: Numerical accuracy analysis [DJF, SVR; PDR, CDR, QR]. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.1.8a","Requirement","ECSS-Q-ST-80_0720235",1,"Created","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, -; -]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.1.1a","Requirement","ECSS-Q-ST-80_0720236",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.1.2a","Requirement","ECSS-Q-ST-80_0720237",1,"Created","The software requirements shall be: \n    1. correct;\n    2. unambiguous;\n    3. complete;\n    4. consistent;\n    5. verifiable;\n    6. traceable."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.1.3a","Requirement","ECSS-Q-ST-80_0720238",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.2.1a","Requirement","ECSS-Q-ST-80_0720239",1,"Created","The software design shall meet the non-functional requirements as documented in the technical specification."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.2.2a","Requirement","ECSS-Q-ST-80_0720240",1,"Created","The software shall be designed to facilitate testing."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.2.3a","Requirement","ECSS-Q-ST-80_0720241",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.1a","Requirement","ECSS-Q-ST-80_0720242",1,"Created","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)."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.2a","Requirement","ECSS-Q-ST-80_0720243",1,"Created","The test documentation shall cover the test environment, tools and test software, personnel required and associated training requirements."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.3a","Requirement","ECSS-Q-ST-80_0720244",1,"Created","The criteria for completion of each test and any contingency steps shall be specified."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.4a","Requirement","ECSS-Q-ST-80_0720245",1,"Created","Test procedures, data and expected results shall be specified."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.5a","Requirement","ECSS-Q-ST-80_0720246",1,"Created","The hardware and software configuration shall be identified and documented as part of the test documentation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.2.3.6a","Requirement","ECSS-Q-ST-80_0720247",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.1a","Requirement","ECSS-Q-ST-80_0720248",1,"Created","For the development of software intended for reuse, ECSS-E-ST-40 clauses 5.2.4.7 and 5.4.3.6 shall apply."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.2a","Requirement","ECSS-Q-ST-80_0720249",1,"Created","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. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.3a","Requirement","ECSS-Q-ST-80_0720250",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.4a","Requirement","ECSS-Q-ST-80_0720251",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.5a","Requirement","ECSS-Q-ST-80_0720252",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.6a","Requirement","ECSS-Q-ST-80_0720253",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.3.7a","Requirement","ECSS-Q-ST-80_0720254",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.4.1a","Requirement","ECSS-Q-ST-80_0720255",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.4.2a","Requirement","ECSS-Q-ST-80_0720256",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.4.3a","Requirement","ECSS-Q-ST-80_0720257",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.4.4a","Requirement","ECSS-Q-ST-80_0720258",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.4.5a","Requirement","ECSS-Q-ST-80_0720259",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.5.1a","Requirement","ECSS-Q-ST-80_0720260",1,"Created","The supplier shall establish procedures for firmware device programming and duplication of firmware devices.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.5.2a","Requirement","ECSS-Q-ST-80_0720261",1,"Created","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]."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","7.5.3a","Requirement","ECSS-Q-ST-80_0720262",1,"Created","The supplier shall ensure that the firmware programming equipment is calibrated."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<1>a","Requirement","ECSS-Q-ST-80_0720263",1,"Created","The SPAP shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<2>a","Requirement","ECSS-Q-ST-80_0720264",1,"Created","The SPAP shall list the applicable and reference documents to support the generation of the document."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<3>a","Requirement","ECSS-Q-ST-80_0720265",1,"Created","The SPAP shall include any additional terms, definition or abbreviated terms used."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<4>a","Requirement","ECSS-Q-ST-80_0720266",1,"Created","The SPAP shall include or refer to a description of the system and software products being developed."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.1>a","Requirement","ECSS-Q-ST-80_0720267",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.1>b","Requirement","ECSS-Q-ST-80_0720268",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.2>a","Requirement","ECSS-Q-ST-80_0720269",1,"Created","The SPAP shall describe the responsibilities of the software product assurance function."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.3>a","Requirement","ECSS-Q-ST-80_0720270",1,"Created","The SPAP shall describe the resources to be used to perform the software product assurance function."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.3>b","Requirement","ECSS-Q-ST-80_0720271",1,"Created","The description in B.2.1<5.3>a shall include human resources and skills, hardware and software tools."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.4>a","Requirement","ECSS-Q-ST-80_0720272",1,"Created","The SPAP shall describe the reporting to be performed by software product assurance."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.5>a","Requirement","ECSS-Q-ST-80_0720273",1,"Created","The SPAP shall describe the quality models applicable to the project and how they are used to specify the quality requirements."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.6>a","Requirement","ECSS-Q-ST-80_0720274",1,"Created","The SPAP shall describe the contribution of the software product assurance function to the project risk management."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.7>a","Requirement","ECSS-Q-ST-80_0720275",1,"Created","The SPAP shall describe the contribution of the software product assurance function to the next level suppliers selection and control."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.8>a","Requirement","ECSS-Q-ST-80_0720276",1,"Created","The SPAP shall describe the methods and tools used for all the activities of the development cycle, and their level of maturity."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.9>a","Requirement","ECSS-Q-ST-80_0720277",1,"Created","1.The SPAP shall state the scope and objectives of process assessment."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.9>b","Requirement","ECSS-Q-ST-80_0720278",1,"Created","2.The SPAP shall describe the methods and tools to be used for process assessment and improvement."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<5.10>a","Requirement","ECSS-Q-ST-80_0720279",1,"Created","The SPAP shall specify the quality measures related to the operations and maintenance processes (alternatively, a separate SPAP is produced)."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.1>a","Requirement","ECSS-Q-ST-80_0720280",1,"Created","The SPAP shall refer to the software development cycle description in the software development plan. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.1>b","Requirement","ECSS-Q-ST-80_0720281",1,"Created","If not covered in the software development plan, the life cycle shall be described."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.1>c","Requirement","ECSS-Q-ST-80_0720282",1,"Created","The life cycle shall include a milestone immediately before the starting of the software validation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.2>a","Requirement","ECSS-Q-ST-80_0720283",1,"Created","The SPAP shall describe all plans to be produced and used in the project."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.2>b","Requirement","ECSS-Q-ST-80_0720284",1,"Created","The relationship between the project plans and a timely planning for their preparation and update shall be described."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.3>a","Requirement","ECSS-Q-ST-80_0720285",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.4>a","Requirement","ECSS-Q-ST-80_0720286",1,"Created","The SPAP shall describe the contribution of the software product assurance function to the proper implementation of documentation and configuration management."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.4>b","Requirement","ECSS-Q-ST-80_0720287",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.4>c","Requirement","ECSS-Q-ST-80_0720288",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.5>a","Requirement","ECSS-Q-ST-80_0720289",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.6>a","Requirement","ECSS-Q-ST-80_0720290",1,"Created","The SPAP shall describe the approach for the reuse of existing software, including delta qualification. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.7>a","Requirement","ECSS-Q-ST-80_0720291",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.8>a","Requirement","ECSS-Q-ST-80_0720292",1,"Created","The SPAP shall describe or list by reference all procedures and standards applicable to the development of the software in the project."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.8>b","Requirement","ECSS-Q-ST-80_0720293",1,"Created","The software product assurance measures to ensure adherence to the project procedures and standards shall be described. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<6.8>c","Requirement","ECSS-Q-ST-80_0720294",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<7>a","Requirement","ECSS-Q-ST-80_0720295",1,"Created","The SPAP shall describe the approach taken to ensure the quality of the software product. "]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<7>b","Requirement","ECSS-Q-ST-80_0720296",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<8>a","Requirement","ECSS-Q-ST-80_0720297",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","B.2.1<8>b","Requirement","ECSS-Q-ST-80_0720298",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<1>a","Requirement","ECSS-Q-ST-80_0720299",1,"Created","The SPAMR shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<2>a","Requirement","ECSS-Q-ST-80_0720300",1,"Created","The SPAMR shall list the applicable and reference documents to support the generation of the document."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<3>a","Requirement","ECSS-Q-ST-80_0720301",1,"Created","The SPAMR shall include any additional terms, definition or abbreviated terms used."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<4>a","Requirement","ECSS-Q-ST-80_0720302",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<4>b","Requirement","ECSS-Q-ST-80_0720303",1,"Created","The SPAMR shall contain reporting on the verification of the measures applied for the handling of critical software."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<5>a","Requirement","ECSS-Q-ST-80_0720304",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<5>b","Requirement","ECSS-Q-ST-80_0720305",1,"Created","The SPAMR shall include reporting on the correct use of methods and tools."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<6>a","Requirement","ECSS-Q-ST-80_0720306",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<7>a","Requirement","ECSS-Q-ST-80_0720307",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<7>b","Requirement","ECSS-Q-ST-80_0720308",1,"Created","The results of the software maturity analysis shall also be reported."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<8>a","Requirement","ECSS-Q-ST-80_0720309",1,"Created","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."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<9>a","Requirement","ECSS-Q-ST-80_0720310",1,"Created","The SPAMR shall include reporting on the status of software problem reports and nonconformances relevant to software."]
["ECSS-Q-ST-80C","ECSS - Superseded v0.9","C.2.1<10>a","Requirement","ECSS-Q-ST-80_0720311",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1a","Requirement","ECSS-Q-ST-10-09_0350001",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1b","Requirement","ECSS-Q-ST-10-09_0350002",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1c","Requirement","ECSS-Q-ST-10-09_0350003",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1d","Requirement","ECSS-Q-ST-10-09_0350004",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1e","Requirement","ECSS-Q-ST-10-09_0350005",1,"Created","The supplier shall complete the nonconformance report in conformance with Annex A, and submit it to the internal NRB. "]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1f","Requirement","ECSS-Q-ST-10-09_0350006",1,"Created","The supplier shall describe the nonconformance clear, unambiguous and sufficiently detailed that it can be understood by personnel not involved in its detection."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.1g","Requirement","ECSS-Q-ST-10-09_0350007",1,"Created","The supplier shall ensure traceability between the NCR and the quality and manufacturing records related to the nonconforming item."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.1a","Requirement","ECSS-Q-ST-10-09_0350008",1,"Created","The NRB shall be the sole technical authority for the treatment of nonconformances occurring in the frame of a business agreement."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-Q-ST-10-09_0350009",1,"Created","All NRB members shall make dispositions and decisions by consensus."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.1c","Requirement","ECSS-Q-ST-10-09_0350010",1,"Created","The NRB chairman shall involve higher management levels in case of conflict."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.1a","Requirement","ECSS-Q-ST-10-09_0350011",1,"Created","The supplier shall nominate and authorize the internal NRBs core members for the business agreement."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.1b","Requirement","ECSS-Q-ST-10-09_0350012",1,"Created","The responsibilities and authorities of each member shall be assigned."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.1c","Requirement","ECSS-Q-ST-10-09_0350013",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.1d","Requirement","ECSS-Q-ST-10-09_0350014",1,"Created","Immediately after the reporting of a nonconformance, the chairman shall convene an internal NRB."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.2a","Requirement","ECSS-Q-ST-10-09_0350015",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.2b","Requirement","ECSS-Q-ST-10-09_0350016",1,"Created","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”."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.2c","Requirement","ECSS-Q-ST-10-09_0350017",1,"Created","In case of doubt, the internal NRB shall classify nonconformances as major."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3a","Requirement","ECSS-Q-ST-10-09_0350018",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3b","Requirement","ECSS-Q-ST-10-09_0350019",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3c","Requirement","ECSS-Q-ST-10-09_0350020",1,"Created","The internal NRB shall analyse whether human error or poor workmanship are the primary or secondary cause for the nonconformance."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3d","Requirement","ECSS-Q-ST-10-09_0350021",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3e","Requirement","ECSS-Q-ST-10-09_0350022",1,"Created","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."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.3f","Requirement","ECSS-Q-ST-10-09_0350023",1,"Created","The internal NRB shall document the results of the investigation in the nonconformance report."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.2.2.5c","Requirement","ECSS-Q-ST-10-09_0350029",1,"Created","The supplier shall provide a nonconformance report in conformance to Annex A, including a proposed disposition."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","5.4.1d","Requirement","ECSS-Q-ST-10-09_0350050",1,"Created","The supplier shall maintain a list of scrapped items which are finally disposed."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","6.2.1b","Requirement","ECSS-Q-ST-10-09_0350075",1,"Created","The supplier shall apply the requirements in this clause 6.2 to the following software products:\n    1. on-board software,\n    2. verification software (e.g. simulators, and test beds),\n    3. mission control software (ground based), and\n    4. support software for development of the 6.2.1b.1 to 3 above."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-10-09_0350092",1,"Created","The NCR shall identify the supplier of the nonconforming item."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","A.2.1<29>a","Requirement","ECSS-Q-ST-10-09_0350122",1,"Created","The NCR shall contain the document identification number of the failure analysis report on customer NRB level."]
["ECSS-Q-ST-10-09C","ECSS - Superseded v0.9","A.2.1<34>a","Requirement","ECSS-Q-ST-10-09_0350127",1,"Created","The NCR shall contain the names of the members of the customer NRB and respective companies."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","6.3a","Requirement","ECSS-Q-ST-70-10_0590018",1,"Created","The nonconformances shall be dispositioned in conformance with ECSS-Q-ST-10-09."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","6.5.1e","Requirement","ECSS-Q-ST-70-10_0590032",1,"Created","The test pattern layout and design shall be in conformance with the referenced IEC specification if applicable:\n    1. Single and double sided PCBs with plated-through holes: IEC 60326-5.\n    2. Rigid multilayer PCBs with interlayer connections: IEC 62326-4.\n    3. Single and double sided flexible PCBs with through connections: IEC 60326-8.\n    4. Flex-rigid multilayer PCBs with through connections: IEC 60326-11."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","6.6a","Requirement","ECSS-Q-ST-70-10_0590053",1,"Created","The qualification authority shall grant qualification approval to the PCB manufacturer based on the examination and acceptance of the qualification programme."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.2.3i","Requirement","ECSS-Q-ST-70-10_0590078",1,"Created","The nonconformance criteria for arbitrary defects of conductors and terminal pads shall be as follows:\n1.\ta £ 20 % of x and minimum conductor width > requirement\tm\n2.\ta > 20 % of x.................................................................................................................M\n3.\tminimum conductor width < requirement..........................................................................M\n4.\tb £ x.............................................................................................................................m\n5.\tb > x.............................................................................................................................M\n6.\tOpposite peaks: if z < 80 % of y\tM\n7.\tIsolated peaks or valleys: h > 20 % of x and z < requirement..............................................M\n8.\tConducting island: a + h > 20 % of y and the isolation spacing < requirement.......................M\n9.\tMinimum remaining spacing y - a < requirement................................................................M\n10.\ta > 20 % of y..................................................................................................................M\n11.\tb > y..............................................................................................................................M\n12.\tCover layer (flexible PCBs) covering part of solder pad (see Figure 7-3)\t.M\nNOTE \tIntermittent and irregular metallisation defects on conductors are edge roughness (peak or valley), pits, pin holes, voids, protrusions or indentations, as shown in Figure 7-1, Figure 7-2 and Figure 7-3."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.2.8.2a","Requirement","ECSS-Q-ST-70-10_0590102",1,"Created","The test shall be carried out in conformance with tests 6a and 6b of IEC 60326-2-am 1 (1992-06)."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.2.8.3b","Requirement","ECSS-Q-ST-70-10_0590107",1,"Created","The test shall be carried out in conformance with clause 7.2.8.2."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.3.2a","Requirement","ECSS-Q-ST-70-10_0590132",1,"Created","The test shall be carried out in conformance with test 14a of IEC 60326-2-am 1 (1992-06) and IEC 60068-2-20-am 2 (1987-01), test TC."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.3.3.1i","Requirement","ECSS-Q-ST-70-10_0590149",1,"Created","The nonconformance criteria for the peel strength shall be as follows:\n    1. Peel strength < requirement\t\t\t\t\t\t\t\tM"]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.3.4.2b","Requirement","ECSS-Q-ST-70-10_0590179",1,"Created","The relative quantities of tin and lead shall be determined by atomic absorption spectrometry.\n    NOTE This is the proposed method for SnPb. Any other method resulting in the same degree of precision can be used."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.3.5.1.1a","Requirement","ECSS-Q-ST-70-10_0590204",1,"Created","The test shall be carried out in conformance with test 5 of IEC 60326-2-am 1 (1992-06)."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.3.6.1g","Requirement","ECSS-Q-ST-70-10_0590225",1,"Created","It shall be weighed to the nearest milligram in the minute following its removal from the water."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.4.2.1c","Requirement","ECSS-Q-ST-70-10_0590235",1,"Created","After conditioning for 6 h at (140 ± 2) °C, the board shall be floated in a 63/37 solder bath maintained at (287 ± 6) °C."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.4.3k","Requirement","ECSS-Q-ST-70-10_0590256",1,"Created","A microsection shall be performed on the soldered holes to evaluate possible cracking of the copper of the through-hole plating."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","7.6.3f","Requirement","ECSS-Q-ST-70-10_0590277",1,"Created","Surplus flux shall be allowed to flow off the specimen by keeping it upright for 5 min."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","8.8a","Requirement","ECSS-Q-ST-70-10_0590303",1,"Created","All operators and inspectors shall be suitably trained for their task and for the understanding of the necessary quality assurance requirements."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","9.3a","Requirement","ECSS-Q-ST-70-10_0590324",1,"Created","The base materials shall be in conformance with ECSS-Q-ST-70, IEC specifications and IPC-4101 and shall be the following:\n1.\tFlexible copper­clad polyimide film."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","B.2.1<4>a","Requirement","ECSS-Q-ST-70-10_0590349",1,"Created","The report shall contain the results of the qualification programme."]
["ECSS-Q-ST-70-10C","ECSS - Superseded v0.9","D.2.1<2>b","Requirement","ECSS-Q-ST-70-10_0590354",1,"Created","The evaluation test report of the delivered PCB shall be in conformance with Annex A."]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","5.2.3.4e","Requirement","ECSS-Q-ST-70-11_0600035",1,"Created","The thickness of gold over nickel plating shall be between 1 mm and 7 mm."]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","5.3.3a","Requirement","ECSS-Q-ST-70-11_0600047",1,"Created","The PCB manufacturer shall test an in house associated test coupon to demonstrate the compliance to the inspection criteria of microsections as described in clause 6.3."]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","6.2.1a","Requirement","ECSS-Q-ST-70-11_0600072",1,"Created","Each board shall be inspected with the naked eye for correct marking."]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","6.2.2h","Requirement","ECSS-Q-ST-70-11_0600082",1,"Created","The nonconformance criteria for plated­through holes shall be as follows:\n1.\tIncompletely drilled, additional or missing holes..................................................................................................M\n2.\tPartially or completely missing metallization....................................................................................................... M\n3.\tComponent holes ³ 0,6 mm filled or partially filled with solder resulting in a diameter smaller than the requirement...m/M"]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","6.3.1a","Requirement","ECSS-Q-ST-70-11_0600101",1,"Created","The test shall be carried out in conformance with tests 1c and 15b of IEC 60326-2-am 1 (1992-06)."]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","6.3.3g","Requirement","ECSS-Q-ST-70-11_0600122",1,"Created","The nonconformance criteria for the copper plating inside buried, blind, via and component holes shall be as follows:\n1.\tVoid in copper plating in holes\tM"]
["ECSS-Q-ST-70-11C","ECSS - Superseded v0.9","7.6b","Requirement","ECSS-Q-ST-70-11_0600147",1,"Created","The limits for the dimensional characteristics shall be as follows:\n1.\tExternal dimension tolerance: ±0,2 mm;\n2.\tThickness tolerance: ±10 %;\n3.\tMaximum active board size: supplier’s specification;\n4.\tMaximum board thickness: 3,2 mm;\n5.\tPositioning between registration mark and edge of circuit: \nD maximum 0,20 mm;\n6.\tConductor width:\n(a)\tInternal: 120 mm minimum;\n(b)\tExternal: 200 mm minimum (for fine pitch 120 mm width is tolerated if less than 5 mm from component pad);\n7.\tConductor spacing:\n(a)\tInternal: 150 mm minimum;\n(b)\tExternal: 300 mm minimum (for fine pitch 150 mm spacing is tolerated if less than 5 mm from component pad);\n8.\tConductor tolerance (minimum/maximum): supplier’s specification;\n9.\tTolerance on diameter of terminal pads: supplier’s specification;\n10.\tMinimum drilled hole diameter:\n(a)\tComponent hole: in conformance with ECSS-Q-ST-70-08;\n(b)\tVia hole: 0,25 mm minimum \t\nand maximum aspect ratio t/d = 6;\n(c)\tBuried via: supplier’s specification\t\nand maximum aspect ratio t/d = 6;\n(d)\tBlind via produced sequentially: supplier’s specification and maximum aspect ratio t/d = 6;\n11.\tTolerance on diameter of plated­through holes:\n(a)\tNominal Æ ³ 0,7: D maximum 0,15 mm for component hole;\n(b)\tNominal Æ < 0,7: D maximum 0,20 mm;\n12.\tTolerance on diameter of non­plated­through holes: D maximum 0,20 mm;\n13.\tPositioning of holes with respect to reference mark: ±0,10 mm;\n14.\tRelative misregistration pad/hole: £ 0,15 mm;\n15.\tMisalignment determined by measuring minimum annular ring:\n(a)\tExternal layers: solder side: 0,20 mm;\n(b)\tExternal layers: component side (reduced pads): 0,10 mm;\n(c)\tExternal layers: non­soldering hole: 0,10 mm;\n(d)\tInternal layers: 0,05 mm;\n16.\tLayer to layer registration: ±100 mm;\n17.\tNumber of layers: 18 maximum."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","5.3d","Requirement","ECSS-Q-ST-70-38_0210015",1,"Created","The supplier shall identify the need for additional testing to be approved by the Approval authority."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","6.8.2a","Requirement","ECSS-Q-ST-70-38_0210043",1,"Created","Equipment used to deposit solder pastes shall be of a screening, stencilling, dispensing, roller coating or dotting type. "]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","7.2.4g","Requirement","ECSS-Q-ST-70-38_0210068",1,"Created","Tools used for removing solder paste from the container shall not contaminate the paste dispensed or that remaining within."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","7.8.6a","Requirement","ECSS-Q-ST-70-38_0210083",1,"Created","Boards shall be made of materials and manufactured in conformance with the requirements of ECSS-Q-ST-70-10 and procured in conformance with ECSS-Q-ST-70-11. \n    NOTE CTE compensated boards use a standard construction with compensated materials such as low CTE substrate or cores. Typical cores are copper-plated invar and copper-plated molybdenum. "]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","7.9.2c","Requirement","ECSS-Q-ST-70-38_0210095",1,"Created","Castellated chip carrier components shall have no discontinuities in the metallized terminal areas on the mounting pattern of the device. "]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","8.5c","Requirement","ECSS-Q-ST-70-38_0210120",1,"Created","Baking times and temperatures shall be documented.\n    NOTE 1 Typical baking conditions are from 6 h to 24 h at 125 C depending on the JEDEC classification, except for components delivered in reels for which a lower temperature and longer time are used. \n    NOTE 2 It is good practice to store components under nitrogen, dry air (20 % RH maximum) or partial vacuum."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","9.7.6c","Requirement","ECSS-Q-ST-70-38_0210141",1,"Created","Except for RF applications, devices with electrical elements deposited on an external surface (such as resistors) shall be mounted with that surface facing away from the printed circuit board or substrate. \n    NOTE See Figure 9-1 for details."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","11.5.5a","Requirement","ECSS-Q-ST-70-38_0210169",1,"Created","Joints to castellated device terminations shall meet the dimensional and solder fillet requirements of Table 11-4 and Figure 11-4.\n    NOTE 1 The stand-off enables adequate cleaning beneath the assembled LCCC and also to enhance solder fatigue life (see also clause 9.7.6f\n    NOTE 2 Devices bigger than LCCC 16 are not expected to be used for space applications when mounted on Class 1 substrates."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","11.5.8a","Requirement","ECSS-Q-ST-70-38_0210172",1,"Created","The outer row of solder joints to area array devices shall be visually inspected by looking from the side in accordance with the requirements in 11.5.1 and Table 11-7 and with the rejection criteria specified in 13.3 and 13.4."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","14.1c","Requirement","ECSS-Q-ST-70-38_0210193",1,"Created","Both, the verification of the assembly by hand and machine soldering shall be made in accordance with this clause 14."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","14.4a","Requirement","ECSS-Q-ST-70-38_0210216",1,"Created","When passive components are functionally tested, and when continuity tests on series-connected packages are made using internal wiring of packages (daisy-chain):\n    1. No signal loss shall be accepted.\n        NOTE 1 When performed, electrical testing can best be conducted during the complete thermal cycle.\n        NOTE 2 Devices can be interconnected to multilayered circuit boards. \n    2. A drift of less than 10 % of resistance shall be accepted when the continuity tests are performed at room temperature.\n        NOTE Devices having soldered connections that cannot be inspected (due to access, small size or opaque conformal coating) are expected to be monitored during environmental testing by electrical test."]
["ECSS-Q-ST-70-38C","ECSS - Superseded v0.9","14.10g","Requirement","ECSS-Q-ST-70-38_0210240",1,"Created","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."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.1.2b","Requirement","ECSS-Q-ST-20_0380004",2,"Normative Change","Personnel performing or evaluating special processes shall be trained and certified according to standards accepted by the customer.\nNOTE \tThe term “special process” is defined in ECSS-S-ST-00-01."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.2.6h","Requirement","ECSS-Q-ST-20_0380029",1,"Unchanged","The supplier shall ensure that the inspection, measuring and test equipment is capable of the specified accuracy and precision."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.2.7.2b","Requirement","ECSS-Q-ST-20_0380041",2,"Normative Change","The supplier shall place the following items in designated segregated areas:\n1.\tlimited life materials,\n2.\tsuspended limited life materials,\n3.\tnonconforming items awaiting NRB disposition,\n4.\tscrapped items,\n5.\titems designated to be stored separately for health or safety reasons."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.3.2.1a","Requirement","ECSS-Q-ST-20_0380055",1,"Unchanged","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."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.4.1.3b","Requirement","ECSS-Q-ST-20_0380079",1,"Unchanged","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."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.3.1d","Requirement","ECSS-Q-ST-20_0380107",1,"Unchanged","Process witness samples shall be stored in controlled conditions."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.6.2b","Requirement","ECSS-Q-ST-20_0380126",1,"Unchanged","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."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.9.1c","Requirement","ECSS-Q-ST-20_0380146",1,"Unchanged","The supplier shall establish and maintain records of temporary installations and removals."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.9.2d","Requirement","ECSS-Q-ST-20_0380151",1,"Unchanged","The logbook shall accompany the hardware whenever it is placed in the custody of another organization"]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.7.5.1b","Requirement","ECSS-Q-ST-20_0380186",1,"Unchanged","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."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","5.8.3.1b","Requirement","ECSS-Q-ST-20_0380193",1,"Unchanged","Procurement documents shall identify validation and receiving inspection requirements, and conform to the requirements in clause 5.4.2."]
["ECSS-Q-ST-20C Rev.1","ECSS - Superseded v0.9","A.2.1<8>a","Requirement","ECSS-Q-ST-20_0380212",1,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","4.1.3a","Requirement","ECSS-Q-ST-70_0490003",2,"Deleted","<< deleted >>"]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","4.2.4e","Requirement","ECSS-Q-ST-70_0490024",1,"Unchanged","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.\nNOTE \tFor example, by non-disclosure agreement."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","4.4a","Requirement","ECSS-Q-ST-70_0490029",1,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","5.1.5d","Requirement","ECSS-Q-ST-70_0490210",1,"Created","The levels of offgassing and toxicity specified in the requirement 5.1.5c shall be agreed with the customer."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","5.1.15a","Requirement","ECSS-Q-ST-70_0490056",2,"Normative Change","Moisture absorption shall be prevented during manufacture and storage of hygroscopic materials. "]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","5.2.2d","Requirement","ECSS-Q-ST-70_0490240",1,"Created","Cadmium and Zinc shall not be used for ground support equipment exposed to vacuum or when in contact with the flight hardware.\nNOTE \tFor example during thermal vacuum testing phases on ground."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","5.6.1a","Requirement","ECSS-Q-ST-70_0490078",2,"Normative Change","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."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","6.2b","Requirement","ECSS-Q-ST-70_0490099",1,"Unchanged","Type reduction actions shall be implemented at all levels of the programme."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","6.4.2b","Requirement","ECSS-Q-ST-70_0490103",1,"Unchanged","Critical parts shall be identified in the DMPL and included in the critical items list."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","6.7.1b","Requirement","ECSS-Q-ST-70_0490127",1,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","7.4a","Requirement","ECSS-Q-ST-70_0490140",1,"Unchanged","The supplier shall establish and maintain a declared processes list in conformance with Annex C."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","A.2.1<1>b","Requirement","ECSS-Q-ST-70_0490168",1,"Unchanged","If new groups are created, for a given project, these shall have numbers over 21."]
["ECSS-Q-ST-70C Rev.1","ECSS - Superseded v0.9","D.2.1a","Recommendation","ECSS-Q-ST-70_0490277",1,"Created","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."]
["ECSS-Q-ST-70-05C","ECSS - Superseded v0.9","5.1.1d","Requirement","ECSS-Q-ST-70-05_0540004",1,"Created","Warning and caution notes shall be included in instructions for operation, storage, transport, testing, assembly, maintenance and repair."]
["ECSS-Q-ST-70-05C","ECSS - Superseded v0.9","5.2.3.3c","Requirement","ECSS-Q-ST-70-05_0540029",1,"Created","The cleaned tissue shall be stored/kept in a clean container."]
["ECSS-Q-ST-70-05C","ECSS - Superseded v0.9","5.4.3.1i","Requirement","ECSS-Q-ST-70-05_0540051",1,"Created","The standards materials used for the calibration lines shall be of high purity."]
["ECSS-Q-ST-70-05C","ECSS - Superseded v0.9","5.4.3.5d","Requirement","ECSS-Q-ST-70-05_0540072",1,"Created","For indirect methods, all solvents used shall have a NVR of less than 5 μg/g and an infrared absorption of the NVR of less than 0,0005 AU ml-1.\n    NOTE If the rinsing method is used (see Annex D and Annex E), a detection limit in the order of 10-8 g cm-2 can be obtained depending on the surface area analyzed (e.g. for a 15 cm2 witness plate)."]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.1.1a","Requirement","ECSS-Q-ST-70-31_0660001",1,"Created","The adequacy of a paint process shall be demonstrated through a verification programme."]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.2.2.1d","Requirement","ECSS-Q-ST-70-31_0660015",1,"Created","Coated surfaces shall be shielded from contact by using appropriate bags or sheets.\n    ","NOTE The suitable bags are for example plastic bags with desiccators, sheet of tissue-paper, sheet of polyethylene foam."]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.3.1.2d","Requirement","ECSS-Q-ST-70-31_0660048",1,"Created","For large pieces, or pieces that for other reasons cannot be ultrasonically cleaned, surfaces shall be carefully cleaned by hand with cleaning solvents and clean tissues.\n    ","NOTE The cleaning solvents are for example ketons, alcohols or ionic liquids."]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.3.1.3d","Requirement","ECSS-Q-ST-70-31_0660053",1,"Created","The hardware shall be protected from random temperature extremes, high humidity and physical damage."]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.3.6.1e","Requirement","ECSS-Q-ST-70-31_0660087",1,"Created","If the area to repair is larger than 10 % of the total surface, the paint shall be removed from the total surface by using paint stripper or mechanical stripping. "]
["ECSS-Q-ST-70-31C","ECSS - Superseded v0.9","4.4f","Requirement","ECSS-Q-ST-70-31_0660100",1,"Created","Outgassing properties shall be measured according to ECSS-Q-ST-70-02."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.6a","Requirement","ECSS-Q-ST-70-71_1260018",1,"Created","All high-strength heat treated parts which are acid cleaned, plated or exposed to other hydrogen-producing processes shall be subjected to a baking process.\n","NOTE\tHigh-strength heat treated parts are > 1225 MPa UTS."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.8d","Requirement","ECSS-Q-ST-70-71_1260027",1,"Created","All welds used for structural applications shall undergo a NDI program that shall be submitted for customer approval.\n","NOTE\tECSS-E-ST-32-01 contains additional requirements specific to welds used for Potential Fracture Critical Items applications."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.10a","Requirement","ECSS-Q-ST-70-71_1260045",1,"Created","The supplier shall demonstrate that the performances of the selected optical glasses or coatings are not degraded below the specified acceptable levels by ionizing radiation, particle, UV radiation and ATOX for the intended application."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.12h","Requirement","ECSS-Q-ST-70-71_1260069",1,"Created","When perforated tapes are not used, the process of tape application and removal of bubbles shall be documented."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.15e","Requirement","ECSS-Q-ST-70-71_1260090",1,"Created","The supplier shall assess the need of using pre-coating to ensure proper adhesion between the part and the potting compound or sealant and reduce residual stresses created during curing."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.17f","Requirement","ECSS-Q-ST-70-71_1260108",1,"Created","The leaching of filler materials shall be assessed with respect to their potential hazard to associated equipment."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.2.19d","Requirement","ECSS-Q-ST-70-71_1260136",1,"Created","Resins used in PCBs for space hardware shall be qualified in conformance with requirements from clause 5 to clause 9 of ECSS-Q-ST-70-10."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.3.4c","Requirement","ECSS-Q-ST-70-71_1260161",1,"Created","Pre-treatment processes for the surfaces to be painted shall be selected and controlled to ensure adhesion of the paint to the substrate.\n","NOTE\tPre-treatment processes include for example cleaning, abrasion and priming."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.3.6j","Requirement","ECSS-Q-ST-70-71_1260175",1,"Created","Equipment and procedures used for welding shall be certified for their capability to produce welds and weld repairs."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.3.9.1a","Requirement","ECSS-Q-ST-70-71_1260188",1,"Created","All surface treatments process specifications shall include the qualified thickness range."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.3.12.3b","Requirement","ECSS-Q-ST-70-71_1260213",1,"Created","Annealing processes shall be selected to avoid degradation of the material."]
["ECSS-Q-ST-70-71C","ECSS - Superseded v0.9","4.3.15.5g","Requirement","ECSS-Q-ST-70-71_1260238",1,"Created","Solder sleeves shall not be used in flight hardware due to their retention of solder flux and inspection difficulties."]
["ECSS-Q-ST-60-14C","ECSS - Superseded v0.9","6.1.1b","Requirement","ECSS-Q-ST-60-14_0470019",1,"Created","Component families not covered in Table 6-1 shall be subject to special procedures to be defined by the program.\n    ","NOTE The 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."]
["ECSS-Q-ST-60-14C","ECSS - Superseded v0.9","6.1.2b","Requirement","ECSS-Q-ST-60-14_0470023",1,"Created","For ceramic chip or moulded capacitors, electrical measurement shall be done after 4 hours of stabilisation at 125°C for Type II ceramic.\n    ","NOTE See (2) in Table 6-1."]
["ECSS-Q-ST-60-14C","ECSS - Superseded v0.9","6.3a","Requirement","ECSS-Q-ST-60-14_0470044",1,"Created","The relifing date code shall correspond to the week code of the first test performed on the lot. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.1.4b","Requirement","ECSS-Q-ST-60_0480012",2,"Normative Change","The list specified in 4.1.4a shall be kept under configuration control (issue and identification of changes). "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.2.2.4b","Requirement","ECSS-Q-ST-60_0480040",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.2.3.2.2b","Requirement","ECSS-Q-ST-60_0480061",1,"Unchanged","The complete manufacturer assessment, including the survey report and the associated corrective actions, shall be part of the evaluation report."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.3.2g","Requirement","ECSS-Q-ST-60_0480085",1,"Unchanged","The supplier shall keep each procurement specification under configuration control."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.3.4c","Requirement","ECSS-Q-ST-60_0480093",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.3.8d","Requirement","ECSS-Q-ST-60_0480108",1,"Unchanged","The results of RVT shall be documented by a report. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","4.5.2d","Requirement","ECSS-Q-ST-60_0480133",1,"Unchanged","For ESCC qualified components the supplier shall apply the ESCC basic specification no 22800."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.1.2.1a","Requirement","ECSS-Q-ST-60_0480158",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.2.2.1b","Requirement","ECSS-Q-ST-60_0480177",1,"Unchanged","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. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.2.3.1d","Requirement","ECSS-Q-ST-60_0480202",2,"Normative Change","An evaluation plan shall be sent to the customer for approval, and include the following elements:\n    1. Constructional Analysis (as per clause 5.2.3.3),\n    2. Evaluation Testing (as per clause 5.2.3.4),\n    3. Radiation Hardness (as per clause 5.2.3.4b.5). "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.2.3.1e","Requirement","ECSS-Q-ST-60_0480203",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.3.3e","Requirement","ECSS-Q-ST-60_0480238",1,"Unchanged","For active parts (transistors, diodes) packaged in TO3, DO4 or DO5, the PIND test method shall be submitted to the customer’s review. ","NOTE See also clause 5.2.2.2e.2."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.3.6d","Requirement","ECSS-Q-ST-60_0480246",2,"Normative Change","If the buy-off is replaced by an incoming inspection at the procurement entity's facilities; it shall be declared in the PAD submitted to the customer for approval."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.4a","Requirement","ECSS-Q-ST-60_0480271",1,"Unchanged","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","5.5.4a","Requirement","ECSS-Q-ST-60_0480282",1,"Unchanged","The traceability of individual components during manufacturing and testing shall be maintained as required by the procurement specifications."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.2.1b","Requirement","ECSS-Q-ST-60_0480464",1,"Created","The selection, evaluation and approval of commercial EEE components for class 3 programmes shall be performed in conformance with clause 6.2 from ECSS-Q-ST-60-13 standard."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.2.2.2a","Requirement","ECSS-Q-ST-60_0480320",1,"Unchanged","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. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.2.3.1b","Requirement","ECSS-Q-ST-60_0480341",1,"Unchanged","The supplier shall plan and carry out the evaluation."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.3.1d","Requirement","ECSS-Q-ST-60_0480365",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.3.8b","Requirement","ECSS-Q-ST-60_0480388",2,"Normative Change","RVT shall be performed in accordance with internationally recognized standards, such as ESCC Basic Specifications No. 22900.\n    ","NOTE Additional information on test methods is given in MIL-STD-750 Test Method 1019, MIL-STD-883 Test Method 1019. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.4c","Requirement","ECSS-Q-ST-60_0480409",2,"Normative Change","On request, handling and storage procedures shall be sent to the customer for review."]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","6.6.4a","Requirement","ECSS-Q-ST-60_0480427",2,"Normative Change","For FPGA, ECSS-Q-ST-60-02 shall apply. "]
["ECSS-Q-ST-60C Rev. 2","ECSS - Superseded v0.9","A.2.2a","Permission","ECSS-Q-ST-60_0480521",1,"Created","The CCP may be part of the overall project PA plan (see clause 4.1.2.2b)."]
["ECSS-Q-ST-70-07C","ECSS - Superseded v0.9","5.3b","Requirement","ECSS-Q-ST-70-07_0560018",1,"Created","The audit shall also include a further on-site review of the documentation listed in clauses B.2.1b and B.2.1h."]
["ECSS-Q-ST-70-07C","ECSS - Superseded v0.9","5.6a","Requirement","ECSS-Q-ST-70-07_0560043",1,"Created","For all materials and processes utilized in soldering and cleaning operations, ECSS-Q-ST-70-08 and ECSS-Q-ST-70-10 shall apply."]
["ECSS-Q-ST-70-07C","ECSS - Superseded v0.9","B.2.1f","Requirement","ECSS-Q-ST-70-07_0560072",1,"Created","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."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","5.2d","Requirement","ECSS-Q-ST-70-08_0570006",1,"Created","Working areas shall be kept free from any tools or equipment not used for the current task."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","5.3b","Requirement","ECSS-Q-ST-70-08_0570011",1,"Created","Areas used for assembly or cleaning of parts and areas where toxic or volatile vapours are generated or released shall include a local air extraction system."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","5.5.3c","Requirement","ECSS-Q-ST-70-08_0570035",1,"Created","If the packaging is not ESD safe, it shall be labelled accordingly.\n    NOTE The objective of ESD protection is to prevent ESD to the item contained within, to allow for dissipation of charge, and to prevent charging of the ESDS item by an external electrostatic field."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","5.6.6.3b","Permission","ECSS-Q-ST-70-08_0570546",1,"Created","The enamel may be removed by mechanical means provided that visual inspection using a minimum magnification of x40 is carried out to ensure that the conductor is undamaged."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","6.1e","Requirement","ECSS-Q-ST-70-08_0570083",1,"Created","Subassemblies, assemblies and mounting hardware identified as having lead-free surfaces (plated or metallised) shall be protected by process or design to prevent metallic whisker formation in the expected end-use application/environment. "]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","6.4c","Requirement","ECSS-Q-ST-70-08_0570104",1,"Created","Solvents shall not remove component identification markings."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","6.6.1b","Requirement","ECSS-Q-ST-70-08_0570117",1,"Created","When a brass terminal is used it shall be plated with a barrier layer of copper or nickel of 3 µm to 10 µm.\n    NOTE 1 A barrier layer is necessary on brass items to prevent the diffusion, and subsequent surface oxidation, of zinc\n    NOTE 2 It is good practice to use a copper barrier layer on brass terminals because nickel is magnetic and can have a poor solderability."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","7.2.1.3a","Requirement","ECSS-Q-ST-70-08_0570151",1,"Created","The conductor shall not be damaged by the insulation removal process.\n    NOTE Example: Conductor damage includes twisting, ringing, nicks, cuts or scores."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","7.2.1.4.2a","Requirement","ECSS-Q-ST-70-08_0570156",1,"Created","For PTFE-insulated wire, the minimum distance between the insulation and the solder fillet shall be 1 mm.\n    NOTE The minimum clearance distance for PTFE insulation accommodates cold flow."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","7.2.4d","Requirement","ECSS-Q-ST-70-08_0570185",1,"Created","Liquid solder shall not come into contact with the component body or its glass meniscus."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","7.2.6.2a","Requirement","ECSS-Q-ST-70-08_0570203",1,"Created","Solder shall be melted onto the conductor using a heated soldering iron."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","7.7.1c","Requirement","ECSS-Q-ST-70-08_0570228",1,"Created","Prepared PCBs shall be stored in accordance with clause 7.7.3."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","8.1.5e","Requirement","ECSS-Q-ST-70-08_0570249",1,"Created","Leads shall not be temporarily constrained against spring-back force during soldering.\n    NOTE Residual stresses are produced in the lead material or solder joint."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","8.3b","Requirement","ECSS-Q-ST-70-08_0570271",1,"Created","Swage-type terminals that are mounted in a plated-through hole shall be secured to the PCB by an elliptical funnel swage in accordance with Figure 8-6 (b).\n    NOTE An elliptical funnel swage enables complete filling of the plated-through hole with solder."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","8.4.2c","Requirement","ECSS-Q-ST-70-08_0570280",1,"Created","The clinched lead shall not extend beyond the edge of the conductor pattern, see Figure 8-7 and Figure 8-8."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","8.6d","Requirement","ECSS-Q-ST-70-08_0570301",1,"Created","Before soldering, the operator shall ensure that there is no contact between the solder fillet to be formed and the gold plating."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","9.3.1f","Permission","ECSS-Q-ST-70-08_0570568",1,"Created","More than one wire may be installed in a single slot of a terminal post provided that the combined diameters of the wires are less than the width of the slot."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","9.8a","Requirement","ECSS-Q-ST-70-08_0570352",1,"Created","Connections that are not protected by insulation grommets, potting, or conformal coating shall be protected by insulating sleeving.\n    NOTE Example: Hook terminals, solder cups and bus wires."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","9.9.4.1c","Requirement","ECSS-Q-ST-70-08_0570373",1,"Created","The cut sleeving shall be threaded over one of the wires to be joined."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","9.9.4.2e","Requirement","ECSS-Q-ST-70-08_0570378",1,"Created","Wires shall be spliced using lap joints."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","10.2.2a","Requirement","ECSS-Q-ST-70-08_0570404",1,"Created","A concave fillet of solder shall be present between the terminal and the sides of the conductor."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","10.3.4d","Requirement","ECSS-Q-ST-70-08_0570425",1,"Created","Solder shall be introduced:\n    1. initially at the junction of the soldering iron bit and the joint.\n        NOTE Liquid solder between the tip and the connection promotes heat transfer.\n    2. once heat transfer has been achieved, only to the joint."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","12.1c","Requirement","ECSS-Q-ST-70-08_0570450",1,"Created","Additional magnification shall be used to resolve suspected anomalies or defects."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","13.3c","Requirement","ECSS-Q-ST-70-08_0570472",1,"Created","The bakeout temperature shall be between 60 °C and 80 °C\""]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","13.4a","Requirement","ECSS-Q-ST-70-08_0570477",1,"Created","At least one microsection shall be made on each configuration after vibration testing and temperature cycling."]
["ECSS-Q-ST-70-08C","ECSS - Superseded v0.9","14.8c","Requirement","ECSS-Q-ST-70-08_0570498",1,"Created","The training programme shall include procedures for the training, certification, maintenance of certified status, recertification and revocation of certified status for soldering and inspection personnel."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","5.3.3a","Requirement","ECSS-Q-ST-30-11_0140010",1,"Created","For a particular type or manufacturer, when a specific derating rule is defined in the appendix of the approved ESCC detail specification issued by the ESCC Executive, it shall take precedence over the generic requirement of this standard."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","6.6.1a","Recommendation","ECSS-Q-ST-30-11_0140169",1,"Created","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."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","6.12.2a","Requirement","ECSS-Q-ST-30-11_0140057",1,"Created","Parameters of connectors RF from family-group code 02-05 shall be derated as per Table 6-11."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","6.21.2a","Requirement","ECSS-Q-ST-30-11_0140091",1,"Created","Parameters of Integrated circuits from family-group code 08-50 to 08-60 and 08-69 shall be derated as per Table 6-21."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","6.23.2b","Requirement","ECSS-Q-ST-30-11_0140099",1,"Created","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."]
["ECSS-Q-ST-30-11C Rev.1","ECSS - Superseded v0.9","6.28.2a","Requirement","ECSS-Q-ST-30-11_0140131",1,"Created","Parameters of Transistors from family-group code 12-01 to 12-04 and 12-09 shall be derated as per Table 6-33."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.1.1a","Requirement","ECSS-Q-ST-60-13_0460001",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.2.1b","Requirement","ECSS-Q-ST-60-13_0460491",1,"Created","The selection, evaluation and approval of commercial EEE components for class 1 programmes shall be performed in conformance with clause 4.2 from ECSS-Q-ST-60-13."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.2.2.4b","Requirement","ECSS-Q-ST-60-13_0460040",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.2.3.4c","Requirement","ECSS-Q-ST-60-13_0460482",1,"Created","Evaluation tests shall be performed as specified in Figure 4-1 and Table 4-1."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.2.3.4d","Requirement","ECSS-Q-ST-60-13_0460483",1,"Created","Omission of any of the elements of tests specified in Figure 4-1 and Table 4-1, or the introduction of alternative activities, shall be justified in the JD.","NOTE For mounting process (including baking for PED), see ECSS-Q-ST-70-38 and ECSS-Q-ST-70-08."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.3.7e","Permission","ECSS-Q-ST-60-13_0460576",1,"Created","In case the incoming inspection has been performed by a procurement agent, the incoming inspection performed by the end-user, may be reduced to the following minimum:\n    1. Packing checking,\n    2. Quantity verification."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.3.10d","Requirement","ECSS-Q-ST-60-13_0460498",1,"Created","As part of the relifing process, a DPA on 3 pieces shall be performed on each lot in accordance with the clause 4.3.9."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.5.4e","Requirement","ECSS-Q-ST-60-13_0460141",1,"Created","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 trace code number) within one week."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","4.6.4h","Permission","ECSS-Q-ST-60-13_0460578",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.2.2.3b","Requirement","ECSS-Q-ST-60-13_0460189",1,"Created","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. "]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.2.2.3g","Requirement","ECSS-Q-ST-60-13_0460194",1,"Created","The supplier shall implement a Radiation Hardness Assurance Programme, in conformance with the requirements of 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. "]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.2.3.4a","Requirement","ECSS-Q-ST-60-13_0460213",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.3.2a","Requirement","ECSS-Q-ST-60-13_0460227",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.3.8f","Requirement","ECSS-Q-ST-60-13_0460527",1,"Created","Parts submitted to RVT shall be screened as specified in clause 5.3.3 to be fully representative of flight parts."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-Q-ST-60-13_0460276",1,"Created","The supplier shall establish and maintain a nonconformance control system in accordance with the general requirements in ECSS-Q-ST-10-09."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","5.6.4g","Requirement","ECSS-Q-ST-60-13_0460297",1,"Created","The lot acceptance procedure, as defined in clause 5.3.5, shall be performed on devices coming from the flight lot/date code and programmed on the same kind of hardware tools and compatible software."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.1.4f","Requirement","ECSS-Q-ST-60-13_0460311",1,"Created","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."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.2.2.4b","Requirement","ECSS-Q-ST-60-13_0460330",1,"Created","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. "]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.2.3.4c","Requirement","ECSS-Q-ST-60-13_0460538",1,"Created","Evaluation tests shall be performed as specified in Table 6-1."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.3.3f","Requirement","ECSS-Q-ST-60-13_0460466",1,"Created","When a component is available in a qualified version according to quality level specified in Table 7-3 it shall be selected."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.3.10c","Requirement","ECSS-Q-ST-60-13_0460552",1,"Created","Humidity test and lifetest shall be performed in accordance with the clause 6.3.5 in case if these tests have not been performed on the lot during the evaluation or the procurement phase.","NOTE Humidity test includes HAST or THB."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.4a","Requirement","ECSS-Q-ST-60-13_0460407",1,"Created","The supplier shall establish and implement procedures for handling and storage of components in order to prevent possible degradation."]
["ECSS-Q-ST-60-13C","ECSS - Superseded v0.9","6.6.4e","Requirement","ECSS-Q-ST-60-13_0460431",1,"Created","For FPGA types without a clear and defined heritage, a post-programming burn-in shall be applied, in conformance with ESCC9000 subclause 8.21, for a minimum duration of 160 h.","NOTE FPGA types with defined heritage are documented in the report: ESCC REP 010 SCSB Decisions Regarding OTP FPGA PPBI, available on https://escies.org."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","5.1.4a","Requirement","ECSS-Q-ST-70-38_0210004",2,"Normative Change","The PID shall be submitted to the Approval Authority for approval.","NOTE\tThe approval can be achieved by PID signature or minutes of meeting being signed by the Approval Authority.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","6.6.7a","Requirement","ECSS-Q-ST-70-38_0210028",2,"Normative Change","Requirements from clause 5.6.7 from ECSS-Q-ST-70-08 shall apply for “Soldering irons and resistance soldering equipment”."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","6.8.2c","Requirement","ECSS-Q-ST-70-38_0210045",1,"Unchanged","Equipment used to apply solder preforms shall ensure alignment of the preform with the land or device lead and termination."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","7.2.1a","Requirement","ECSS-Q-ST-70-38_0210057",1,"Unchanged","Solder paste, ribbon, wire and preforms shall be used provided that the alloy and flux meet the requirements in clause 7.2.2."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","7.8a","Requirement","ECSS-Q-ST-70-38_0210288",1,"Created","Printed Circuit Boards shall be designed in conformance with the requirements of clause 14 of ECSS-Q-ST-70-12."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","7.9.1k","Requirement","ECSS-Q-ST-70-38_0210292",1,"Created","Reprocessing shall not damage the device.","NOTE\tReprocessing of ceramic chip capacitors is advised to be avoided due to potential crack formation.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","8.1.1a","Requirement","ECSS-Q-ST-70-38_0210111",2,"Normative Change","Requirements from clause 7.2 from ECSS-Q-ST-70-08, clause “Preparation of conductors, terminals and solder cups” shall apply."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","9.4a","Requirement","ECSS-Q-ST-70-38_0210124",2,"Normative Change","Requirements from clause 8.4 from ECSS-Q-ST-70-08 shall apply for \"Lead attachment to through holes\"."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","9.7.6g","Permission","ECSS-Q-ST-70-38_0210499",1,"Created","The active element may be facing the substrate in case required by electrical performance. ","NOTE\tFor example: RF applications.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","9.7.9c","Requirement","ECSS-Q-ST-70-38_0210149",2,"Normative Change","Adhesive shall be mixed and cured in accordance with the manufacturer’s procedures. "]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","11.5.8a","Requirement","ECSS-Q-ST-70-38_0210172",2,"Normative Change","The outer row of solder joints to area array devices shall be visually inspected by looking from the side in accordance with the requirements in 11.5.1 and Table 11-8 and with the rejection criteria specified in clauses 13.3 and 13.4."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","11.5.12a","Requirement","ECSS-Q-ST-70-38_0210342",1,"Created","Leaded devices with plane termination shall meet the dimensional and solder fillet requirements of Table 11-12 and Figure 11-14."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","13.3a","Requirement","ECSS-Q-ST-70-38_0210187",2,"Normative Change","The following are some characteristics of unsatisfactory conditions, any of which shall be cause for rejection:\n1.\tcharred, burned or melted insulation of devices,\n2.\tconductor pattern separation from circuit board,\n3.\tburns on base materials,\n4.\t<<deleted>>\n5.\texcessive solder (including peaks, icicles and bridging), see clause 11.5,\n6.\tflux residue, solder splatter, solder balls, or other foreign matter on circuitry, beneath devices or on adjacent areas,\n7.\tdewetting,\n8.\tinsufficient solder, see clause 11.5,\n9.\tpits, holes or voids where bottom is not visible,\n10.\tgranular or disturbed solder joints,\n11.\tfractured or cracked solder connection,\n12.\tcut, nicked, gouged or scraped conductors or conductor pattern,\n13.\t<<deleted>>\n14.\t<<deleted>>\n15.\tdamaged conductor pattern,\n16.\tbare copper or base metal, excluding the ends of cut wire or leads or sides of tracks and soldering footprints on substrate,\n17.\tsoldered joints made directly to gold-plated terminals or gold-plated conductors using tin-lead solders,\n18.\tcold solder joints,\n19.\tdevice body embedded within solder fillet,\n20.\topen solder joints (e.g. tombstoning),\n21.\tprobe marks present on the metallization of chip devices caused by electrical testing after assembly,\n22.\tglass seal does not conform to MIL-STD-883 Method 2009,\n23.\tany nonconformance with clause 11.5, \n24.\tmeasling which violates the minimum insulation distance,\n25.\tdelamination, except within region of the breakout regions for multi-panel processed,\n26.\texposed base metal excluding area of cut leads in the soldered connection,\n27.\tcracks detected in glass diodes outside the relevant devices procurement standard,\n28.\tbent connector pins outside the relevant devices procurement specification,\n29.\tdamage of the lead, device or PCB beyond that defined in the procurement standard of the item,\n30.\tdegraded insulation material of the connector in contact area,\n31.\tbubble or void in the conformal coating or potting that are bridging conductive elements,\n32.\tbubble, void or delamination in conformal coating and or potting between high voltage conductors,\n33.\tlack of intended conformal coating,\n34.\tunintended and continuous adhesive forming a bridge in contact with terminals, component body or solder joints,\n35.\texcessive degolding,\n36.\tinsufficient degolding,\n37.\tdirect bonding on glass device body with epoxy,\n38.\tseparation of adhesive from the bonded surface,\n39.\tseparation of conformal coating from the surface,\n40.\tany longitudinal misalignment on sensitive devices,\n41.\tlongitudinal misalignment of end capped and end metallized devices,\n42.\tpresence of cracks in the ceramic of devices or cover of device.","NOTE\t1\tFor requirement 13.3a.29, end cap metallization peeling crack in device, missing metallization are examples of damage.\nNOTE\t2\tFor requirement 13.3a.29, cracks in ceramics mainly occur in chip capacitors, and leadless device with thermal plane termination.\nNOTE\t3\tFor the requirement 13.3a.32, high voltage applications are defined in ECSS-E-HB-20-05.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.1j","Requirement","ECSS-Q-ST-70-38_0210200",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.3b","Requirement","ECSS-Q-ST-70-38_0210215",1,"Unchanged","The supplier shall present a verification programme for approval.","NOTE\tOwing to the different modes of failure resulting from vibration and temperature cycling, the supplier can use any sequence of environmental testing.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.4.1c","Requirement","ECSS-Q-ST-70-38_0210392",1,"Created","Capacitors and “SMD - xx” devices shall be excluded from electrical monitoring.","NOTE\tCapacitor and “SMD-xx” devices such SMD05, SMD1, SMD2 and SMD5C are excluded as the failure mechanism is crack in ceramic.\n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.4.1h","Requirement","ECSS-Q-ST-70-38_0210397",1,"Created","For each assembly method and type of devices at least 32 devices shall be assembled for electrical monitoring.","NOTE\t1\tMachine reflow, hand soldering are the examples of assembly method.\nNOTE\t2\tThe assembly of the capability and the electrical verification samples can be made on the same board. \n"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.7c","Requirement","ECSS-Q-ST-70-38_0210224",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.9.2d","Requirement","ECSS-Q-ST-70-38_0210232",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.9.5l","Requirement","ECSS-Q-ST-70-38_0210447",1,"Created","The maximum increase of each individual daisy chain resistance, across the entire temperature cycling range during 1500 thermal cycles, shall not be more than 10 % of initial resistance recorded during the first five cycles."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.12a","Requirement","ECSS-Q-ST-70-38_0210245",1,"Unchanged","The approval status of the supplier shall be withdrawn when any of the following status justify its withdrawal:\n1.\tRepetitive supply problems and manufacturing defects.\n2.\tUndeclared changes to the PID.\n3.\tContinuous non-compliance with the PID."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","14.13f","Requirement","ECSS-Q-ST-70-38_0210461",1,"Created","A delta-verification programme in accordance with the DRD from Annex G shall be submitted for approval to the Approval Authority."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","15.5a","Requirement","ECSS-Q-ST-70-38_0210250",2,"Normative Change","Requirements from clause 14.5 from ECSS-Q-ST-70-08 shall apply for \"Traceability\"."]
["ECSS-Q-ST-70-38C Rev.1 Corr.1","ECSS - Superseded v0.9","F.2.1<8>a","Requirement","ECSS-Q-ST-70-38_0210489",1,"Created","The PID shall contain a list of all machines and tools utilised during the SMT activity."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","4.2.11.2c","Requirement","ECSS-E-ST-20-07_0080025",1,"Created","Each unit housing shall be bonded to the nearby spacecraft structure from the equipment bonding stud."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","4.2.13.2e","Requirement","ECSS-E-ST-20-07_0080042",1,"Created","Overshields shall be bonded to chassis ground:\n    1. at both ends,\n    2. using a 360° direct contact or a bond strap of less than 30 nH\n        NOTE See NOTE of clause 4.2.11.2e."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.2.4d","Requirement","ECSS-E-ST-20-07_0080067",1,"Created","The LISN circuit shown in Figure 5-2 shall be used.\n    NOTE 1 The LISN can be split in several cases, one per power lead.\n    NOTE 2 The series inductances represent the inductances of the wiring; the series resistances represent the resistances of the wiring and of the central protections.\n    NOTE 3 The 50W resistors result in 100W at high frequency, similar to the characteristic impedance of the line.\n    NOTE 4 The feed-through capacitors provide a short-circuit at high frequency and make the LISN symmetrical\n    NOTE 5 Connecting the regulation wires of the laboratory supply at the LISN input in order to provide sufficiently low impedance at low frequency is an appropriate method. The source impedance is then dominated by the series resistances in the LISN. Alternatively, a large capacitor (between 1 mF and 10 mF) will be used."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.2.4i","Requirement","ECSS-E-ST-20-07_0080072",1,"Created","The LISN impedance shall be measured at least annually under the following conditions:\n    1. the impedance, measured between the power output lead on the EUT side of the LISN and the metal enclosure of the LISN,\n    2. an unterminated power input terminal on the power source side of the LISN."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.2.6.6.3a","Requirement","ECSS-E-ST-20-07_0080094",1,"Created","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."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.2.9.1d","Requirement","ECSS-E-ST-20-07_0080119",1,"Created","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."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.2.10.4e","Requirement","ECSS-E-ST-20-07_0080144",1,"Created","Data shall be reported with frequency resolution of 1 %."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.3.5b","Requirement","ECSS-E-ST-20-07_0080158",1,"Created","If the bond is only used for charging control, the bonding resistance shall be measured with a dc-current in the range 10 to 100 µA, under only one polarity, with a 2-wires ohmmeter.\n    NOTE If the bond is only used for charging control the clauses 5.3.10a and 5.3.10b do not apply."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.4.6.3e","Requirement","ECSS-E-ST-20-07_0080191",1,"Created","The antenna positions shall be determined as follows:\n    1. For testing below 200 MHz:\n        (a) For setups with the side edges of the boundary 3 m or less, one position, with the antenna centred with respect to the side edges of the boundary.\n        (b) For setups with the side edges of the boundary greater than 3 m, N antenna positions at spacing as shown in Figure 5-15, where N is the edge-to-edge boundary distance (in metres) divided by 3 and rounding up to an integer. \n    2. For testing from 200 MHz up to 1 GHz, place the antenna in such a number of positions that the entire width of each EUT enclosure and the first 35 cm of cables and leads interfacing with the EUT enclosure are within the 3 dB beamwidth of the antenna.\n    3. For testing at 1 GHz and above, place the antenna in such a number of positions that the entire width of each EUT enclosure and the first 7 cm of cables and leads interfacing with the EUT enclosure are within the 3 dB-beamwidth of the antenna."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.4.6.4a","Requirement","ECSS-E-ST-20-07_0080192",1,"Created","The measurement equipment shall be turned on and waited until it is stabilized."]
["ECSS-E-ST-20-07C","ECSS - Superseded v0.9","5.4.11.4c","Requirement","ECSS-E-ST-20-07_0080226",1,"Created","The EUT shall be tested as follows:\n    1. Procedure when using electric field sensors:\n        (a) Establish an unmodulated electric field at the test start frequency by using an amplifier and transmit antenna, and gradually increase the electric field level until it reaches the limit specified by application of clause 4.2.8.\n        (b) Set the signal source to 1 kHz pulse modulation, 50 % duty cycle and apply the modulation.\n        (c) Repeat the test at all frequency tests while maintaining field strength levels in accordance with the associated limit, and monitor EUT performance for susceptibility effects.\n    2. Procedure when calibrating with the receive antenna:\n        (a) Remove the receive antenna and reposition the EUT in conformance with 5.4.11.3e.\n        (b) Set the signal source to 1 kHz pulse modulation, 50 % duty cycle, establish an electric field at the test start frequency by using an amplifier and transmit antenna, and gradually increase the input power level until it corresponds to the level recorded during the calibration routine.\n        (c) Repeat the test at all test frequencies while assuring the transmitter input power is adjusted in accordance with the calibration data collected, and constantly monitor the EUT for susceptibility conditions.\n    3. If susceptibility is noted, determine the threshold level in accordance with 5.2.10.3.\n    4. Perform testing over the frequency range with the transmit antenna vertically polarized, and repeat the testing with the transmit antenna horizontally polarized.\n        NOTE The settings needed to achieve the specified field level in vertical polarization are reused as is for the test in horizontal polarization.\n    5. Repeat 5.4.11.4c.4 for each transmit antenna position determined in 5.4.11.3e."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","4.3.2g","Requirement","ECSS-E-ST-20-08_0090012",1,"Created","The accuracy of the electrical performance test on PVA level shall be better than or equal to the calibration loss factor used in the power analysis."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.3.2.7a","Requirement","ECSS-E-ST-20-08_0090033",1,"Created","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."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.3.3.12b","Requirement","ECSS-E-ST-20-08_0090058",1,"Created","The boundary requirements on minimum and maximum thickness, in conformance with requirement 5.3.3.12a, shall be guaranteed by a controlled application process demonstrated on separate samples."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.4.4a","Requirement","ECSS-E-ST-20-08_0090077",1,"Created","Components other than SCAs, bare cells and coverglasses shall be identified in conformance with the traceability requirements of Class 1 components, and PAD DRD of ECSS-Q-ST-60.\n    NOTE For requirements on the identification and traceability of parts and materials, see clauses 6.1.4, 7.1.3 and 8.3.3 for SCAs, bare cells and coverglass, respectively."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.1.2f","Requirement","ECSS-E-ST-20-08_0090085",1,"Created","Except in conformance with requirement 5.5.1.2e, each type of test shall be performed on a dedicated qualification coupon built specifically for the test. "]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.1.3.4g","Requirement","ECSS-E-ST-20-08_0090110",1,"Created","Monitoring of the continuity of the solar cell circuits shall:\n    1. be performed in conformance with clause 5.5.3.3.2,\n    2. take place during cycles for the complete activity,\n    3. be performed on a regular, at least daily basis for a number of cycles, such that:\n        (a) during 10 % of these cycles of the cell circuit, and\n        (b) during 90 % of these cycles on the protection diode network shall be monitored.\n    4. be performed by measuring both cell circuit continuity, at the beginning and at the end of the cycles in conformance to the relevant percentage specified in requirement 5.5.1.3.4g.3."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.1.7a","Requirement","ECSS-E-ST-20-08_0090128",1,"Created","The test sequence, test definitions and requirements related to the EMC of the PVA shall be agreed between the supplier and the customer and given in the SCD-PVA."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.3.2.9b","Permission","ECSS-E-ST-20-08_0091069",1,"Created","Tarnishing of the diode body or attachment serpentines may be present."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.3.2.21b","Requirement","ECSS-E-ST-20-08_0090182",1,"Created","There shall be no loose material on the coupon."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.3.4.2c","Requirement","ECSS-E-ST-20-08_0090203",1,"Created","The results shall be in conformance with those stated in the SCD-PVA."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.3.5.2d","Requirement","ECSS-E-ST-20-08_0090210",1,"Created","The measurement at averaged operational temperature can be replaced by measurement of the SCA capacitance at operational temperature."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","5.5.3.10.1b","Recommendation","ECSS-E-ST-20-08_0091073",1,"Created","A non-destructive test method should be used for the inspection specified in requirement 5.5.3.10.1a."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.1.2d","Requirement","ECSS-E-ST-20-08_0090255",1,"Created","Deviations from this Standard applicable to the SCD-SCA shall:\n    1. be agreed between the customer and the supplier;\n    2. not affect the reliability and performances of the SCAs;\n    3. only be those specified in requirement 6.1.2c."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.2.1a","Requirement","ECSS-E-ST-20-08_0090278",1,"Created","Before starting production of the qualification lot, the manufacturer shall compile a production test schedule, showing by date and duration, production and test activities, including all major processing operations and key stages in the production and testing. "]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.3.1.6b","Requirement","ECSS-E-ST-20-08_0090302",1,"Created","Adhesive voids along the cover edge shall not exceed 0,6 mm in depth."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.3.1.8a","Requirement","ECSS-E-ST-20-08_0090307",1,"Created","For the rear side contact, outside the welding area, the following conditions shall be met:\n    1. Drops and spatter do not exceed 0,1 mm in diameter and 0,05 mm in height. \n    2. The maximum deep of edge delaminations do not exceed 0,75 mm.\n    3. Other defects do not exceed a total of 2 % of the cell contact area.\n    4. The area of worm shaped bulges is 3 % of the total cell contact area, or less.\n    5. The maximum length of the hypotenuse of the triangular area of visible semiconductor at the corners of the solar cell (c) is in conformance with Table 6-2."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.3.6.2a","Requirement","ECSS-E-ST-20-08_0090332",1,"Created","For Subgroup B step 15 (in conformance with Table 6-1), the solar absorptance and the hemispherical emittance shall be measured according to ECSS-Q-ST-70-09 on at least two samples."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.3.13.2b","Requirement","ECSS-E-ST-20-08_0090364",1,"Created","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."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","6.4.3.15.3c","Requirement","ECSS-E-ST-20-08_0090379",1,"Created","The current output measured at the intervals specified in requirement 6.4.3.15.2g shall demonstrate an exponential decay. "]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.1.1.2d","Requirement","ECSS-E-ST-20-08_0090400",1,"Created","Deviations from this Standard applicable to the SCD-BSC shall:\n    1. be agreed between the customer and the supplier;\n    2. include alternative requirements equivalent to those of this Standard;\n    3. not affect the reliability and performances of the BSCs;\n    4. only be those specified in requirement 7.1.1.2c. "]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.3.1a","Requirement","ECSS-E-ST-20-08_0090411",1,"Created","Acceptance tests shall be performed on the following:\n    1. components for delivery;\n    2. components used for qualification."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.4.1d","Requirement","ECSS-E-ST-20-08_0090431",1,"Created","The supplier shall provide details of the outcome of the qualification programme to the customer."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.5.1.4.3a","Requirement","ECSS-E-ST-20-08_0090452",1,"Created","Cracks and fingerprints shall not be present."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.5.4c","Requirement","ECSS-E-ST-20-08_0090477",1,"Created","Data for all electrical performance parameters at the different solar cell temperatures shall be provided."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.5.7.1.2b","Requirement","ECSS-E-ST-20-08_0090493",1,"Created","The chamber temperature shall then be increased to 60 °C minimum."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.5.13.2d","Requirement","ECSS-E-ST-20-08_0090524",1,"Created","The nominal rate shall be lower than 5 × 1011 e- cm-2 s-1."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","7.5.14.2a","Requirement","ECSS-E-ST-20-08_0090529",1,"Created","Subgroup P shall be constituted as follows (in conformance with requirement 7.4.2.2d):\n    1. 4 high-grade solar cells,\n    2. 16 mid-grade solar cells and\n    3. 4 low-grade solar cells.\n        NOTE See cell grading in SCD-BSC."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.4a","Requirement","ECSS-E-ST-20-08_0090565",1,"Created","A process identification document (PID) for the coverglasses to be qualified shall be prepared by the supplier in conformance with Annex F."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.6.1c","Requirement","ECSS-E-ST-20-08_0090576",1,"Created","If a purchase order is placed for a procurement lot of a previously qualified coverglass, the qualification tests need not to be repeated if the following conditions are satisfied:\n    1. No changes are made to the design, function or mechanical parameters of the coverglass.\n    2. The same SCD-CVG is applicable.\n    3. No changes are made to the PID. "]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.7.3.2a","Requirement","ECSS-E-ST-20-08_0090601",1,"Created","The values and tolerances of the refractive index, measured using the following V-block refractometer method, shall be stated in the SCD-CVG: \n    1. Prepare the samples by cutting 22 mm × 22 mm square samples and clamp them together to give a small block approximately 6 mm in thickness. \n    2. Place this block into the V of a V-block prism made of a glass of refractive index similar to that of the sample under test. \n    3. To achieve the optical contact, use a matching refractive index fluid. \n    4. Measure first a reference block of known refractive index in order to calibrate the apparatus. \n        NOTE The instrument gives an absolute measurement referenced to this Standard with an accuracy better than ±10-4 over the range of 1,47 to 1,65. \n    5. Use a sodium d-line as the light source."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.7.5.1b","Requirement","ECSS-E-ST-20-08_0090612",1,"Created","The wavelength tolerance shall be l ± 2 nm and a reflectance tolerance of (R ± 1) %, where l and R are as stated in the SCD-CVG."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.7.13.2d","Requirement","ECSS-E-ST-20-08_0090648",1,"Created","The nominal rate shall be lower than the value stated in the SCD-CVG."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","8.10a","Requirement","ECSS-E-ST-20-08_0090669",1,"Created","All deliverable hardware specified in the order shall be delivered together with documentation in conformance with the requirements specified in clause 8.9."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.2.1.2.2a","Requirement","ECSS-E-ST-20-08_0090674",1,"Created","The conditions and methods of external protection diode testing shall conform to the external protection diode source control drawing (SCD-EPD).\n    NOTE The external protection diode specification consists of two parts, the generic specification (this Standard) and the SCD-EPD. The SCD-EPD contains the technical specification for a diode type relevant to acceptance testing, as well as for the qualification testing. For the preparation of the SCD-EPD for external protection diodes, refer to Annex E, checklist for SCD-EPD."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.4.4c","Requirement","ECSS-E-ST-20-08_0090694",1,"Created","If requirement 9.4.4b is not met, as the sample size shall be stated in SCD-BSC or SCD-EPD."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.5.4.3a","Requirement","ECSS-E-ST-20-08_0090721",1,"Created","The total quantity of test samples shall be a minimum in conformance with Table 9-3 (for IPD) or Table 9-4 (for EPD)."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.6.6.2d","Requirement","ECSS-E-ST-20-08_0090746",1,"Created","The duration of the test shall be 30 days."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.6.11.2b","Requirement","ECSS-E-ST-20-08_0090762",1,"Created","The ultimate pull strength of each tab shall be as stated in the SCD-BSC or SCD-EPD."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.6.14.2a","Requirement","ECSS-E-ST-20-08_0090773",1,"Created","Temperature behaviour of all samples in subgroup C shall be measured."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","9.6.18.2c","Requirement","ECSS-E-ST-20-08_0090798",1,"Created","The duration of the life test shall be in conformance with the duration of the mission."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","10.1.2c","Requirement","ECSS-E-ST-20-08_0090819",1,"Created","For bare solar cells and SCAs, testing, the largest dimension of the detector shall be less than half of the smallest dimensions of the cell, with a minimum dimension of 1 cm for rectangular detector, or a minimum area of 1cm² for circular detector."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","10.2.4b","Requirement","ECSS-E-ST-20-08_0090848",1,"Created","The standard cells shall be kept in the dark during storage periods of more than one month."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","11.2.2.1b","Recommendation","ECSS-E-ST-20-08_0091094",1,"Created","The voltage should be measured at the test specimen terminals."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","A.2.1<7.4>a","Requirement","ECSS-E-ST-20-08_0090891",1,"Created","In conformance with clause 5.5.1.7, the SCD-PVA shall state the test sequence, test definitions and requirements for the EMC test."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","A.2.1<8.3>b","Requirement","ECSS-E-ST-20-08_0090895",1,"Created","For insulation resistance, the SCD-PVA shall state the minimum insulation resistance, in MW, at a test voltage specified in V, for the configurations specified in clause 5.5.3.3.3."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","B.2.1<6.3>a","Requirement","ECSS-E-ST-20-08_0090918",1,"Created","In conformance with clause 6.4.3.4, the SCD-SCA shall include the six equidistant solar cell temperatures to which the test is performed."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","C.2.1<6.6>a","Requirement","ECSS-E-ST-20-08_0090943",1,"Created","In conformance with clause 7.5.6.2, the SCD-BSC shall include the interval of reflectance for silicon BSR cells, at 1,5 mm, as a percentage (%)."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","D.2.1<4>a","Requirement","ECSS-E-ST-20-08_0090968",1,"Created","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."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","D.2.1<8.4>a","Requirement","ECSS-E-ST-20-08_0090981",1,"Created","In conformance with clause 8.7.3, the SCD-CVG shall include a figure showing the nominal values and tolerances for the following electro-optical properties:\n    1. bulk resistivity and surface resistivity;\n    2. refractive index."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","E.2.1<7.11>a","Requirement","ECSS-E-ST-20-08_0091015",1,"Created","In conformance with requirement 9.6.17.2f, the SCD-EPD shall include:\n1.\tFor level 1: The voltage (VREV), current (Ifw), times (T1, T2 and T3) and temperatures.\n2.\tFor level 2: The voltage (VREV), current (Ifw), times (T1, T2 and T3) and temperatures."]
["ECSS-E-ST-20-08C","ECSS - Superseded v0.9","G.2.1a","Requirement","ECSS-E-ST-20-08_0091020",1,"Created","The PVA-DDP of coupons for the delivery review board (DRB) shall include, as a minimum, the following items:\n    1. table of contents;\n    2. certificate of conformance;\n    3. shipping documents;\n    4. configuration item data list (CIDL);\n    5. product manufacturing and control file (PMCF);\n    6. parts, materials and processes (PMP) list;\n    7. list of requests for deviations;\n    8. list of requests for waivers;\n    9. list of nonconformances, including copies of nonconformance reports (NCRs) NRB documentation including failure analysis and failed coupon list;\n    10. history record;\n    11. connector mate and de-mate record;\n    12. serialized components list;\n    13. in-process inspection test results, including positioning in the manufacturing flow chart;\n    14. open work or open test;\n    15. replacement or temporary installation record;\n    16. acceptance and qualification test procedures and test reports;\n    17. assembly drawings and circuit diagram;\n    18. notes and comments;\n    19. operation and maintenance manuals and user restrictions;\n    20. minutes of delivery review board (DRB) meetings;\n    21. lower level data documentation packages (DDPs)."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","4.3.1b","Requirement","ECSS-E-ST-50-05_0900021",1,"Created","Prior to the design phase of any spacecraft project, the project shall request the frequency assignments for the spacecraft. "]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","5.5.1.1a","Requirement","ECSS-E-ST-50-05_0900039",1,"Created","The spurious emissions, including harmonics, generated by spacecraft and Earth station transmitters shall not exceed the levels given in Table 5-6.\n    NOTE This is consistent with ITU/RR/AP3."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","5.5.6c","Requirement","ECSS-E-ST-50-05_0900060",1,"Created","Spacecraft shall limit their transmission of RF power towards the Earth to the periods when telecommunications or tracking operations are carried out. \n    NOTE 1 See also 4.2\n    NOTE 2 Example of space-Earth link telecommunication is reception of telemetry and data."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","6.1.4.2.3c","Requirement","ECSS-E-ST-50-05_0900085",1,"Created","At each transition in the PCM waveform, the subcarrier shall be reversed in phase."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","6.1.10d","Requirement","ECSS-E-ST-50-05_0900103",1,"Created","Phase noise of the unmodulated carrier, integrated between 1 Hz and 10 kHz, shall be less than the following values:\n    1. 4° r.m.s. at SHF (7 145 MHz - 7 190 MHz, and 8 400 MHz - 8 450 MHz).\n    2. 10° r.m.s. at EHF (31,8 GHz - 32,3 GHz and 34,2 GHz - 34,7 GHz)."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","6.2.1b","Requirement","ECSS-E-ST-50-05_0900112",1,"Created","For symbol rates in excess of 2 Msps (for the bands below 8 500 MHz) or 20 Msps (only for the 31,8 GHz - 32,3 GHz band) as defined by Figure 6 2, only TCM 8PSK (for the 8 025 MHz - 8 400 MHz band), filtered-OQPSK (for the bands below 8 500 MHz) or GMSK (for all bands) shall be used.\n    NOTE Users are encouraged to also use modulation with suppressed carrier in the range of symbol rates from 60 ksps to 1 Msps for the bands below 8 500 MHz."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","6.2.3.4c","Requirement","ECSS-E-ST-50-05_0900137",1,"Created","The amplitude imbalance between the two quadrature carriers shall be less than 0,5 dB."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","6.2.3.5d","Requirement","ECSS-E-ST-50-05_0900150",1,"Created","In the case of impairments the following conditions shall be met:\n    1. For an I-Q implementation of the modulator:\n        (a) A phase angle between the two quadrature carriers of (90 ± 5)°.\n        (b) An amplitude imbalance between the two quadrature carriers of less than 0,5 dB.\n        (c) A modulation such that for each channel, the suppression of the signal from the other channel is more than 21 dB.\n    2. For any implementation, a synchronization of the symbol clocks within ±2 % of the symbol period or 1 ns, whichever is larger. \n    3. For digital implementation:\n        (a) A FIR filter impulse response of at least 4 bits long for category B applications and 5 bits long for category A applications.\n        (b) A minimum number of bits for the FIR coefficient quantization of 12."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","7.2.1j","Recommendation","ECSS-E-ST-50-05_0900282",1,"Created","The following values, consistent with a transponder second order phase-lock loop bandwidth 2 BL = 800 Hz and a damping factor 0,7 < z < 1,2, should be used:\n    1. Maximum sweep rate: 32 kHz/s.\n    2. Maximum discontinuity: 10 Hz.\n    3. Maximum sweep range: ±150 kHz."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","8.3.2e","Recommendation","ECSS-E-ST-50-05_0900290",1,"Created","Margins for budgets based on the design value, favourable tolerance, adverse tolerance, mean value, mean -3s and worst case RSS should be calculated as follows:\n    1. The margin for mean - 3s is:\nmargin for mean parameters  .\n    2. The worst case RSS margin is:\nmargin for design parameters  .\n        NOTE Note that the calculation of the variances of the margin from the sum of variances of its components, which have different density functions, is valid only if all the variances are of approximately the same magnitude. "]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","9.2.5a","Requirement","ECSS-E-ST-50-05_0900234",1,"Created","The constellation mapper for SEF = 2 shall conform to Figure 9-4."]
["ECSS-E-ST-50-05C Rev. 1","ECSS - Superseded v0.9","9.2.6.2a","Recommendation","ECSS-E-ST-50-05_0900299",1,"Created","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. "]
["ECSS-E-ST-32-08C","ECSS - Superseded v0.9","4.2.10a","Requirement","ECSS-E-ST-32-08_0220018",1,"Created","For all solid surfaces, moving or in static contact with other solid surfaces, and intended to be separated it shall be demonstrated by test that the increase in separation force during this physical contact does not exceed the specified limit.\n    NOTE For very clean surfaces strong adhesion occurs at the regions of real contact, a part of which can result from to cold-welding."]
["ECSS-E-ST-32-08C","ECSS - Superseded v0.9","4.5.1a","Requirement","ECSS-E-ST-32-08_0220039",1,"Created","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."]
["ECSS-E-ST-32-08C","ECSS - Superseded v0.9","4.6.4d","Requirement","ECSS-E-ST-32-08_0220061",1,"Created","Measurements shall be performed in the main direction of reinforcement and in the transverse direction.\n    NOTE 1 The most common properties to be assessed to validate a new generated composite material are:\n        · tensile strength;\n        · elastic modulus;\n        · compression strength;\n        · CTE (Coefficient of Thermal Expansion);\n        · CME (Coefficient of Moisture Absorption);\n        · through thickness thermal conductivity;\n        · in plane shear strength.\n    NOTE 2 Where the material is quasi-isotropic, measurements in the second direction can be useful to check the isotropicity of the material."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","5.2.3.1b","Requirement","ECSS-E-ST-10_0790013",1,"Created","The system engineering organisation shall ensure that the technical requirements specifications it establishes conform to ECSS-E-ST-10-06 and its DRD in Annex A."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","5.2.3.3a","Requirement","ECSS-E-ST-10_0790018",1,"Created","The system engineering organisation shall identify requirements impacting strongly on system risk."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","5.3.2e","Requirement","ECSS-E-ST-10_0790043",1,"Created","The system engineering organisation shall establish environment conditions for product verification."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","5.4.2.1b","Requirement","ECSS-E-ST-10_0790074",1,"Created","The system engineering organisation shall ensure that the configuration includes all lower decomposition levels."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","5.6.1e","Requirement","ECSS-E-ST-10_0790090",1,"Created","The system engineering organization shall ensure the availability of product and process data which enables the complete system to be produced, tested, delivered, operated, maintained, and properly disposed of."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","6.2d","Requirement","ECSS-E-ST-10_0790115",1,"Created","The system engineering organisation shall identify the critical elements."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","6.4b","Requirement","ECSS-E-ST-10_0790121",1,"Created","The system engineering organization shall propose solutions (including identification of criticalities and risks) to meet the perceived needs."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","B.2.1<4>b","Requirement","ECSS-E-ST-10_0790142",1,"Created","Description of how the system works in each mission phase\n    1. Performance drivers\n    2. Constraints\n    3. Main events\n    4. Operations scenarios\n        NOTE For example: For a spacecraft, the following phase:\n            · Launch preparation \n            · Launch and Early Orbit Phase \n            · In Orbit Commissioning \n            · Nominal Operations \n            · Spacecraft Disposal "]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","D.2.1<4.2>a","Requirement","ECSS-E-ST-10_0790163",1,"Created","The SEP shall list the specified system engineering outputs as defined in ECSS-E-ST-10 clause 6 for the specific project phase(s) covered in the SEP.\n    NOTE An overview of document delivery is given in Annex A."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","D.2.1<5.3>b","Requirement","ECSS-E-ST-10_0790188",1,"Created","In relation to requirements traceability and demonstration of verification (compliance with requirements, VCD), the specific methods and tools shall be described (including interfaces to next lower level suppliers), and reuse of elements (e.g. COTS) identified."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","E.2.2a","Permission","ECSS-E-ST-10_0790394",1,"Created","The content of the TP may be merged with the content of the SEP."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","G.2.1<8>a","Requirement","ECSS-E-ST-10_0790235",1,"Created","The DDF shall contain the information on the system or product engineering database that contains the complete set of design parameters, or a reference to it.\n    NOTE Information about the set of design parameters is provided in ECSS-E-TM-10-10."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","H.2.1<4>a","Requirement","ECSS-E-ST-10_0790240",1,"Created","The function tree document shall provide the complete list of functions that the system or product shall perform, and contain a graphical representation where the main specified function(s) (i.e. at the top level of the tree) is/are decomposed into lower level functions."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","K.2.1<8.2.2>a","Requirement","ECSS-E-ST-10_0790275",1,"Created","The DJF shall present the implementation of the qualification plan and the status thereof, addressing the detailed definition of qualification activities (e.g. analysis, test, ROD, and inspection), including the detailed definition of the tests, the prediction of expected test results, test success criteria, test specifications, and model validations.\n    NOTE Details on test specifications are provided in ECSS-E-ST-10-03 Annex B."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","K.2.1<11>b","Requirement","ECSS-E-ST-10_0790287",1,"Created","The DJF shall include or refer to the DJF of lower level elements of the product."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","N.2.1<1>a","Requirement","ECSS-E-ST-10_0790312",1,"Created","The RTM shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","P.2.1<2>a","Requirement","ECSS-E-ST-10_0790333",1,"Created","The PUM shall list the applicable and reference documents in support of the generation of the document."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","P.2.1<4.10>a","Requirement","ECSS-E-ST-10_0790357",1,"Created","The PUM shall describe the conditions, procedures and logistics for the maintenance of the product, be it integrated or stand-alone.\n    NOTE The description can refer to the document that conforms to the Integrated Logistic Support Plan in conformance with ECSS-M-ST-70."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","P.2.1<5.4>a","Requirement","ECSS-E-ST-10_0790364",1,"Created","The PUM shall include:\n    1. description of software design,\n    2. product constituent software,\n    3. application process service software, and\n    4. memory map."]
["ECSS-E-ST-10C","ECSS - Superseded v0.9","Q.2.1<1>b","Requirement","ECSS-E-ST-10_0790385",1,"Created","Any open issue, assumption and constraint relevant to this document shall be stated and described."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.1.2i","Requirement","ECSS-E-ST-31-02_1190013",1,"Created","Quantity of units required for the qualification process shall be specified in the TS.\n    ","NOTE TS exclude requirements such as cost, methods of payment, time or place of delivery."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.5.1c","Requirement","ECSS-E-ST-31-02_1190041",1,"Created","Formal close-out of qualification at lower level shall be performed prior to close-out at higher level."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.5.5.1a","Requirement","ECSS-E-ST-31-02_1190066",1,"Created","The following generic performance characteristics of a TPHTE shall be determined and verified against specified data:\n    1. Ability to sustain the combination of the predicted worst mechanical loads:\n        (a) External mechanical loads.\n        (b) Internal loads due to the saturation pressure of the heat carrier fluid within the TPHTE exposure temperature range.\n        (c) Thermo-mechanical loads due to temperature cycling and CTE mismatch within the TPHTE exposure temperature range.\n        (d) Loads imposed by volume change due to freezing/thawing of the heat carrier within the TPHTE exposure temperature range.\n    2. Safe life item and fatigue-life demonstration\n        (a) Safe life item demonstration, performed by analysis or test or both in conformance with ECSS-E-ST-32-01 for TPHTE not submitted to a proof pressure or for which the proof factor used in the proof pressure test is less than 1,5.\n        (b) Fatigue-life demonstration, performed by analysis or test or both in conformance with ECSS-E-ST-32 for TPHTE for which the proof factor used in the proof pressure test is equal or larger than 1,5.\n    3. Thermal parameters:\n        (a) Minimum and maximum heat transport capability over the TPHTE thermal performance temperature range.\n            NOTE For heat pipes only the maximum heat transport capability is of interest.\n        (b) Evaporator heat flux over the TPHTE thermal performance temperature range.\n        (c) Heat transfer coefficient in the evaporator and condenser.\n        (d) Overall thermal resistance of the device.\n    4. Operational characteristics\n        (a) Maximum heat load applied in one step at discrete temperatures over the specified range.\n        (b) Start-up behaviour from frozen conditions, if the exposure temperature range includes freezing of the working fluid.\n        (c) For cryogenic TPHTE, start-up from the super-critical state of the working fluid.\n    5. Leak-before-burst.\n    6. Lifetime performance:\n        (a) Long-term compatibility between fluid and wetted materials (materials in contact with the fluid).\n        (b) Space radiation effects in order to demonstrate that fluid de-composition does not adversely affect specified TPHTE performance during the product life cycle."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.6.6b","Requirement","ECSS-E-ST-31-02_1190094",1,"Created","The supplier shall analyse the number of cycles above the 2000 cycles, to which the TPHTE can be exposed before reaching the Woehler curve."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.6.8a","Requirement","ECSS-E-ST-31-02_1190102",1,"Created","Leak test shall be performed at ambient temperature using a detection method agreed with the customer."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.6.9.2.4a","Requirement","ECSS-E-ST-31-02_1190121",1,"Created","After a full depriming (emptying the capillary structure), a start-up procedure shall be determined."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","5.6.13c","Requirement","ECSS-E-ST-31-02_1190149",1,"Created","It shall be demonstrated that non-condensable gas generation over the lifetime meets the specification for lifetime performance."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","A.2.1<4>a","Requirement","ECSS-E-ST-31-02_1190172",1,"Created","The technical specification shall describe the concept, the expected product architecture and the functioning principles on which it is based."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","C.2.1<1>a","Requirement","ECSS-E-ST-31-02_1190193",1,"Created","The RRPT shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","E.2.1<7>a","Requirement","ECSS-E-ST-31-02_1190214",1,"Created","The TSPE shall describe the applicable test facility requirements together with the instrumentation and measurement accuracy, data acquisition and test space segment equipment to be used."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","E.2.1<10>a","Requirement","ECSS-E-ST-31-02_1190219",1,"Created","The TSPE shall list the requirements for the involved documentation, including test procedure, test report and PA and QA records."]
["ECSS-E-ST-31-02C","ECSS - Superseded v0.9","H.2.1<1>a","Requirement","ECSS-E-ST-31-02_1190251",1,"Created","The VRPT shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.2.4.2a","Requirement","ECSS-E-ST-33-01_0820006",1,"Created","Existing parts and components used in mechanisms shall have been previously qualified for the intended application according to a qualification procedure approved by the customer.\n    NOTE Existing parts and components relate to parts and components that were not specifically developed for this specific application and cover commercially available and off-the-shelf hardware."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.4.2c","Requirement","ECSS-E-ST-33-01_0820031",1,"Created","The envelope of movement for each moving part shall be defined."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.5.2.6c","Requirement","ECSS-E-ST-33-01_0820043",1,"Created","In manned space systems, flammable, toxic and unstable materials shall not be used."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.3.3.3c","Requirement","ECSS-E-ST-33-01_0820078",1,"Created","The integrity of the anti-creep barrier shall be verifiable by indicators.\n    NOTE For example, UV-detectable."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.3.4.2d","Requirement","ECSS-E-ST-33-01_0820083",1,"Created","If pre-loading is not applied by 4.7.3.4.2c solutions, sliding shall be facilitated by a lubricated sliding sleeve, bush or dedicated tribological coating."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.5.2.2d","Requirement","ECSS-E-ST-33-01_0820104",1,"Created","For the derivation of the operational loads, the related induced reaction of the spacecraft shall be taken into account. "]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.5.3.2b","Requirement","ECSS-E-ST-33-01_0820125",1,"Created","T (or force F) shall be greater or equal than Tmin (or Fmin) as calculated in the clause 4.7.5.3.1."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.5.4.5b","Requirement","ECSS-E-ST-33-01_0820155",1,"Created","Except for gears and ball or journal bearings, the contact between the mating surfaces shall be characterized.\n    NOTE Characterisation includes surfaces roughness, hardness, material properties, and contact geometry."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.5.4.12a","Recommendation","ECSS-E-ST-33-01_0820410",1,"Created","Pyrotechnic and other release and locking device actuators should be redundant.\n    NOTE Example of such actuators are thermal knives, memory metal and paraffin actuators."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.7.2a","Requirement","ECSS-E-ST-33-01_0820193",1,"Created","Electrical wires shall be insulated from the structure and from each other by not less than 10 MW measured with a DC voltage of 500 V applied."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.7.5a","Requirement","ECSS-E-ST-33-01_0820203",1,"Created","With the exception of the bonding strap for grounding, all electrical connections to the mechanism shall be made through electrical connectors of a type qualified for the intended application."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.7.8.9a","Requirement","ECSS-E-ST-33-01_0820228",1,"Created","Harnesses and cables to moving parts shall be characterized in terms of hysteresis and stiffness in representative configuration over the full range of displacement and over the specified qualification levels in terms of temperature range, lifetime, speed effects."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.8.2.13b","Requirement","ECSS-E-ST-33-01_0820261",1,"Created","The functional performance of the control system shall be analysed for\n    1. stability,\n    2. bandwidth,\n    3. dynamic and static accuracy,\n    4. resolution, and\n    5. generation of and susceptibility to disturbances at the interfaces of the mechanism."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.8.2.19a","Requirement","ECSS-E-ST-33-01_0820275",1,"Created","Electrical parts stress analysis shall be performed to demonstrate that the electrical parts conform to the derating requirements. \n    NOTE For derating see ECSS-Q-ST-30-11."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.8.3.3.7c","Requirement","ECSS-E-ST-33-01_0820300",1,"Created","The compatibility of the fluid lubricant with the mechanism materials and other lubricants used within the mechanism shall be verified."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.8.3.3.9c","Requirement","ECSS-E-ST-33-01_0820305",1,"Created","Motor windings 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 at least five times the worst-case flight operating voltage applied for a duration of 2 min or until a steady state resistance value is measured."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","4.8.3.4.2b","Requirement","ECSS-E-ST-33-01_0820326",1,"Created","The acceptance test sequence shall be agreed by the customer."]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","A.2.1<6>b","Requirement","ECSS-E-ST-33-01_0820352",1,"Created","The SMS shall include the limits for outgassing, creeping and potential sources of contamination.\n    NOTE 1 This limits have a strong impact on the design of the fluid lubricated system. \n    NOTE 2 For generic requirements on outgassing limits, see requirement 4.7.3.3.2b                                                 "]
["ECSS-E-ST-33-01C","ECSS - Superseded v0.9","C.2.1<1>c","Requirement","ECSS-E-ST-33-01_0820373",1,"Created","The MAV shall include any additional definition, abbreviation or symbol used."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.1a","Requirement","ECSS-E-ST-10-02_0740001",1,"Created","The verification process shall demonstrate that the deliverable product meets the specified customer requirements and is capable of sustaining its operational role through:\n    1. Verification planning;\n    2. Verification execution and reporting;\n    3. Verification control and close-out."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.2.2.1e","Requirement","ECSS-E-ST-10-02_0740011",1,"Created","If the impact of the requirement is major, a risk mitigation plan (part of the VP) shall be defined which includes a cross check based on two independent analyses (in terms of model used and suppliers)."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.2.3c","Requirement","ECSS-E-ST-10-02_0740032",1,"Created","Formal close-out of qualification and acceptance at lower levels shall be performed prior to close-out at higher level."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.2.6.1d","Requirement","ECSS-E-ST-10-02_0740057",1,"Created","Formal verification procedures shall be established and applied to tools which are specified as deliverable items."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.3.2.1c","Requirement","ECSS-E-ST-10-02_0740087",1,"Created","The supplier shall provide the Test reports (TRPT) for the reviews as agreed with the customer \n    NOTE Guidelines are provided in Annex G. "]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","5.3.2.5d","Requirement","ECSS-E-ST-10-02_0740104",1,"Created","The supplier shall provide a Verification report (VRPT) for the reviews as agreed with the customer \n    NOTE Guidelines are provided in Annex G."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","A.2.1<2>a","Requirement","ECSS-E-ST-10-02_0740129",1,"Created","The VP shall list the applicable and reference documents in support to the generation of the document."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","A.2.1<7>a","Requirement","ECSS-E-ST-10-02_0740134",1,"Created","The VP shall describe the selected combination of the different verification methods at the applicable verification levels and stages, in general and for each requirement type/group (including software). "]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","C.2.1<1>b","Requirement","ECSS-E-ST-10-02_0740156",1,"Created","Open issues, assumptions and constraints relevant to this document shall be stated and described."]
["ECSS-E-ST-10-02C","ECSS - Superseded v0.9","F.2.1<1>b","Requirement","ECSS-E-ST-10-02_0740181",1,"Created","Open issues, assumptions and constraints relevant to this document shall be stated and described."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.2.2f","Requirement","ECSS-E-ST-33-11_0280014",1,"Created","It shall be agreed with the customer which performance characteristics shall be declared as mean values with associated standard deviation (see 4.2.2g). "]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.2.5.3a","Requirement","ECSS-E-ST-33-11_0280028",1,"Created","For phases A and B of the component, the methodology for dimensioning explosive devices shall be justified."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.5.2.2c","Requirement","ECSS-E-ST-33-11_0280061",1,"Created","The pre-arm function shall remain in its switched state after operation until the fire function has reverted to its initial state."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.5.2.3d","Requirement","ECSS-E-ST-33-11_0280066",1,"Created","The select function shall be used to control only one explosive function."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.8.1.4b","Requirement","ECSS-E-ST-33-11_0280096",1,"Created","Inert components, dummies and test models used for test purposes shall be visibly different from live items with the colour code in Table 4-2.\n    NOTE This is to prevent confusion and to ensure incorrect items are not used for flight or qualification."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.8.2.5b","Requirement","ECSS-E-ST-33-11_0280113",1,"Created","Protective features shall be provided to \n    1. prevent initiation, \n    2. prevent change of state of barriers,\n    3. prevent parasitic paths,\n    4. be tested to verify effectiveness."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.8.3.1b","Requirement","ECSS-E-ST-33-11_0280138",1,"Created","Protective features shall \n    1. be provided to prevent unintended initiation, \n    2. be provided to prevent loss of performance,\n    3. be tested to verify effectiveness."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.9f","Requirement","ECSS-E-ST-33-11_0280159",1,"Created","The nature and condition of age-sensitive materials shall be identified and documented in the DMPL."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.10.3f","Requirement","ECSS-E-ST-33-11_0280182",1,"Created","Shields shall not be used for current carrying.\n    NOTE Shields can be multiple-point grounded to the structure. "]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.10.6c","Requirement","ECSS-E-ST-33-11_0280190",1,"Created","The power provided at the power distribution points shall be such that the requirements of 4.8.2.6 allowing for losses are met."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.10.11.2a","Requirement","ECSS-E-ST-33-11_0280211",1,"Created","The electrically actuated safe and arm device shall not have current flow exceeding 2 mA in the disarm or safe command circuit during the arming cycle nor in the arm command circuit during disarm or safing;"]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.11.1.1a","Requirement","ECSS-E-ST-33-11_0280229",1,"Created","Clauses from 4.11.1.2 until 4.11.6 shall apply to explosive components, which cannot be fully tested before flight. "]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.11.3.3c","Requirement","ECSS-E-ST-33-11_0280262",1,"Created","The connector thread or closing mechanism shall be self locking."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.12.1a","Requirement","ECSS-E-ST-33-11_0280283",1,"Created","For any explosively actuated device which incorporates initiation and explosive charges the requirements of Clause 4.11 shall apply."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.13.1c","Requirement","ECSS-E-ST-33-11_0280308",1,"Created","Test equipment shall be energy limited in conformance with 4.8.4.\n    NOTE E.g. electrical, optical."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.13.3b","Requirement","ECSS-E-ST-33-11_0280315",1,"Created","The status of explosive safety barriers shall be monitored when the space vehicle induces a catastrophic risk.\n    NOTE The space vehicle comprises e.g. the launcher, satellite, spacecraft."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.14.3.6b","Requirement","ECSS-E-ST-33-11_0280335",1,"Created","Only planned and approved activities shall be performed, in conformance with approved procedures."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.15.3a","Requirement","ECSS-E-ST-33-11_0280360",1,"Created","No explosive component shall be stored with other types of equipment."]
["ECSS-E-ST-33-11C","ECSS - Superseded v0.9","4.16.3a","Requirement","ECSS-E-ST-33-11_0280383",1,"Created","Confirmation of operation shall be made available immediately."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","6.3.3.1a","Requirement","ECSS-E-ST-20-06_0070017",1,"Created","The applicability of the electrical continuity requirements shall be established in accordance with the diagram in Figure 6-1."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","6.3.3.3b","Requirement","ECSS-E-ST-20-06_0070022",1,"Created","Any point on a blanket shall be within 1 m of a bonding strap. "]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","6.6.1j","Requirement","ECSS-E-ST-20-06_0070043",1,"Created","Tests shall be performed at temperature of use in space.\n    NOTE This is because temperature has a large effect on conductivity in dielectric materials. As temperature falls, resistivity rises."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","7.2.3.1b","Requirement","ECSS-E-ST-20-06_0070075",1,"Created","Testing of solar arrays shall demonstrate that the plasma created by a primary ESD or resulting from another triggering mechanism does not lead to a self sustained secondary arc and does not lead to the degradation of the solar array.\n    NOTE 1 Examples are:\n        · Potential triggering mechanisms are primary ESDs, hypervelocity impacts, thruster firings and other plasma sources.\n        · Possible degradation of solar arrays are contamination, loss of insulation, and cell degradation\n    NOTE 2 Risk assessment of by-pass diode degradation should be covered by a specific EMC immunity test to ESD effects."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","7.2.3.2l","Requirement","ECSS-E-ST-20-06_0070090",1,"Created","Before testing, it shall be verified that cells diodes are conductive.\n    NOTE This can be done by passing a small current through the string. This current is usually taken to be about 10 mA (to avoid unrealistic heating)."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","9.3c","Requirement","ECSS-E-ST-20-06_0070115",1,"Created","Testing of circuits shall be performed at equipment level by the application of voltage spikes on input, output and power lines. \n    NOTE This determines whether filtering is adequate."]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","10.2.1a","Requirement","ECSS-E-ST-20-06_0070122",1,"Created","The insulation shall be thick enough to withstand the maximum voltage on the cable. "]
["ECSS-E-ST-20-06C","ECSS - Superseded v0.9","11.3.5b","Permission","ECSS-E-ST-20-06_0070178",1,"Created","The assessment specified in 11.3.5a may be made by in-flight observations.\n    NOTE 1 For example, by using Langmuir probes. \n    NOTE 2 Otherwise, calculation or computer simulation can be used to make this assessment. This analysis is expected to take into consideration the flow rate of the gas, its temperature and its rate of ionization."]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","4.1.2.2c","Requirement","ECSS-E-ST-60-20_0920004",1,"Created","The date of measurement shall be expressed as a (scalar) number indicating the delay relative to a known external time reference agreed with the customer."]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","4.1.8.2b","Requirement","ECSS-E-ST-60-20_0920025",1,"Created","The image output time shall be verified by test using the hardware agreed between the customer and supplier.\n    NOTE 1 The hardware used to perform the test is the hardware used to download the image from the star sensor.\n    NOTE 2 For example:\n        • “The Star Sensor shall be capable of performing a full Image Download of the entire Field of View at 12-bit resolution. The image output time shall be less than 10 seconds.”\n        • “The Star Sensor shall be capable of performing a partial Image Download at 12-bit resolution of a n×n section of the Field of View. The image output time shall be less than 10 seconds.”"]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","5.2.2a","Requirement","ECSS-E-ST-60-20_0920045",1,"Created","Software models of single star measurement error shall be validated for single star performance (at zero body rates) against on-ground tests using artificial stellar sources.\n    NOTE Denoting the confidence level to be verified as PC, and assuming that the performance confidence level result to be obtained is to an accuracy DP with 95 % estimation confidence level, the number of Monte-Carlo runs to be performed is greater than  ."]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","5.5.4.3b","Requirement","ECSS-E-ST-60-20_0920076",1,"Created","Radiation effects shall be supported by test results.\n    NOTE E.g. “The Star Sensor shall have a FOV spatial error less than 10 arcsec on X,Y axes and 40 arcsec on Z axis for spatial period smaller than 5 degrees.”"]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","5.5.9b","Permission","ECSS-E-ST-60-20_0920152",1,"Created","On-ground tests may be performed.\n    NOTE E.g. “The Star Sensor shall have a Measured Output Bandwidth of greater than 10 Hz.” "]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","5.9.4a","Requirement","ECSS-E-ST-60-20_0920113",1,"Created","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.” "]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","5.11.1a","Requirement","ECSS-E-ST-60-20_0920128",1,"Created","Additional performance conditions, defined in 5.10.1 shall be applied."]
["ECSS-E-ST-60-20C Rev. 1","ECSS - Superseded v0.9","A.2.1<5>b","Requirement","ECSS-E-ST-60-20_0920149",1,"Created","For sensors with the autonomous attitude tracking capability, the FMM description shall include the autonomous attitude tracking capability."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.2.5.2f","Requirement","ECSS-E-ST-33-01_0820023",2,"Normative Change","Unless redundancy is achieved by the provision of a complete redundant mechanism, active parts of mechanisms, such as sensors, motor windings, brushes, actuators, switches and electronics, shall be redundant."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.5.2.9b","Requirement","ECSS-E-ST-33-01_0820048",1,"Unchanged","ECSS-Q-ST-70-71 clause “Atomic oxygen” shall apply."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.3.2c","Requirement","ECSS-E-ST-33-01_0820070",1,"Unchanged","The dry lubricant application process shall be verified with respect to lubricant performance and repeatability."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.3.3.2b","Requirement","ECSS-E-ST-33-01_0820075",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.4.2e","Requirement","ECSS-E-ST-33-01_0820095",1,"Unchanged","The mechanism design shall take into account the worst-case combinations (including uncertainties) of:\n1.\textremes of operational and survival steady­state, \n2.\ttransient temperatures, \n3.\tmechanism heat dissipation, and\n4.\tthe temperature gradients across the mechanism.","NOTE \tFailure to consider the effects of differential expansion can lead to a catastrophic failure.\n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.5.2.6i","Requirement","ECSS-E-ST-33-01_0820401",1,"Created","For safety critical mechanisms in crewed space missions, verification by an analysis-only approach shall be approved by the safety approval authority."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.5.4.2a","Requirement","ECSS-E-ST-33-01_0820135",1,"Unchanged","Unless monitored at spacecraft system level, the design of mechanisms shall include means to monitor the execution of its main functions. "]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.5.4.5e","Requirement","ECSS-E-ST-33-01_0820158",1,"Unchanged","Except for gears and ball or journal bearings, sliding at the separable contact surfaces before separation shall be prevented, in order to avoid potential contact surface property changes. "]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.5.4.7a","Requirement","ECSS-E-ST-33-01_0820164",2,"Normative Change","Dimensioning and sizing of gears shall be performed in conformance with, ISO 6336-1, ISO 6336-2, ISO 6336-3, ISO 677, and ISO 678."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.5.4.12f","Requirement","ECSS-E-ST-33-01_0820181",1,"Unchanged","If critical, contamination shall be measured."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.7.5b","Recommendation","ECSS-E-ST-33-01_0820467",1,"Created","Flying leads should be avoided. "]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.7.8.5j","Requirement","ECSS-E-ST-33-01_0820229",1,"Unchanged","Harnesses and cables to moving parts shall be taken into account in the control system design."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.8.2.7a","Requirement","ECSS-E-ST-33-01_0820251",2,"Normative Change","An analysis shall be provided of the predicted hertzian contact or yield or bending stresses of moving surfaces in contact under worst-case conditions to verify the compliance with the material allowables of the chosen material couple, lubricant and other coating used.","NOTE \tSurfaces in contact encompass separable and sliding contacts, and bearings.\n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.8.3.1a","Requirement","ECSS-E-ST-33-01_0820276",1,"Unchanged","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"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.8.3.3.6a","Requirement","ECSS-E-ST-33-01_0820296",2,"Normative Change","Solid lubricated ball bearing cage material, design and performance shall be verified by testing."]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.8.3.3.12a","Requirement","ECSS-E-ST-33-01_0820313",1,"Unchanged","The model and lifetime testing shall be representative with respect to the following parameters:\n1.\tThermal conditions, loading conditions, contact stress, motion profile and speed during testing, representative of the operational conditions.\n2.\tLubrication regime representative of worst-cases expected operational conditions, and for durations factored as agreed by the customer.","NOTE \tThe duration factors are defined in clause 4.8.3.3.14. \n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","4.8.3.4.2a","Requirement","ECSS-E-ST-33-01_0820325",1,"Unchanged","New builds of qualified designs shall be acceptance tested to verify that the actual manufactured hardware is free from manufacturing defects. "]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","A.2.1<3>b","Requirement","ECSS-E-ST-33-01_0820342",1,"Unchanged","If the mechanism is not maintenance free during storage and ground life, the SMS shall list the maintenance requirements, including for each of them:\n1.\tnumber of operations,\n2.\tfrequency of operations,\n3.\tspecial tooling and test equipment,\n4.\tcalibration and adjustments, \n5.\tfault identification and repair, and\n6.\tenvironment for maintainability operation.","NOTE \tSee 4.2.4.4b.\n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","A.2.1<6>e","Requirement","ECSS-E-ST-33-01_0820355",1,"Unchanged","The SMS shall list the shock load requirements for latches and locks.","NOTE \tFor the derivation of such requirements, see 4.7.5.4.3i.\n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","D.2.1<11>b","Requirement","ECSS-E-ST-33-01_0820393",1,"Unchanged","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"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","F.2.1<1>a","Requirement","ECSS-E-ST-33-01_0820425",1,"Created","The MSVP shall contain a description of the scope and applicability of the document.","NOTE \tFor example: This document provides information on the design and verification approach of the “name” mechanism for the “name” project. \n"]
["ECSS-E-ST-33-01C Rev.1","ECSS - Superseded v0.9","G.2.1<5>c","Requirement","ECSS-E-ST-33-01_0820450",1,"Created","The MSVR shall cross-reference any separate test analyses."]
["ECSS-E-ST-32-10C Rev. 1","ECSS - Superseded v0.9","4.3.2.1c","Requirement","ECSS-E-ST-32-10_0110022",1,"Created","For satellites and man rated spacecraft, when loads including thermal induced loads are relieving, both FOSU and FOSY shall be 1,0 or less.\n    ","NOTE See ECSS-E-ST-32."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","5.2.3.9a","Requirement","ECSS-E-ST-50-12_0910023",1,"Created","The wall thickness of the protective sheath for the shielded differential signal pair shall be 0,15 mm nominal."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","5.2.5.2a","Requirement","ECSS-E-ST-50-12_0910048",1,"Created","The minimum bend radius of complete cable shall be 45 mm."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","5.3.5c","Recommendation","ECSS-E-ST-50-12_0910356",1,"Created","The connection referred in b. should be performed via a parallel resistor and capacitor.\n    ","NOTE See clause 5.4 for the cable connection to pin 3 of the connector."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","5.4.3a","Requirement","ECSS-E-ST-50-12_0910075",1,"Created","The connector contacts shall be terminated as shown in Figure 5-3 and Table 5-3.\n    ","NOTE The cable signal wires cross over to achieve a transmit to receive interconnection, e.g. Dout+ is connected to Din+ ."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","6.6.1a","Requirement","ECSS-E-ST-50-12_0910096",1,"Created","The minimum data signalling rate at which a SpaceWire link shall operate is 2 Mb/s.\n    ","NOTE 1 The minimum data signalling rate is the lowest data signalling rate at which a SpaceWire link can operate.\nNOTE 2 The minimum data signalling rate is set by the disconnect timeout (clause 8.9.2.1 and 8.11.2) to greater than 1,18 Mb/s, i.e. 1/850 ns."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","7.4b","Requirement","ECSS-E-ST-50-12_0910113",1,"Created","The parity bit shall cover the previous eight bits of a data character or two bits of a control character, the current parity bit, and the current data-control flag. "]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.3r","Requirement","ECSS-E-ST-50-12_0910147",1,"Created","If no Time-Code, FCT or N-Char are sent, then the transmitter shall send NULL to indicate that the link is still active (and to prevent the disconnect detection mechanism from being triggered at the other end of the link)."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.5.2.5f","Requirement","ECSS-E-ST-50-12_0910168",1,"Created","In the Started state the sending from the transmitter of at least one NULL shall be requested before moving to the Connecting state. "]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.5.3.7.4b","Requirement","ECSS-E-ST-50-12_0910193",1,"Created","Escape error detection shall be enabled whenever the receiver is enabled after the first NULL is received."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.5.3.9a","Requirement","ECSS-E-ST-50-12_0910195",1,"Created","The character sequence error shall be detected by the state machine in the link interface."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.9.2.5.2a","Requirement","ECSS-E-ST-50-12_0910220",1,"Created","As a character sequence error can only occur during link initialization, it shall not be flagged up to the network level as a link error (see clause 8.9.5)."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","8.12.2m","Requirement","ECSS-E-ST-50-12_0910245",1,"Created","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."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","10.2.3e","Requirement","ECSS-E-ST-50-12_0910267",1,"Created","A NULL routing table entry shall mean that the routing table entry is undefined and if referenced shall lead to an invalid address error \n    ","NOTE See clause 10.5.4."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","10.2.7.2a","Requirement","ECSS-E-ST-50-12_0910292",1,"Created","Configuration registers within routing switches that implement packet distribution shall be used to specify the output ports to send packets."]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","10.4b","Requirement","ECSS-E-ST-50-12_0910297",1,"Created","SpaceWire nodes and SpaceWire routing switches shall be interconnected with SpaceWire links. "]
["ECSS-E-ST-50-12C","ECSS - Superseded v0.9","12.2.4c","Requirement","ECSS-E-ST-50-12_0910318",1,"Created","If typical 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 encoder-decoder 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.”"]
["ECSS-E-ST-32-10C Rev.2","ECSS - Superseded v0.9","4.2.1b","Requirement","ECSS-E-ST-32-10_0110015",1,"Unchanged","The application logic for factors of safety as given in Figure 4-1 shall be applied in a “recursive” manner from system level to subsystem level or lower levels of assembly."]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","4.2.2d","Requirement","ECSS-E-ST-10-04_0760007",1,"Created","For planetary mass values the 2003 standards of the International Earth Rotation Services IERS, as described in IERS Technical Note 32 [RN.2], shall be used."]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","7.2.1.2a","Requirement","ECSS-E-ST-10-04_0760028",1,"Created","The NRLMSISE-00 model for species densities shall not be mixed with the JB-2006 model for total density."]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","9.2.1.1d","Requirement","ECSS-E-ST-10-04_0760055",1,"Created","The dates of Minima and Maxima that shall be used for solar cycles 1 to 23 and the algorithm for forecasting future Minima and Maxima are presented in Annex B.1 and Table B-1.\nNOTE \t1\tAs it is difficult to define the % of solar MIN and MAX to apply for missions not scheduled in Max or Min periods, a more conservative analysis can be obtained for all periods using AE8MAX for electron fluxes and AP8MIN for proton fluxes."]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","9.2.3a","Requirement","ECSS-E-ST-10-04_0760075",1,"Created","The ISO 15390 Model [RN.19] of galactic cosmic rays shall be used for GCR flux calculations. \nNOTE \tAlthough cosmic ray fluxes increase gradually with heliocentric distance, it is a reasonable engineering approximation for current missions to assume uniformity throughout the heliosphere. "]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","9.3b","Requirement","ECSS-E-ST-10-04_0760080",1,"Created","The specification of a mission environment shall include:\n1.\tMission­average proton and electron energy spectra from trapped radiation issued from the chosen models (according to mission orbit and time). \n2.\tThe fluence spectrum of solar protons for the complete mission with geomagnetic shielding applied.\n3.\tMaximum instantaneous energy spectra of trapped electrons, trapped protons and solar energetic protons (geomagnetically shielded) for the mission, for internal charging and sensor interference analysis.\n4.\tThe ion LET flux spectrum derived from the GCR flux spectra for the appropriate solar cycle phase, together with the worst 5 minute solar energetic particle LET spectrum, including:\n(a)\tContributions from all ions from Z = 1 to Z = 92. \n(b)\tGeomagnetic shielding. \n(c)\tMaterial shielding. If no justification is available for another value, 1 g cm-2 of aluminium shielding is used.\n5.\tThe ion LET fluence spectrum derived from the GCR fluence spectra for the appropriate solar cycle phase, together with the fluence spectra from a number of events at worst day CREME96 solar energetic particle LET spectrum, including:\n(a)\tContributions from all ions from Z = 1 to Z = 92. \n(b)\tGeomagnetic shielding. \n(c)\tMaterial shielding. If no justification is available for another value, 1 g cm-2 of aluminium shielding is used.\nNOTE \tFor solar cycle 23 the number of CREME96 worst days was 5-7.\n6.\tOrbital time­behaviour of radiation­belt (if any), cosmic ray and solar energetic particle fluxes if the mission has a susceptibility to radiation background in sensors.\n7.\tAdditional contributions from on­board nuclear/radioactive sources.\n8.\tUncertainties of the radiation models as applied for the given mission."]
["ECSS-E-ST-10-04C","ECSS - Superseded v0.9","10.2.5b","Requirement","ECSS-E-ST-10-04_0760107",1,"Created","Impact risk analyses based on the number of impacts N shall be conducted through the application of Poisson statistics."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","4.1.3c","Requirement","ECSS-E-ST-20_0020009",1,"Created","High Priority telecommand decoding and generation shall be independent from the main on-board processor and its software.\n    NOTE That implies the high level command decoder, command generator and their power supply to be entirely implemented in a dedicated module in a secure and independent way."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","4.2.1u","Requirement","ECSS-E-ST-20_0020041",1,"Created","Any on-board autonomous protection override, leading to hazardous situation for the mission (category 1 and 2 criticality), shall not be implemented. \n    NOTE E.g. an LCL function for instance protecting the main power Bus against a short circuit at Bus user level or Main Bus over-voltage protection."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","4.2.3n","Requirement","ECSS-E-ST-20_0020062",1,"Created","The accidental de-mating of connectors (where it is a realistic case) or any internal connector failure shall not lead to catastrophic consequences."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","4.2.4n","Requirement","ECSS-E-ST-20_0020077",1,"Created","Redundant units within a system shall be verified by test at system level."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.2.2.2d","Requirement","ECSS-E-ST-20_0020093",1,"Created","A plan shall be established for the maintenance and periodical review of the budget established in requirement 5.2.2.2c during all project phases.\n    NOTE These budgets take into account:\n        · spacecraft-sun distance, \n        · sun and eclipse durations,\n        · solar aspect angle,\n        · pointing accuracy,\n        · environmental temperature and degradation effects,\n        · reliability and safety aspects,\n        · any one failure in the system (two failures for manned mission) not counting solar array string and battery cell failure,\n        · Failure detection, isolation and recovery scenarios. "]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.5.2j","Requirement","ECSS-E-ST-20_0020114",1,"Created","At solar array level, one short between a solar cell string and a conductive panel structure shall not produce any solar array power loss."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.6.2d","Requirement","ECSS-E-ST-20_0020139",1,"Created","In case verification by analysis of 5.6.2c is not conclusive a complementary verification by test shall be performed."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.6.4c","Recommendation","ECSS-E-ST-20_0020396",1,"Created","Flight batteries should not be used for ground operations to prevent any possible damage and subsequent degradation of life performance."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.7.2q","Requirement","ECSS-E-ST-20_0020186",1,"Created","During integration phase the power system shall be able to start up from any of its power sources irrespective of the connection of the other power source."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.7.3c","Requirement","ECSS-E-ST-20_0020191",1,"Created","The minimum energy reserve in the battery shall be enough to guarantee the mission and a safe recovery of the spacecraft under all conditions. \n    NOTE Take into account that the charge rate plays a major role in the effectiveness of battery recharge."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.7.5g","Requirement","ECSS-E-ST-20_0020210",1,"Created","If an increase of conducted emission exceeding specified limit by more than 6 db is identified from the unit level analysis of 5.7.5f, then a system level analysis shall be conducted to ensure that compatibility is maintained.\n    NOTE Rationale for this requirement:\n6 dB is the margin usually taken between unit and subsystem when building up the EMC compatibility at system level. It means that failed equipment uses that EMC margin but does not perturb further the system."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","5.8.2g","Requirement","ECSS-E-ST-20_0020238",1,"Created","The harness restraining systems on the structure shall not bring about any stress at connector level."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","6.3.2.2a","Requirement","ECSS-E-ST-20_0020263",1,"Created","The electromagnetic environment seen by the spacecraft and the EMC requirements during the pre-launch and launch phases shall be according to those described in the applicable launchers user's manuals.\n    NOTE Specific EMC requirements during the pre-launch and launch phase are described in an Interface Control document established on a contractual basis between the launching company and the customer."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","6.3.8.3a","Requirement","ECSS-E-ST-20_0020285",1,"Created","Classification of cables, and cables shield shall be in conformance with the requirements for “Wiring” specified in ECSS-E-ST-20-07."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","7.2.1.2.1a","Requirement","ECSS-E-ST-20_0020293",1,"Created","All antenna terms used in all documentation (DDF, DJF, Test Report, Test Procedures, ICD and EIDP) shall follow the definitions found in IEEE 145:1993 ”Antenna Terms”."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","7.2.2.3.1g","Requirement","ECSS-E-ST-20_0020312",1,"Created","All metallic parts in a radiating element shall be connected to the equipment DC ground to avoid electrostatic discharge (ESD)."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","7.2.2.4.3a","Requirement","ECSS-E-ST-20_0020337",1,"Created","The dielectric losses of plastic component in the RF power path shall be quantified and their impact on antenna performances assessed.\n    NOTE Components made from homogeneous plastic are usually limited to small parts (e.g. spacers or washers)."]
["ECSS-E-ST-20C","ECSS - Superseded v0.9","7.4.4c","Requirement","ECSS-E-ST-20_0020361",1,"Created","The test frequencies, number of carriers and power levels of these carriers shall be those as identified in 7.4.3b."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.1e","Requirement","ECSS-E-ST-35-06_0200005",1,"Created","Operation and use shall not generate or release contamination."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.2.2.3j","Requirement","ECSS-E-ST-35-06_0200030",1,"Created","Valves and regulators subject to reverse flow shall incorporate an outlet filter."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.2.2.5b","Requirement","ECSS-E-ST-35-06_0200035",1,"Created","Cavities or dead end tubing shall allow for thermal and vacuum drying.\n    ","NOTE See Annex B."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.3.4o","Requirement","ECSS-E-ST-35-06_0200068",1,"Created","The joining process shall not introduce contamination into the critical surface area or bring contaminants into contact with propellants, pressurants or simulation fluids."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.3.5m","Requirement","ECSS-E-ST-35-06_0200082",1,"Created","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."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.4.2b","Requirement","ECSS-E-ST-35-06_0200103",1,"Created","The results of 4.4.2a shall be reported in Annex A and Annex C.\n    ","NOTE It does not contribute to the proper functioning of the propulsion system to specify a very small NVR level to components or subsystems with small critical areas. This can even lead to immeasurable quantities of NVR. In general, the smaller the component or subsystem, the larger the allowable NVR per surface area."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","4.4.4h","Requirement","ECSS-E-ST-35-06_0200115",1,"Created","Water shall be equivalent to ISO 14951-10:2000."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","5.3.2.1b","Requirement","ECSS-E-ST-35-06_0200154",1,"Created","Mechanical pre-cleaning shall be performed before or during chemical cleaning."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","5.3.2.1c","Requirement","ECSS-E-ST-35-06_0200155",1,"Created","If there are foreign deposits due to mechanical pre-cleaning, these shall be removed.\n    ","NOTE Mechanical pre-cleaning includes e.g. wire brushing, shot blasting (wet and dry), grinding, abrasive blasting (wet or dry), the use of aluminium oxide-abrasive-coated papers and cloths."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","5.5.1a","Requirement","ECSS-E-ST-35-06_0200180",1,"Created","The selected drying methods shall be justified and reported in conformance with Annex B."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","5.5.3.3c","Requirement","ECSS-E-ST-35-06_0200197",1,"Created","Upon qualification of the drying procedure for each hardware configuration, the established drying cycle requirements shall be implemented. "]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","6.1.1g","Requirement","ECSS-E-ST-35-06_0200227",1,"Created","The minimum power of the UV source shall be 100 W."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","6.2.5a","Requirement","ECSS-E-ST-35-06_0200252",1,"Created","With agreement of the customer, the aqueous-based, fluid-flush samples shall be analysed for particle population and NVR as follows:\n    1. Particle population analysis (aqueous) using the particle analyses of 6.2.4.2 for final verification of cleanliness of the end product under the following conditions:\n        (a) the sampling and analysis methods have demonstrated accuracy and repeatability, \n        (b) The accuracy and repeatability correlate with accepted analytical methods, \n    2. NVR analysis (aqueous) for the final verification of cleanliness of the end product under the following conditions:\n        (a) the sampling and analysis methods have demonstrated accuracy and repeatability, \n        (b) The accuracy and repeatability correlate with accepted analytical methods, "]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","6.3.3e","Requirement","ECSS-E-ST-35-06_0200269",1,"Created","Procedures and practices shall be established to maintain system cleanliness. "]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","6.4.3c","Requirement","ECSS-E-ST-35-06_0200279",1,"Created","It shall be ensured that no condensation, sublimation or freezing occurs during the dryness verification, to be defined in Annex B."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","8.1d","Requirement","ECSS-E-ST-35-06_0200304",1,"Created","Clean bags shall have been cleaned internally and verified in conformance with clause 7.5. "]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","10.2d","Requirement","ECSS-E-ST-35-06_0200325",1,"Created","Immediately upon completion of step c, dryness shall be verified to meet clause 4.4.3."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","A.2.1<5>a","Requirement","ECSS-E-ST-35-06_0200351",1,"Created","The CRA shall present the analysis of the function and performance of the propulsion hardware under consideration of the fluids and the environment and ground support equipment used during assembly, integration, test, storage, transportation and mission."]
["ECSS-E-ST-35-06C Rev.1","ECSS - Superseded v0.9","C.2.1<6>a","Requirement","ECSS-E-ST-35-06_0200372",1,"Created","The dryness results part shall contain:\n    1. Check box for requirement application\n    2. Identification of procedure used\n    3. Specification of gases used\n    4. Liquid removed\n    5. Definition of success criterion\n    6. Record of test result\n    7. Date of tests."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","6.3.2a","Requirement","ECSS-E-ST-32-01_0810024",1,"Created","The evaluation procedure for a PFCI considered as a safe life item shall be in conformance with Figure 6-3, for metallic items, and Figure 6-4, for composite, bonded and sandwich items."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","6.3.2b","Requirement","ECSS-E-ST-32-01_0810025",1,"Created","Except where it is explicitly specified otherwise, the initial crack or damage size used for the verification (by analysis or test) of safe life items shall be detectable by the applied NDI with at least 90% probability and 95% confidence."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","6.3.5.2b","Requirement","ECSS-E-ST-32-01_0810049",1,"Created","The maximum tensile stress based on net cross-sectional area in the part at limit load shall be no greater than 30 percent of the ultimate tensile strength for the metal used."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","7.2.4c","Requirement","ECSS-E-ST-32-01_0810074",1,"Created","The stress spectrum shall be provided to the customer for approval."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","7.2.8i","Requirement","ECSS-E-ST-32-01_0810099",1,"Created","For cyclic plastic deformation, EPFM crack-growth methodology shall be used, which is subject to customer approval."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","8.2.2.2d","Requirement","ECSS-E-ST-32-01_0810109",1,"Created","For non-hazardous leak before burst (NHLBB) vessels, all areas which cannot be verified LBB, shall be verified as safe life.\n    NOTE For example, at load introduction (e.g. boss area) and in other thick-walled regions, when agreed with the customer."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","8.3.2b","Requirement","ECSS-E-ST-32-01_0810128",1,"Created","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."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","8.4.3.3a","Requirement","ECSS-E-ST-32-01_0810149",1,"Created","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."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","8.7c","Requirement","ECSS-E-ST-32-01_0810179",1,"Created","The sustained crack growth analysis shall apply factors to the sustained stresses of the stress spectrum as specified in Table 8-1, depending on the duration of each load event that induces sustained stress."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.3.1b","Requirement","ECSS-E-ST-32-01_0810200",1,"Created","NDI shall be performed for the complete items.\n    NOTE The NDI to be applied to an item (or region of an item) is based on the most critical location of the item (or region of the item)."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.3.3d","Requirement","ECSS-E-ST-32-01_0810221",1,"Created","Where etching or inspection cannot be performed on the finished part, that etching and penetrant-inspection shall be performed at the latest practical stage of finishing.\n    NOTE For example, before final machining of parts with precision tolerances, or at the assembly level before holes are drilled."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.4.3.1b","Requirement","ECSS-E-ST-32-01_0810246",1,"Created","The radiographic quality level shall be equal or better than 2-1T (clause 6.9 of ASTM E 1742)."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.4.3.4d","Requirement","ECSS-E-ST-32-01_0810261",1,"Created","The interface surface finish shall be Ra = 3,2 mm or lower."]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.5.2.2.1b","Requirement","ECSS-E-ST-32-01_0810273",1,"Created","The capability of an NDI method (i.e. the reliably detectable defect size) shall be demonstrated by test on specimens with induced defects. "]
["ECSS-E-ST-32-01C Rev. 1","ECSS - Superseded v0.9","10.7.2.2a","Requirement","ECSS-E-ST-32-01_0810298",1,"Created","The part shall meet the requirements in 6.3 for safe parts using the detected defect in conformance with 10.7.2.2b."]
["ECSS-E-ST-50-01C","ECSS - Superseded v0.9","5.3a","Requirement","ECSS-E-ST-50-01_0240004",1,"Created","The basic convolutional code shall have the characteristics shown in Table 5-1.\n    ","NOTE 1 The encoding rule can be represented by the following equations:\ns1(t) = i(t) + i(t-1) + i(t-2) + i(t-3) + i(t-6)    \tmodulo 2\ns2(t) = i(t) + i(t-2) + i(t-3) + i(t-5) + i(t-6) + 1\tmodulo 2\nwhere the equations use modulo 2 addition, and s1 is the first output symbol, s2 is the second output symbol and i(t) is the input information at time t.\nNOTE 2 An encoder block diagram is shown in Figure 5-1\nNOTE 3 The output symbol sequence is:\n "]
["ECSS-E-ST-50-01C","ECSS - Superseded v0.9","8.4b","Requirement","ECSS-E-ST-50-01_0240037",1,"Created","The ASM for one codeblock (or transfer frame) shall immediately follow the end of the preceding codeblock (or transfer frame).\n    ","NOTE This implies that there are no intervening bits (i.e. data or fill) preceding the ASM."]
["ECSS-E-ST-50-01C","ECSS - Superseded v0.9","8.6.2c","Requirement","ECSS-E-ST-50-01_0240042",1,"Created","The embedded ASM shall consist of a 32-bit (4-octet) marker with the pattern shown in Figure 8-5.\n    ","NOTE This pattern is represented in hexadecimal notation as: \n352EF853"]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-E-ST-50-03_0880013",1,"Created","The Transfer Frame Primary Header shall consist of six fields, positioned contiguously, in the following sequence:\n    1. Master Channel Identifier\t\t12 bits\n    2. Virtual Channel Identifier\t\t3 bits\n    3. Operational Control Field Flag\t1 bit\n    4. Master Channel Frame Count\t8 bits\n    5. Virtual Channel Frame Count\t8 bits\n    6. Transfer Frame Data Field Status\t16 bits","NOTE 1 All six fields are always present in a Transfer Frame Primary Header.\nNOTE 2 Figure 5-2 shows the format of the Transfer Frame Primary Header.\nNOTE 3 The Transfer Frame Primary Header covers the following main functions:\n            · to identify the data unit as a TM Transfer Frame;\n            · to identify the master channel and virtual channel to which the frame belongs;\n            · to provide a counting mechanism for the virtual channels and the master channel;\n            · to provide status fields related to the data in the Transfer Frame Data Field.                               "]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.2.6b","Requirement","ECSS-E-ST-50-03_0880036",1,"Created","The Virtual Channel Frame Count shall be contained within bits 24-31 of the Transfer Frame Primary Header."]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.2.7.6d","Requirement","ECSS-E-ST-50-03_0880060",1,"Created","If at least one packet starts in the Transfer Frame Data Field, the First Header Pointer shall contain the location of the first octet of the first packet that starts in the Transfer Frame Data Field. \n    ","NOTE If the last packet in the Transfer Frame Data Field of frame X spills over into frame Y of the same virtual channel (X<Y), the First Header Pointer in frame Y ignores the residue of the split packet and indicates the start of the first packet that starts in frame Y."]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.3.4.2a","Requirement","ECSS-E-ST-50-03_0880085",1,"Created","The length of the Transfer Frame Secondary Header shall be 32 bits.\n    ","NOTE The Transfer Frame Secondary Header has a length of 4 octets, so the Transfer Frame Secondary Header Length contains the value 3."]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.4.3.5a","Requirement","ECSS-E-ST-50-03_0880104",1,"Created","The packet extraction function shall be applied independently for each virtual channel."]
["ECSS-E-ST-50-03C","ECSS - Superseded v0.9","5.6.1c","Requirement","ECSS-E-ST-50-03_0880132",1,"Created","If present, the Frame Error Control Field shall occur within every TM Transfer Frame transmitted within the same physical channel throughout a mission phase.\n    ","NOTE 1 The purpose of this field is to provide a capability for detecting errors which can be introduced into the frame during the transmission and data handling process.\nNOTE 2 When applied to an encoded block of less than 32 768 bits (4096 octets), the code has the following capabilities:\n        · All error sequences composed of an odd number of bit errors are detected.\n        · All error sequences containing at most two bit errors anywhere in the encoded block are detected.\n        · If a random error sequence containing an even number of bit errors (greater than or equal to 4) occurs within the block, the probability that the error is undetected is approximately 2-15 (or 3 × 10-5).\n        · All single error bursts spanning 16 bits or less are detected provided no other errors occur within the block."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","5.2.1b","Requirement","ECSS-E-ST-50-04_0890002",1,"Created","The length of a TC Segment shall be an integer number of octets."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","5.4.5c","Permission","ECSS-E-ST-50-04_0890272",1,"Created","Packets with different Packet Version Numbers may be blocked into the same data unit."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","5.5.4.2d","Requirement","ECSS-E-ST-50-04_0890049",1,"Created","The MAP Identifier for the control MAP shall have the same value as the data MAP except that the most significant bit shall be set to ‘1’."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","6.2.2.3c","Requirement","ECSS-E-ST-50-04_0890074",1,"Created","The Bypass Flag shall be set as follows:\n    1. ‘0’ for a type-A Transfer Frame;\n    2. ‘1’ for a type-B Transfer Frame."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","6.2.2.9d","Requirement","ECSS-E-ST-50-04_0890095",1,"Created","In type-B Transfer Frames the Frame Sequence Number shall be set to zero.\n    ","NOTE The Bypass Flag defined in clause 6.2.2.3 indicates if a TC Transfer Frame is type-A or type-B."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","6.2.4.1b","Requirement","ECSS-E-ST-50-04_0890102",1,"Created","The Frame Error Control Field shall follow, without gap, the Transfer Frame Data Field."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","6.3.12a","Requirement","ECSS-E-ST-50-04_0890126",1,"Created","The Retransmit Flag shall be set as follows:\n    1. ‘0’ when the FARM-1 does not request retransmission;\n    2. ‘1’ when the FARM-1 requests retransmission of type-A Transfer Frames, starting with the frame whose sequence number is indicated in the Report Value field of the CLCW.\n        ","NOTE This flag is used by the COP-1 procedures as defined in clause 7.9."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","7.4.2.3a","Requirement","ECSS-E-ST-50-04_0890147",1,"Created","A directive notification signal shall have the following parameters:\n    1. Request identifier\n    2. Virtual channel identification\n    3. Notification type."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","7.5.2a","Requirement","ECSS-E-ST-50-04_0890170",1,"Created","The buffer management mechanism shall ensure that FARM-1 always knows whether a back-end buffer is available."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","7.8.4d","Requirement","ECSS-E-ST-50-04_0890194",1,"Created","The third octet of a Set V(R) control command shall contain the new value for V(R).\n    ","NOTE On receipt of the Set V(R) control command, FARM-1 sets the Receiver_Frame_Sequence_Number, V(R), to the value contained in the third octet."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","8.2.1b","Requirement","ECSS-E-ST-50-04_0890219",1,"Created","A BCH codeblock shall consist of two major fields, positioned contiguously, in the following sequence:\n    1. Information 56 bits\n    2. Error Control 8 bits\n        ","NOTE Both fields are always present. Figure 8-1 shows the format of a BCH codeblock."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","8.2.3.1b","Requirement","ECSS-E-ST-50-04_0890224",1,"Created","The Error Control field shall be contained in bits 56 to 63 of the BCH codeblock."]
["ECSS-E-ST-50-04C","ECSS - Superseded v0.9","9.2.1b","Requirement","ECSS-E-ST-50-04_0890256",1,"Created","The pattern of the acquisition sequence shall be alternating \"ones\" and \"zeroes\", starting with either a \"one\" or a \"zero\".\n    ","NOTE 1 The acquisition sequence is a data structure forming a preamble which provides for initial symbol synchronization within the incoming stream of detected symbols.\nNOTE 2 The length of the acquisition sequence is selected according to the mission telecommand link performance specifications.\nNOTE 3 The length of the acquisition sequence can be effectively increased by transmitting the idle sequence defined in clause 9.2.3\n\t\t\t\t\t\t\t\t\t\t\t"]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.2.3.3c","Requirement","ECSS-E-ST-50_0970011",1,"Created","The supplier shall provide the simulations and demonstrations used to verify the design, to resolve design conflicts, and to select options (CSVP), in conformance with the DRD in Annex D, and"]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.4.4d","Requirement","ECSS-E-ST-50_0970036",1,"Created","For critical operations, execution of the essential commands shall not depend on software functions.\n    ","NOTE Example of critical operations is switching the transmitters on and off."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.5.2a","Requirement","ECSS-E-ST-50_0970043",1,"Created","The design of the space communication system shall enable essential telemetry to be acquired from critical monitoring points and transmitted to the ground, even when all other systems, including the CDMU, are non-operational."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.6.13.2a","Requirement","ECSS-E-ST-50_0970083",1,"Created","Formatted data units used on the space link shall include an identifier that identifies the source, the destination, or both source and destination of the data unit.\n    ","NOTE The data unit identifier need only be unique to the specific spacecraft domain. Universally unique identification of the source and or destination can therefore involve reference to several identifiers in combination, such as the data unit identifier in combination with the spacecraft identifier."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.6.13.3a","Requirement","ECSS-E-ST-50_0970084",1,"Created","Formatted data units used on the space link shall include a sequence identifier that identifies the data units position in a stream of data units on the space link in order to detect duplication or omission of data units."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","5.7.2.4a","Requirement","ECSS-E-ST-50_0970109",1,"Created","The space network shall provide a network management service that maintains the space network routing and configuration tables in order to provide high reliability and availability of the space network."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","A.2.1<5>b","Requirement","ECSS-E-ST-50_0970125",1,"Created","The CSRD shall summarize the major project milestones relating to the ground segment."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","B.2.1<9>b","Requirement","ECSS-E-ST-50_0970156",1,"Created","The CSBD shall describe all of the operational procedures relating to the maintenance of the communication system."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","D.2.1<3>a","Requirement","ECSS-E-ST-50_0970181",1,"Created","The CSVP shall describe the main objectives and characteristics of the space mission."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","E.2.1<1>a","Requirement","ECSS-E-ST-50_0970193",1,"Created","The CSADD shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-50C","ECSS - Superseded v0.9","G.2.1<2>a","Requirement","ECSS-E-ST-50_0970208",1,"Created","The CSPD shall list the applicable and reference documents in support to the generation of the document."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","4.3.2.1b","Requirement","ECSS-E-ST-10-03_0750012",1,"Created","The definition of the blocks of requirement 4.3.2.1a shall be agreed between the customer and supplier.\n    ","NOTE 1 Test block definition depends mainly on the item under test, the facility and the contractual agreement. A test block can include one or more tests. For equipment, usually one test block covers the full test programme.\nNOTE 2 Typical test blocks for space segment elements are:\nIntegration\nAlignment\nLeak/proof pressure\nMechanical (Static load test, sinusoidal, acoustic, random, modal survey, shock)\nEMC conducted\nEMC radiated/auto-compatibility/RF\nThermal (TB/TV test)\nFunctional and performance test\nFinal preparation"]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","4.3.3.4c","Requirement","ECSS-E-ST-10-03_0750033",1,"Created","The way the requirement 4.3.3.4b is achieved shall be agreed between the customer and the supplier."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","4.4.3d","Requirement","ECSS-E-ST-10-03_0750058",1,"Created","Any anomaly of test instrumentation, detected at the first calibration sequence after the test, shall be reported."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","4.6.4b","Requirement","ECSS-E-ST-10-03_0750084",1,"Created","High level (system or element) functional testing shall be performed in preference to individual low level tests.\n    ","NOTE Post-landing testing is performed on space products to be recovered at the end of mission and on products which are re-flown."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.1.1d","Requirement","ECSS-E-ST-10-03_0750105",1,"Created","In case of internal redundancy, functional tests shall be performed on both chains taking into account the type of redundancy (e.g. hot or cold)."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.2.1a","Requirement","ECSS-E-ST-10-03_0750126",1,"Created","The following physical properties of space segment equipment shall be determined using tools and techniques that conform to the required accuracy:\n    1. Dimensions and interfaces; \n    2. Mass;\n    3. Centre of gravity with respect to a given coordinate system for three mutually perpendicular axes;\n    4. Momentum of inertia with respect to the given coordinate system.\n        ","NOTE For space segment equipment with simple shapes, the centre of gravity location and momenta of inertia can be determined by calculation."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.2.3c","Requirement","ECSS-E-ST-10-03_0750132",1,"Created","In order to evaluate the space segment equipment integrity a resonance search shall be performed before and after the random vibration test."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.2.8a","Requirement","ECSS-E-ST-10-03_0750157",1,"Created","The performance parameters shall be measured when subjected to the maximum predicted micro-vibration environment."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.4.1h","Requirement","ECSS-E-ST-10-03_0750182",1,"Created","Test profile, test configuration, number of cycles, extreme temperatures, temperature rate of change, stability criteria, dwell time duration, tests to be performed and success criteria shall be defined in the test specification."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.4.1q","Requirement","ECSS-E-ST-10-03_0750191",1,"Created","Test methods and test set-up shall be defined according to the thermal environment characteristics, the TCS thermal design and the space segment equipment itself."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","5.5.5.5a","Requirement","ECSS-E-ST-10-03_0750209",1,"Created","The multipaction test shall be performed in conformance with ECSS‐E‐20-01."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.1.2.1e","Requirement","ECSS-E-ST-10-03_0750234",1,"Created","Additional functional tests to be performed before and after each environmental exposure and transport(s) shall be agreed with the customer.","NOTE Those tests are limited to RFT to provide the criteria for judging successful survival of the space segment."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.1.4c","Requirement","ECSS-E-ST-10-03_0750259",1,"Created","To reduce the risk of error accumulation during mission test, the space segment element shall be kept uninterrupted ON according to the test profile, to be agreed with the customer, in terms of modes, modes transition and modes duration.\n    ","NOTE The definition of the mission test takes into account the typical mission scenario, able to completely exercise all modes and transitions and all software functions under an interrupted operational environment."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.2.5b","Requirement","ECSS-E-ST-10-03_0750281",1,"Created","Propellant storage tanks shall be at least mass and stiffness representative during transient testing.","NOTE Simulated propellant can be used."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.2.7h","Requirement","ECSS-E-ST-10-03_0750302",1,"Created","Space segment equipment, being part of the space segment element, that operates during launch shall be operated and monitored during the test."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.3.2a","Requirement","ECSS-E-ST-10-03_0750327",1,"Created","Requirements of ECSS-E-ST-32-02 clauses 5.4.1 and 5.4.5 shall be applied for pressure cycling tests."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.4.1h","Requirement","ECSS-E-ST-10-03_0750341",1,"Created","Equipment switch on capabilities shall be demonstrated."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","6.5.4.3b","Requirement","ECSS-E-ST-10-03_0750354",1,"Created","Pressure value for the thermal ambient test shall be as per type of mission.","NOTE i.e. Mars mission, Space Station pressure "]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","7b","Requirement","ECSS-E-ST-10-03_0750379",1,"Created","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."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","A.2.1<4>a","Requirement","ECSS-E-ST-10-03_0750392",1,"Created","The AITP shall briefly describe the selected models and their built status with reference to the verification plan (see ECSS-E-ST-10-02)."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","C.2.1<6>a","Requirement","ECSS-E-ST-10-03_0750426",1,"Created","The TPRO shall describe the test set-up to be used."]
["ECSS-E-ST-10-03C","ECSS - Superseded v0.9","C.2.1<11>a","Requirement","ECSS-E-ST-10-03_0750431",1,"Created","The TPRO shall describe how the applicable documentation is used to support the test activity."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","4.2.8a","Requirement","ECSS-E-ST-20-07_0080014",1,"Unchanged","Intrasystem EMC shall be achieved by:\n    1. allocation of equipment-level EMI requirements documented in the EMCCP, including:\n        (a) limits on conducted and radiated emission,\n        (b) susceptibility thresholds.\n            NOTE Recommended data is defined in Annex A for equipment and subsystems."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","4.2.13.1c","Requirement","ECSS-E-ST-20-07_0080036",1,"Unchanged","Bundles of different categories shall be separated either by a separation distance of 5 cm from the outer circumference or by a metallic screen when they are routed on parallel paths.\n    NOTE Overshields or spacecraft walls can be used to fulfil the requirement."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.2.4b","Requirement","ECSS-E-ST-20-07_0080065",1,"Unchanged","LISNs shall not be used on output power leads."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.2.6.6.1b","Requirement","ECSS-E-ST-20-07_0080086",1,"Unchanged","Shielded cables or shielded leads (including power leads and wire grounds) within cables shall be used only if they have been specified in installation requirements."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.2.6.7e","Requirement","ECSS-E-ST-20-07_0080104",1,"Unchanged","When active electrical loading is used, it shall be ensured that the active load meets the ambient requirements of 5.2.2 when connected to the setup, and that the active load does not respond to susceptibility signals.\n    NOTE Example of active electrical loading is the test set."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.2.9.4i","Requirement","ECSS-E-ST-20-07_0080133",1,"Unchanged","Each plot of emission data shall be reported with a minimum amplitude resolution of 1 dB."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.2.10.2b","Requirement","ECSS-E-ST-20-07_0080138",1,"Unchanged","CW test signals shall be used for susceptibility signals at a frequency smaller than 100 kHz."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.3.7b","Permission","ECSS-E-ST-20-07_0080267",1,"Created","Wherever 0 dB EMISM is a requirement, functional tests at spacecraft level may be accepted as a verification of EMC."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.4.6.3b","Requirement","ECSS-E-ST-20-07_0080188",1,"Unchanged","The measurement system shall be checked by configuring the test equipment as shown in Figure 5-13."]
["ECSS-E-ST-20-07C Rev. 1","ECSS - Superseded v0.9","5.4.9.2a","Requirement","ECSS-E-ST-20-07_0080208",2,"Normative Change","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."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.1.2b","Requirement","ECSS-E-ST-20_0020002",1,"Unchanged","In order to minimize the number of interface types, standard interface circuitry shall be defined to be applied throughout a project."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.1.2d","Requirement","ECSS-E-ST-20_0020004",2,"Normative Change","The application of the nominal signals or a faulty signal to an un-powered interface shall not cause damage to that interface.","NOTE \tThis requirement covers all types of interfaces. Standard interfaces are covered in clauses 4.2.4.3 and 4.2.4.4 of ECSS-E-ST-50-14.\n"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.2.1i","Requirement","ECSS-E-ST-20_0020029",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.2.3a","Requirement","ECSS-E-ST-20_0020049",1,"Informative Change","A connector carrying source power or external test connectors on units shall have no contact areas exposed to possible short circuit during mating and de-mating process. ","NOTE \tThey generally are female type connectors.\n"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.2.4k","Requirement","ECSS-E-ST-20_0020074",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","4.3.1b","Requirement","ECSS-E-ST-20_0020408",1,"Created","In case verification by analysis of an electrical part or circuit is not possible by lack of data, complementary verification by test shall be performed.","NOTE \tElectrical part or circuit encompasses in particular to EEE components, solar cell or solar array, battery cell or battery assembly.\n"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.2o","Requirement","ECSS-E-ST-20_0020119",2,"Normative Change","Provision shall be made to prevent failure due to operation in shadow. "]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.5.3c","Requirement","ECSS-E-ST-20_0020124",2,"Normative Change","I(V) solar cells characteristics shall be computed in BOL and EOL conditions at maximum and minimum operating temperatures according to the mission profile."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.6.3e","Requirement","ECSS-E-ST-20_0020154",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.7.2a","Requirement","ECSS-E-ST-20_0020170",2,"Normative Change","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."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.7.3f","Requirement","ECSS-E-ST-20_0020194",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.7.6d","Requirement","ECSS-E-ST-20_0020215",1,"Unchanged","The failure of the monitoring function of 5.7.6c shall not cause the protection elements to fail."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.8.1t","Requirement","ECSS-E-ST-20_0020425",1,"Created","In alternative to, and under the same assumptions of requirement 5.8.1r, the magnitude of the source impedance shall be smaller than the magnitude of the load impedance by at least a factor 10."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","5.8.2g","Requirement","ECSS-E-ST-20_0020238",1,"Unchanged","The harness restraining systems on the structure shall not bring about any stress at connector level."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","6.2.3c","Requirement","ECSS-E-ST-20_0020258",1,"Informative Change","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"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","6.3.4.3c","Requirement","ECSS-E-ST-20_0020273",2,"Normative Change","Occurrence of an arc discharge during transmission of a command to the space vehicle from an external source as a ground station shall not result in any unintended action, whether the command is executed or not.","NOTE \tAn external source can be a ground station.\n"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","7.2.2.2.4a","Requirement","ECSS-E-ST-20_0020305",1,"Unchanged","For array-fed reflector antennas clauses 7.2.2.2.2 (Reflector/Lens antennas) and 7.2.2.2.3 (Array antennas) shall apply."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","7.2.2.3.6b","Requirement","ECSS-E-ST-20_0020330",1,"Informative Change","Deviations from the nominal geometry of the supporting structure shall be quantified and their impact on antenna performances assessed. ","NOTE \tTypical deviations are due to manufacturing errors, thermo-elastic effects and modification of the material characteristic in the orbit environment, moisture release in composites.\n"]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","7.2.2.4.2b","Requirement","ECSS-E-ST-20_0020335",1,"Unchanged","Thermally induced changes of dimension and shape in all composite and combined metal-composite antenna parts shall be quantified and their impact on antenna performances assessed."]
["ECSS-E-ST-20C Rev.1","ECSS - Superseded v0.9","7.4.4a","Requirement","ECSS-E-ST-20_0020359",1,"Unchanged","Testing at the lowest intermodulation order as identified in 7.4.3c shall be performed to ensure that the amplitudes of the passive intermodulation products are below the specified interference level. "]
["ECSS-S-ST-00C","ECSS - Superseded v0.9","9.2b","Requirement","ECSS-S-ST-00_1000002",1,"Created","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."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.2.2.3b","Requirement","ECSS-E-ST-10-02_0740020",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.2.4.2d","Requirement","ECSS-E-ST-10-02_0740190",1,"Created","For product categories A, B and C, the supplier shall state the qualification status at the EQSR (Equipment Qualification Status Review)."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.2.6.5b","Requirement","ECSS-E-ST-10-02_0740066",1,"Unchanged","Non-validated analytical software tools shall be subjected to a validation process prior to their use."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.3.2.1c","Requirement","ECSS-E-ST-10-02_0740087",2,"Normative Change","The supplier shall provide the Test reports for the reviews as agreed with the customer ","NOTE \tSee ECSS-E-ST-10 Table A-1 for review deliverables. \n"]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.3.2.6c","Requirement","ECSS-E-ST-10-02_0740107",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","5.4.2e","Requirement","ECSS-E-ST-10-02_0740118",2,"Normative Change","The supplier's VCB representative shall ensure the Verification Control Board (VCB) endorses the final issue of the Verification Control Document (VCD)."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","A.2.1<8>b","Recommendation","ECSS-E-ST-10-02_0740194",1,"Created","Analysis, review­of­design, inspection and test programmes should be detailed through dedicated activity sheets, or through reference to the AIT Plan. "]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","C.2.1<4>c","Requirement","ECSS-E-ST-10-02_0740161",2,"Normative Change","The Test Report shall provide a synthesis of the test results."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","D.2.1<3>a","Requirement","ECSS-E-ST-10-02_0740169",2,"Normative Change","The Review-of-Design Report shall list the applicable dictionary or glossary and the meaning of specific terms or abbreviations utilized in the document with the relevant meaning."]
["ECSS-E-ST-10-02C Rev.1","ECSS - Current v0.9","F.2.1<5>c","Requirement","ECSS-E-ST-10-02_0740188",1,"Unchanged","Open issues shall be clearly stated and described."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","5.2.3.6a","Requirement","ECSS-E-ST-10_0790023",2,"Deleted","<<deleted>>."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","5.3.4a","Requirement","ECSS-E-ST-10_0790047",2,"Normative Change","The system engineering function shall define the analysis methods and tools to be used during the product life cycle, as well as the related models and data exchanges between the tools, and document these in the SEP in conformance with Annex D."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","5.4.1.4a","Requirement","ECSS-E-ST-10_0790070",2,"Normative Change","The system engineering function shall establish and maintain a design definition file in conformance with Annex G."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","5.6.3b","Requirement","ECSS-E-ST-10_0790095",2,"Normative Change","The system engineering function shall ensure that engineering data can be exchanged in electronic form between the different organizations in charge of the elements of the product decomposition levels via agreed and validated interfaces."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","5.6.9c","Requirement","ECSS-E-ST-10_0790111",2,"Normative Change","The system engineering function shall implement and control agreed actions assigned to it, arising from change proposals and nonconformances.","NOTE \t1\tChange is related to a request for deviation.\nNOTE \t2\tNonconformance is related to a request for waiver.\nNOTE \t3\tThe change procedure/control is defined as part of the configuration management as defined in ECSS-M-ST-40.\n"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","6.5b","Requirement","ECSS-E-ST-10_0790124",2,"Deleted","<<deleted, modified and inserted as informative text in clause 4>>"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","B.2.1<1>a","Requirement","ECSS-E-ST-10_0790138",1,"Unchanged","The MDD shall contain a description of the purpose, objective, content and the reason prompting its preparation (e.g. logic, organization, process or procedure)."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","D.2.1<4.2>a","Requirement","ECSS-E-ST-10_0790163",1,"Unchanged","The SEP shall list the specified system engineering outputs as defined in ECSS-E-ST-10 clause 6 for the specific project phase(s) covered in the SEP.","NOTE\tAn overview of document delivery is given in Annex A.\n"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","E.2.1<2>a","Requirement","ECSS-E-ST-10_0790192",1,"Unchanged","The TP shall list the applicable and reference documents in support to the generation of the document and include the reference to the following applicable documents:\n1.\tSEP\n2.\tTechnology matrix (as defined in ECSS-E-ST-10, Annex F)\n3.\tFunction tree\n4.\tSpecification tree."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","F.2.1<4>b","Requirement","ECSS-E-ST-10_0790209",2,"Normative Change","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."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","G.2.1<2>b","Requirement","ECSS-E-ST-10_0790214",1,"Unchanged","The DDF shall include the reference to the following applicable documents:\n1.\tBusiness agreement\n2.\tSystem engineering plan (as defined in ECSS-E-ST-10 Annex D)\n3.\tCoordinate system document (as defined in ECSS-E-ST-10-09 Annex A)\n4.\tTechnical requirements specification (TS)\n5.\tProduct assurance plan\n6.\tConfiguration management plan (as defined in ECSS-M-ST-40)\n7.\tConfiguration status report (as defined in ECSS-M-ST-40)."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","G.2.1<8>a","Requirement","ECSS-E-ST-10_0790235",2,"Normative Change","The DDF shall contain the information on the system or product engineering data repository that contains the complete set of design parameters, or a reference to it.","NOTE\tInformation about the set of design parameters is provided in ECSS-E-TM-10-10.\n"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","K.2.1<2>b","Requirement","ECSS-E-ST-10_0790256",1,"Unchanged","The applicable document list shall contain the reference to the relevant product specifications, and the relevant DDF and system engineering plan."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","K.2.1<11>a","Requirement","ECSS-E-ST-10_0790286",1,"Unchanged","The DJF shall integrate or refer to the documents that conform to the:\n1.\tECSS-E-ST-10 Annex L, Trade-Off-Report - DRD\n2.\tECSS-E-ST-10 Annex Q, Analysis Report - DRD\n3.\tECSS-E-ST-10 Annex O, Requirement Justification File - DRD\n4.\tECSS-E-ST-10 Annex N, Requirements Traceability Matrix - DRD\n5.\tECSS-E-ST-10-02 Annex B, Verification Control Document - DRD\n6.\tECSS-E-ST-10-02 Annex C, Test Report - DRD\n7.\tECSS-E-ST-10-02 Annex D, Review Of Design Report - DRD\n8.\tECSS-E-ST-10-02 Annex E, Inspection Report - DRD\n9.\tECSS-E-ST-10-02 Annex F, Verification Report - DRD"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","M.2.1<2>b","Requirement","ECSS-E-ST-10_0790307",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","O.2.1<4>a","Requirement","ECSS-E-ST-10_0790325",1,"Unchanged","The RJF shall present and justify the 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"]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","P.2.1<4.2>a","Requirement","ECSS-E-ST-10_0790339",1,"Unchanged","The PUM shall include the following:\n1.\tdescription of product-level autonomy provisions in the areas of fault management (FDIR);\n2.\tdefinition, for each autonomous function, of the logic or rules used and of its internal (product constituents) and external interfaces. "]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9","P.2.1<4.11>c","Requirement","ECSS-E-ST-10_0790360",1,"Unchanged","The PUM shall identify the risks during and after disposal."]
["ECSS-E-ST-10C Rev.1","ECSS - Current v0.9",null,"Requirement","ECSS-E-ST-10_0790385",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-10-06C","ECSS - Current v0.9","8.2.1a","Requirement","ECSS-E-ST-10-06_0770018",1,"Created","Each technical requirement shall be described in quantifiable terms."]
["ECSS-E-ST-10-06C","ECSS - Current v0.9","8.3.2a","Requirement","ECSS-E-ST-10-06_0770039",1,"Created","The verbal form “shall” shall be used whenever a provision is a requirement."]
["ECSS-E-ST-10-09C","ECSS - Current v0.9","5.2.3c","Requirement","ECSS-E-ST-10-09_0230010",1,"Created","A transformation chain structure shall be built to link coordinate systems used by two or more subsystems \n    ","NOTE See Annex B for guidelines and examples."]
["ECSS-E-ST-10-09C","ECSS - Current v0.9","5.2.3d","Requirement","ECSS-E-ST-10-09_0230011",1,"Created","The nominal value, in numeric or parametric form, of the transformation between two coordinate systems shall be specified."]
["ECSS-E-ST-10-09C","ECSS - Current v0.9","5.4.2a","Requirement","ECSS-E-ST-10-09_0230037",1,"Created","If a coordinate system is time dependent, then its time scale shall be defined."]
["ECSS-E-ST-10-09C","ECSS - Current v0.9","5.4.9a","Requirement","ECSS-E-ST-10-09_0230062",1,"Created","A transformation between coordinate systems shall be defined in the parent coordinate system in three ways: verbally, mathematically and graphically.\n    ","NOTE E.g. see Table B-1 and Table B-2 in Annex B."]
["ECSS-E-ST-10-09C","ECSS - Current v0.9","A.2.1<8>a","Requirement","ECSS-E-ST-10-09_0230083",1,"Created","The CSD shall describe in a graphical representation the top-level chain of transformations for the project."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.2.1.1a","Requirement","ECSS-E-ST-10-11_0780001",1,"Created","The HFE parameters listed in 4.2.1.2 to 4.2.1.6 shall be characterised during design, development and assessment of space projects that includes presence of humans in the loop."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.4.3.3b","Requirement","ECSS-E-ST-10-11_0780038",1,"Created","To provide for the allocation of functions to the crews the TA shall be developed during phase A when human in the loop is foreseen."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.4.3.5c","Requirement","ECSS-E-ST-10-11_0780043",1,"Created","The fidelity level of the design solution shall be compatible with the assessment objective."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.6.5a","Requirement","ECSS-E-ST-10-11_0780069",1,"Created","To create an environment that supports and maintains human health, safety and well-being all relevant functions and resources shall be provided as specified in ECSS-E-ST-34."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.7.6b","Requirement","ECSS-E-ST-10-11_0780090",1,"Created","Work station shall be either outfitted with equipment (including lights) and tools (including restrains) to support the foreseen crew activities or shall be provided with the necessary restraints and hook points to enable their outfitting."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.9.3c","Requirement","ECSS-E-ST-10-11_0780115",1,"Created","All resources and boundary conditions shall be compatible with the work/rest cycles of the crew as defined according to clause 4.5.4."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.10.1.2a","Requirement","ECSS-E-ST-10-11_0780136",1,"Created","Table 4-1 provides an overview of human factors principles and techniques and the technological design space, applied in different stages (analysis, design, implementation and maintenance) of the continuous evaluation process. Techniques in italics shall be done always, whereas the other elements are recommended for more complex and/or critical systems."]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.10.3.3d","Requirement","ECSS-E-ST-10-11_0780155",1,"Created","HFE test reports shall be prepared according to the DRD in Annex D. "]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","4.11.3.1a","Requirement","ECSS-E-ST-10-11_0780167",1,"Created","For testing on ground an assessment of the gravity effects shall be performed.\n    NOTE 1 Ground HFE Test with human subjects is considered representative only when effect of gravity have limited influence or when ground simulation using zero-gravity space analogue environments (NBF or PF) typical limitations (water resistance and buoyancy of objects and subjects for NBF and time limitations for the PF) have limited influence on the test objectives. \n    NOTE 2 NBF and PF test are considered ground HFE tests. "]
["ECSS-E-ST-10-11C","ECSS - Current v0.9","C.2.1<2>a","Requirement","ECSS-E-ST-10-11_0780188",1,"Created","The HFE continuous assessment process report shall list the applicable and reference documents to support the generation of the document."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","5.6.2a","Requirement","ECSS-E-ST-10-12_0980026",1,"Created","Before PDR, a worst-case assessment of unit shielding shall be made (i.e. minimum shielding thickness)\n    NOTE Before PDR an accurate geometrical model of a satellite is not generally available. As a consequence it is not possible to estimate the dose level expected at a part and so the final achieved RDM cannot be accurately assessed. "]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","6.3.2.1a","Requirement","ECSS-E-ST-10-12_0980042",1,"Created","The effect of the parts packaging in the radiation shielding model shall be assessed as follows:\n    1. Place the target point inside the package, located on top or inside the active region of the volume \n        NOTE The objective is to get the best possible estimate of the deposited dose at die level, the target point. The active region is typically a silicon chip.\n    2. For hybrid devices containing several sensitive dies, use one target point per die.\n        NOTE The reason is that the calculated dose level can vary significantly depending on the die location.\n    3. For situations where the total ionising dose from X-ray or g-ray fields is the largest contribution, assess the influence of local high-Z materials and include it in the calculations.\n        NOTE Example of high-Z materials are gold contacts or tungsten silicide layers and vias."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","8.5.1a","Requirement","ECSS-E-ST-10-12_0980063",1,"Created","The radiation damage assessment shall use either the DDEF of mono-energetic protons, electrons, or neutrons calculated as specified in clause 8.5.2.1, or the TNID, calculated as specified in clause 8.5.2.2."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","8.5.2.2a","Requirement","ECSS-E-ST-10-12_0980068",1,"Created","TNID shall be calculated by one of the following procedures:\n    1. If the NIEL as a function of energy, particle type and target material is known, calculate the TNID through the integration over energy of the NIEL function (multiplied by fluence) for each particle species on the target material.\n    2. Otherwise, calculate the NIEL as a function of energy for the material and particle type following a methodology agreed with the customer and calculate the TNID through the integration over energy of the NIEL function (multiplied by fluence) for each particle species on the target material.\n        NOTE Methodologies described by Jun et al or Messenger et al [4] [5] can be used for this purpose."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","9.4.1.7a","Requirement","ECSS-E-ST-10-12_0980091",1,"Created","If SET is mitigated by circuit design, the effects of spurious pulses shall be minimized as follows:\n    1. Test the equipment performance under different filter conditions for SET and SED effects by propagating a perturbation signal in the final electrical design of the hardware itself to study its influence at the system level. \n        NOTE This approach is used when there is sufficient access to inject test pulses to the range of circuit nodes, or using a circuit simulation mode.\n    2. Use a circuit simulation model, and verify the accuracy of the different components in the circuit model for propagating large amplitude signals, up to the maximum amplitude expected from the SET/SED.\n        NOTE Typical applied amplitudes and signal durations are provided in ECSS-E-HB-10-12 Section 8.5.9 (Table 9) as a function of semiconductor family type. Note, however, that these are not the only devices to be tested for SET/SED."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","10.4.4a","Requirement","ECSS-E-ST-10-12_0980115",1,"Created","Nuclear interaction rates in the sensitive volume and surrounding materials (the radioactive decay products from which can affect the sensitive volume) shall be calculated by one of the following methods:\n    1. By using the formula of Clause 10.4.9.2 if all of the following conditions are met:\n        (a) the sensitive volume of the sensor and surrounding material producing background in the sensor are so small that the incident particle spectrum changes by less than 10% in either intensity of energy after passing through the volume;\n        (b) the pathlength distribution in the sensitive volume and surrounding material changes by less than 10% as a result of multiple scattering;\n        (c) the probability of secondary nuclear interactions is 10 times lower than the primary interaction rate.\n    2. By a radiation transport simulation agreed with the customer.\n        NOTE For guidelines, see ECSS-E-HB-10-12 Section 5.7."]
["ECSS-E-ST-10-12C","ECSS - Current v0.9","11.5b","Requirement","ECSS-E-ST-10-12_0980140",1,"Created","When calculating the protection and operational quantities as specified in requirement 11.5a, the influence of shielding in attenuating the primary particle environment and modification to its spectrum at the location of the astronaut shall be evaluated as follows:\n    1. Perform initial calculations as specified in Clause 6.2.2 to assess the influence of shielding for worst-case shielding, environment and secondary production. \n    2. If these indicate that the protection limits are exceeded, perform more detailed calculations using a detailed sector shielding calculation or Monte-Carlo analysis, calculation, as specified in Clauses 6.2.3 and 6.2.4, respectively. "]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.1.6b","Requirement","ECSS-E-ST-31_0800010",1,"Created","For bodies other than the earth, the applicable natural environment shall be agreed with the system authority."]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.3.3b","Requirement","ECSS-E-ST-31_0800038",1,"Created","The TCS shall fulfil specific requirements considering type and routing of the harness, grounding, electrical conductivity.\n    NOTE Propose changes to the layout, routing, and external wrapping of any harness and cabling, so as to avoid unacceptable or unbalanced concentration of heat dissipation;"]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.3.4.1b","Requirement","ECSS-E-ST-31_0800043",1,"Created","The TCS shall be designed for effects of heat soak after firing of thrusters."]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.4.4a","Requirement","ECSS-E-ST-31_0800064",1,"Created","The TCS design shall use space qualified EEE components."]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.5.2.3c","Requirement","ECSS-E-ST-31_0800092",1,"Created","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)."]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.6.1c","Requirement","ECSS-E-ST-31_0800111",1,"Created","For procurement of mechanical parts, the requirements of ECSS-Q-ST-70 clause 6.6 shall apply."]
["ECSS-E-ST-31C","ECSS - Current v0.9","4.9.3b","Requirement","ECSS-E-ST-31_0800136",1,"Created","The TCS supplier shall deliver the documentation as detailed in Table 5-1."]
["ECSS-E-ST-31C","ECSS - Current v0.9","B.2.1<4>b","Requirement","ECSS-E-ST-31_0800163",1,"Created","The document shall describe input data and modelling assumptions for view-factor and external flux calculation. \n    NOTE For example: Environment, geometry description, thermo-optical properties, insulated and non-insulated areas, moving bodies."]
["ECSS-E-ST-31C","ECSS - Current v0.9","B.2.1<4>e","Requirement","ECSS-E-ST-31_0800166",1,"Created","Geometrical interfaces between spacecraft and appendices or bodies used in the radiative calculation and not directly related to the spacecraft shall be described.\n    NOTE For example: COLUMBUS Module and ISS, spacecraft and solar array, spacecraft and test facility."]
["ECSS-E-ST-31C","ECSS - Current v0.9","C.2.1<7>c","Requirement","ECSS-E-ST-31_0800191",1,"Created","The description shall include a justification of assumed uncertainties."]
["ECSS-E-ST-31C","ECSS - Current v0.9","E.2.1<1>a","Requirement","ECSS-E-ST-31_0800212",1,"Created","The TCS thermal balance test specification shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-31C","ECSS - Current v0.9","F.2.1<4>a","Requirement","ECSS-E-ST-31_0800228",1,"Created","The TCS detailed design description shall summarize the driving design requirements (reference to other documents for details) for the subsystem, including:\n    1. Mission requirements\n    2. Definition of orbits, which are relevant for the subsystem design (i.e. orbits for warm and cold design cases)\n    3. Timeline and load cases\n    4. Spacecraft geometry and coordinate system\n    5. Temperature limit, temperature gradients and temperature stability requirements\n    6. Properties of spacecraft equipment (i.e. thermal, mechanical, heat dissipation)."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.2.4.1c","Requirement","ECSS-E-ST-32-02_0260028",1,"Created","The new service life shall be determined by fatigue-life or safe-life demonstration as required for this type of pressurized hardware."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.3.2.2b","Permission","ECSS-E-ST-32-02_0260440",1,"Created","The first qualification test article specified in 4.3.2.2a may be deleted with customer approval."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.3.3.1c","Requirement","ECSS-E-ST-32-02_0260061",1,"Created","A strength and stability demonstration shall be performed by analysis and test."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.3.3.2i","Requirement","ECSS-E-ST-32-02_0260080",1,"Created","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. \n    ","NOTE For example: destabilizing load with constant minimum internal pressure or maximum additive load with a constant MDP."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.3.4.2c","Requirement","ECSS-E-ST-32-02_0260101",1,"Created","A second qualification test article shall be submitted to the following chronology of operations:\n    1. NDI;\n    2. proof pressure test;\n    3. leak test;\n    4. vibration tests;\n    5. pressure cycling test;\n    6. leak test;\n    7. design burst pressure test;\n    8. burst test."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.4.2.1g","Requirement","ECSS-E-ST-32-02_0260126",1,"Created","For corrosion effects (control and prevention), the requirements in ECSS-E-ST-32 shall apply."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.4.3.1i","Requirement","ECSS-E-ST-32-02_0260147",1,"Created","For corrosion effects (control and prevention), the requirements in ECSS-E-ST-32 shall apply."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.4.3.2b","Permission","ECSS-E-ST-32-02_0260452",1,"Created","The pressure cycling and design burst pressure tests specified in 4.4.3.2a may be deleted with customer approval."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.4.4.2c","Requirement","ECSS-E-ST-32-02_0260178",1,"Created","For CPS, NDI operations shall be applied to the composite wall."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.5.1.2f","Requirement","ECSS-E-ST-32-02_0260194",1,"Created","For hydrogen embrittlement phenomena, requirements shall be applied in conformance with ECSS-E-ST-32-08."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.5.2.3f","Requirement","ECSS-E-ST-32-02_0260225",1,"Created","NDI operations shall be applied to the over-wrap, in addition to NDI on the liner."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.5.3.2l","Requirement","ECSS-E-ST-32-02_0260246",1,"Created","For ‘process control’, requirements shall be in conformance with ECSS-Q-ST-70."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.6.1.2i","Requirement","ECSS-E-ST-32-02_0260271",1,"Created","For hydrogen embrittlement phenomena, requirements shall be applied in conformance with ECSS-E-ST-32-08."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.6.1.3b","Requirement","ECSS-E-ST-32-02_0260276",1,"Created","All heat pipes and hazardous fluids containers shall be submitted to a design burst pressure test."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.6.2.2k","Requirement","ECSS-E-ST-32-02_0260298",1,"Created","For material selection, material design allowables and their characterisation, requirements shall be applied in conformance with clause 5.6 and ECSS-E-ST-32."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","4.6.3.2h","Requirement","ECSS-E-ST-32-02_0260323",1,"Created","Qualification tests shall be conducted according to clause 4.6.3.3 to demonstrate the structural adequacy of the design."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","5.2c","Requirement","ECSS-E-ST-32-02_0260344",1,"Created","Proof pressure and design burst pressure shall be derived from the MDP using the factor of safety given in clause 4."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","5.3.4f","Requirement","ECSS-E-ST-32-02_0260370",1,"Created","Pressure cycles shall be applied to the pressurized hardware, with the upper pressure equal to MDP and the lower pressure greater than or equal to zero."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","5.4.7a","Requirement","ECSS-E-ST-32-02_0260393",1,"Created","The pressure shall be increased until burst occurs."]
["ECSS-E-ST-32-02C Rev. 1","ECSS - Current v0.9","5.7.2c","Requirement","ECSS-E-ST-32-02_0260414",1,"Created","The NDI procedures are based on using multiple NDI methods to perform survey inspections or diagnostic inspections as follows: \n    1. survey NDI inspections shall be conducted when the location of the potential damage or flaw zone is unknown;\n    2. diagnostic NDI inspections shall be performed within a localized suspect zone to characterize the type and extent of the damage or flaw."]
["ECSS-E-ST-32-03C","ECSS - Current v0.9","4.4a","Requirement","ECSS-E-ST-32-03_0100004",1,"Created","The static behaviour of the structure shall be described by the reduced stiffness and mass matrices, and reduced force vector relative to the retained degrees of freedom."]
["ECSS-E-ST-32-03C","ECSS - Current v0.9","5.4.3d","Requirement","ECSS-E-ST-32-03_0100029",1,"Created","For each set of DOFs, mentioned in 5.4.3.a, and for each of the six unit rigid body motions (three unit translations and three unit rotations) residual nodal forces FR shall be computed by using the formula:\n "]
["ECSS-E-ST-32-08C Rev. 1","ECSS - Current v0.9","4.2.4a","Requirement","ECSS-E-ST-32-08_0220004",2,"Normative Change","For homogeneous materials the Kic or Kiscc shall be measured according to procedures approved by the customer at MPCB."]
["ECSS-E-ST-32-08C Rev. 1","ECSS - Current v0.9","4.2.7d","Requirement","ECSS-E-ST-32-08_0220013",1,"Unchanged","For hygroscopic materials used in high stability structural applications, the CME shall be determined by test."]
["ECSS-E-ST-32-08C Rev. 1","ECSS - Current v0.9","4.4.1a","Requirement","ECSS-E-ST-32-08_0220034",1,"Unchanged","Galvanic corrosion due to contact between dissimilar materials shall be precluded."]
["ECSS-E-ST-32-08C Rev. 1","ECSS - Current v0.9","4.6.2e","Requirement","ECSS-E-ST-32-08_0220055",1,"Unchanged","Composite materials shall be characterized by elementary tests on samples."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","4.1.4c","Requirement","ECSS-E-ST-32-11_0250005",1,"Created","The modal survey test shall provide the damping characteristics of the test item."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","4.2.4g","Requirement","ECSS-E-ST-32-11_0250027",1,"Created","The number of spare parts shall be sufficient to replace malfunctioning hardware during the modal survey test."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","5.3.3c","Requirement","ECSS-E-ST-32-11_0250052",1,"Created","For clamped structures, the number of sensors to be provided for the test fixture (as a minimum, at the interface) shall be such that the test boundary conditions specified in 5.3.2 can be verified."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","5.4.4a","Requirement","ECSS-E-ST-32-11_0250077",1,"Created","Measurements shall be performed to check the structurally linear behaviour of the test article. \n    NOTE For example, measuring the frequency response functions or tuning the mode shapes at different excitation levels."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","5.7.1.4b","Requirement","ECSS-E-ST-32-11_0250091",1,"Created","The off-diagonal elements shall be less than 10 %.\n    NOTE 1 High off-diagonal values can indicate an inadequate isolation of the respective modes, especially if they are closely spaced in the frequency band, or if they are not very well tuned.\n    NOTE 2 The degree of orthogonality of two measured modes with respect to the analytical mass matrix can be used as a criterion for the validity of the test results, for example to check the accuracy of the measurements and to detect duplicate modes.\n    NOTE 3 The orthogonality can be highly dependent on the validity of the mass matrix (accuracy of TAM)."]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","5.8.1.3a","Requirement","ECSS-E-ST-32-11_0250104",1,"Created","As a minimum, the following steps shall be performed during the test analysis correlation:\n    1. Selection of analysis DOFs: reduce the number of analysis mode shapes such that they are compatible with the experimental DOFs (number of accelerometers).\n        NOTE In general, the test modes have significantly fewer DOFs than the analysis mode shapes.\n    2. Mode pairing: differentiate the mode pairs between analysis and test in order of the highest MAC or cross-orthogonality values, and calculate the eigenfrequency differences for these pairs.\n        NOTE For mode pairs not in the same order as the eigenfrequency sequence, the MAC can incorrectly indicate corresponding pairs.\n    3. Cross-orthogonality: perform a general quality check of the FEM by means of the cross-orthogonality check. "]
["ECSS-E-ST-32-11C","ECSS - Current v0.9","6.4.1a","Requirement","ECSS-E-ST-32-11_0250125",1,"Created","The reference FEM and the state of representation of the test article shall be described in the test prediction document in conformance with the “Test prediction” DRD in ECSS-E-ST-32."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.3.6a","Requirement","ECSS-E-ST-32_0050031",1,"Created","The natural frequencies of a structure shall be within specified bandwidths preventing dynamic coupling with major excitation frequencies \n    NOTE For example launch vehicle fundamental frequencies."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.5.1a","Requirement","ECSS-E-ST-32_0050048",1,"Created","To ensure structural integrity, the requirement to inspect a component, assembly or structure shall be met during the following:\n    1. at various stages throughout manufacture,\n    2. at various stages during assembly,\n    3. after testing, and\n    4. in-service."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.5.9b","Permission","ECSS-E-ST-32_0050754",1,"Created","For unpressurized metal structures, B-values may be used in redundant structure in which the failure of a component can result in a safe redistribution of applied loads to other load-carrying structures."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.5.10.2c","Requirement","ECSS-E-ST-32_0050074",1,"Created","The material properties other than those specified in 4.5.10.2a and 4.5.10.2b shall be defined by average values."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.6.2.7a","Requirement","ECSS-E-ST-32_0050113",1,"Created","The structure shall be verified against the effects of the interaction with fluids (e.g. sloshing, POGO, cavitation effects and pressure fields)."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.6.2.10c","Requirement","ECSS-E-ST-32_0050121",1,"Created","Effects on stability of boundary conditions, defects and geometrical imperfections in the structure shall be included in the buckling analysis.\n    NOTE Geometrical imperfections refer to any deviation from the nominal shape including effect due to assembly tolerances."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.6.3.2h","Requirement","ECSS-E-ST-32_0050146",1,"Created","Test data shall be used to validate mathematical models for specific needs."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.6.3.14a","Requirement","ECSS-E-ST-32_0050164",1,"Created","The adequacy of the structure to withstand thermal loads shall be verified by test."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.7.4a","Requirement","ECSS-E-ST-32_0050193",1,"Created","Requirements for tooling, including assembly jigs and fixtures, shall include the following\n    1. materials used in manufacture,\n    2. geometry of the parts,\n    3. number of parts, and\n    4. production rate."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.7.6b","Requirement","ECSS-E-ST-32_0050198",1,"Created","To avoid all hazards to personnel or equipment, items that contain hazardous materials or those with specific storage requirements shall be marked according to ad-hoc procedures."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.8.5c","Requirement","ECSS-E-ST-32_0050219",1,"Created","The following shall be input to in-orbit repair procedures:\n    1. requirements for extra-vehicular activity,\n    2. transportability of materials to space (e.g. stability and outgassing properties of adhesives, hazardous cleaning and preparation chemicals),\n    3. preparation of surfaces or damage removal (e.g. availability of appropriate hand-tools, control of dust, vapours and contamination, and avoidance of space debris generation), and\n    4. repair manufacture difficulties."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","4.10i","Requirement","ECSS-E-ST-32_0050246",1,"Created","The supplier shall provide Mathematical model description and delivery in conformance with Annex I."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","A.2.1<4.5>a","Requirement","ECSS-E-ST-32_0050266",1,"Created","The CADMDD shall indicate the consistent unit system of measures, and related unit symbols. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","A.2.1<6.2>a","Requirement","ECSS-E-ST-32_0050291",1,"Created","If balance masses are present in the model, a description shall be provided in the CADMDD. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","B.2.1<5.2>a","Requirement","ECSS-E-ST-32_0050314",1,"Created","The DL document shall report all the feared mechanical failure modes of the structure, or structure components, associated with the above load, environment and lifetime conditions, as identified through a comprehensive FMECA. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","B.2.1<5.4>a","Requirement","ECSS-E-ST-32_0050318",1,"Created","The DL document shall identify and report the dimensioning envelope life cycles resulting from the most unfavourable expected sequences of the above combined dimensioning load events."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","C.2.1<4.5>b","Requirement","ECSS-E-ST-32_0050343",1,"Created","The units for mass, force, length, temperature and time shall be explicitly reported."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","E.2.1<4.1>b","Requirement","ECSS-E-ST-32_0050368",1,"Created","Reference shall be made to the available drawings."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","E.2.1<6.3>a","Requirement","ECSS-E-ST-32_0050379",1,"Created","Fatigue and strength data for the actual material and geometry (i.e. alloy, production form, heat treatment and stress concentration factor) shall be reported."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","G.2.1<4>a","Requirement","ECSS-E-ST-32_0050415",1,"Created","The PFCIL, FCIL and FLLIL shall describe the structure and introduce to the terminology for major structure components. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","H.2.1<7>a","Requirement","ECSS-E-ST-32_0050436",1,"Created","The MMPA shall report the applicable mechanical A or B allowables of the applied structural materials and processes, as stemming from the above collected mechanical material properties."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","I.2.1<4.2>c","Requirement","ECSS-E-ST-32_0050447",1,"Created","The MMDD shall reference the set of the applied drawings in order to explain the actual status of the design and to define the structure components to be analyzed."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","I.2.1<7.3>b","Requirement","ECSS-E-ST-32_0050467",1,"Created","A figure reproducing the each idealized item shall be included, in order to direct compare the idealized and the physical structural item."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","I.2.1<10.1>a","Requirement","ECSS-E-ST-32_0050488",1,"Created","The MMDD shall describe the set of point constraints and relationships. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","J.2.1<4.3>a","Requirement","ECSS-E-ST-32_0050513",1,"Created","This MDRA shall describe all the coordinate systems used."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","J.2.1<8>a","Requirement","ECSS-E-ST-32_0050529",1,"Created","The MDRA shall describe the main outcome of the analysis performed, reporting all key conclusions. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","K.2.1<4.3>a","Requirement","ECSS-E-ST-32_0050540",1,"Created","The SSA shall describe the reference coordinate systems used in the analysis, by giving the following information:\n    1. the identification number or name;\n    2. the type (rectangular, cylindrical spherical);\n    3. reference, if any, to mathematical model coordinate systems."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","K.2.1<8.2>e","Requirement","ECSS-E-ST-32_0050565",1,"Created","The following outputs of the stress analysis shall be included:\n    1. stresses for static and quasi-static structural integrity at design yield and ultimate level;\n    2. stresses for structural durability (fatigue, fracture and creep) at design limit level."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","K.2.1<10.2>a","Requirement","ECSS-E-ST-32_0050580",1,"Created","The SSA shall be include exhaustive information w.r.t. all the analysis related to the each item, by including or addressing all the analysis data and results, and the used procedures and methods. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","L.2.1<5>a","Requirement","ECSS-E-ST-32_0050612",1,"Created","The SAB shall present for each desired alignment performance the following information :\n    1. identification of the reported alignment performance figure;\n    2. reference frames used for the alignment performance description;\n    3. alignment figure with its associated uncertainties."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","M.2.1<5.2>c","Requirement","ECSS-E-ST-32_0050637",1,"Created","If a mathematical model is used to perform buckling analysis, the related MMDD shall be referenced."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","N.2.1<7>a","Requirement","ECSS-E-ST-32_0050658",1,"Created","The SMS shall include recommendations to use correctly the data included in this document."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","O.2.1<1>a","Requirement","ECSS-E-ST-32_0050662",1,"Created","The TAC shall contain a description of the purpose, objective, applicability, content and the reason prompting its preparation"]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","O.2.1<9>a","Requirement","ECSS-E-ST-32_0050685",1,"Created","The TAC shall describe the results of the test-analysis final correlation. "]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","P.2.1<6.6>c","Requirement","ECSS-E-ST-32_0050710",1,"Created","The TE shall include a reviewing of the interface requirements for strength, stiffness, and interface degrees of freedom for the test article’s support fixture."]
["ECSS-E-ST-32C Rev. 1","ECSS - Current v0.9","Q.2.1<4.1>a","Requirement","ECSS-E-ST-32_0050730",1,"Created","The TP shall describe the structure and introduce to the terminology for major structure components. "]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.2.3.1.2b","Requirement","ECSS-E-ST-34_0830007",1,"Created","When an ECLSS is not in operation during a given phase of the mission, standby mode conditions shall be defined."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.2.3.2b","Requirement","ECSS-E-ST-34_0830032",1,"Created","The accuracy for the stabilized dry bulb temperature in the habitable volume shall be specified."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.2.3.4a","Requirement","ECSS-E-ST-34_0830037",1,"Created","The range and the accuracy to monitor the atmosphere relative humidity in the habitable volumes shall be specified."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.2.10.2b","Requirement","ECSS-E-ST-34_0830066",1,"Created","The capability to provide shielding to maintain the ionizing radiation below the specified limits shall be provided."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.3.5.2a","Requirement","ECSS-E-ST-34_0830084",1,"Created","Means for protecting humans from hazardous atmospheres (e.g. IVA, isolating the hazardous atmosphere, or breathing from masks) shall be provided."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.4.2.5a","Requirement","ECSS-E-ST-34_0830105",1,"Created","The quantity of stored oxygen shall be monitored."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.4.5.3.2","Requirement","ECSS-E-ST-34_0830220",1,"Created","Produced food quality shall be controlled."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.4.5.4.1","Requirement","ECSS-E-ST-34_0830222",1,"Created","Food quality, quantity and palatability shall be monitored."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.5.2.5a","Requirement","ECSS-E-ST-34_0830146",1,"Created","The capability to dispose excess water shall be provided.\n    ","NOTE Disposal includes overboard dumping and transfer to a returning vehicle. This requirement is mission or design dependent."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.4.6.1.9a","Requirement","ECSS-E-ST-34_0830171",1,"Created","Rover operations shall be supported."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.6.2a","Requirement","ECSS-E-ST-34_0830184",1,"Created","Interfaces of the ECLSS with ground support shall be provided."]
["ECSS-E-ST-34C","ECSS - Current v0.9","4.9.2a","Requirement","ECSS-E-ST-34_0830218",1,"Created","The organization responsible for the ECLSS shall issue the specification to lower-level suppliers for the procurement of ECLSS sub-units."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.5.1.7a","Requirement","ECSS-E-ST-35-01_0840025",1,"Created","If a multi-tank layout is used, inadvertent propellant transfer between tanks shall be prevented by design."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.5.4.1b","Recommendation","ECSS-E-ST-35-01_0840350",1,"Created","If the flight version of the system is divided into independent blocks, they should be separated by safety barriers such as pyrovalves, latch valves or burst membranes. "]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.5.7c","Requirement","ECSS-E-ST-35-01_0840052",1,"Created","Item 4.5.7b shall be supported by analysis, simulation, or testing or all of them."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.5.14.2a","Requirement","ECSS-E-ST-35-01_0840077",1,"Created","The difference in thrust between two thrusters operating in pair on the same branch shall meet the thrust mismatch requirements."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.5.19.2a","Requirement","ECSS-E-ST-35-01_0840098",1,"Created","The GSE design and the procedures to operate it shall prevent the spillage or venting of dangerous materials."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.6.2.3.1a","Requirement","ECSS-E-ST-35-01_0840120",1,"Created","The transient analyses of clause 4.6.2.3 shall be reported in conformance with the Propulsion transient analysis report DRD in ECSS-E-ST-35."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.6.3.4.2a","Requirement","ECSS-E-ST-35-01_0840145",1,"Created","The non-volatile residue content of liquid to enter the propulsion system shall be specified in the standards for these liquids."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.6.3.7a","Requirement","ECSS-E-ST-35-01_0840150",1,"Created","In those cases where verification by analysis is considered inadequate, tests shall be performed to verify the adequacy of the design of the propulsion system with respect to pressure and flow transients."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","4.8.4b","Requirement","ECSS-E-ST-35-01_0840188",1,"Created","After operation of a propulsion system, special procedures shall be established in case manned interventions are planned.\n    NOTE After the operation of a propulsion system, a number of safety barriers no longer exist."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.2.2f","Requirement","ECSS-E-ST-35-01_0840197",1,"Created","The propulsion system shall provide the means for propellant gauging during the mission."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.5.1.3b","Requirement","ECSS-E-ST-35-01_0840222",1,"Created","The analysis specified in 5.5.1.3a shall be reported in conformance with the Propulsion transients analysis report DRD inECSS-E-ST-35."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.5.4.1a","Requirement","ECSS-E-ST-35-01_0840247",1,"Created","The development shall allow for an incremental verification at component, subsystem and propulsion system level, if a fully representative functional test cannot be performed after the integration of the system on the spacecraft."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.5.5.1c","Requirement","ECSS-E-ST-35-01_0840253",1,"Created","The potential hazard due to external contamination to the thruster shall be analysed.\n    NOTE Example of contamination to the thruster: by chemical propulsion or debris."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.5.12.2a","Requirement","ECSS-E-ST-35-01_0840274",1,"Created","The thrust random variation around its mean value, or thrust noise, shall be maintained within the specified range.\n    NOTE Thrust noise is usually composed of contributions from the thruster, the propellant feed system and the power electronics."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.5.14.1a","Requirement","ECSS-E-ST-35-01_0840295",1,"Created","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."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.6.2.3a","Requirement","ECSS-E-ST-35-01_0840321",1,"Created","In case multiple electric thrusters are used simultaneously, the mutual effects of the electrostatic and magnetic fields on thrusters and EP system performance shall be assessed."]
["ECSS-E-ST-35-01C","ECSS - Current v0.9","5.7.2a","Requirement","ECSS-E-ST-35-01_0840346",1,"Created","For production and manufacturing, clause 4.7.2 shall be applied."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.3.4b","Requirement","ECSS-E-ST-35-02_1100018",1,"Created","The Report for acoustic noise phenomena shall be delivered in conformance with the DRD of Annex A."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.5.2.2a","Requirement","ECSS-E-ST-35-02_1100040",1,"Created","The MEOP shall be calculated as specified in ECSS-E-ST-32 clause 4.2.7 ‘Limit loads’.\n    ","NOTE 1 The MDP is calculated as defined in ECSS-E-ST-32 clause 3.2.27 ‘MDP’.\nNOTE 2 If model uncertainties are included in the MEOP determination, Km is 1 for the calculation of MDP."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.5.2.3c","Requirement","ECSS-E-ST-35-02_1100044",1,"Created","The propulsion system shall have electrical continuity, including grounding."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.5.5.3.1b","Requirement","ECSS-E-ST-35-02_1100069",1,"Created","The pressure and mass flow rate time histories shall be calculated including:\n    1. the range of the driving parameters,\n    2. uncertainties, \n    3. scattering."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.8.2c","Recommendation","ECSS-E-ST-35-02_1100164",1,"Created","Depending on SRM technical requirements and in agreement between the customer and the supplier, additional verification by test should be performed for qualification of components, subsystems and systems of solid propulsion systems.\n    ","NOTE Table 4-3 presents examples where additional verification by test can be performed."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","4.10.2.1a","Requirement","ECSS-E-ST-35-02_1100103",1,"Created","During the operation of a lower stage propulsion system, the propulsion system of the next stage to be activated shall be\n    1. maintained in the condition for ignition, or\n    2. brought into the condition for ignition.\n        ","NOTE E.g. arming sequence, thermal control, nozzle actuation, TVC on."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","B.2.1<2>c","Requirement","ECSS-E-ST-35-02_1100137",1,"Created","The AR-MSDS shall provide the total mass of live materials."]
["ECSS-E-ST-35-02C","ECSS - Current v0.9","B.2.1<3>b","Requirement","ECSS-E-ST-35-02_1100142",1,"Created","The AR-MSDS shall describe the pyrotechnic propagation accident."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","7.2a","Requirement","ECSS-E-ST-35-03_1110007",1,"Created","The development logic shall include a requirement verification plan in conformance with ECSS-E-ST-10-02 ‘verification plan’.\n    ","NOTE Example of verification methods are analyses, tests."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","8.2a","Requirement","ECSS-E-ST-35-03_1110028",1,"Created","For interface requirements ECSS-E-ST-35 clause 4.4 shall apply."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.4.3.3b","Requirement","ECSS-E-ST-35-03_1110049",1,"Created","The liquid propulsion system shall provide valves and lines to flush, purge or vent the subsystems or components identified in 9.4.3.3a."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.4.4.3e","Requirement","ECSS-E-ST-35-03_1110074",1,"Created","The acceptability of propellant depletion shall be integrated in the “development logic” clause 7.2."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.4.5.3.1c","Requirement","ECSS-E-ST-35-03_1110089",1,"Created","Water-hammer phenomena shall have no detrimental effect on the structural and the functional behaviour of the propulsion system."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.3.1a","Requirement","ECSS-E-ST-35-03_1110101",1,"Created","Nominal engine performance and deviation shall be defined at a reference operating point."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.3.4.3e","Requirement","ECSS-E-ST-35-03_1110126",1,"Created","For multi engine stage, criteria shall be defined for thrust profile deviations between engines."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.4.5l","Requirement","ECSS-E-ST-35-03_1110157",1,"Created","For active cooling system, the outlet coolant flow temperature shall be measured."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.4.8.1c","Requirement","ECSS-E-ST-35-03_1110173",1,"Created","The design of the injector shall limit the heat load on the chamber wall to a level in compliance with the combustion chamber life requirement."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.4.8.4d","Requirement","ECSS-E-ST-35-03_1110198",1,"Created","For deployable nozzle, the deployment time shall conform to the launch vehicle requirements."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.6.2m","Requirement","ECSS-E-ST-35-03_1110219",1,"Created","When boost pump are used, the justification of their use shall be expressed at the liquid propulsion system level including performance, reliability and cost.\n    ","NOTE Performance includes mass, pressurisation system, mass budget."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.6.2p","Requirement","ECSS-E-ST-35-03_1110222",1,"Created","Requirements concerning non-uniformity of the flow pattern at the pump inlet shall be documented in the technical specification."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.8.2c","Requirement","ECSS-E-ST-35-03_1110250",1,"Created","A margin for 9.5.8.2b shall be established and specified."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.5.9.7d","Requirement","ECSS-E-ST-35-03_1110271",1,"Created","Flow fluctuation induced by bellows shall be avoided."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","9.6q","Requirement","ECSS-E-ST-35-03_1110290",1,"Created","Dimensioning load cases shall be established by using a selection process of all load case combinations during the whole life of the propulsion system."]
["ECSS-E-ST-35-03C","ECSS - Current v0.9","14.2b","Requirement","ECSS-E-ST-35-03_1110318",1,"Created","In case of launch abort, procedures shall be prepared, qualified and implemented to reset the propulsion system to a safe condition."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","5.1.2a","Requirement","ECSS-E-ST-35-10_1050022",1,"Created","The relevant propulsion configuration shall be analyzed for compatibility issues using cases and incompatibilities listed in Annex C and Annex D."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","5.2.1.1a","Requirement","ECSS-E-ST-35-10_1050027",1,"Created","The supplier shall assess and report in conformance with Annex A compatibility problems due to the state of the propellant originating from:\n    1. saturation with pressurant gases during pressurized ground storage;\n    2. contamination during storage and transport."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","6.2.3.3a","Requirement","ECSS-E-ST-35-10_1050055",1,"Created","The compatibility test procedure shall specify:\n    1. The following parameters:\n        (a) the test temperature or test temperatures;\n        (b) the test pressure or test pressures;\n        (c) the type of gas to blanket the container;\n        (d) the level of submersion of the solid;\n        (e) the number of samples to be tested;\n        (f) the duration of the test with a minimum of two weeks;\n        (g) a reference test on the fluid alone;\n        (h) a reference test on the solid alone.\n    2. The selection of the test container, including:\n        (a) the dimensions of the micro calorimeter, calorimeter or test vessel;\n        (b) the amount of fluid in the container in view of contamination and accuracies;\n        (c) the characteristics of the container together with the test specimen and the fluid (e.g. surface conditions, passivation, and compatibility);\n        (d) the applicable safety procedures;\n        (e) the possibility to hermetically seal the container (e.g. gas blanketing, pressure measurement);\n    3. The acquisition of the following data before and after the test:\n        (a) weight of the solid and the liquid;\n        (b) dimensions of the solid;\n        (c) the surface condition, by examination of a sample surface by SEM or other microscope at a minimum magnification in agreement with the test objectives;\n            NOTE 1 This is to see changes in the surface condition due to e.g. corrosion, dissolution. \n            NOTE 2 In case the observed changes in the surface conditions warrant this, more detailed investigations of the solid can be performed after the test.\n        (d) chemical analysis of the composition of the liquid;\n            NOTE The objective here is to identify changes in the composition of the liquid.\n        (e) chemical analysis of the NVR and particulates after the test.\n    4. The acquisition of the following data after the test \n        (a) weight of the particulates;\n        (b) level of contamination of the liquid by elements stemming from the solid after the test.\n    5. The preparation of the container, including:\n        (a) cleanliness;\n        (b) passivation;\n            NOTE The process depends on the fluid.\n        (c) dryness;\n        (d) leak tightness.\n    6. The instrumentation to be used, with the following characteristics:\n        (a) micro calorimeter or calorimeter, with a sensitivity of and an accuracy in agreement with the test objectives;\n        (b) pressure measurement device with a sensitivity, an inaccuracy and a stability in agreement with the test objectives;\n        (c) temperature measurement device with a sensitivity, an inaccuracy and a stability in agreement with the test objectives."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","6.5.2b","Requirement","ECSS-E-ST-35-10_1050074",1,"Created","The test shall be carried out under conditions representative of the service environment.\n    NOTE This is particularly important in terms of electrolyte chemical composition and temperature."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","6.7.2.3c","Requirement","ECSS-E-ST-35-10_1050099",1,"Created","The test temperature shall be below the first transition point 6.7.2.1c, above the upper temperature of the qualification temperature range."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","6.8.3.3c","Requirement","ECSS-E-ST-35-10_1050123",1,"Created","The compatibility test shall be performed according to 6.2.3.3, where the solid material has been replaced by one of the two liquids."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","6.8.4.1a","Recommendation","ECSS-E-ST-35-10_1050193",1,"Created","The pressurant gas (e.g. He, N2) dissolution level in the propellant should be determined."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-E-ST-35-10_1050148",1,"Created","The CAAR shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-35-10C","ECSS - Current v0.9","B.2.1<3>b","Requirement","ECSS-E-ST-35-10_1050174",1,"Created","The CLTP shall include any additional term, definition, abbreviated term and symbol used."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.2.3a","Requirement","ECSS-E-ST-35_0850026",1,"Created","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."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.3.1e","Requirement","ECSS-E-ST-35_0850040",1,"Created","The operational limits of the systems, subsystems or components shall also be documented."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.9.1b","Requirement","ECSS-E-ST-35_0850065",1,"Created","The supplier shall provide a cleanliness analysis report in conformance with ECSS-E-ST-35-06 ‘Cleanliness Requirements Analysis (CRA) for spacecraft propulsion components, subsystems and systems’, as part of the DJF."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.9.3h","Requirement","ECSS-E-ST-35_0850077",1,"Created","Icing phenomena shall be prevented in the filters."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.13d","Requirement","ECSS-E-ST-35_0850092",1,"Created","Chemical stability of the propellants shall be demonstrated by tests."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.5.15c","Requirement","ECSS-E-ST-35_0850117",1,"Created","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. "]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","4.8.2.1f","Requirement","ECSS-E-ST-35_0850138",1,"Created","The test objectives shall include the model improvement and validation."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-E-ST-35_0850159",1,"Created","The AR-P shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","A.2.1<6.1>a","Requirement","ECSS-E-ST-35_0850169",1,"Created","Since analysis covers both model computations and elaboration of measurements, the AR-P 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 propulsion performance 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 was obtained."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","B.2.1<4.1>a","Requirement","ECSS-E-ST-35_0850190",1,"Created","The AR-G shall describe the gauging system or subsystem and introduce its terminology. "]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","C.2.1<8>a","Requirement","ECSS-E-ST-35_0850227",1,"Created","The thermal analysis shall include a summary of the results and an assessment of the limitations of the performed work. "]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","D.2.1<5>c","Requirement","ECSS-E-ST-35_0850237",1,"Created","The AR-Pl shall include the description of the reference conditions used for the analysis."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","E.2.1<4.2>a","Requirement","ECSS-E-ST-35_0850262",1,"Created","The AR-N shall describe the coordinate systems used in the nozzle- discharge system."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","F.2.1<3>b","Requirement","ECSS-E-ST-35_0850287",1,"Created","The AR-S shall include any additional term, definition, abbreviated term or symbol used."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","F.2.1<5>a","Requirement","ECSS-E-ST-35_0850292",1,"Created","The AR-S shall describe the sloshing and the effects sloshing can have on propulsion subsystems and systems."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","G.2.1<4.1>b","Requirement","ECSS-E-ST-35_0850314",1,"Created","Reference shall be made to the applicable design definition file, inclusive its revision status and the specific study requirements. "]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","H.2.1<3>a","Requirement","ECSS-E-ST-35_0850339",1,"Created","The UM shall use the terms, definitions, abbreviated terms and symbols used in ECSS-E-ST-35."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","H.2.1<5.7>d","Requirement","ECSS-E-ST-35_0850360",1,"Created","The UM shall include the tests to be performed."]
["ECSS-E-ST-35C Rev. 1","ECSS - Current v0.9","I.2.1<6.2>c","Requirement","ECSS-E-ST-35_0850386",1,"Created","The MM-PA shall describe the conditions under which the results of numerical calculations are independent of discretization, i.e. the significant digits as defined in I.2.1<6.2>b do not change with further discretization."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.2.3.1a","Requirement","ECSS-E-ST-40_0860004",1,"Created","The customer shall specify the requirements needed for planning and setting up the system verification and validation process related to software.\n","EXPECTED OUTPUT: Verification and validation process requirements [RB, SSS; SRR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.2.4.2a","Requirement","ECSS-E-ST-40_0860009",1,"Created","The customer shall specify the support to be provided by the software supplier in order to integrate the software at system level.\n    NOTE For example: Raining, maintenance, configuration and test support.\n","EXPECTED OUTPUT: System level integration support requirements [RB, SSS; SRR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.3.4.3a","Requirement","ECSS-E-ST-40_0860039",1,"Created","After completion of the design of software items, coding and testing, integration and validation with respect to the technical specification, a critical design review (CDR) shall take place. \nAIM: - To review the design definition file, including software  architectural design, detailed design, code and users manual;\n- To review the design justification file, including the completeness of the software unit testing, integration and validation with respect to the technical specification.\n","EXPECTED OUTPUT: Approved design definition file and design justification file [DDF, DJF; CDR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.4.2.3b","Requirement","ECSS-E-ST-40_0860056",1,"Created","The supplier shall use a method to support the construction of the logical model.\n","EXPECTED OUTPUT: Software logical model method [TS, SRS; PDR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.5.2.6a","Requirement","ECSS-E-ST-40_0860081",1,"Created","The behavioural design of the software units shall be described by means of techniques using automata and scenarios.\n","EXPECTED OUTPUT: Software behavioural design model techniques [DDF, SDD; CDR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.5.4.1a","Requirement","ECSS-E-ST-40_0860090",1,"Created","The supplier shall complement the software integration test plan to define the integration of the software units and software components into the software item, providing the following data:\n    1. test design;\n    2. test case specification;\n    3. test procedures;\n    4. test data.\n","EXPECTED OUTPUT: Software integration test plan (update) [DJF, SUITP; CDR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.8.2.2a","Requirement","ECSS-E-ST-40_0860128",1,"Created","If the project warrants an independent verification effort, a qualified organization shall be selected for conducting the verification. \n","EXPECTED OUTPUT: Independent software verification plan - organization selection [DJF, - ; PDR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.8.3.4a","Requirement","ECSS-E-ST-40_0860133",1,"Created","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]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.8.3.13c","Requirement","ECSS-E-ST-40_0860156",1,"Created","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]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","5.10.2.1c","Requirement","ECSS-E-ST-40_0860174",1,"Created","The maintainer shall implement (or establish the organizational interface with) the configuration management process (ECSS-M-ST-40) for managing modifications.\n","EXPECTED OUTPUT: Maintenance plan - configuration management process [MF, - ; QR, AR, ORR]."]
["ECSS-E-ST-40C","ECSS - Current v0.9","B.2.1<3>a","Requirement","ECSS-E-ST-40_0860207",1,"Created","The SSS shall include any additional terms, definition or abbreviated terms used."]
["ECSS-E-ST-40C","ECSS - Current v0.9","B.2.1<5.3>b","Requirement","ECSS-E-ST-40_0860228",1,"Created","The requirements of the following shall be either be listed in the SSS or referred to in the IRD:\n    1. communication interfaces,\n    2. hardware interfaces,\n    3. software interfaces,\n    4. HMI,"]
["ECSS-E-ST-40C","ECSS - Current v0.9","B.2.1<6.1>a","Requirement","ECSS-E-ST-40_0860242",1,"Created","The SSS shall include the requirements needed for planning and setting up the system verification and validation process related to software\n    NOTE Specific customer requirements (e.g. availability or usage of customer furnished equipment like ETM, EM, FM and related ground systems) are needed in order to plan and to set up the system level verification and validation processes related to software. Furthermore, it is important to define for each testing or mission phase, or mission increment as far as applicable, any usage of hardware/software simulators , as representative flight and ground environments, for system payloads’ and experiments’ (pre-) integration testing, hardware/software compatibility as well for acceptance testing. "]
["ECSS-E-ST-40C","ECSS - Current v0.9","C.2.1<4.3>b","Recommendation","ECSS-E-ST-40_0860672",1,"Created","The nature of exchanges with external systems should be listed."]
["ECSS-E-ST-40C","ECSS - Current v0.9","D.2.1<5.2>a","Requirement","ECSS-E-ST-40_0860280",1,"Created","The SRS shall describe the capabilities to be provided by the software item under definition."]
["ECSS-E-ST-40C","ECSS - Current v0.9","D.2.1<5.17>a","Requirement","ECSS-E-ST-40_0860305",1,"Created","This SRS shall list any requirement applicable to adaptation data and to specific installation."]
["ECSS-E-ST-40C","ECSS - Current v0.9","E.2.1<5.3>d","Requirement","ECSS-E-ST-40_0860327",1,"Created","The definition of each interface shall include at least the provided service, the description (name, type, dimension), the range and the initial value."]
["ECSS-E-ST-40C","ECSS - Current v0.9","F.2.1<5.2>c","Requirement","ECSS-E-ST-40_0860352",1,"Created","For real-time software, the software dynamic architecture shall be summarized describing its selected computational model. \n    NOTE An analysable computational model generally consists in defining: \n        · the types of components (objects) participating to the real-time behaviour, from which the system is constructed (e.g. active-periodic, active-sporadic, protected, passive, actors, process, blocks, drivers)\n        · the scheduling type (e.g. sequential or multithreaded), the scheduling model (e.g. cyclic or pre-emptive, fixed or dynamic priority based), and the analytical model (e.g. Rate Monotonic Scheduling, Deadline Monotonic Scheduling, Earliest Deadline First), under which the system is executed and its associated mechanisms\n        · the means of communication between components/objects (e.g. mailboxes, entry parameters) \n        · the means of synchronization between components or objects (e.g. mutual exclusion, protected object entries, basic semaphores)\n        · If applicable , the means of distribution and internode communication (e.g. virtual nodes, Remote Procedure Call) \n        · the means of providing timing facilities (e.g. real clock, with or without interrupt, multiple interrupting count-down, relative or absolute delays, timers time-out) and (optional for non flight software): \n        · the means of providing asynchronous transfer of control (e.g. watchdog to transfer control from anywhere to the reset sequence, software service of the underlying run-time system to cause transfer of control within the local scope of the thread) "]
["ECSS-E-ST-40C","ECSS - Current v0.9","F.2.1<5.3>a","Requirement","ECSS-E-ST-40_0860357",1,"Created","The SDD shall describe:\n    1. The software components, constituting the software item.\n    2. The relationship between the software components.\n    3. The purpose of each software component.\n    4. For each software component, the development type (e.g. new development, software to be reused).\n    5. If the software is written for the reuse, \n        · its provided functionality from an external point of view, and\n        · its external interfaces.\n    6. Handling of existing reused components.\n        NOTE See Annex N."]
["ECSS-E-ST-40C","ECSS - Current v0.9","G.2.1<5.1>a","Requirement","ECSS-E-ST-40_0860396",1,"Created","The SRelD shall \n    1. summarize the main information on the software configuration item, and \n    2. describe the changes implemented since previous version."]
["ECSS-E-ST-40C","ECSS - Current v0.9","H.2.1<5>a","Requirement","ECSS-E-ST-40_0860404",1,"Created","The SUM shall include a description of the intended uses of the software, in terms of capabilities, operating improvements, and benefits expected from its use."]
["ECSS-E-ST-40C","ECSS - Current v0.9","H.2.1<11.2>a","Requirement","ECSS-E-ST-40_0860425",1,"Created","The SUM shall include a welcoming introduction to the software."]
["ECSS-E-ST-40C","ECSS - Current v0.9","J.2.1<3>a","Requirement","ECSS-E-ST-40_0860450",1,"Created","The SValP shall include any additional terms, definition or abbreviated terms used."]
["ECSS-E-ST-40C","ECSS - Current v0.9","J.2.1<4.3>a","Requirement","ECSS-E-ST-40_0860457",1,"Created","A reference to the master schedule given in the software development plan shall be included."]
["ECSS-E-ST-40C","ECSS - Current v0.9","K.2.1<7.1>a","Requirement","ECSS-E-ST-40_0860497",1,"Created","The SUITP shall describe the software integration strategy"]
["ECSS-E-ST-40C","ECSS - Current v0.9","K.2.1<7.6>a","Requirement","ECSS-E-ST-40_0860502",1,"Created","The SUITP shall address separately the activities to be performed for manually and automatically generated code, although they have the same objective (ECSS-Q-ST-80 clause 6.2.8.2 and 6.2.8.7)."]
["ECSS-E-ST-40C","ECSS - Current v0.9","K.2.1<10.2.1>a","Requirement","ECSS-E-ST-40_0860529",1,"Created","The SUITP shall include a statement specifying the test procedure uniquely. "]
["ECSS-E-ST-40C","ECSS - Current v0.9","L.2.1<6.2.2>a","Requirement","ECSS-E-ST-40_0860549",1,"Created","The SVS w.r.t. TS or RB shall describe the test items and the features to be tested. "]
["ECSS-E-ST-40C","ECSS - Current v0.9","L.2.1<10>a","Requirement","ECSS-E-ST-40_0860574",1,"Created","The SVS w.r.t. TS or RB shall list the validation requirements related to the validation test platform to be used (for example, benches or simulators capabilities and their representativity with respect to e.g. real time constraints, target or real hardware equipments on which the software is specified to operate)."]
["ECSS-E-ST-40C","ECSS - Current v0.9","N.2.1<3>a","Requirement","ECSS-E-ST-40_0860597",1,"Created","The SRF shall include any additional terms, definition or abbreviated terms used."]
["ECSS-E-ST-40C","ECSS - Current v0.9","N.2.1<5>b","Requirement","ECSS-E-ST-40_0860601",1,"Created","For each software item, the SRF shall provide the availability and quality status (completeness, correctness, etc.) of the following information:\n    1. software requirements documentation;\n    2. software architectural and detailed design documentation;\n    3. forward and backward traceability between system requirements;\n    4. software requirements, design and code;\n    5. unit tests documentation and coverage;\n    6. integration tests documentation and coverage;\n    7. validation documentation and coverage;\n    8. verification reports;\n    9. performance (e.g. memory occupation, CPU load);\n    10. 1operational performances;\n    11. 1residual non conformance and waivers;\n    12. 1user operational documentation (e.g. user manual);\n    13. 1code quality (adherence to coding standards, metrics)."]
["ECSS-E-ST-40C","ECSS - Current v0.9","O.2.1<5.2.3>a","Requirement","ECSS-E-ST-40_0860626",1,"Created","The SDP shall describe scope and purpose of each identified review, relevant deliverable and expected outputs. "]
["ECSS-E-ST-40C","ECSS - Current v0.9","O.2.1<5.6>a","Requirement","ECSS-E-ST-40_0860647",1,"Created","The SDP shall include the coverage matrix of the applicable tailoring of ECSS-E-ST-40 clause 5, or provide a reference to it."]
["ECSS-E-ST-50-02C","ECSS - Current v0.9","4.2.2.2a.2","Requirement","ECSS-E-ST-50-02_0870015",1,"Created","each code is synchronised to the tone such that phase transitions due to the code occur when the unmodulated tone phase is 90°;"]
["ECSS-E-ST-50-02C","ECSS - Current v0.9","4.2.3.2.2d","Requirement","ECSS-E-ST-50-02_0870030",1,"Created","Frequency instability of the telemetry signal shall be taken into account in the equations in provision 4.2.3.2.2a.\n    NOTE The interference level is strongly dependent on the ranging signal-to-noise density ratio (S/N0) in the spacecraft’s transponder. These provisions are applicable for high S/N0 ratios. When the conditions specified in provisions 4.2.3.2.2a to 4.2.3.2.2d cannot be satisfied, the tone frequency is selected by means of an optimization tailored to the requirements of the mission concerned."]
["ECSS-E-ST-50-02C","ECSS - Current v0.9","4.5.6d","Requirement","ECSS-E-ST-50-02_0870055",1,"Created","In the case of standard off-the-self transponders designed for multiple versions, the ranging tone selection shall be carried out taking into account available transponder noise bandwidths to minimize the loss in the effective Space-to-Earth link ranging modulation index."]
["ECSS-E-ST-50-02C","ECSS - Current v0.9","4.5.10a","Requirement","ECSS-E-ST-50-02_0870062",1,"Created","The transponder end-to-end technological loss (see Annex B) for both category A and category B missions shall be less than or equal to 1 dB. \n    NOTE This includes all internal transponder contributions in the demodulation and modulation process taking into account also phase noise and quantization effects (in case of digital implementation of the ranging function). "]
["ECSS-E-ST-50-02C","ECSS - Current v0.9","4.6.3.3b","Requirement","ECSS-E-ST-50-02_0870082",1,"Created","The measurement accuracy of the station ranging system shall be 1 ns or 1/1000 of the tone period, whichever is larger."]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","5.1.1.11a","Requirement","ECSS-E-ST-60-30_1160016",1,"Created","It shall be demonstrated that the AOCS design does not prevent meeting the requirements imposed by the mission and payload constraints.\n    ","NOTE These constraints can come from payload (e.g. forbidden attitudes, limited mechanical or magnetic disturbances, and sensitivity to environment) or from mission needs (e.g. antenna pointing for communication and operational constraints)."]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","5.2.1.1b","Requirement","ECSS-E-ST-60-30_1160037",1,"Created","The modification of periodically updated AOCS parameters shall be implemented through dedicated TCs."]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","5.2.4a","Requirement","ECSS-E-ST-60-30_1160057",1,"Created","The AOCS shall identify the need for in-flight calibration of sensors and actuators, and specify the tools and procedures to perform them. "]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","5.3.2.7a","Requirement","ECSS-E-ST-60-30_1160068",1,"Created","The AOCS contribution to the system level a posteriori relative pointing knowledge performance shall be lower than TBS microradians over a duration of TBS seconds, at TBS % confidence level, using the TBS (temporal, ensemble or mixed) statistical interpretation.\n    ","NOTE 1 The responsibility of the AOCS on this performance is usually limited to the AOCS sensors performances, the ground processing definition (when performed on ground), and the demonstration of the achievable final performance.\nNOTE 2 If the final performance is achieved using non-AOCS information, as mission or instrument data, the requirement cannot be made applicable to the AOCS only."]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","5.4.3d","Requirement","ECSS-E-ST-60-30_1160089",1,"Created","The simulation models used in the AOCS functional simulator and the avionics test bench for dynamics effects shall be justified.\n    ","NOTE Dynamics effects can arise from thermal snap, liquid sloshing and flexible modes of appendages."]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","A.2.1e","Requirement","ECSS-E-ST-60-30_1160125",1,"Created","The AOCS design definition file shall provide the mode logic information:\n    1. Organization and sequence of the AOCS modes along the whole mission profile versus satellite modes\n    2. Hardware versus operational modes matrix\n    3. Summary of the mode transitions"]
["ECSS-E-ST-60-30C","ECSS - Current v0.9","E.2.1b","Requirement","ECSS-E-ST-60-30_1160140",1,"Created","The AOCS UM shall provide a description of the operational constraints, including:\n    1. the hardware constraints applicable in flight,\n    2. the detailed constraints resulting from the AOCS mode architecture and AOCS mode design."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","5.5.3d","Requirement","ECSS-E-ST-50-13_1010020",1,"Created","For Table 5-4, in case the unit contains only one RT pair, the RT B/D address pins shall be copies of the RT A/C address pins."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","7.3.1a","Requirement","ECSS-E-ST-50-13_1010045",1,"Created","For SendData primitive using pre-allocated bandwidth with populated content (predefined transfers, Type I), the Table 7-4 shall apply."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","7.4.1b","Requirement","ECSS-E-ST-50-13_1010049",1,"Created","For ReceiveData primitive using pre-allocated bandwidth with unpopulated content (Type II), the Table 7-8 shall apply."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.2.2.2d","Requirement","ECSS-E-ST-50-13_1010072",1,"Created","The RT application shall support the case when a Time Message precedes a Time Synchronization Message as well as the case when there is Time Synchronization Message without a preceding Time Message."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.3.3a","Requirement","ECSS-E-ST-50-13_1010097",1,"Created","The BC shall provide a capability allowing each message to be transferred during a Communication Frame to have its transmission start time fixed relative to the start of the frame, defined by the middle transition of the synchronization field of the command word.\n    NOTE This allows for a deterministic scheduling of all transfers made on the bus."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.6.1.1i","Requirement","ECSS-E-ST-50-13_1010117",1,"Created","The last message (see requirement 8.6.1.1g), or a single message if the data block contains 64 bytes or less, shall transfer what remains of the data block including a possible single Filler Octet."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.6.2.2a","Requirement","ECSS-E-ST-50-13_1010144",1,"Created","A Reset Data Block Transfer Service request, consisting of an Acquisition Transfer Request as defined in clause 8.6.2.2d with the Reset flag set to ‘1’, shall be sent by each RT using this service before the first time the service is used, or if needed otherwise.\n    NOTE This requirement aims at ensuring a deterministic startup condition and a clear condition in case of restart due to for instance a terminal reconfiguration."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.7.3d","Requirement","ECSS-E-ST-50-13_1010169",1,"Created","Word 2 to 14 of SA 1R shall be reserved for command extension (to be defined by the application)."]
["ECSS-E-ST-50-13C","ECSS - Current v0.9","8.7.3e","Requirement","ECSS-E-ST-50-13_1010170",1,"Created","Word 15 to 31 of SA_1 shall be reserved for Remote Terminal configuration parameters (to be defined by the application)."]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","5.2.1.3a","Requirement","ECSS-E-ST-50-14_0940019",1,"Created","If the actual scenario differs from the one defined in 5.2.1.2, the interface shall not be directly used.\n\tNOTE 1 For example, if the specific application uses higher conversion accuracy or has different operational conditions, e.g. higher displacement.\n\tNOTE 2 In particular, ground displacement heavily affects the achievable conversion accuracy. Different scenario or specified performances can, for instance, ask for source impedance balancing. "]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","5.3.5.2.2a","Requirement","ECSS-E-ST-50-14_0940037",1,"Created","The maximum error in  Rth, DRth, expressed as a function of Dx, shall be:\n                                                "]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","7.1.3.1a","Requirement","ECSS-E-ST-50-14_0940062",1,"Created","The source circuit shall meet the characteristics specified in Table 7-1."]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","8.3.4.3a","Requirement","ECSS-E-ST-50-14_0940087",1,"Created","The DATA_CLK_OUT signal shall comprise sixteen low going pulses during each data transfer operation."]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","8.4.4.4a","Requirement","ECSS-E-ST-50-14_0940109",1,"Created","The core element shall provide a DATA_CLK_OUT signal. "]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","8.4.4.7a","Requirement","ECSS-E-ST-50-14_0940114",1,"Created","Peripheral elements shall ignore the DATA_OUT signal when the GATE_WRITE signal is not asserted.\n    ","NOTE The reason is that during quiescence, i.e. when no data transfer is taking place, the DATA_OUT signal can change (e.g. if it is shared with other peripheral elements). "]
["ECSS-E-ST-50-14C","ECSS - Current v0.9","8.8.2b","Requirement","ECSS-E-ST-50-14_0940135",1,"Created","Serial digital interface circuit electrical characteristics shall meet the requirements specified in Table 8-4.\n    ","NOTE 1 Table 8-4 includes characteristics for compatibility with RS-422 (indicated with the number (422) in the table), and specific characteristics\nNOTE 2 The values specified here-in grant correct operations in the following conditions:\n        · maximum signal frequency: 1 MHz;\n        · maximum cable length: 16 m;\n        · cable type: Twisted Shielded Pair 120 W Impedance.\nNOTE 3 Compliance to the parameters indicated by the note (422) in Table 8-4 can be achieved by use of the following circuits:\n\tHS-26C(T)31RH\n\tHS-26C(T)32RH\n\tHS-26CLV31RH\n\tHS-26CLV32RH\n\tItems 1 and 2 are 5 V supplied devices, items 3 and 4 are 3,3 V supplied devices. These devices can interoperate and comply with the specification in Table 8-4."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.1.1a","Requirement","ECSS-E-ST-50-52_1080001",1,"Created","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."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.1.15a","Requirement","ECSS-E-ST-50-52_1080035",1,"Created","The Data CRC field shall be an 8-bit field that contains an 8-bit Cyclic Redundancy Code (CRC) covering each byte in the data and mask field starting with the byte after the Header CRC and ending with the byte before the Data CRC."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.3.1.6a","Requirement","ECSS-E-ST-50-52_1080056",1,"Created","The Key field shall be as defined in clause 5.1.5."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.3.2.1a","Requirement","ECSS-E-ST-50-52_1080069",1,"Created","The format of the reply to a write command shall contain the fields shown in Figure 5-2.\n    ","NOTE A reply is sent by the target back to initiator of the write command or to some other node as defined by the Reply Address field if requested in the write command. The reply indicates the success or failure of the write command by the value in the Status field."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.3.3.4.1a","Requirement","ECSS-E-ST-50-52_1080087",1,"Created","When a Packet is received at the target and the Protocol Identifier field is 0x01 the packet shall be regarded as an RMAP packet."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.3.3.6.1a","Requirement","ECSS-E-ST-50-52_1080108",1,"Created","If authorisation is given by the target user application, the data contained in the write command shall be written into the memory location in the target specified by the Extended Address and Address fields (Write Data in Figure 5-3)."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.3.3.8a","Requirement","ECSS-E-ST-50-52_1080133",1,"Created","If the Reply bit in the command field is set (1) requesting a reply and the write command was executed successfully, the target shall send a reply packet with the status field set to 0x00 indicating that there was no error to the node specified by the Reply Address and Initiator Logical Address fields of the write command (Write Reply)."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.4.1.6a","Requirement","ECSS-E-ST-50-52_1080155",1,"Created","The Key field shall be as defined in clause 5.1.5. "]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.4.2.10a","Requirement","ECSS-E-ST-50-52_1080180",1,"Created","The Data Length field format shall be as defined in clause 5.1.11."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.4.2.13a","Requirement","ECSS-E-ST-50-52_1080185",1,"Created","The Data CRC shall contain an 8-bit CRC as defined in clauses 5.1.15 and 5.2."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.4.3.10b","Recommendation","ECSS-E-ST-50-52_1080438",1,"Created","If the read memory operation memory fails, the target should update the error information to reflect the memory access error if the target supports error information gathering."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.1.2a","Requirement","ECSS-E-ST-50-52_1080232",1,"Created","The Target SpaceWire Address field shall be as defined in clause 5.1.1."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.1.15a","Requirement","ECSS-E-ST-50-52_1080257",1,"Created","The Mask field shall be used by the target application to define how the data written to memory is formed.\n    ","NOTE 1 The way the read data and mask are combined is application dependent.\nNOTE 2 For example, data written can be selected on a bit by bit basis from the data sent in the command when the corresponding mask bit is set (1) or from the data read in the reply when the mask bit is clear (0).\nNOTE 3 Written Data = (Mask AND Command_Data) OR (NOT Mask AND Read_Data).\nNOTE 4 This example is illustrated in Figure 5-16. The target user application can implement different schemes for example test and set."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.2.11a","Requirement","ECSS-E-ST-50-52_1080278",1,"Created","The Header CRC field shall contain a CRC as defined in clauses 5.1.12 and 5.2."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.3.4.12a","Requirement","ECSS-E-ST-50-52_1080305",1,"Created","When checking the Header CRC indicates no error present in the header and if there is more data in the data field than specified in the Data Length field of the read-modify-write command header, then the target shall:\n    1. Neither read data from, nor write data to 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."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.3.9a","Requirement","ECSS-E-ST-50-52_1080380",1,"Created","If the read-modify-write command was executed successfully, the target shall send a reply packet to the node specified by the Reply Address and Initiator Logical Address fields of the read command (RMW Reply)."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.5.3.11b","Recommendation","ECSS-E-ST-50-52_1080460",1,"Created","If the read or write operations to memory fails, the target should update the error information to reflect the “memory access” error if the target supports error information gathering."]
["ECSS-E-ST-50-52C","ECSS - Current v0.9","5.7.2c","Requirement","ECSS-E-ST-50-52_1080384",1,"Created","If a reply has been requested then the RMAP command not implemented or not authorised error shall be sent back to the initiator (or other node).\n    ","NOTE See clause 5.6."]
["ECSS-E-ST-50-53C","ECSS - Current v0.9","5.2.3.2b","Requirement","ECSS-E-ST-50-53_1090017",1,"Created","If the packet arrived is terminated by EEP or the Reserved field is non-zero the CCSDS Packet and the User Application Value shall be null."]
["ECSS-E-ST-50-53C","ECSS - Current v0.9","5.5.2b","Requirement","ECSS-E-ST-50-53_1090042",1,"Created","The initiator user application shall pass the following information to the initiator:\n    1. Target SpaceWire Address\n    2. Target Logical Address\n    3. CCSDS Packet\n    4. Packet Length\n    5. User Application Value"]
["ECSS-E-ST-60-10C","ECSS - Current v0.9","4.2.2.3a","Requirement","ECSS-E-ST-60-10_1020012",1,"Created","For each error source, a mean and standard deviation shall be allocated along each axis.\n    NOTE 1 The mean and standard deviation differ depending on which error indices are being assessed. Guidelines for obtaining these parameters are given in Annex B                                                 \n    NOTE 2 The variance can be considered equivalent to the standard deviation, as they are simply related. The root sum square (RSS) value is only equivalent in the case that the mean can be shown to be zero. \n    NOTE 3 Further information about the shape of the distribution is only needed in the case that the approximations used for budgeting are insufficient."]
["ECSS-E-ST-60-10C","ECSS - Current v0.9","5.2.2c","Requirement","ECSS-E-ST-60-10_1020027",1,"Created","The technique (or techniques) used to demonstrate the stability shall be described and justified.\n    NOTE Several methods are available for this purpose. For example stability of a linear time-invariant system can be demonstrated by examining the eigenvalues of the closed loop state matrix."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.1d","Requirement","ECSS-E-ST-70-01_1060004",1,"Created","The nominal execution sequence for an OBCP shall be:\n    1. declaration body;\n    2. preconditions body;\n    3. main body;\n    4. confirmation body."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.2.6e","Requirement","ECSS-E-ST-70-01_1060025",1,"Created","It shall be possible to mix compatible engineering units freely within an expression."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.3.1c","Requirement","ECSS-E-ST-70-01_1060056",1,"Created","It shall be possible to collapse and expand the view of an OBCP, either globally or locally at the level of a step."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.4.2.3c","Requirement","ECSS-E-ST-70-01_1060076",1,"Created","At the end of its execution, the OBCP shall return autonomously to the “inactive” state (Transition: “Completion”)."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.4.4.4b","Requirement","ECSS-E-ST-70-01_1060097",1,"Created","The following characteristics of the loading policy shall be defined:\n    1. whether the loading policy is reprogrammable;\n    2. how the loading policy is affected by reset or reboot of the OBSW, switch-over to a redundant processor or loss of power to on-board memories."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","5.4.4.5d","Requirement","ECSS-E-ST-70-01_1060102",1,"Created","The allocation of on-board resources for running OBOPs shall be independent from the allocation of on-board resources for running OBAPs.\n    NOTE For example, CPU time, memory."]
["ECSS-E-ST-70-01C","ECSS - Current v0.9","6.2.1c","Requirement","ECSS-E-ST-70-01_1060121",1,"Created","The output of the OBCP system management process shall be the consolidation of the required capabilities of the OBCP engine, the preparation environment, the ground execution environment and engineering processes."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","4.5e","Requirement","ECSS-E-ST-70-11_0290009",1,"Created","The FDIR design shall ensure that the space segment is safe without ground segment intervention for the specified duration in the presence of a single failure."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.2.3c","Requirement","ECSS-E-ST-70-11_0290034",1,"Created","The allocation of bandwidth to different virtual channels shall be modifiable during the mission."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.3.1m","Requirement","ECSS-E-ST-70-11_0290049",1,"Created","Where telemetry measurements are processed on-board, the capability shall be provided to downlink the raw data to the ground segment, on request.\n    ","NOTE For example, AOCS sensor data."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.3.1y","Requirement","ECSS-E-ST-70-11_0290061",1,"Created","The capability shall be provided to request that housekeeping telemetry source packets are only sent to ground segment if there has been a change in value of specified contained parameters by more than a specified threshold."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.5.1a","Requirement","ECSS-E-ST-70-11_0290082",1,"Created","Telecommands shall be available to command all on-board equipment and functions under all nominal and envisaged contingency conditions.\n    ","NOTE This implies the provision of a high priority command to re-establish command processing in the event of processor failure."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.5.4c","Requirement","ECSS-E-ST-70-11_0290107",1,"Created","Except for telecommands that are executed purely by hardware (e.g. CPDU commands), verification of the acceptance stage shall be provided for all telecommands."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.6.2h","Requirement","ECSS-E-ST-70-11_0290131",1,"Created","The capability shall be provided to trigger any on-board reconfiguration activities that put the space segment into a predefined safe state:\n    1. autonomously, and\n    2. by ground commanding."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.7.5.2l","Requirement","ECSS-E-ST-70-11_0290154",1,"Created","Where FDIR functions are based on several inputs (e.g. sensor readings, and unit status), which are independently tested to determine a failure condition, the capability shall be provided to enable and disable each such input by telecommand."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.7.5.7b","Requirement","ECSS-E-ST-70-11_0290179",1,"Created","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. "]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.8.2f","Requirement","ECSS-E-ST-70-11_0290199",1,"Created","The capability shall be provided to request a report of the current set of parameters being evaluated."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.8.3g","Requirement","ECSS-E-ST-70-11_0290206",1,"Created","The capability shall be provided to request a memory dump from a contiguous memory area (e.g. by specifying the start address and the length of the dump)."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.8.5m","Requirement","ECSS-E-ST-70-11_0290231",1,"Created","The on-board operations schedule service shall detect any situation that prevents the on-board transfer of a telecommand to its destination application process."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.8.7b","Requirement","ECSS-E-ST-70-11_0290252",1,"Created","Taking into account factors such as downlink bandwidth and ground contact periods, a given mission shall be capable of defining a maximum telemetry source packet length which is less than the maximum specified by ECSS-E-ST-50-03."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.8.9f","Requirement","ECSS-E-ST-70-11_0290264",1,"Created","The capability shall be provided to assign priorities to parallel retrievals from different stores.\n    ","NOTE These priorities can be assigned to maximize the utilization of the downlink bandwidth."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.9.1k","Requirement","ECSS-E-ST-70-11_0290303",1,"Created","Any communication between the ground and an on-board software function or software task shall be effected by means of telecommand and telemetry source packets specifically designed for the purpose.\n    ","NOTE The objective is to ensure that memory dump and memory load packets (for example) are not used for this purpose. They are not adequate for changes of this operational significance."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.9.1l","Requirement","ECSS-E-ST-70-11_0290304",1,"Created","Whenever a condition that forces a processor reset is detected by software, an event report shall be generated prior to enforcement of the reset."]
["ECSS-E-ST-70-11C","ECSS - Current v0.9","5.9.4f","Recommendation","ECSS-E-ST-70-11_0290364",1,"Created","In normal conditions the avionics of 3-axis controlled spacecraft should maintain the knowledge of the current 3-axis attitude."]
["ECSS-E-ST-70C","ECSS - Current v0.9","5.2.2.2b","Requirement","ECSS-E-ST-70_0060007",1,"Created","The output of these tasks shall be the mission operations concept document (MOCD) in conformance with Annex C."]
["ECSS-E-ST-70C","ECSS - Current v0.9","5.3.2c","Recommendation","ECSS-E-ST-70_0060394",1,"Created","Where a given entity is operated independently, the operations for that entity should be contained in a sub-plan of the MOP."]
["ECSS-E-ST-70C","ECSS - Current v0.9","5.5.3a","Requirement","ECSS-E-ST-70_0060052",1,"Created","The outputs of the operations teams build-up and training process shall be the ones specified in Table 5-8."]
["ECSS-E-ST-70C","ECSS - Current v0.9","5.8.2.2c","Requirement","ECSS-E-ST-70_0060075",1,"Created","Technical facilities shall be augmented as necessary to accommodate the additional operations staff.\n    NOTE For example, by the use of common or multi-mission facilities such as control rooms."]
["ECSS-E-ST-70C","ECSS - Current v0.9","5.8.2.3e","Requirement","ECSS-E-ST-70_0060080",1,"Created","Health monitoring of the space and ground segments shall be performed."]
["ECSS-E-ST-70C","ECSS - Current v0.9","6.2.1a","Requirement","ECSS-E-ST-70_0060105",1,"Created","The inputs to the ground segment definition process shall be the ones identified in Table 6-1."]
["ECSS-E-ST-70C","ECSS - Current v0.9","6.3.2g","Requirement","ECSS-E-ST-70_0060138",1,"Created","Acceptance test reports shall be produced for each ground system."]
["ECSS-E-ST-70C","ECSS - Current v0.9","6.4.2.3b","Requirement","ECSS-E-ST-70_0060152",1,"Created","The OS shall support the corresponding validation tests and the production of the associated reports, including ground segment verification reports and a ground segment preliminary acceptance report.\n    NOTE The different stages of ground segment acceptance are addressed in clause 7.5.3."]
["ECSS-E-ST-70C","ECSS - Current v0.9","6.6.2d","Requirement","ECSS-E-ST-70_0060173",1,"Created","Mission data shall remain accessible for a duration agreed with the ground segment customer.\n    NOTE The intention of this requirement is to conform to relevant regulations and to the mission requirements."]
["ECSS-E-ST-70C","ECSS - Current v0.9","7.3.3c","Requirement","ECSS-E-ST-70_0060185",1,"Created","Phase B shall end with a ground segment preliminary design review (GSPDR), which follows the successful completion of the space system PDR."]
["ECSS-E-ST-70C","ECSS - Current v0.9","7.6.3c","Requirement","ECSS-E-ST-70_0060204",1,"Created","Phase E2 shall be concluded by the end-of-life review (ELR), which shall verify that the mission has completed its useful operation or service and that the procedures for disposal are in place."]
["ECSS-E-ST-70C","ECSS - Current v0.9","B.2.1<6>a","Requirement","ECSS-E-ST-70_0060225",1,"Created","The MAR shall provide the following information:\n    1. ground station coverage;\n    2. eclipse phases and daily durations;\n    3. Earth occultation phases;\n    4. attitude control strategy;\n        NOTE For example, to maintain antenna Earth-pointing, to respect thermal control constraints.\n    5. payload operational constraints;\n        NOTE Sensor blinding by Earth or Sun.\n    6. transfer manoeuvre strategy."]
["ECSS-E-ST-70C","ECSS - Current v0.9","D.2.1<4>a","Requirement","ECSS-E-ST-70_0060250",1,"Created","The OEP shall identify the following:\n    1. the major milestones driving the operations engineering processes;\n    2. the operations engineering lifecycle phases;\n    3. the principal operations reviews and their objectives;\n    4. the operations engineering critical path."]
["ECSS-E-ST-70C","ECSS - Current v0.9","E.2.1<4.6.2>a","Requirement","ECSS-E-ST-70_0060267",1,"Created","The SSUM shall describe all nominal and back-up modes (at the system level), including:\n    1. their purpose (i.e. circumstances under which they are used),\n    2. operational constraints,\n    3. resource utilization,\n    4. the expected satellite behaviour within each mode,\n    5. the definition of the associated modes for each platform subsystem and payload, and\n    6. ground monitoring requirements."]
["ECSS-E-ST-70C","ECSS - Current v0.9","F.2.1<3.2>a","Requirement","ECSS-E-ST-70_0060297",1,"Created","The OVP shall describe the management structure for the conduct of the operational validation, including the individual responsibilities of the following operations teams (as applicable):\n    1. the mission operations team;\n    2. the ground operations team;\n    3. the flight dynamics team;\n    4. the mission exploitation team.\n    5. the simulations officer(s);\n    6. any independent QA group that is involved in the operational validation."]
["ECSS-E-ST-70C","ECSS - Current v0.9","F.2.1<5>a","Requirement","ECSS-E-ST-70_0060302",1,"Created","The OVP shall describe the ground segment readiness test plan, mission readiness tests (MRTs), data flow tests (DFTs), including:\n    1. an overall test plan, and\n    2. for each individual test:\n        (a) the test timetable (start time, duration),\n        (b) the test configuration including, for instance, the identification of all ground segment systems or equipment to be used and initialization requirements as applicable,\n            NOTE For example, hardware, software and database versions.\n        (c) any applicable test constraints,\n        (d) manpower resources, and\n        (e) the test procedures to be used (cross-reference may be made to other documents)."]
["ECSS-E-ST-70C","ECSS - Current v0.9","I.2.2<6>c","Requirement","ECSS-E-ST-70_0060339",1,"Created","Pre-conditions shall refer to one or more of the following:\n    1. Mission phase;\n    2. Ground segment configuration;\n    3. Space segment configuration;\n    4. Orbit position or environmental conditions;\n    5. Status of other procedures."]
["ECSS-E-ST-70C","ECSS - Current v0.9","J.2.1<1>a","Requirement","ECSS-E-ST-70_0060349",1,"Created","The introduction shall describe the purpose and objective of the CFISRD."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","4.2.2a","Requirement","ECSS-E-ST-50-05_0900016",1,"Unchanged","The same RFI mitigation methods specified in 4.2.1.2.1 for the 2 200 MHz - 2 290 MHz band shall be applied to the 8 025 MHz - 8 400 MHz band.\n    NOTE The 8 025 MHz - 8 400 MHz band is the only direct data transmission band allocated to the Earth Exploration Satellite service below 20 GHz. Its occupation density is similar to that of the 2 200 MHz - 2 290 MHz band; additionally the interference situation is aggravated by the fact that most of the Earth Exploration-Satellites use very similar (polar) orbits."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","5.3b","Requirement","ECSS-E-ST-50-05_0900037",1,"Unchanged","Earth stations shall be capable of transmitting right-hand or left-hand circular polarization upon discretion of the user. \n    NOTE 1 For practical reasons, spacecraft generally use the same sense of polarization for the Earth-space link and the space-Earth link.\n    NOTE 2 Most Earth stations have the capability of combining two orthogonal circular polarizations on the space-Earth link."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.1.3a","Requirement","ECSS-E-ST-50-05_0900063",1,"Unchanged","PCM data signals shall be limited to the waveforms and symbol rates given in Table 6-1 as follows.\n    1. For the RF carrier bands of 2 025 MHz - 2 120 MHz, 7 145 MHz - 7 235 MHz, and 34 200 MHz - 34 700 MHz (telecommand):\n        (a) Use of NRZ-M for category B is prevented.\n        (b) Use of 4 ksps only with 16 kHz subcarrier.\n            NOTE Requirement 6.1.3a.1(a) is a restriction of CCSDS recommendation 401 (2.2.3) but is justified by the better performance of NRZ-L for Category B missions.\n    2. For the RF carrier bands of 2 200 MHz - 2 300 MHz, 8 400 MHz - 8 500 MHz and 31 800 MHz - 32 300 MHz (telemetry), SP-L is prevented for symbol rates below 10 ksps.\n        NOTE For the definition of the PCM waveforms and symbol duration, refer to Figure 6-1 and Figure 6-2.                       "]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.1.4.2.3b","Requirement","ECSS-E-ST-50-05_0900084",1,"Unchanged","The subcarrier frequency shall be an integer multiple of the symbol rate."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.1.5a","Requirement","ECSS-E-ST-50-05_0900089",1,"Unchanged","To ensure recovery of the symbol clock by the ground demodulators, the transition density in the transmitted PCM waveform shall not be less than the following values: \n    1. 125 in any sequence of 1 000 consecutive symbols for category A;\n    2. 275 in any sequence of 1 000 consecutive symbols for category B. "]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.1.11f","Requirement","ECSS-E-ST-50-05_0900110",1,"Unchanged","The out-of-band emission due to the modulation shall comply with the spectral roll-off of clause 6.3."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.2.3.4b","Requirement","ECSS-E-ST-50-05_0900136",1,"Unchanged","The phase angle between the two quadrature carriers shall be (90 ±5)°."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.2.6b","Requirement","ECSS-E-ST-50-05_0900161",1,"Unchanged","Phase noise of the unmodulated carrier, integrated between 100 Hz and 1 MHz shall be less than 2° r.m.s. at UHF for the 2 200 MHz - 2 300 MHz band."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","6.2.7b","Requirement","ECSS-E-ST-50-05_0900166",1,"Unchanged","Discrete lines in the transmitted RF signal spectrum, caused by baseband or RF bandwidth limitations, non-linearity of the channel, or any other effects shall be less than -45 dBc inside the occupied bandwidth."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","8.2.2a","Requirement","ECSS-E-ST-50-05_0900200",1,"Unchanged","The first draft of the document shall be prepared in the Phase B (preliminary definition) of the project by the responsible engineering department using inputs from the study or project manager. "]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","8.3.2i","Recommendation","ECSS-E-ST-50-05_0900293",1,"Created","Margins based on design parameters should exceed 3 dB, and those on the RSS worst case and the mean -3s should exceed 0 dB.\n\n    a. These recommendations have been derived from practical experience."]
["ECSS-E-ST-50-05C Rev. 2","ECSS - Current v0.9","9.2.6.1a","Requirement","ECSS-E-ST-50-05_0900238",1,"Unchanged","Channel filtering shall be obtained by one of the following two methods:\n    - Square-root raised-cosine (SRRC) baseband shaping filter located prior to the modulator, with a channel roll-off factor a of 0,35 (or 0,5) as described in 9.2.6.2.\n       NOTE This waveform shaping is used in association with a linear modulator and power amplifier.\n    - Post-amplifier shaping using an output filter located at the output of the non-linear power amplifier as described in point 9.2.6.3.\n       NOTE In this case a NRZ-like shaping is used in conjunction with a non-linear 8-phase modulator."]
["ECSS-E-ST-70-32C","ECSS - Current v0.9","5.2c","Requirement","ECSS-E-ST-70-32_0950021",1,"Created","The capability shall be provided to request the execution of an activity and wait for the confirmation of execution before continuing."]
["ECSS-E-ST-70-32C","ECSS - Current v0.9","5.2x","Permission","ECSS-E-ST-70-32_0950058",1,"Created","The conditions specified for a procedure (or step) precondition or confirmation may be any combination of the following:\n    1. wait until a given absolute time;\n    2. wait for a given interval of time to elapse;\n    3. wait until a given condition becomes true;\n    4. wait until a given event occurs;\n    5. test whether a given condition is true;\n    6. request the user to specify the outcome."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.2.2a","Requirement","ECSS-E-ST-70-31_0270013",1,"Created","It shall be possible to define the data relating to the instantiation of an activity namely, the activity reference, the values of the activity argument or a reference to a predefined set of argument values and any directives that apply for the instantiation of the activity.\n    ","NOTE 1 E.g.: to define corrective actions to be taken in specific circumstances (limit violations, activity failures etc.).\nNOTE 2 E.g.: to define arguments of activities (e.g. a PUS service 11 subtype 4 request which inserts telecommand packets in the on-board schedule).\nNOTE 3 E.g.: telecommand directives can include for example: the MAP ID to be used; whether the telecommand is to be sent in AD or BD mode; the specification of the telecommand verification packets to be generated in response to this telecommand."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.2.3d","Requirement","ECSS-E-ST-70-31_0270018",1,"Created","Engineering units shall be supported."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.3.2.2a","Requirement","ECSS-E-ST-70-31_0270053",1,"Created","For each product identified within the electronic database, the data specified in Table 6-2 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.4.1a","Requirement","ECSS-E-ST-70-31_0270065",1,"Created","All monitoring and control data shall be provided using the English language."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.5.5.2.2a","Requirement","ECSS-E-ST-70-31_0270090",1,"Created","For the data types of the packet fields of the telecommand verification service, the additional data shown in Table 6-18 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.5.5.6.3a","Requirement","ECSS-E-ST-70-31_0270104",1,"Created","For each event raised by this service, the additional data specified in Table 6-32 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.5.5.10.3b","Requirement","ECSS-E-ST-70-31_0270117",1,"Created","For each event of type “scheduling event”, the additional data specified in Table 6-45 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.5.11a","Requirement","ECSS-E-ST-70-31_0270142",1,"Created","For system elements of type “store” (see clause 6.5.5.13.3 for the related PUS on-board storage and retrieval service), the additional data specified in Table 6-68 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.6.6.4a","Requirement","ECSS-E-ST-70-31_0270163",1,"Created","For reporting data that is status consistency checked, the data specified in Table 6-88 shall be provided."]
["ECSS-E-ST-70-31C","ECSS - Current v0.9","6.7.5.3a","Requirement","ECSS-E-ST-70-31_0270186",1,"Created","For activities of type “onboard procedure”, the additional data specified in Table 6-110 shall be provided."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.3.2.1b","Requirement","ECSS-E-ST-20-08_0090023",1,"Unchanged","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."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.3.3.9a","Requirement","ECSS-E-ST-20-08_0090048",1,"Unchanged","A FMECA shall be performed for the design of the solar array. "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.4.3.3a","Requirement","ECSS-E-ST-20-08_0090067",1,"Unchanged","A wet insulation test shall be performed by the supplier to prove the integrity of the bare coupon insulation layer, as follows: \n    1. Verify continuity between the conductive layer under the insulation to the test connection point. \n    2. For the wet insulation test, use ethyl, isopropyl alcohol, or otherwise an equivalent fluid agreed with the customer, as contact fluid during the measurements.\n    3. Apply a voltage which corresponds to the breakthrough value for short term exposure of the applied insulation material (Espec V/mm) times the minimum guaranteed thickness. \n        NOTE For example, for Espec= 20 V/mm and a (50 ± 10) mm insulation layer, a test voltage of 800 V applies."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.4.3.6b","Requirement","ECSS-E-ST-20-08_0090075",1,"Unchanged","Continuity of harness, wires and diodes shall be checked, and measured after final assembly."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.1.3.3h","Requirement","ECSS-E-ST-20-08_0090100",1,"Unchanged","The production of the qualification coupons shall be representative of the full processing of the flight hardware. "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.1.5.2b","Requirement","ECSS-E-ST-20-08_0090126",1,"Unchanged","Testing shall demonstrate that the observed primary arcs do not produce any type of damage to the solar array or to the cells."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.2.4d","Requirement","ECSS-E-ST-20-08_0090133",1,"Unchanged","The bake-out test shall be performed as part of the coupon acceptance test sequence only in the cases where the bake-out is included in the manufacturing process or in the acceptance test of the flight panels."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.3.2.18a","Requirement","ECSS-E-ST-20-08_0090173",1,"Unchanged","All identification markings specified by the customer shall be firmly adhered to the locations identified on the assembly drawing."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.3.2.18b","Requirement","ECSS-E-ST-20-08_0090174",1,"Unchanged","Identification markings shall be clearly legible."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.3.4.2a","Requirement","ECSS-E-ST-20-08_0090201",1,"Unchanged","The electrical power performance at the string level shall be measured at a reference temperature of 25 °C at the interface connector."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.5.3.8b","Requirement","ECSS-E-ST-20-08_0090225",1,"Unchanged","The reflectance shall be measured over a range from 280 nm to 2 500 nm."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","5.6.2b","Requirement","ECSS-E-ST-20-08_0090246",1,"Unchanged","Failure analysis of these coupons 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."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.1a","Requirement","ECSS-E-ST-20-08_0090271",1,"Unchanged","All SCA procurement lots shall be qualified. "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.2.3a","Requirement","ECSS-E-ST-20-08_0090284",1,"Unchanged","Qualification testing shall proceed as given in Table 6-1."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.3.1.5e","Requirement","ECSS-E-ST-20-08_0090299",1,"Unchanged","The coverglass shall not contain bubbles having a projected area larger than 0,02 mm2."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.3.4e","Requirement","ECSS-E-ST-20-08_0090325",1,"Unchanged","The temperature coefficients of short-circuit current, open circuit voltage, voltage at maximum power and current at maximum power shall be derived by least-square curve fitting."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.3.11.2f","Requirement","ECSS-E-ST-20-08_0090357",1,"Unchanged","The sequence of tests in Table 6-1 shall be arranged so SCAs of subgroup D are irradiated at Fp."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","6.4.3.15.2d","Requirement","ECSS-E-ST-20-08_0090372",1,"Unchanged","The test shall be performed in a vacuum (i.e. pressure less than 10-3 Pa). "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.1.1.2b","Requirement","ECSS-E-ST-20-08_0090398",1,"Unchanged","The SCD-BSC shall be prepared by the supplier in conformance with Annex C and provided to the customer for reviewing and agreement."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.3.2.2.2b","Requirement","ECSS-E-ST-20-08_0090419",1,"Unchanged","The specified test voltage (Vtest) shall be defined in the SCD-BSC."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.4.2.3a","Requirement","ECSS-E-ST-20-08_0090441",1,"Unchanged","Qualification testing shall proceed as given in Table 7-2."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.5.1.4.1a","Requirement","ECSS-E-ST-20-08_0090447",1,"Unchanged","The location and maximum dimensions for allowable defects related to edge chips, corner chips and surface nicks shall be in conformance with Figure 7-1 and Table 7-3."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.5.3.2d","Requirement","ECSS-E-ST-20-08_0090472",1,"Unchanged","During measurement, the cells shall be kept at a constant temperature (+/- 0,5 °C). "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.5.6.3c","Requirement","ECSS-E-ST-20-08_0090488",1,"Unchanged","The coverglass as stated in the SCD-BSC shall be used."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.5.12.2c","Requirement","ECSS-E-ST-20-08_0090519",1,"Unchanged","The pull direction shall:\n    1. be either 0°, 45° or 90°; \n    2. be as stated in the SCD-BSC."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.5.13.2d","Requirement","ECSS-E-ST-20-08_0090524",1,"Unchanged","The nominal rate shall be lower than 5 × 1011 e- cm-2 s-1."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","7.8a","Requirement","ECSS-E-ST-20-08_0090549",1,"Unchanged","All deliverable hardware specified in the order shall be delivered together with documentation in conformance with the requirements specified in clause 7.7."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.6.1a","Requirement","ECSS-E-ST-20-08_0090574",1,"Unchanged","Qualification shall be granted by the customer."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.7.1.3.7a","Requirement","ECSS-E-ST-20-08_0090597",1,"Unchanged","Coverglasses shall not have dirty or contaminated surfaces.\n    NOTE For further information, see MIL-PRF-13830."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.7.7a","Requirement","ECSS-E-ST-20-08_0090618",1,"Unchanged","When a conductive coating is incorporated in the coverglass, the surface resistivity shall be measured, using the equipment stated in the SCD-CVG, as follows:\n    1. Measure the resistance between two indium-tin soldered buzzbars applied to the coverglass, as shown in Figure 8-5.\n    2. Calculate the surface resistivity from the resistance and the length a, and b, defined in Figure 8-5 using the following equation:\n \nwhere\nR \tis the measured resistance;\nRS\tis the surface resistivity.\n                              "]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.7.12.2d","Requirement","ECSS-E-ST-20-08_0090643",1,"Unchanged","The temperature of the coverglass shall be kept below 60 °C during the test."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.7.13.2e","Requirement","ECSS-E-ST-20-08_0090649",1,"Unchanged","Tests shall be performed in vacuum (pressure below 10-3 Pa) or in inert gas atmosphere."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","8.10b","Requirement","ECSS-E-ST-20-08_0090670",1,"Unchanged","One set of documents shall be sent to the customer."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.4.4d","Requirement","ECSS-E-ST-20-08_0090695",1,"Unchanged","The data documentation of acceptance tests shall be delivered together with the delivered cells/diodes and the qualification test lot."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.5.2e","Requirement","ECSS-E-ST-20-08_0090708",1,"Unchanged","The integral protection diodes shall be equipped with front interconnectors as step 7 in Table 7-2."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.6.6.2a","Requirement","ECSS-E-ST-20-08_0090743",1,"Unchanged","All protection diodes in subgroup O shall be placed in a chamber at ambient pressure."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.6.6.2f","Requirement","ECSS-E-ST-20-08_0090748",1,"Unchanged","Water condensation on the surface of the protection diodes shall be prevented."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.6.15.2c","Requirement","ECSS-E-ST-20-08_0090777",1,"Unchanged","Provision 9.6.15.2b shall be performed for the following variables, as stated in the SCD-BSC or SCD-EPD:\n    1. At different temperatures (including maximum and minimum operating temperature with margins and sustained operation in forward bias). \n    2. For different times.\n    3. Up to a forward current, IDIODE-FORWARD., which is as a minimum, equal to 1,1 times the expected string current at solar array level at the maximum mission temperature specified in the solar array specification.\n    4. Up to a reverse voltage, VDIODE-REVERSE. which is as a minimum, equal to n times the expected solar cell open circuit voltage at the minimum mission temperature specified in the solar array specification, being \n        (a) n =1,33 for acceptance testing and \n        (b) n=1,5 for qualification testing)"]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","9.6.17.3a","Requirement","ECSS-E-ST-20-08_0090795",1,"Unchanged","The diode characteristics test shall satisfy the pass-fail criteria stated in the SCD-BSC or SCD-EPD."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","10.1.2d","Requirement","ECSS-E-ST-20-08_0090820",1,"Unchanged","In the case of coupons, the detector shall not be bigger than the SCAs bonded to it."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","10.2.2.3.5a","Requirement","ECSS-E-ST-20-08_0090845",1,"Unchanged","Correlation measurements between the SWS in daily use and a primary standard shall be made at intervals mutually agreed upon between the supplier and the customer."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","11.2.2.1a","Recommendation","ECSS-E-ST-20-08_0091096",1,"Created","The time domain capacitance measurement test set-up, should comprise the following test equipment:\n    1. A continuous or pulsed solar simulator according to the requirements specified in clause 10.\n    2. A solar array capacity tester which supplies a synchronizable fast switch to perform a controlled short-circuit release at the open circuit condition of the qualification coupon or SCA under test.\n    3. A digital-analogue oscilloscope to capture the voltage-current transient during the short-circuit release at the open circuit condition.\n    4. A twisted harness of short length to reduce the parasitic inductance of the harness from the test specimen to the capacity tester."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","A.2.1<7.3>a","Requirement","ECSS-E-ST-20-08_0090890",1,"Unchanged","In conformance with clause 5.5.1.6, the SCD-PVA shall state the test sequence, test definitions and requirements for the erosion of materials test."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","A.2.1<8.3>b","Requirement","ECSS-E-ST-20-08_0090895",1,"Unchanged","For insulation resistance, the SCD-PVA shall state the minimum insulation resistance, in MW, at a test voltage specified in V, for the configurations specified in clause 5.5.3.3.3."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","B.2.1<6.14>a","Requirement","ECSS-E-ST-20-08_0090929",1,"Unchanged","In conformance with clause 6.4.3.16, the SCD-SCA shall include the test temperature, in °C and the capacitance test method as specified either in clause 11.1 or 11.2 of this Standard."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","C.2.1<6.5>c","Requirement","ECSS-E-ST-20-08_0090942",1,"Unchanged","In conformance with clause 7.3.2.2.4 the SCD-BSC shall include the intervals in mA for electrical grading"]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","D.2.1<3>a","Requirement","ECSS-E-ST-20-08_0090967",1,"Unchanged","The SCD-CVG shall include any additional definition, abbreviation or symbol used."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","D.2.1<7.6>a","Requirement","ECSS-E-ST-20-08_0090976",1,"Unchanged","The SCD-CVG shall include the same provisions as for the thermal cycling for qualification tests (in conformance with clause D.2.1<8>)."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","E.2.1<2>a","Requirement","ECSS-E-ST-20-08_0090994",1,"Unchanged","The SCD-EPD shall list the applicable and reference documents to support the generation of the document."]
["ECSS-E-ST-20-08C Rev. 1","ECSS - Current v0.9","F.2.2b","Requirement","ECSS-E-ST-20-08_0091019",1,"Unchanged","In the case specified in requirement 11.2.2.4a, a reference to the document shall be included. "]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","5.1.2a","Requirement","ECSS-E-ST-50-15_1270011",1,"Created","The maximum bus length shall be implemented in accordance with ISO 11898-2:2003 clause 7.5."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","5.3.2a","Requirement","ECSS-E-ST-50-15_1270032",1,"Created","Transceivers shall comply with the physical medium attachment sub-layer specification of ISO 11898-2:2003 clause 7.2.","NOTE\tAn excerpt of ISO 11898-2:2003 specification is illustrated in Table 5-1."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","5.4.2a","Requirement","ECSS-E-ST-50-15_1270054",1,"Created","If a device supports more bit rates than specified in requirement 5.4.1a it shall support one or more of the following rates:\n1.\t500 kbps\n2.\t250 kbps\n3.\t125 kbps"]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","6.5.3a","Requirement","ECSS-E-ST-50-15_1270073",1,"Created","All devices shall implement the minimum Bootup service as specified in CANopen CiA 301 V4.2.0 section 7.2.8.2.3."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","6.10g","Requirement","ECSS-E-ST-50-15_1270091",1,"Created","The Node-ID shall be configurable when the node is in a specific maintenance mode only."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","7.1.1b","Permission","ECSS-E-ST-50-15_1270255",1,"Created","Each device on the CAN network that maintains time information may use Spacecraft Universal Time Coordinated (UTC) as defined in ECSS-E-70-41 Annex C."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","7.2.2g","Requirement","ECSS-E-ST-50-15_1270126",1,"Created","There shall be one Local Time PDO for each node maintaining local time.","NOTE\tThe various transmission types defined in CANopen allow to use a number of different methods to transmit the Spacecraft Time PDO and Local Time PDOs. However, the details are application specific and out of scope for this standard."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","8.3.3c","Requirement","ECSS-E-ST-50-15_1270153",1,"Created","Each Slave node shall be a consumer of the Master Heartbeat messages sent by the Redundancy Master."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","9.4.4b","Requirement","ECSS-E-ST-50-15_1270186",1,"Created","The optional parameters “Inhibit time” and “event time” of PDO shall not be used."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","9.4.10e","Requirement","ECSS-E-ST-50-15_1270210",1,"Created","If in Table 9-12 a device supports PDOs, the according PDO communication parameter and PDO mapping entries in the Object dictionary shall be implemented.","NOTE\tThe Object dictionary can be read-only."]
["ECSS-E-ST-50-15C","ECSS - Current v0.9","10.3.1b","Requirement","ECSS-E-ST-50-15_1270218",1,"Created","The connector shall not use a non-conductive finish as specified in requirement 4.2.13.2c.1 of ECSS-E-ST-20-07. "]
["ECSS-E-ST-10-24C","ECSS - Current v0.9","5.1a","Requirement","ECSS-E-ST-10-24_1290001",1,"Created","An interface management plan shall be established by the interface responsible to describe the Interface Management approach."]
["ECSS-E-ST-10-24C","ECSS - Current v0.9","5.5f","Requirement","ECSS-E-ST-10-24_1290025",1,"Created","The ICD shall be consolidated to the frozen status, prior to the CDR of the first product involved in the interface."]
["ECSS-E-ST-10-24C","ECSS - Current v0.9","A.2.1<4>h","Requirement","ECSS-E-ST-10-24_1290046",1,"Created","In addition to the general requirements defined in ECSS-E-ST-10-06, for each interface requirement the applicability to each interface end shall be specified."]
["ECSS-E-ST-10-24C","ECSS - Current v0.9","C.2.1<4>a","Requirement","ECSS-E-ST-10-24_1290070",1,"Created","The applicable dictionary or glossary and the meaning of specific terms or abbreviation utilized in IDD shall be defined."]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.2.2.1.1a","Requirement","ECSS-E-ST-20-20_1320011",1,"Created","The RLCL class shall be selected among one shown in Table 3-2 and comply with related class performance.","NOTE \tThe performance of the LCL classes are typically achieved by using several MOSFET switches.\n"]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.2.7.2.1a","Recommendation","ECSS-E-ST-20-20_1320120",1,"Created","An LCL/HLCL should always start in OFF conditions."]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.2.13.3.1b","Requirement","ECSS-E-ST-20-20_1320046",1,"Created","It shall be possible to command the LCL/HLCL and the relevant additional switch in series by a different, individual command, or a different commanding path."]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.4.1.3.1a","Requirement","ECSS-E-ST-20-20_1320074",1,"Created","Maximum leakage current for LCL/RLCL/HLCL shall be 100 µA."]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.4.4.2.1a","Requirement","ECSS-E-ST-20-20_1320090",1,"Created","The LCL/RLCL/HLCL enable ON threshold shall be configurable up to 90 % of the nominal DC maximum bus voltage value."]
["ECSS-E-ST-20-20C","ECSS - Current v0.9","5.5.3.1.1a","Requirement","ECSS-E-ST-20-20_1320114",1,"Created","For LCL/RLCL, at those frequencies in which the load and the source impedance are equal in magnitude, the difference between the load impedance phase and the source impedance phase shall be greater than abs(±150°±n*360°).","NOTE \tn is a positive integer including 0,\n\tabs is the absolute value operator.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.3.3.1g","Requirement","ECSS-E-ST-70-41_1330017",1,"Created","Each message type shall either be:\n1.\ta request type, or\n2.\ta report type.","NOTE 1\tFor item 1, refer to clause 5.3.5.2.\nNOTE 2\tFor item 2, refer to clause 5.3.3.3.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.3.5.2.2a","Requirement","ECSS-E-ST-70-41_1330037",1,"Created","Each request type shall be linked to at most one data report type.","NOTE 1\tAn example of a request type that is linked to a data report type is the \"report parameter monitoring definitions\" request type. The linked data report type, playing the role of the response type, is the \"parameter monitoring definition report\", refer to requirement 6.12.3.10a.\nNOTE 2\tAs stated in requirement 5.3.3.3b, each data report type defines exactly one notification type. The link that exists between a request type and a report type implies that each instruction type defined by that request type is linked to the notification type defined by that report type.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.3.5.2.3j","Requirement","ECSS-E-ST-70-41_1330048",1,"Created","For each request type, the request-specific functionality that the subservice performs when executing a request of that type shall be declared when specifying that request type."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.4.3.3.1b","Requirement","ECSS-E-ST-70-41_1330069",1,"Created","At any time, each on-board memory identifier shall uniquely identify exactly one on-board memory that is unique across the entire spacecraft."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.4.5d","Requirement","ECSS-E-ST-70-41_1330084",1,"Created","The set of file attributes supported by each on-board file system shall be declared when specifying that file system.","NOTE\tFor example, the file type, its creation date.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.4.11.3.1d","Requirement","ECSS-E-ST-70-41_1330116",1,"Created","Each report shall be of exactly one report type."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","5.4.11.3.3a","Requirement","ECSS-E-ST-70-41_1330121",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.1.4.3c","Requirement","ECSS-E-ST-70-41_1330145",1,"Created","Each failed acceptance notification shall contain:\n1.\tthe identifier of the request that failed the acceptance verification;\n2.\tthe failure notice made of:\n(a)\ta failure code;\n(b)\tauxiliary data, if any, used to explain the reason for the failed acceptance.","NOTE\tFor item 2, see requirements 6.1.4.3d and 6.1.4.3e.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.2.4.2c","Requirement","ECSS-E-ST-70-41_1330169",1,"Created","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"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.2.5.3h","Requirement","ECSS-E-ST-70-41_1330192",1,"Created","For each valid request to distribute register dump commands, the device access subservice shall generate a single register dump report that contains all related register dump notifications."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.2.7.1.3g","Requirement","ECSS-E-ST-70-41_1330217",1,"Created","For each valid instruction to acquire data from a physical device, the device access subservice shall:\n1.\ttransmit the acquisition command to the physical device by using the protocol-specific data and the applicable protocol;\n2.\tcheck the data acquisition return code that reports on the result of the transmission;\n3.\tif the data acquisition is successful, generate a single physical device data notification that includes:\n(a)\tthe transaction identifier;\n(b)\tthe data acquisition return code;\n(c)\tthe auxiliary data associated to that data acquisition return code, if any;\n(d)\tthe data block corresponding to the acquired data.\n4.\tif the data acquisition fails, generate a failed execution notification that includes:\n(a)\tthe transaction identifier;\n(b)\tthe transaction execution status, which consists of the data acquisition, the return code and associated auxiliary data.","NOTE\tA physical device data report contains a single physical device data notification.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.2.7.2.3i","Requirement","ECSS-E-ST-70-41_1330237",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.3.1a","Requirement","ECSS-E-ST-70-41_1330244",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.3.4.2e","Requirement","ECSS-E-ST-70-41_1330265",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.3.7c","Requirement","ECSS-E-ST-70-41_1330290",1,"Created","Each instruction to generate a one shot report for a housekeeping parameter report structure shall contain:\n1.\tthe housekeeping parameter report structure identifier of the report to generate."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.4.2c","Requirement","ECSS-E-ST-70-41_1330319",1,"Created","Each diagnostic parameter report structure shall consist of:\n1.\ta diagnostic parameter report structure identifier;\n2.\tthe collection interval used to generate the corresponding reports;\n3.\tan ordered list of zero or more simply commutated parameters;\n4.\tan ordered list of zero or more super commutated parameter sets, each set consisting of:\n(a)\tthe number of sampled values to report for each parameter of that set, and\n(b)\tthe ordered list of one or more parameters contained within that set;\n5.\ta status indicating whether the periodic generation action of the corresponding diagnostic parameter reports is enabled or disabled.","NOTE 1\tThe diagnostic parameter report structures are uniquely identified by the combination of the application process that hosts the diagnostic reporting subservice provider and a diagnostic parameter report structure identifier.\nNOTE 1\tThe collection interval is expressed as units of the minimum sampling interval, refer to requirement 5.4.3.2c.\nNOTE 2\tFor item 4(a), the number of sampled values to report for each parameter of the set is named \"super commutated sample repetition number\".\nNOTE 3\tFor item 5, this status is named \"housekeeping parameter report periodic generation action status\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.4.5e","Requirement","ECSS-E-ST-70-41_1330337",1,"Created","For each instruction to disable the periodic generation of a diagnostic parameter report that it rejects, the diagnostic reporting subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.4.6c","Requirement","ECSS-E-ST-70-41_1330342",1,"Created","Each instruction to create a diagnostic parameter report structure shall contain:\n1.\tthe diagnostic parameter report structure identifier to create;\n2.\tthe collection interval;\n3.\tthe list of simply commutated parameters in the required order;\n4.\tthe list of super commutated parameter sets in the required order.","NOTE 1\tThe ordering of the simply and super commutated parameter sets corresponds to the order of the corresponding sampled values in the diagnostic parameter reports.\nNOTE 1\tSee clause 6.3.4.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.4.10d","Requirement","ECSS-E-ST-70-41_1330370",1,"Created","The diagnostic reporting subservice shall reject any request to append parameters to a diagnostic parameter report structure if any of the following conditions occurs:\n1.\tthe periodic generation action status of the diagnostic parameter report is enabled;\n2.\tthat request contains an instruction that refers to a diagnostic parameter report structure that is unknown;\n3.\tthat request contains an instruction that refers to a parameter that is unknown;\n4.\tthat request contains an instruction that refers to simply commutated parameters to add to a definition that contains super commutated parameters;\n5.\tthat request contains an instruction that refers to a parameter that is already present in the definition;\n6.\tthe resources allocated to the hosting of diagnostic parameter report structures are exceeded."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.5.1b","Requirement","ECSS-E-ST-70-41_1330389",1,"Created","The parameter functional reporting configuration subservice shall be able to control the generation of each diagnostic parameter report generated by the diagnostic reporting subservices of the parent housekeeping service."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.5.4.2f","Requirement","ECSS-E-ST-70-41_1330414",1,"Created","The parameter functional reporting configuration subservice shall process any valid instruction that is contained within a request to delete parameter functional reporting definitions regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.3.5.6.2d","Requirement","ECSS-E-ST-70-41_1330435",1,"Created","For each request to remove parameter report definitions from a parameter functional reporting definition that is rejected, the parameter functional reporting configuration subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.4.3.1a","Requirement","ECSS-E-ST-70-41_1330452",1,"Created","The maximum number of parameter statistics definitions that the parameter statistics reporting subservice can contemporaneously evaluate at any time shall be declared when specifying that subservice."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.4.5.2b","Requirement","ECSS-E-ST-70-41_1330466",1,"Created","Each request to report the parameter statistics shall contain:\n1.\tif the subservice provides the capability to explicitly state in each request to report the parameter statistics, whether or not to reset the parameter statistics after the generation of the parameter statistics report, the resetting indication.\n2.\texactly one instruction to report the parameter statistics.","NOTE 1\tFor the capability in item 1, refer to requirement 6.4.5.1b.\nNOTE 1\tThe instructions to report the parameter statistics contain no argument.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.4.6.3b","Requirement","ECSS-E-ST-70-41_1330487",1,"Created","Each request to disable the periodic parameter statistics reporting shall contain exactly one instruction to disable the periodic parameter statistics reporting.","NOTE\tThe instructions to disable the periodic parameter statistics reporting contain no argument.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.5.4f","Requirement","ECSS-E-ST-70-41_1330520",1,"Created","For each event notification that it generates, the event reporting subservice shall generate an event report of the related event severity level, which contains that notification.","NOTE\tThe message subtype identifier of the event report message type indicates the event severity level, refer to requirement 6.5.4a.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.5.5.3e","Requirement","ECSS-E-ST-70-41_1330534",1,"Created","For each instruction to disable the report generation of an event definition that it rejects, the event reporting subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.3.3.1f","Requirement","ECSS-E-ST-70-41_1330559",1,"Created","For each request to load raw memory data areas that is rejected, the raw data memory management subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.3.5a","Requirement","ECSS-E-ST-70-41_1330584",1,"Created","The raw data memory management subservice capability to check raw memory data shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[6,9] check raw memory data\". The responses are data reports of message type \"TM[6,10] checked raw memory data report\".\nNOTE 2\tChecking memory and reporting the calculated checksum for ground checksum comparison, avoids downlinking on-board memory areas that are suspected to be faulty.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.3.5b","Requirement","ECSS-E-ST-70-41_1330585",1,"Created","Each request to check raw memory data shall contain:\n1.\tif the raw data memory management subservice manages more than one memory, the identifier of the memory;\n2.\tone or more instructions to check a raw memory data.","NOTE\tFor item 1, refer to requirement 6.6.3.2a. If the raw data memory management subservice manages only one memory, the instructions apply to that memory.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.3.7g","Requirement","ECSS-E-ST-70-41_1330611",1,"Created","For each instruction to dump a raw memory data area to file that it rejects, the raw data memory management subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.4.5c","Requirement","ECSS-E-ST-70-41_1330636",1,"Created","The structured data memory management subservice shall reject any request to dump object memory data if any of the following conditions occurs:\n1.\tthat request refers to a memory identifier that is unknown;\n2.\tthe base identifier in that request refers to a memory object that is unknown;\n3.\tthe subservice does not have read access to the memory referred to in that request;\n4.\tthat request implies a response to transmit a telemetry packet that exceeds the maximum packet size of the CCSDS space packet protocol.","NOTE\tFor item 4, refer to requirement 5.4.11.3.2b.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.4.6j","Requirement","ECSS-E-ST-70-41_1330653",1,"Created","For each valid request to check object memory data, the structured data memory management subservice shall generate a single checked object memory data report that contains \n1.\tif the structured data memory management subservice manages more than one memory, the identifier of the memory;\n2.\tthe base identifier;\n3.\tall related checked object memory data notifications.","NOTE 1\tFor item 1, refer to requirement 6.6.4.2a.\nNOTE 2\tFor item 2, refer to requirement 6.6.4.3a.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.5.1b","Requirement","ECSS-E-ST-70-41_1330683",1,"Created","Each request to abort all memory dumps shall contain exactly one instruction to abort all memory dumps.","NOTE\tThe instructions to abort all memory dumps contain no argument.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.6.2.3a","Requirement","ECSS-E-ST-70-41_1330704",1,"Created","For each memory for which the write protection can be controlled by the memory management service, the service shall maintain a status indicating whether the memory is write protected or write unprotected.","NOTE 1\tThis status is named \"memory write protection status\".\nNOTE 1\tThe actual implementation of the write protection is memory dependent i.e. write protection by hardware or by software.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.6.6.2.4e","Requirement","ECSS-E-ST-70-41_1330709",1,"Created","For each request to enable the write protection of a memory that is rejected, the memory configuration subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.9.3a","Requirement","ECSS-E-ST-70-41_1330735",1,"Created","The time management service shall have access to the spacecraft time reference.","NOTE\tThis Standard does not specify how the on-board clock that provides the spacecraft time reference is implemented. It can, for example, be a free running counter or a clock synchronized to a GPS receiver.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.9.4.4b","Requirement","ECSS-E-ST-70-41_1330756",1,"Created","When the time report generation rate is changed, the time reporting subservice shall immediately use the new time report generation rate to determine the next transfer frame that triggers a sampling of the spacecraft time reference."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.4.3.2c","Requirement","ECSS-E-ST-70-41_1330781",1,"Created","For each valid instruction to enable the time-based schedule execution function, the time-based scheduling subservice shall:\n1.\tset the time-based schedule execution function status to \"enabled\".","NOTE\tEnabling the time-based schedule execution function does not depend on the presence of scheduled activities in the schedule.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.5.2.1d","Requirement","ECSS-E-ST-70-41_1330807",1,"Created","The time-based scheduling subservice shall reject any instruction to enable a time-based sub-schedule if:\n1.\tthat instruction refers to an unknown sub-schedule."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.6.2.1c","Requirement","ECSS-E-ST-70-41_1330828",1,"Created","Each instruction to create a time-based scheduling group shall contain:\n1.\tthe identifier of the group;\n2.\tthe group status at creation time."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.6.2.2a","Requirement","ECSS-E-ST-70-41_1330833",1,"Created","The time-based scheduling subservice shall provide the capability to delete time-based scheduling groups if the capability to create time-based scheduling groups is provided by that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[11,23] delete time-based scheduling groups\".\nNOTE 1\tFor the capability to create time-based scheduling groups, refer to clause 6.11.6.2.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.6.3.2f","Requirement","ECSS-E-ST-70-41_1330854",1,"Created","The time-based scheduling subservice shall process any valid instruction that is contained within a request to disable time-based scheduling groups regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.9.3a","Requirement","ECSS-E-ST-70-41_1330889",1,"Created","The time-based scheduling subservice capability to time-shift scheduled activities identified by request identifier shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[11,7] time-shift scheduled activities identified by request identifier\".\nNOTE 2\tThat capability implies that the subservice provides the capability to identify scheduled activities by request identifier (refer to requirement 6.11.9.1a).\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.9.4h","Requirement","ECSS-E-ST-70-41_1330905",1,"Created","For each valid request to Summary-report time-based scheduled activities identified by request identifier, the time-based scheduling subservice shall generate a single time-based schedule summary report that contains all related time-based schedule summary notifications.","NOTE\tThe time-based schedule summary report is specified in clause 6.11.7.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.10.3e","Requirement","ECSS-E-ST-70-41_1330926",1,"Created","For each request to delete the time-based scheduled activities identified by a filter that is rejected, the time-based scheduling subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.11.10.5c","Requirement","ECSS-E-ST-70-41_1330936",1,"Created","Each instruction to summary-report the time-based scheduled activities identified by a filter shall contain the filter to identify the scheduled activities to report consisting of:\n1.\ta time window, consisting of:\n(a)\tthe type of the time window that is one of \"select all\", \"from time tag\", \"to time tag\", \"from time tag to time tag\";\n(b)\tfor \"from time tag\" and \"from time tag to time tag\", the from time tag;\n(c)\tfor \"to time tag\" and \"from time tag to time tag\", the to time tag;\n2.\tif sub-schedules are supported, zero or more sub-schedules;\n3.\tif groups are supported, zero or more groups.","NOTE 1\tFor item 2, refer to requirement 6.11.4.1a.\nNOTE 2\tFor item 3, refer to requirement 6.11.4.1b.\nNOTE 3\tFor the filtering mechanism, including the interaction of the parts of the filter, refer to clause 6.11.10.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.2.3.1b","Requirement","ECSS-E-ST-70-41_1330953",1,"Created","The event reporting subservice that is associated to the on-board monitoring service shall be declared when specifying that on-board monitoring service."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.3.5.2a","Requirement","ECSS-E-ST-70-41_1330977",1,"Created","The parameter monitoring subservice shall provide the capability to disable the parameter monitoring function.","NOTE 1\tThe corresponding requests are of message type \"TC[12,16] disable the parameter monitoring function\".\nNOTE 2\tFor the capability to enable the parameter monitoring function, refer to clause 6.12.3.5.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.3.7a","Requirement","ECSS-E-ST-70-41_1331003",1,"Created","The parameter monitoring subservice shall provide the capability to report the contents of the check transition list.","NOTE\tThe corresponding reports are data reports of message type \"TM[12,12] check transition report\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.3.9.2d","Requirement","ECSS-E-ST-70-41_1331024",1,"Created","For each request to delete all parameter monitoring definitions that is rejected, the parameter monitoring subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.3.11a","Requirement","ECSS-E-ST-70-41_1331049",1,"Created","The parameter monitoring subservice capability to report the status of each parameter monitoring definition shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[12,13] report the status of each parameter monitoring definition\". The responses are data reports of message type \"TM[12,14] parameter monitoring definition status report\".\nNOTE 2\tThat capability requires the capability for that subservice to enable parameter monitoring definitions, refer to clause 6.12.3.6.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.4.3c","Requirement","ECSS-E-ST-70-41_1331070",1,"Created","For each functional monitoring definition, the functional monitoring subservice shall maintain a status indicating the result of the check performed.","NOTE 1\tThis status is named \"FMON checking status\".\nNOTE 1\tThe FMON checking status can have any of the following values: \"unchecked\", \"invalid\", \"running\" or \"failed\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.4.5.3b","Requirement","ECSS-E-ST-70-41_1331089",1,"Created","Each request to disable functional monitoring definitions shall contain one or more instructions to disable a functional monitoring definition."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.4.6.1g","Requirement","ECSS-E-ST-70-41_1331101",1,"Created","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"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.4.7.2e","Requirement","ECSS-E-ST-70-41_1331122",1,"Created","For each instruction to delete a functional monitoring definition that it rejects, the functional monitoring subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.12.4.9c","Requirement","ECSS-E-ST-70-41_1331136",1,"Created","For each valid instruction to report the status of each functional monitoring definition, the functional monitoring subservice shall:\n1.\tgenerate, for each functional monitoring definition in the FMON list, a single functional monitoring definition status notification that includes:\n(a)\tthe identifier of that functional monitoring definition;\n(b)\tif the functional monitoring subservice supports the capability for protecting functional monitoring definitions, its FMON protection status;\n(c)\tits FMON status;\n(d)\tits FMON checking status.","NOTE\tFor item 1(b), refer to requirement 6.12.4.6.1a.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.13.3.3.2a","Requirement","ECSS-E-ST-70-41_1331153",1,"Created","The receiving entity of the large packet downlink subservice shall have the capability to process all part reports that it receives.","NOTE\tThis process is called \"large packet acceptance and reconstruction process\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.13.4.3.2e","Requirement","ECSS-E-ST-70-41_1331174",1,"Created","The receiving entity of the large packet uplink subservice shall abort the uplink operation when the reception timer reaches the uplink reception timeout.","NOTE\tSee requirement 6.13.4.1c.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.2.4b","Requirement","ECSS-E-ST-70-41_1331199",1,"Created","Each diagnostic parameter report forward-control definition shall contain:\n1.\tthe identifier of the application process;\n2.\ta list of zero or more related diagnostic parameter report structure identifiers. ","NOTE 1\tAn empty diagnostic parameter report forward-control configuration (i.e. no diagnostic parameter report forward-control definition is defined) implies that the subservice blocks all diagnostic parameter reports.\nNOTE 1\tA diagnostic parameter report is forwarded to ground only if the application process forward-control configuration does not block that report and one of the following conditions occurs:\n·\ta diagnostic parameter report forward-control definition with no diagnostic parameter report structure identifiers is defined for the application process identifier of that report;\n·\ta diagnostic parameter report forward-control definition with a diagnostic parameter report structure identifier is defined for the application process identifier and the diagnostic parameter report structure identifier of that report.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.4.1j","Requirement","ECSS-E-ST-70-41_1331222",1,"Created","The real-time forwarding control subservice shall process any valid instruction that is contained within a request to add report types to the application process forward-control configuration regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.5.1a","Requirement","ECSS-E-ST-70-41_1331246",1,"Created","The real-time forwarding control subservice shall provide the capability to add structure identifiers to the housekeeping parameter report forward-control configuration if that subservice provides the capability to control, per housekeeping parameter report structure, the forwarding of housekeeping parameter reports.","NOTE 1\tThe corresponding requests are of message type \"TC[14,5] add structure identifiers to the housekeeping parameter report forward-control configuration\".\nNOTE 2\tFor the capability to control, per housekeeping parameter report structure, the forwarding of housekeeping parameter reports, refer to requirement 6.14.3.2.1a.\nNOTE 3\tFor the capability to delete structure identifiers from the housekeeping parameter report forward-control configuration, refer to clause 6.14.3.5.2. \n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.5.3d","Requirement","ECSS-E-ST-70-41_1331271",1,"Created","For each valid request to report the content of the housekeeping parameter report forward-control configuration, the real-time forwarding control subservice shall generate a single housekeeping parameter report forward-control configuration content report that includes all related housekeeping parameter report forward-control definition notifications."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.6.2i","Requirement","ECSS-E-ST-70-41_1331290",1,"Created","The real-time forwarding control subservice shall process any valid instruction that is contained within a request to delete structure identifiers from the diagnostic parameter report forward-control configuration regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.7.1a","Requirement","ECSS-E-ST-70-41_1331298",1,"Created","The real-time forwarding control subservice shall provide the capability to delete event definition identifiers from the event report blocking forward-control configuration if that subservice provides the capability to control, per event definition, the forwarding of event reports.","NOTE 1\tThe corresponding requests are of message type \"TC[14,13] delete event definition identifiers from the event report blocking forward-control configuration\". \nNOTE 1\tFor the capability to control, per event definition, the forwarding of event reports, refer to requirement 6.14.3.2.1c.\nNOTE 2\tFor the capability to add event definition identifiers to the event report blocking forward-control configuration, refer to clause 6.14.3.7.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.14.3.7.3d","Requirement","ECSS-E-ST-70-41_1331323",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.3.1b","Requirement","ECSS-E-ST-70-41_1331344",1,"Created","For each packet that it receives, the storage and retrieval subservice shall:\n1.\ttime stamp that packet;\n2.\tstore that time-stamped packet into the enabled stores that match the storage selection criteria for those stores."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.4.2i","Requirement","ECSS-E-ST-70-41_1331372",1,"Created","For each valid instruction to change the open retrieval start time tag of a packet store, the storage and retrieval subservice shall:\n1.\tset the open retrieval start time tag of the specified packet store to the value specified in the request."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.5.1b","Requirement","ECSS-E-ST-70-41_1331391",1,"Created","For each packet store managed by the storage and retrieval subservice, that subservice shall maintain a status indicating whether the by-time-range retrieval function of that packet store is enabled or disabled.","NOTE\tThis status is named \"packet store by-time-range retrieval status\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.5.2d","Requirement","ECSS-E-ST-70-41_1331396",1,"Created","The storage and retrieval subservice shall reject any instruction to start the by-time-range retrieval of a packet store if any of the following conditions occurs:\n1.\tthat instruction refers to a packet store that does not exist;\n2.\tthat subservice does not support concurrent retrieval requests executing in parallel and the packet store open retrieval status of that packet store is in-progress;\n3.\tthe retrieval start time in that instruction is later than the retrieval end time;\n4.\tthe storage time period of that instruction is fully in the past and the packet store contains no packet with a time stamp in that time period;\n5.\tthat instruction refers to a packet store whose by-time-range retrieval status is \"enabled\".","NOTE\tFor item 2, refer to requirement 6.15.3.1i.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.7.1h","Requirement","ECSS-E-ST-70-41_1331419",1,"Created","For each valid instruction to delete the content of all packet stores up to the specified time, the storage and retrieval subservice shall:\n1.\tfor each packet store maintained by that subservice, delete the contents of that packet store from the earliest packet in that store up to and including the last packet with a storage time less than or equal to the time specified in that request."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.8.4c","Requirement","ECSS-E-ST-70-41_1331443",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.3.9.3e","Requirement","ECSS-E-ST-70-41_1331468",1,"Created","For each request to change a packet store type to bounded that is rejected, the storage and retrieval subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.2.1a","Requirement","ECSS-E-ST-70-41_1331489",1,"Created","Whether the packet selection subservice provides the capability to control, per housekeeping parameter report structure, the storage of housekeeping parameter reports shall be declared when specifying that subservice.","NOTE 1\tSee clause 6.15.4.2.3.\nNOTE 2\tFor the housekeeping parameter reports, refer to clause 6.3.3.3.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.2.5c","Requirement","ECSS-E-ST-70-41_1331505",1,"Created","The maximum number of event definition identifiers that can be contained within an event report blocking storage-control definition shall be declared when specifying the packet selection subservice."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.4.1f","Requirement","ECSS-E-ST-70-41_1331520",1,"Created","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. "]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.4.2l","Requirement","ECSS-E-ST-70-41_1331541",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.5.2h","Requirement","ECSS-E-ST-70-41_1331573",1,"Created","For each instruction to delete an application process from 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. "]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.6.1i","Requirement","ECSS-E-ST-70-41_1331592",1,"Created","The packet selection subservice shall process any valid instruction that is contained within a request to add structure identifiers to the diagnostic parameter report storage-control configuration regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.7.1a","Requirement","ECSS-E-ST-70-41_1331613",1,"Created","The packet selection subservice shall provide the capability to add event definition identifiers to the event report blocking storage-control configuration of a packet store if that subservice provides the capability to control, per event definition, the storage of event reports.","NOTE 1\tThe corresponding requests are of message type \"TC[15,34] add event definition identifiers to the event report blocking storage-control configuration\".\nNOTE 1\tFor the capability to control, per event definition, the storage of event reports, refer to requirement 6.15.4.2.1c.\nNOTE 2\tFor the capability to delete event definition identifiers from the event report blocking storage-control configuration, refer to clause 6.15.4.7.2. \n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.15.4.7.3c","Requirement","ECSS-E-ST-70-41_1331638",1,"Created","Each instruction to report the content of the event report blocking control configuration shall include:\n1.\tthe packet store identifier of the packet store. "]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.2.2a","Requirement","ECSS-E-ST-70-41_1331659",1,"Created","For each on-board control procedure service that contains both, an OBCP management subservice and an OBCP engine management subservice, the two subservice providers shall be hosted by the same application process."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.3.2a","Requirement","ECSS-E-ST-70-41_1331665",1,"Created","The on-board control procedure service shall be able to collect the values of each on-board parameter that is accessible to the application processes that can be addressed by the on-board control procedure service.","NOTE\tThe accessible application processes are those specified by requirement 6.18.3.1a. \n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.4.4.3e","Requirement","ECSS-E-ST-70-41_1331690",1,"Created","The OBCP management subservice shall reject any request to load an OBCP by reference 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 already in the OBCP engine;\n3.\tthat request contains an instruction that refers to a file that does not exist;\n4.\tthat request contains an instruction that refers to a file that is not recognized as an OBCP file;\n5.\tthe on-board file determined by the loading policy does not exist;\n6.\tthe OBCP code in the file fails the checksum verification;\n7.\tthe OBCP cannot be loaded due to the lack of OBCP engine available resources."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.4.4.6b","Requirement","ECSS-E-ST-70-41_1331706",1,"Created","Each request to load by reference and activate an OBCP shall contain exactly one instruction to load by reference and activate an OBCP."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.4.4.10d","Requirement","ECSS-E-ST-70-41_1331737",1,"Created","For each request to abort all OBCPs and report that is rejected, the OBCP management subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.4.5.1c","Requirement","ECSS-E-ST-70-41_1331742",1,"Created","The OBCP management subservice shall reject any request to report the execution status of each OBCP if:\n1.\tthe OBCP engine is not running."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.4.6.3d","Requirement","ECSS-E-ST-70-41_1331763",1,"Created","The OBCP management subservice shall reject any request to activate and execute one OBCP step 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;\n3.\tthat request contains an instruction that refers to an observability level that is invalid;\n4.\tthat request contains an instruction that refers to an OBCP that is active."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.18.5.1.1a","Requirement","ECSS-E-ST-70-41_1331788",1,"Created","The OBCP engine management subservice shall provide the capability to start the OBCP engine.","NOTE 1\tThe corresponding requests are of message type \"TC[18,21] start the OBCP engine\".\nNOTE 2\tFor the capability to stop the OBCP engine, refer to clause 6.18.5.1.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.19.5.2b","Requirement","ECSS-E-ST-70-41_1331810",1,"Created","When the enabled event-action function detects the occurrence of an event that is used by an enabled event-action definition, the event-action subservice shall immediately trigger the related action.","NOTE 1\tTriggering an action implies releasing the associated request.\nNOTE 1\tOnce the action has been triggered and the request released, no change is made to the event-action status of that event-action definition, i.e. it remains enabled.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.19.8.1c","Requirement","ECSS-E-ST-70-41_1331835",1,"Created","Each instruction to add an event-action definition shall contain:\n1.\tthe system identifier of the event definition; \n2.\tthe action consisting of the request to release when the event report is detected.","NOTE\tFor the system identifier of the event definition, refer to requirement 6.19.4b.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.19.8.6a","Requirement","ECSS-E-ST-70-41_1331856",1,"Created","The event-action subservice capability to report event-action definitions shall be declared when specifying that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[19,10] report event-action definitions\". The responses are data reports of message type \"TM[19,11] event-action definition report\".\nNOTE 2\tThat capability requires the capability for that subservice to add event-action definitions, refer to clause 6.19.8.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.20.4.2e","Requirement","ECSS-E-ST-70-41_1331882",1,"Created","For each instruction to set a parameter value that it rejects, the parameter management subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.20.5.2a","Requirement","ECSS-E-ST-70-41_1331887",1,"Created","The parameter management subservice capability to change raw memory parameter definitions shall be declared when specifying that subservice.","NOTE\tThe corresponding requests are of message type \"TC[20,4] change raw memory parameter definitions\".\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.21.2.1.1a","Requirement","ECSS-E-ST-70-41_1331908",1,"Created","Each request sequencing service shall contain at least one request sequencing subservice."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.21.5.5e","Requirement","ECSS-E-ST-70-41_1331942",1,"Created","For each request to activate a request sequence that is rejected, the request sequencing subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.21.5.8d","Requirement","ECSS-E-ST-70-41_1331959",1,"Created","For each valid request to abort all request sequences and report, the request sequencing subservice shall generate a single aborted request sequence report that includes all related aborted request sequence notifications."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.2.2a","Requirement","ECSS-E-ST-70-41_1331980",1,"Created","Each application process shall host at most one position-based scheduling subservice provider."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.6.2b","Requirement","ECSS-E-ST-70-41_1331989",1,"Created","Each scheduled activity definition shall be identified by a scheduled activity identifier that corresponds to the identifier of the request contained in that definition.","NOTE\tFor the request identifier, refer to requirement 5.4.11.2.1c.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.6.6d","Requirement","ECSS-E-ST-70-41_1332011",1,"Created","For each request to insert activities into the position-based schedule that is rejected, the position-based scheduling subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.7.2.2a","Requirement","ECSS-E-ST-70-41_1332032",1,"Created","The position-based scheduling subservice shall provide the capability to disable position-based sub-schedules if the capability to enable position-based sub-schedules is provided by that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[22,21] disable position-based sub-schedules\".\nNOTE 2\tFor the capability to enable position-based sub-schedules, refer to clause 6.22.7.2.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.8.2.2f","Requirement","ECSS-E-ST-70-41_1332057",1,"Created","The position-based scheduling subservice shall process any valid instruction that is contained within a request to delete position-based scheduling groups regardless of the presence of faulty instructions."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.8.3.2h","Requirement","ECSS-E-ST-70-41_1332075",1,"Created","For each valid instruction to disable all position-based scheduling groups, the position-based scheduling subservice shall:\n1.\tfor each scheduling group maintained by that subservice, set the status of that group to \"disabled\"."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.11.2d","Requirement","ECSS-E-ST-70-41_1332104",1,"Created","The position-based scheduling subservice shall reject any instruction to delete a position-based scheduled activity identified by request identifier if:\n1.\tthat request identifier is unknown."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.11.3b","Requirement","ECSS-E-ST-70-41_1332109",1,"Created","Each request to position-shift scheduled activities identified by request identifier shall contain:\n1.\ta delta position,\n2.\tone or more instructions to position-shift a scheduled activity identified by request identifier.","NOTE\tThe delta position in a request to position-shift scheduled activities identified by request identifier applies to all the instructions in that request.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.12.3c","Requirement","ECSS-E-ST-70-41_1332143",1,"Created","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"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.22.12.5d","Requirement","ECSS-E-ST-70-41_1332156",1,"Created","The position-based scheduling subservice shall reject any request to summary-report the position-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 position window type;\n2.\tthat request contains an instruction that refers to a \"from position tag\" that is greater than a \"to position tag\"."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.4.1.1a","Requirement","ECSS-E-ST-70-41_1332177",1,"Created","The file handling subservice shall provide the capability to create a file.","NOTE 1\tThe corresponding requests are of message type \"TC[23,1] create a file\".\nNOTE 2\tFor the capability to delete a file, refer to clause 6.23.4.1.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.4.3.2a","Requirement","ECSS-E-ST-70-41_1332202",1,"Created","The file handling subservice shall provide the capability to unlock a file if the capability to lock a file is provided by that subservice.","NOTE 1\tThe corresponding requests are of message type \"TC[23,6] unlock a file\".\nNOTE 2\tFor the capability to lock a file, refer to clause 6.23.4.3.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.4.5.2b","Requirement","ECSS-E-ST-70-41_1332225",1,"Created","The type of directory deletion provided by the file handling subservice shall be declared when specifying that subservice."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.4.5.2f","Requirement","ECSS-E-ST-70-41_1332229",1,"Created","For each request to delete a directory that is rejected, the file handling subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.5.2.2e","Requirement","ECSS-E-ST-70-41_1332254",1,"Created","For each request to copy a file that is rejected, the file copy subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.5.3.1e","Requirement","ECSS-E-ST-70-41_1332272",1,"Created","For each instruction to suspend a file copy operation that it rejects, the file copy subservice shall generate the failed start of execution notification for that instruction."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","6.23.5.4.2e","Requirement","ECSS-E-ST-70-41_1332301",1,"Created","For each request to abort all file copy operations involving a repository path that is rejected, the file copy subservice shall generate a failed start of execution notification."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","7.3.3b","Requirement","ECSS-E-ST-70-41_1332329",1,"Created","The PFCs specified in Table 7-3 shall be used for packet fields carrying enumerated values."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","7.3.8e","Requirement","ECSS-E-ST-70-41_1332358",1,"Created","For each packet field containing a fixed-length octet-string whose length is deduced, the definition used to deduce that length shall be declared when specifying the related packet field type. ","NOTE\tThe deduced length corresponds to a fixed length PFC.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","7.3.10c","Requirement","ECSS-E-ST-70-41_1332371",1,"Created","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"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","7.4.3.1j","Requirement","ECSS-E-ST-70-41_1332395",1,"Created","The PFC of the time field of telemetry packets shall be declared when specifying the time service used by the spacecraft.","NOTE\tFor the time service, refer to clause 6.9.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.1.1a","Requirement","ECSS-E-ST-70-41_1332419",1,"Created","Each packet transporting a request verification report shall be of service type 1."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.2.2.4b","Requirement","ECSS-E-ST-70-41_1332458",1,"Created","For each telecommand packet transporting a request to distribute register dump commands, the application data field shall have the structure specified in Figure 8-13."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.3.2.5a","Requirement","ECSS-E-ST-70-41_1332494",1,"Created","Each telecommand packet transporting a request to enable the periodic generation of housekeeping parameter reports shall be of message subtype 5. ","NOTE\tFor the corresponding system requirements, refer to clause 6.3.3.4.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.3.2.5b","Requirement","ECSS-E-ST-70-41_1332495",1,"Created","For each telecommand packet transporting a request to enable the periodic generation of housekeeping parameter reports, the application data field shall have the structure specified in Figure 8-25."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.3.2.18a","Requirement","ECSS-E-ST-70-41_1332533",1,"Created","Each telecommand packet transporting a request to append parameters to a diagnostic parameter report structure shall be of message subtype 30. ","NOTE\tFor the corresponding system requirements, refer to clause 6.3.4.10.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.3.2.25b","Requirement","ECSS-E-ST-70-41_1332555",1,"Created","For each telecommand packet transporting a request to apply parameter functional reporting configurations, the application data field shall have the structure specified in Figure 8-45."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.4.2.7c","Requirement","ECSS-E-ST-70-41_1332602",1,"Created","To delete all parameter statistics definitions, N shall be set to 0."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.6.2.1a","Requirement","ECSS-E-ST-70-41_1332635",1,"Created","Each telecommand packet transporting a request to load object memory data shall be of message subtype 1. ","NOTE\tFor the corresponding system requirements, refer to clause 6.6.4.4.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.6.2.6b","Requirement","ECSS-E-ST-70-41_1332651",1,"Created","For each telemetry packet transporting a dumped raw memory data report, the source data field shall have the structure specified in Figure 8-71."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.6.2.14b","Requirement","ECSS-E-ST-70-41_1332674",1,"Created","For each telecommand packet transporting a request to disable the scrubbing of a memory, the application data field shall have the structure specified in Figure 8-78."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.9.1b","Requirement","ECSS-E-ST-70-41_1332705",1,"Created","The spacecraft time packets shall not have any packet secondary header field.","NOTE\tThe spacecraft time packets are specified clauses 6.9.4.2 and 6.9.4.3. See also requirement 7.4.3.1a.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.11.2.11b","Requirement","ECSS-E-ST-70-41_1332746",1,"Created","For each telecommand packet transporting a request to detail-report the time-based scheduled activities identified by a filter, the application data field shall have the structure specified in Figure 8-98."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.11.2.21a","Requirement","ECSS-E-ST-70-41_1332773",1,"Created","Each telecommand packet transporting a request to disable time-based sub-schedules shall be of message subtype 21. ","NOTE\tFor the corresponding system requirements, refer to clause 6.11.5.2.2.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.12.1a","Requirement","ECSS-E-ST-70-41_1332803",1,"Created","Each packet transporting an on-board monitoring message shall be of service type 12."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.12.2.8b","Requirement","ECSS-E-ST-70-41_1332840",1,"Created","For each telecommand packet transporting a request to report parameter monitoring definitions, the application data field shall have the structure specified in Figure 8-123."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.12.2.14a","Requirement","ECSS-E-ST-70-41_1332863",1,"Created","Each telemetry packet transporting a parameter monitoring definition status report shall be of message subtype 14. ","NOTE\tFor the corresponding system requirements, refer to clause 6.12.3.11.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.12.2.19b","Requirement","ECSS-E-ST-70-41_1332875",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.12.3.2c","Requirement","ECSS-E-ST-70-41_1332914",1,"Created","The values of the FMON checking status shall be as specified in Table 8-13."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.13.2.7b","Requirement","ECSS-E-ST-70-41_1332932",1,"Created","For each telemetry packet transporting a large packet uplink abortion report, the source data field shall have the structure specified in Figure 8-146."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.14.2.9b","Requirement","ECSS-E-ST-70-41_1332971",1,"Created","For each telecommand packet transporting a request to add structure identifiers to the diagnostic parameter report forward-control configuration, the application data field shall have the structure specified in Figure 8-153."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.14.2.10d","Requirement","ECSS-E-ST-70-41_1332978",1,"Created","To delete an application process from the diagnostic parameter report forward-control configuration, N2 shall be set to 0."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.15.2.1b","Requirement","ECSS-E-ST-70-41_1333003",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.15.2.9b","Requirement","ECSS-E-ST-70-41_1333035",1,"Created","For each telecommand packet transporting a request to summary-report the content of packet stores, the application data field shall have the structure specified in Figure 8-167."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.15.2.18b","Requirement","ECSS-E-ST-70-41_1333066",1,"Created","For each telecommand packet transporting a request to delete packet stores, the application data field shall have the structure specified in Figure 8-175."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.15.2.28c","Requirement","ECSS-E-ST-70-41_1333101",1,"Created","To add all structure identifiers to the diagnostic parameter report storage-control configuration, N2 shall be set to 0."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.15.2.36a","Requirement","ECSS-E-ST-70-41_1333128",1,"Created","Each telecommand packet transporting a request to report the content of the event report blocking storage-control configuration shall be of message subtype 39. ","NOTE\tFor the corresponding system requirements, refer to clause 6.15.4.7.3.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.18.2.5b","Requirement","ECSS-E-ST-70-41_1333166",1,"Created","For each telecommand packet transporting a request to suspend an OBCP, the application data field shall have the structure specified in Figure 8-200."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.18.2.7b","Requirement","ECSS-E-ST-70-41_1333173",1,"Created","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."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.18.2.19b","Requirement","ECSS-E-ST-70-41_1333208",1,"Created","For each telecommand packet transporting a request to start the OBCP engine, the application data field shall be omitted."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.19.3a","Requirement","ECSS-E-ST-70-41_1333246",1,"Created","The values of the event-action function status shall be as specified in Table 8-19."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.20.2.7d","Requirement","ECSS-E-ST-70-41_1333273",1,"Created","For base plus offset addressing scheme, the addressing scheme dependent address field of the parameter definition report shall have the structure specified in Figure 8-227."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.21.2.10a","Requirement","ECSS-E-ST-70-41_1333304",1,"Created","Each telemetry packet transporting a request sequence checksum report shall be of message subtype 10. ","NOTE\tFor the corresponding system requirements, refer to clause 6.21.7.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.21.2.14a","Requirement","ECSS-E-ST-70-41_1333315",1,"Created","Each telemetry packet transporting an aborted request sequence report shall be of message subtype 14. ","NOTE\tFor the corresponding system requirements, refer to clause 6.21.5.8.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.22.2.9b","Requirement","ECSS-E-ST-70-41_1333345",1,"Created","For each telecommand packet transporting a request to detail-report position-based scheduled activities identified by request identifier, the application data field shall have the structure specified in Figure 8-245."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.22.2.20a","Requirement","ECSS-E-ST-70-41_1333374",1,"Created","Each telecommand packet transporting a request to enable position-based sub-schedules shall be of message subtype 20. ","NOTE\tFor the corresponding system requirements, refer to clause 6.22.7.2.1.\n"]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.22.3c","Requirement","ECSS-E-ST-70-41_1333409",1,"Created","The values of the position window type shall be as specified in Table 8-25."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.23.2.5b","Requirement","ECSS-E-ST-70-41_1333428",1,"Created","For each telecommand packet transporting a request to lock a file, the application data field shall have the structure specified in Figure 8-265."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.23.2.22b","Requirement","ECSS-E-ST-70-41_1333479",1,"Created","For each telecommand packet transporting a request to enable the periodic reporting of the file copy status, the application data field shall have the structure specified in Figure 8-282."]
["ECSS-E-ST-70-41C","ECSS - Current v0.9","8.23.3a","Requirement","ECSS-E-ST-70-41_1333486",1,"Created","The values of the operation status shall be as specified in Table 8-27."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","4.3.2b","Requirement","ECSS-E-ST-60-21_1350014",1,"Created","The start-up requirement shall be tested over the whole range of operational temperatures and dynamics."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","4.6.1a","Requirement","ECSS-E-ST-60-21_1350028",1,"Created","A transformation matrix shall be provided by the supplier."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","4.11.1b","Requirement","ECSS-E-ST-60-21_1350053",1,"Created","The anti-aliasing filter frequency shall be defined by the customer.","NOTE\tAnti-aliasing filter performances are defined in clause 5.4.10. \n"]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.2d","Requirement","ECSS-E-ST-60-21_1350074",1,"Created","The test success criteria shall be derived from the customer requirements taking into account the test setup error budget."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.2.2.3d","Requirement","ECSS-E-ST-60-21_1350096",1,"Created","The bias 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 requirements can be combined into a single specification.\n"]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.2.2.5c","Requirement","ECSS-E-ST-60-21_1350101",1,"Created","The operating temperature range and the thermal gradient, spatial or temporal, shall be specified as generic environmental conditions."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.4.2.1b","Requirement","ECSS-E-ST-60-21_1350126",1,"Created","The uncompensated scale factor initial value shall be specified by the customer."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.4.3d","Requirement","ECSS-E-ST-60-21_1350143",1,"Created","The scale factor estimate shall be processed using an external precise time reference ","NOTE\tThe external time reference is usually provided by the test facility.\n"]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.5.3a","Requirement","ECSS-E-ST-60-21_1350173",1,"Created","The measurement of the alignment errors shall be performed via ground test with a motion table. "]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.8.3a","Requirement","ECSS-E-ST-60-21_1350195",1,"Created","The warm-up performance requirements shall be verified by test."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","5.4.10.1a","Requirement","ECSS-E-ST-60-21_1350200",1,"Created","The anti-aliasing filter requirement shall be consistent with the sampling requirement and the output bandwidth requirement."]
["ECSS-E-ST-60-21C","ECSS - Current v0.9","A.2.1<4>b","Requirement","ECSS-E-ST-60-21_1350223",1,"Created","The outputs of the FMM shall include as a minimum:\n1.\tthe measured angular rate and time delivered by the gyro;\n2.\tthe gyro health status."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.1.3c","Requirement","ECSS-E-ST-31-02_1190016",2,"Normative Change","To ensure the uniqueness of a specification, requirement 8.2.5a of ECSS-E-ST-10-06 shall apply. "]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.4c","Requirement","ECSS-E-ST-31-02_1190036",1,"Unchanged","The qualification process shall be structured according to Figure 5-1."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.5.4.2a","Requirement","ECSS-E-ST-31-02_1190063",1,"Unchanged","Equipment for which a delta qualification programme is required as per Table 5-1 shall undergo a delta qualification programme, which is a subset of the full qualification programme of clause 5.5.4.1."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.6.5b","Requirement","ECSS-E-ST-31-02_1190091",2,"Normative Change","Pressure shall be generated on the sealed unit by increasing the temperature of the unit and thus the saturation pressure of the heat carrier fluid.","NOTE\t1\tThis test is called hot proof pressure test.\nNOTE\t2\tWhen the pressure target leads to a temperature higher than the critical temperature then the cold pressure test (before unit sealing) can be considered to reach the proof pressure requirement and a reduced proof factor can be accepted for the hot pressure test on the sealed unit.\n"]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.6.5c","Requirement","ECSS-E-ST-31-02_1190092",1,"Unchanged","In cases where proof pressure test is not feasible, margins against mechanical failure shall be verified by analysis in accordance with ECSS-E-ST-32-02."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.6.9.2.2a","Requirement","ECSS-E-ST-31-02_1190117",1,"Unchanged","The maximum heat transport capability shall be measured for tilt heights from zero to a value at which the heat transport capability falls to a value <5 % of the maximum heat transport capability (at the test temperature)."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","5.6.14.2a","Requirement","ECSS-E-ST-31-02_1190151",2,"Normative Change","CCHP shall be tested according to requirements 5.6.9.2.1a.1, 5.6.9.2.1a.2, 5.6.9.2.1a.3 and 5.6.9.2.1a.4 for one selected configuration [(a), (b) or (c)]."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","6.1a","Requirement","ECSS-E-ST-31-02_1190271",1,"Created","Only the TPHTE whose design has been previously qualified according to clause 5 shall be submitted to the acceptance."]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","A.2.1<4>a","Requirement","ECSS-E-ST-31-02_1190172",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","B.2.1<5>a","Requirement","ECSS-E-ST-31-02_1190182",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","C.2.1<5>b","Requirement","ECSS-E-ST-31-02_1190199",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","F.2.1<3>a","Requirement","ECSS-E-ST-31-02_1190224",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-31-02C Rev.1","ECSS - Current v0.9","G.2.1<4>b","Requirement","ECSS-E-ST-31-02_1190245",2,"Deleted","<<deleted>>"]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.2.1a","Requirement","ECSS-E-ST-33-11_0280005",1,"Unchanged","In case of redundancy, no component shall adversely affect its substitute."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.2.5.3f","Requirement","ECSS-E-ST-33-11_0280033",2,"Normative Change","KMP shall include an “Explosive factor” for uncertainties on the behaviour of explosive materials in the mission profile and its use configuration.","NOTE\t1\tThe uncertainties can be related to ageing, radiations, temperature influence, batch influence,  and chemical compatibility, for example material, gases and humidity.\nNOTE\t2\tUse configuration can be, for example, loading density, confinement and thermal exchanges.\n"]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.5.2.1f","Requirement","ECSS-E-ST-33-11_0280058",1,"Unchanged","Stray circuits or coupling which can result in unintentional firing shall be avoided."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.5.2.5b","Permission","ECSS-E-ST-33-11_0280422",1,"Created","The fire function may be used to activate several of explosive devices."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.7.2d","Requirement","ECSS-E-ST-33-11_0280085",1,"Unchanged","Each interface shall sustain without degradation in both coupled and separated states\n1.\tthe assembly and dismantling duty-cycle, and\n2.\tthe operational and environmental conditions of the application."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.8.2.4a","Requirement","ECSS-E-ST-33-11_0280109",2,"Normative Change","The explosive subsystem power, command, and control electrical circuitry shall limit the generation of electromagnetic fields or conducted noise to a level at least 20 dB below the no-fire power rating. "]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.8.2.12b","Requirement","ECSS-E-ST-33-11_0280133",2,"Normative Change","The supplier shall provide the customer with the magnetic properties of the explosive devices."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.9b","Requirement","ECSS-E-ST-33-11_0280155",1,"Unchanged","Continued exposure to the expected environmental conditions shall not cause degradation or increased sensitivity in excess of agreed limits."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.9e","Requirement","ECSS-E-ST-33-11_0280158",2,"Normative Change","Age-sensitive materials shall only be used where degradation causes no loss of explosive subsystem performance beyond limits agreed with the end-user."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.10.3b","Requirement","ECSS-E-ST-33-11_0280178",1,"Unchanged","Isolators shall provide 20 dB attenuation at the specified electromagnetic frequencies."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.10.9a","Requirement","ECSS-E-ST-33-11_0280201",2,"Normative Change","The arm plug shall:\n1.\tprovide electrical continuity between the supply and firing circuits with electrical properties in any line agreed with the customer,\n2.\tbe compatible with the safe and arm connector,\n3.\tbe scoop-proof,\n4.\tbe lockable,\n5.\tbe visibly identified.","NOTE\t1\tElectrical properties include resistance, isolation, bonding, and Faraday protection.\nNOTE\t2\tExamples of lockable arming plugs are sub-D connector, bayonet or triple-start thread types.\n"]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.11.1.1b","Requirement","ECSS-E-ST-33-11_0280230",2,"Normative Change","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"]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.11.2.5b","Requirement","ECSS-E-ST-33-11_0280251",1,"Unchanged","Under the conditions in column E of Table 4-7, 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)."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.11.7b","Requirement","ECSS-E-ST-33-11_0280272",2,"Normative Change","Under the conditions in column E of Table 4-13, the property in column A in the units in column B shall be between the values in column C (maximum) and column D (minimum)."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.12.2b","Requirement","ECSS-E-ST-33-11_0280288",1,"Unchanged","Re-settable separation nuts shall include a means of verifying that the nut is properly reset before and after its mating bolt or stud installation and torquing."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.12.6c","Requirement","ECSS-E-ST-33-11_0280303",1,"Unchanged","The type of valve NO or NC shall be marked on the device."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.14.3.1d","Requirement","ECSS-E-ST-33-11_0280328",1,"Unchanged","Acceptance tests shall be done at identical limit conditions and levels, whatever the application, to ensure valid reference to previous results and to reduce the numbers of tested items. "]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.15.2e","Requirement","ECSS-E-ST-33-11_0280356",1,"Unchanged","Containers shall not be exposed to environments exceeding those specified. ","NOTE\tIt is good practice to use thermal and shock sensors.\n"]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.15.4h","Requirement","ECSS-E-ST-33-11_0280373",1,"Unchanged","Site safety regulations, provisions and procedures shall be checked for adequacy for explosive activities."]
["ECSS-E-ST-33-11C Rev.1","ECSS - Current v0.9","4.16.1e","Requirement","ECSS-E-ST-33-11_0280378",1,"Unchanged","Diagrams or photographs of consoles and installations shall be provided. "]
["ECSS-E-ST-31-04C","ECSS - Current v0.9","5.3f","Requirement","ECSS-E-ST-31-04_1370006",1,"Created","If a STEP-TAS reader encounters an invalid entity in the input dataset, the reader shall emit appropriate diagnostic messages."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.2b","Requirement","ECSS-E-ST-50-11_1410024",1,"Created","To ensure DC balancing of the transmitted signal, account shall be kept of the current running disparity in the transmitter."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.3.2a","Requirement","ECSS-E-ST-50-11_1410037",1,"Created","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."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.3.7e","Requirement","ECSS-E-ST-50-11_1410062",1,"Created","The Inverse INIT2 control word shall not be generated by the SpaceFibre port.","NOTE\tThe Inverse INIT2 is formed when the PCB layout in a SpaceFibre transmitter or receiver crosses over the two signals, CML+ and CML-, making up the differential signal.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.3.9b","Requirement","ECSS-E-ST-50-11_1410074",1,"Created","The second symbol in the STANDBY control word shall be the Lane Layer Control Word, LLCW, identifier, which has the value D14.6 and identifies the control word as being a control word generated and used by the Lane layer."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.5.1.3c","Requirement","ECSS-E-ST-50-11_1410109",1,"Created","The second symbol in the SDF control word shall identify the control word as being an SDF control word, and has the value D16.2."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.5.1.4c","Requirement","ECSS-E-ST-50-11_1410114",1,"Created","The second symbol in the EDF control word shall be a data symbol with any value from D0.0 to D31.7 and encode a data character containing the Sequence Number of the current data frame."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.5.3.2a","Requirement","ECSS-E-ST-50-11_1410142",1,"Created","ACK control word shall be used to indicate that a data frame, FCT, or broadcast frame has been received without error and in the correct order."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.6a","Requirement","ECSS-E-ST-50-11_1410161",1,"Created","The receive error indication control word shall be used by the Lane layer to indicate that a disparity error, invalid code error or other form of error was detected in the received data stream.","NOTE\tThe receive error indication control word is not sent over the SpaceFibre link. It is used within the receiver to indicate to higher protocol layers that an error has occurred. The receive error indication control word is illustrated in Table 5-8.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.8.2e","Requirement","ECSS-E-ST-50-11_1410186",1,"Created","The virtual channel, (VC), field in the start of data frame, SDF, shall identify the VC sending the data frame and into which it is received, as specified in 5.3.5.1.3d."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.8.4f","Requirement","ECSS-E-ST-50-11_1410207",1,"Created","The B_TYPE field shall contain a broadcast type, which indicates the type of broadcast message and the meaning of the subsequent eight data bytes."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.10g","Requirement","ECSS-E-ST-50-11_1410228",1,"Created","An ALIGN control word shall be able to be inserted within a broadcast, data or idle frame."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.3.10q","Requirement","ECSS-E-ST-50-11_1410238",1,"Created","While any broadcast frames in the error recovery buffer are being resent, new broadcast frames cannot be sent and shall wait for the error recovery buffer to finish resending any broadcast frames it contains.","NOTE\tSee clause 5.7.7 for details of error recovery.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.2.2a","Recommendation","ECSS-E-ST-50-11_1410261",1,"Created","A serial loopback facility should be provided in the SpaceFibre port for test purposes."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.3.2h","Requirement","ECSS-E-ST-50-11_1410279",1,"Created","For data signalling rates in the range 1 Gbit/s to 3,125 Gbit/s, the serial eye pattern mask shall have the intervals specified in Table 5-14.","NOTE\tThe near-end values are measured at the transmitter outputs and the far-end values are measured at the receiver inputs.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.4.3.1a","Requirement","ECSS-E-ST-50-11_1410315",1,"Created","For flight equipment and cable assemblies, Type-A connections conforming to ESCC Specification 3409/001 shall be used."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.4.4.4e","Permission","ECSS-E-ST-50-11_1410342",1,"Created","A Type-B flight cable assembly may use different kinds of connector at each end of the cable assembly."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.4.5.1a","Requirement","ECSS-E-ST-50-11_1410348",1,"Created","For electrical ground support equipment, EGSE, external serial ATA connectors shall be used as specified in Serial ATA Revision 3.0:2009, clause 6.5.1."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.4.6.4g","Requirement","ECSS-E-ST-50-11_1410376",1,"Created","The Type-D EGSE cable assembly shall use the cable specified in clause 5.4.4.6.3."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.5.3h","Requirement","ECSS-E-ST-50-11_1410401",1,"Created","The fibre optic receiver shall have a sensitivity as specified in Table 5-28 or Table 5-29 according to its operating data rate.","NOTE\tIt is quite difficult to have one design that is truly optimized for a wide range of data rates. Table 5-28 provides values for individually-optimized receiver units. Note that the electrical differential output requirements for the fibre optic receiver are defined in clause 5.4.3.2.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.4.6.2.4a","Requirement","ECSS-E-ST-50-11_1410429",1,"Created","Male connectors conforming to clause 5.4.6.2.2 shall be used on Type-B flight fibre optic cable assemblies."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.1b","Requirement","ECSS-E-ST-50-11_1410453",1,"Created","For a single lane link, the Lane layer shall receive data words and Data Link layer control words from the Data Link layer. "]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.2.5b","Recommendation","ECSS-E-ST-50-11_1410479",1,"Created","When in the Disabled state the Lane Initialisation state machine should disable the transmitter driver, receiver and related receive clock-data recovery (CDR)."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.2.5c","Requirement","ECSS-E-ST-50-11_1410480",1,"Created","The Lane Initialisation state machine shall leave the Disabled 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 LaneStart or AutoStart is asserted, move to the Wait state."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.2.10a","Requirement","ECSS-E-ST-50-11_1410505",1,"Created","The Lane Initialisation state machine shall enter the Connected state on one of the following conditions:\n1.\tFrom the Connecting state, when FarEndActive is asserted. \n2.\tFrom the Connecting state, when RxOnly is asserted. \n3.\tFrom the Connecting state, when three INIT2 control words are received without any intervening RXERR control words. \n4.\tFrom the Connecting state, when three INIT3 control words are received with the same initialisation parameters and without intervening RXERR control words."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.5d","Requirement","ECSS-E-ST-50-11_1410535",1,"Created","When enabled, the far-end parallel loopback shall replace the words in the transmit stream, with the words from the receive stream after data rate adjustment."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.5.7j","Requirement","ECSS-E-ST-50-11_1410552",1,"Created","If a disparity error occurs, it shall be indicated to the receive synchronisation state machine and the current symbol set to Rx Error, K0.0."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.1m","Requirement","ECSS-E-ST-50-11_1410577",1,"Created","The Multi-Lane layer shall report far-end capability information for all lanes, which is received in the INIT3 Capability field, to the Data Link layer."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.2a","Requirement","ECSS-E-ST-50-11_1410582",1,"Created","A multi-lane SpaceFibre link shall contain two or more lanes that operate together to provide greater bandwidth than a single lane can provide."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.4.4a","Requirement","ECSS-E-ST-50-11_1410604",1,"Created","Each PRBS data word in an idle frame shall be replicated and sent over all data-sending lanes in the same sending row."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.6.4b","Requirement","ECSS-E-ST-50-11_1410629",1,"Created","Each alignment FIFO shall be able to store three or four words.","NOTE\tA row with ALIGNs is sent one in 8 words. Limiting the size of the alignment FIFO to less than 8 words avoids mixing the reception of ALIGNs sent in different rows. Typical skew is 1 or 2 words maximum.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.8b","Requirement","ECSS-E-ST-50-11_1410650",1,"Created","One end of a unidirectional link shall be transmit only and the other end of that link receive only.","NOTE\tA multi-lane link incorporating some unidirectional lanes is illustrated in Figure 5-38.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.6.10e","Requirement","ECSS-E-ST-50-11_1410668",1,"Created","If the number of active transmitting lanes is greater than the value of the “maximum number of data-sending lanes” configuration parameter, the active transmitting lanes shall be configured as follows:\n1.\tThe active transmitting lanes with the lowest lane numbers are data-sending lanes, where the number of data-sending lanes is the maximum specified in the “maximum number of data-sending lanes” configuration parameter.\n2.\tThe other active transmitting lanes, with higher lane numbers, are hot redundant lanes."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.2.2h","Recommendation","ECSS-E-ST-50-11_1410701",1,"Created","A continuous mode of operation should be included which is activated individually for each virtual channel by a configuration parameter, Continuous Mode (VC)."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.3.2e","Requirement","ECSS-E-ST-50-11_1410722",1,"Created","If an input virtual channel buffer overflows, the SpaceFibre link shall be reset and an error reported.","NOTE\tAn input virtual channel buffer should never overflow. This condition indicates a fatal error for which the only option is to reset the link.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.4.3g","Requirement","ECSS-E-ST-50-11_1410736",1,"Created","A virtual channel that is not scheduled in the current time-slot shall not be allowed to compete for sending data over the link."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.4.5e","Requirement","ECSS-E-ST-50-11_1410749",1,"Created","A virtual channel shall be allocated a portion of the Link Bandwidth that it expects to use, its Normalised Expected Bandwidth, which includes the overhead due to the use of frame delimiters and other control words.","NOTE\t1\tThis information is provided, using management parameters, for all virtual channels regardless of the quality of service they are providing.\nNOTE\t2\tThe Normalised Expected Bandwidth assigned to each virtual channel has to account for any protocol overhead. When data is being sent in one direction only, the transmit side sends SDF-DATA-EDF, the receive side sends FCT-ACK, the transmit side replies with an ACK to the receive side FCT. This means that the best-case protocol overhead for unidirectional transmission is: 2+1/64+2+1 ~ 4% or 64/64+2+1 ~ 96% of effective bandwidth. For a link with a data signalling rate of 2,5 Gbit/s this results in a maximum user data throughput of 1,91 Gbit/s. When data is being sent in both directions at the same time, the transmit side sends the following control words in addition to those sent over a unidirectional link: an ACK for the receive-side data frame and its corresponding FCT to allocate more data space. This means that the best-case protocol overhead for bidirectional transmission is: 2+1+2/64+2+1+2 ~ 7% or 64/64+2+1+2 ~ 93% of effective bandwidth. For a link with a data signalling rate of 2,5 Gbit/s this results in a maximum user data throughput of 1,86 Gbit/s. When sending small data frames or many broadcast messages, the overhead can be higher.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.5c","Requirement","ECSS-E-ST-50-11_1410774",1,"Created","The Broadcast Bandwidth Credit Counter shall monitor and control the aggregate bandwidth of all the broadcast channels."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.6.2.3e","Requirement","ECSS-E-ST-50-11_1410799",1,"Created","The initial seed value 0xFFFF shall be used to calculate the first idle word after link reset. ","NOTE\tAfter link reset, the first idle frame contains the values specified in Figure 5-43.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.6.3.2j","Requirement","ECSS-E-ST-50-11_1410822",1,"Created","When an EDF, EBF, SIF, FCT, or FULL control word with a valid CRC passes into the Data Link layer from the Lane or Multi-Lane layer, its Sequence Number, SEQ_NUM, shall be checked against the current value of the Receive Sequence Counter and Receive Polarity Flag."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.6.3.2n","Requirement","ECSS-E-ST-50-11_1410826",1,"Created","If the Sequence Count of the SEQ_NUM of a received EDF, EBF or FCT is not one more than 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 data frame, FCT or broadcast frame shall be discarded.","NOTE\tA sequence error occurs when the Sequence Count in a SEQ_NUM of a data frame, broadcast frame or FCT is not one more, using modulo 128 arithmetic, than the value in the Receive Sequence Counter or the polarity flag is different. It also occurs when the Sequence Number of an idle frame or FULL control word does not match the value of the Receive Sequence Number. See clause 5.7.7.2.2 for information on what happens when a sequence error occurs. See clause 5.7.7.3 for more information about the value of the polarity flag of the Receive Sequence Number.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.6.6c","Requirement","ECSS-E-ST-50-11_1410851",1,"Created","The start of idle frame control word shall be followed by a series of pseudo-random data words which forms a pseudo random bit sequence when transmitted as specified in clause 5.7.6.2.3."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.7.1l","Requirement","ECSS-E-ST-50-11_1410869",1,"Created","The number of error recovery attempts shall be cleared by power-on reset or interface reset, or by command from the Management Information Base."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.7.3.2a","Requirement","ECSS-E-ST-50-11_1410898",1,"Created","The Valid Positive state shall be entered on the following conditions:\n1.\tLinkReset command.\n2.\tFrom the Error Positive state, when an ACK is requested to be sent."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.7.8.4b","Requirement","ECSS-E-ST-50-11_1410919",1,"Created","When in the RxBroadcastFrame state the Data Word Identification state machine shall initiate the following actions:\n1.\tIndicate that data words being received belong to a broadcast frame.\n2.\tCount the number of data words being received in the broadcast frame."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.1a","Requirement","ECSS-E-ST-50-11_1410944",1,"Created","The SpaceFibre network layer shall transfer SpaceFibre packets, and broadcast messages over a SpaceFibre network.","NOTE\tThe interfaces to and from the Network layer are illustrated in Figure 5-51.\n"]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.1h","Requirement","ECSS-E-ST-50-11_1410951",1,"Created","The Network layer shall pass the current time-slot to the Data Link layer."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.3f","Requirement","ECSS-E-ST-50-11_1410971",1,"Created","Packets shall be sent from an application through an end-point and across a virtual network."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.4c","Requirement","ECSS-E-ST-50-11_1410996",1,"Created","A link shall contain two or more virtual channels."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.8.1l","Requirement","ECSS-E-ST-50-11_1411023",1,"Created","A port shall have a maximum of 32 virtual channels."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.8.3f","Requirement","ECSS-E-ST-50-11_1411044",1,"Created","The connection between a virtual channel in an input port and a virtual channel in an output port shall not change until the packet that is currently being transmitted has finished being sent or is terminated following an error. "]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.8.3k","Requirement","ECSS-E-ST-50-11_1411049",1,"Created","If the specified output port does not have a virtual channel with the same virtual network number as that on which the packet arrived in the input port, the packet shall be discarded and an invalid output port error recorded by the routing switch."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.9.2f","Recommendation","ECSS-E-ST-50-11_1411070",1,"Created","A SpaceFibre routing switch should support logical addressing."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.8.13h","Requirement","ECSS-E-ST-50-11_1411106",1,"Created","A SpaceFibre node shall support virtual network number VN0 and at least one other virtual network."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","5.9.3c","Requirement","ECSS-E-ST-50-11_1411121",1,"Created","The configuration parameters shall be set to the value provided in Table 5-36 upon power-on or interface reset."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","6.2.3.2.4a","Requirement","ECSS-E-ST-50-11_1411144",1,"Created","On receipt of the BROADCAST_MESSAGE.request primitive the SpaceFibre node shall send the broadcast message over the specified broadcast channel immediately, subject to link priority rules."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","6.3.2.3.1a","Requirement","ECSS-E-ST-50-11_1411155",1,"Created","The SpaceFibre interface shall pass an RX_N-CHAR.indication primitive to the SpaceFibre network layer to indicate that an N-Char or Fill has arrived over a particular Virtual Channel."]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","6.4.3.3.4a","Requirement","ECSS-E-ST-50-11_1411191",1,"Created","On receipt of the PHYSICAL_STATUS.indication primitive the Lane layer shall react depending on the Physical layer status. "]
["ECSS-E-ST-50-11C","ECSS - Current v0.9","6.5.2.2.3a","Requirement","ECSS-E-ST-50-11_1411196",1,"Created","The SET_MANAGEMENT_PARAMETER.request primitive shall be generated to change a management parameter in the SpaceFibre port."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.2.6c","Requirement","ECSS-E-ST-50-12_1420020",1,"Created","The SpaceWire Management Information Base shall be responsible for configuring, controlling and monitoring the operation of the other SpaceWire layers."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.2.5b","Requirement","ECSS-E-ST-50-12_1420040",1,"Created","For a SpaceWire cable constructed in accordance with 5.3.2.3a and 5.3.2.3b, and with differential pairs consisting of 28 AWG wires, the constants in Table 5-1 shall be used in conjunction with equation [5-1] to determine the upper limit of the average insertion loss in decibel per meter."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.3.5b","Recommendation","ECSS-E-ST-50-12_1420075",1,"Created","Flying lead connectors used for connection to a PCB should have:\n1.\tAll the leads cropped to a short length of less than 25 mm, each with a length difference of less than 3 mm;\n2.\tThe wires forming each differential signal pairs twisted together.","NOTE\tThis helps to minimize the discontinuity in impedance caused by the connector.\n"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.4.3.3e","Requirement","ECSS-E-ST-50-12_1420102",1,"Created","The inner shields shall be isolated from the outer shield."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.6.1a","Requirement","ECSS-E-ST-50-12_1420120",1,"Created","SpaceWire shall use LVDS signals for transferring data."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.6.2.2g","Requirement","ECSS-E-ST-50-12_1420133",1,"Created","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."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.3.6.2.5h","Recommendation","ECSS-E-ST-50-12_1420155",1,"Created","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."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.4.2f","Requirement","ECSS-E-ST-50-12_1420180",1,"Created","The encoding layer shall inform the data link layer of changes in the encoding layer indicated by the following status flags:\n1.\tDisconnect, which indicates that the link has been disconnected.\n2.\tReceive error, which indicates that an error has been detected in a received symbol.\n3.\tgotNull, which indicates that the first Null control code has been received without any parity errors.","NOTE\tA parity error is an example of a receive error.\n"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.4.6b","Requirement","ECSS-E-ST-50-12_1420210",1,"Created","The gotNull condition shall only be cleared when the RX Enable flag is de-asserted"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.5.2b","Requirement","ECSS-E-ST-50-12_1420232",1,"Created","The data link layer shall pass a sequence of data characters, control characters and control codes to the encoding layer.","NOTE\tThese data characters, control characters and control codes are character encoded, serialised, data-strobe encoded and transmitted by the encoding layer.\n"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.5.2g","Requirement","ECSS-E-ST-50-12_1420237",1,"Created","The data link layer shall indicate to the Network layer when it has a broadcast code ready for passing to the Network layer."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.5.6c","Requirement","ECSS-E-ST-50-12_1420261",1,"Created","When sending of an FCT is requested, it shall be sent as soon as the current character or control code has been sent provided that:\n1.\tNo broadcast code is waiting to be sent."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.5.8.2a","Requirement","ECSS-E-ST-50-12_1420284",1,"Created","When Port Reset is asserted, the Link Error Recovery state machine shall enter the Normal state."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.4.3d","Requirement","ECSS-E-ST-50-12_1420309",1,"Created","When port reset is asserted, the time-code register shall be set to have a time-code value of zero."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.5.3b","Requirement","ECSS-E-ST-50-12_1420330",1,"Created","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."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.5.5f","Requirement","ECSS-E-ST-50-12_1420343",1,"Created","On reset the interrupt relay register shall be cleared to zero."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.5.7c","Requirement","ECSS-E-ST-50-12_1420361",1,"Created","When a port of a routing switch is disabled from receiving interrupt acknowledgement codes, it shall discard any interrupt acknowledgement codes received on that port."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.8.1d","Requirement","ECSS-E-ST-50-12_1420382",1,"Created","A SpaceWire routing switch that has an interrupt relay register shall broadcast distributed interrupt codes as detailed in clause 5.6.5."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.8.7f","Requirement","ECSS-E-ST-50-12_1420411",1,"Created","If an output port is waiting to transmit packet characters, the input port it is connected to shall also wait.","NOTE\tAn output port is waiting to transmit packet characters when it is waiting for FCTs to arrive to indicate that there is space in the input port at the far end of the link.\n"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","5.6.8.12c","Requirement","ECSS-E-ST-50-12_1420429",1,"Created","A packet shall be regarded by a port as being stuck when the following conditions are all fulfilled:\n1.\tIt has started.\n2.\tIt has not yet ended.\n3.\tThe time since the last data character was sent from the input port to the output port is longer than the port time-out period.","NOTE\t1\tA packet is started when the first data character of the packet is passed to the output port.\nNOTE\t2\tA packet is not yet ended until the EOP or EEP for that packet is passed to the output port.\n"]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.1.1.2.2a","Requirement","ECSS-E-ST-50-12_1420454",1,"Created","The SEND_PACKET.request primitive shall have the following parameters:\n1.\tSEND_PACKET.request (End-point, SpaceWire Packet)."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.1.1.3.3a","Requirement","ECSS-E-ST-50-12_1420459",1,"Created","The RECEIVE_PACKET.indication primitive shall be passed to the Receive Packet Service user when a SpaceWire packet is received."]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.2.2.2.1a","Requirement","ECSS-E-ST-50-12_1420497",1,"Created","The BROADCAST_CODE.request primitive shall be used by the network layer to request a port to broadcast a broadcast code over the SpaceWire network. "]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.3.1.2.1a","Requirement","ECSS-E-ST-50-12_1420506",1,"Created","The TX_CHAR.request primitive shall be used by the data link layer to send a character through its output port. "]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.3.2.5.1a","Requirement","ECSS-E-ST-50-12_1420527",1,"Created","The function of the RECEIVE_ERROR.indication primitive shall be to indicate to the data link layer that an error has occurred in the receiver. "]
["ECSS-E-ST-50-12C Rev.1","ECSS - Current v0.9","6.4.2.2.4a","Requirement","ECSS-E-ST-50-12_1420544",1,"Created","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."]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","6.3.3.3c","Requirement","ECSS-E-ST-20-06_0070023",1,"Unchanged","Adjacent blankets greater than 100 cm² in area shall be separately grounded to structure. "]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","6.6.1i","Requirement","ECSS-E-ST-20-06_0070042",1,"Unchanged","For LEO, the current shall be delivered in pulses representative of auroral crossing durations, typically 2 minutes for circular LEO orbits with inclination above 50º. "]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","6.6.3e","Requirement","ECSS-E-ST-20-06_0070182",1,"Created","Assemblies shall be tested with a bonding to ground that is representative of the flight configuration."]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","6.8.4e","Requirement","ECSS-E-ST-20-06_0070070",1,"Unchanged","If assessment of the electric fields and space charge density in a large volume is performed, the 3-D spacecraft charging codes to be used shall be defined.","NOTE \tThese 3-D spacecraft charging codes can consider the detailed geometry of the spacecraft. Various charging codes with different complexity are available for performing the assessment (see Annex C).\n"]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","7.2.3.2k","Requirement","ECSS-E-ST-20-06_0070089",1,"Unchanged","Cells shall be polarized during the test when the discharge occurs."]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","9.3a","Requirement","ECSS-E-ST-20-06_0070113",1,"Unchanged","Inspection of the spacecraft (including structure and cable harnesses) shall be performed to verify that there are no ungrounded metal components."]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","10.3d","Requirement","ECSS-E-ST-20-06_0070135",1,"Unchanged","Circuit analysis shall be performed to verify that the current passing through the deployment mechanism is within the level agreed with the customer. "]
["ECSS-E-ST-20-06C Rev.1","ECSS - Current v0.9","11.2.1e","Permission","ECSS-E-ST-20-06_0070173",1,"Unchanged","If in low thrust systems e.g. FEEPs, in LEO, if it is demonstrated by an analysis which includes the worst case natural currents, that neutralization can be achieved through natural ionospheric currents, a neutralizer may then be omitted. ","NOTE \tThis case is expected to be highly unusual. \n"]
["ECSS-E-ST-32-10C Rev.2 Corr.1","ECSS - Current v0.9","4.1.2b","Requirement","ECSS-E-ST-32-10_0110002",1,"Unchanged","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."]
["ECSS-E-ST-32-10C Rev.2 Corr.1","ECSS - Current v0.9","4.3.1a","Requirement","ECSS-E-ST-32-10_0110019",1,"Unchanged","The test factors KQ and KA shall be selected from Table 4-2."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.2.5.2d","Requirement","ECSS-E-ST-33-01_0820021",1,"Unchanged","Redundancy concepts shall be agreed by the customer.","NOTE \tRedundancy concepts are selected to minimize the number of single points of failure and to conform to the reliability requirements.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.5.2.8b","Requirement","ECSS-E-ST-33-01_0820046",1,"Unchanged","ECSS-Q-ST-70-71 clause “Radiation” shall apply."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.3.1j","Requirement","ECSS-E-ST-33-01_0820067",1,"Unchanged","The lubricant shall conform to the molecular and particulate contamination requirements specified for the entire mission.","NOTE \tFor molecular and particulate contamination, see ECSS-Q-ST-70-01.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.3.3.1c","Requirement","ECSS-E-ST-33-01_0820073",1,"Unchanged","The effect of exposure to on­ground storage and related gravity effects, and other ground or in­orbit accelerations on lubricant distribution shall be validated."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.4.2d","Requirement","ECSS-E-ST-33-01_0820094",1,"Unchanged","Unless the use of active thermal control is previously agreed with the customer, thermal control shall be passive. "]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.5.2.6f","Requirement","ECSS-E-ST-33-01_0820398",1,"Unchanged","In the mechanism requirement specification the Design Limit Loads (DLL) shall be specified.","NOTE \t 1\tIt is good practice to clarify with the customer that the Project factor (KP) and the Model factor (KM) are already included, to avoid duplication of factors.\nNOTE \t2\tDLL are intended to be environmental loads.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.5.4.1b","Requirement","ECSS-E-ST-33-01_0820133",1,"Unchanged","Mechanisms using deformable elements shall be designed to ensure they can only be installed in the correct orientation and position.","NOTE \tExamples of such mechanisms are crush dampers.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.5.4.5c","Requirement","ECSS-E-ST-33-01_0820156",2,"Normative Change","Except for gears and ball or journal bearings, the repeatability of the contact between the mating surfaces shall be verified by the supplier and agreed by the customer.","NOTE \tRepeatability includes contact loads, contact area, contact stress, and alignment.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.5.4.5h","Recommendation","ECSS-E-ST-33-01_0820462",1,"Unchanged","Except for gears and ball or journal bearings, and unless one surface is a self­lubricating material, when metallic material mating or separating surfaces subject to relative motion are used, they should\n1.\thave a minimum hardness of 500 HV, and \n2.\teither:\n(a)\tbe composed of dissimilar material, or \n(b)\tat least one of the two surfaces have a dissimilar coating. ","NOTE \t1\tExample of self-lubricating material is bronze.\nNOTE \t2\tExamples of dissimilar coatings are nitride, carbide or oxide. \nNOTE \t3\tThe use of bonded or sputtered MoS2 or polymeric materials is not excluded.\nNOTE \t4\tThe use of any dissimilar materials with a minimum hardness of 500 HV is often not sufficient to prevent cold welding.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.5.4.12c","Requirement","ECSS-E-ST-33-01_0820178",1,"Unchanged","The conformity of the design, material and manufacture of elements to be cut used in release and locking devices to the reliability requirements specified in the SMS shall be verified by test.","NOTE \tExample of such elements are bolts, rods and cables.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.7.7c","Requirement","ECSS-E-ST-33-01_0820211",1,"Unchanged","Resistive torques or forces shall be measured under worst-case conditions."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.7.8.5h","Recommendation","ECSS-E-ST-33-01_0820470",1,"Unchanged","The ratio between the derivative time constant and the time constant limiting the high frequency gain should not exceed 20."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.8.2.6.3d","Requirement","ECSS-E-ST-33-01_0820248",2,"Unchanged","A sensitivity analysis covering the uncertainty of parameters shall be carried out. ","NOTE \tThe sensitivity analysis is based on parameter variation.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.8.2.12a","Requirement","ECSS-E-ST-33-01_0820258",2,"Unchanged","The mechanism operation shall be verified by analysis using parameters representative of the flight configuration, including electronics, to comply with the specified requirements for induced loads. ","NOTE \tFor example, micro­vibrations. \n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.8.3.1d","Requirement","ECSS-E-ST-33-01_0820279",1,"Unchanged","The tests shall verify that the mechanism conforms to the functional dimensioning requirements specified in clause 4.7.5.3."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.8.3.3.7b","Requirement","ECSS-E-ST-33-01_0820299",1,"Unchanged","Lubricant quantity shall be verified by tests."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","4.8.3.3.16a","Requirement","ECSS-E-ST-33-01_0820322",2,"Unchanged","After completion of the life test, the mechanisms shall be disassembled into its tribological parts and the status of the parts verified with respect to the life test success criteria identified in clause 4.8.3.3.17."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-E-ST-33-01_0820337",1,"Unchanged","The SMS shall contain a description of the purpose, objective, content and the reason prompting its preparation.","NOTE \tFor example: “This document describes the application specific requirements of the <name> mechanism for the <name> project”.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","B.2.1<2>b","Requirement","ECSS-E-ST-33-01_0820365",1,"Unchanged","The primary functions of the mechanism shall be described."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","D.2.1<9>a","Requirement","ECSS-E-ST-33-01_0820390",1,"Unchanged","The user manual shall describe all activities to operate the mechanism on ground, including:\n1.\tPreparation for start up:\n(a)\toperational configuration;\n(b)\tGSE and special tools to be used;\n(c)\titems to be removed;\n(d)\tspecific precautions and safety instructions including limitations in terms of operation and performances;\n(e)\tcleaning instructions;\n(f)\tenvironmental conditions for operation.\n2.\tStep by step Start up operation instructions.\n3.\tFor each operational mode \n(a)\toperational configuration;\n(b)\tGSE and special tools to be used;\n(c)\tspecific precautions and safety instructions including limitations in terms of operation and performances;\n(d)\tenvironmental conditions for operation;\n(e)\tstep by step operation instructions;\n(f)\ttelemetry requirements and health monitoring;\n(g)\trecovery contingencies.","NOTE \tExample of such operational modes are release, calibration, deployment, and pointing, scanning.\n"]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","F.2.1<5>a","Requirement","ECSS-E-ST-33-01_0820436",1,"Unchanged","The MSVP shall provide a description of the approach to achieve compliance to the requirements for safety critical mechanisms."]
["ECSS-E-ST-33-01C Rev.2","ECSS - Current v0.9","G.2.1<5>a","Requirement","ECSS-E-ST-33-01_0820448",1,"Unchanged","The MSVR shall summarize:\n1.\tthe test results, including:\n(a)\tthe list of the requirements to be verified in correlation with the VCD,\n(b)\ttraceability to used documentation,\n(c)\tconformance or deviation including references and signature and date, \n2.\tthe comparison with the requirements, and \n3.\tthe verification close‐out judgment."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","4.1.6.2b","Recommendation","ECSS-E-ST-60-20_0920158",1,"Created","The set of core telemetries defined in Annex I should be used."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","4.4f","Requirement","ECSS-E-ST-60-20_0920039",1,"Unchanged","If the star sensor has the capability of autonomous attitude determination, the supplier shall deliver the on-board star pattern catalogue."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.4c","Requirement","ECSS-E-ST-60-20_0920050",2,"Normative Change","The supplier shall identify the worst case projection in BRF of the value defined in 5.4b. ","NOTE \tDifferent angular rates can be specified with associated required performance.\n"]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.5.4.1c","Requirement","ECSS-E-ST-60-20_0920073",1,"Unchanged","The performance shall be specified under the related performance general conditions."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.5.5.1a","Requirement","ECSS-E-ST-60-20_0920077",2,"Normative Change","A confidence level for the pixel spatial error shall be specified by the customer."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.5.8a","Requirement","ECSS-E-ST-60-20_0920094",2,"Normative Change","A confidence level for the measurement date error shall be specified by the customer."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.9.4.3a","Requirement","ECSS-E-ST-60-20_0920182",1,"Created","The probability of invalid attitude solution shall be estimated considering all possible initial pointing directions within a defined region within the celestial sphere."]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","5.13.2b","Requirement","ECSS-E-ST-60-20_0920186",1,"Created","The verification of continuity of tracking shall follow the following steps:\n1.\tUse of an high-fidelity simulation model in order to cover the whole celestial vault with sufficient granularity.\n2.\tEnsure that the distribution of the single effects, coming from protons impacted the detector, are statistically distributed over the detector.\n3.\tEnsure that each pointing direction assessed is analyzed with several distributions.\n4.\tTake into account, when possible, the energies of the protons spectrum to determine the actual charges deposited in each pixels.\n5.\tVerify end-to-end robustness by a combination of test and simulation to be agreed between the customer and supplier.","NOTE \t1\tA night sky test, instrumental to demonstrate general functionality and performance, cannot be used to demonstrate the capability to deal with solar events.\nNOTE \t2\tThe assessment of the robustness and the performance during a solar event makes use of a large set of pointing directions, since the star population in the field of view is impacted (the centroid accuracy depends on the star magnitude and the energy of the impinging particle).\n"]
["ECSS-E-ST-60-20C Rev. 2","ECSS - Current v0.9","A.2.1<7>a","Requirement","ECSS-E-ST-60-20_0920151",1,"Unchanged","The following information shall be attached to the document:\n1.\tidentification of delivered computer files;\n2.\tFMM source lists based on applied tools."]
["ECSS-E-ST-20-21C","ECSS - Current v0.9","5.2.1e","Requirement","ECSS-E-ST-20-21_1400012",1,"Created","Dedicated connectors dedicated to the actuators electronics outputs shall be implemented."]
["ECSS-E-ST-20-21C","ECSS - Current v0.9","5.2.3f","Recommendation","ECSS-E-ST-20-21_1400031",1,"Created","For long duration actuators, in addition to 5.2.1d, the FIRE OFF commands should be implemented by a standard serial interface."]
["ECSS-E-ST-20-21C","ECSS - Current v0.9","5.4.1d","Requirement","ECSS-E-ST-20-21_1400052",1,"Created","Parasitic inductance seen by the actuator electronics (load plus relevant harness) shall be limited to\n1.\t10 µH for current-driven actuators\n2.\t20 mH for voltage-driven actuators."]
["ECSS-E-ST-20-21C","ECSS - Current v0.9","5.6.3f","Recommendation","ECSS-E-ST-20-21_1400080",1,"Created","The maximum capacitance of actuators should be 1 µF."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.2.2.3c","Recommendation","ECSS-E-ST-35-06_0200384",1,"Unchanged","Fluid paths should be smooth, avoiding stepped transitions.","NOTE This is to avoid entrapment of contamination."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.2.4a","Requirement","ECSS-E-ST-35-06_0200044",1,"Unchanged","Connect/disconnect interfaces shall be protected from contamination by filters or by procedures \n    ","NOTE E.g. purge flow during connection / disconnection."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.3.1a","Requirement","ECSS-E-ST-35-06_0200049",1,"Unchanged","Manufacturing aspects that affect the selection of cleaning techniques shall be reported in conformance with Annex B."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.3.6d","Requirement","ECSS-E-ST-35-06_0200086",1,"Unchanged","Open subsystems and systems shall be handled in a specified environment equal to or better than ECSS-Q-ST-70-01 class M6.5."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.4.1e","Requirement","ECSS-E-ST-35-06_0200096",1,"Unchanged","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”)."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","4.5a","Requirement","ECSS-E-ST-35-06_0200121",1,"Unchanged","Cleanliness test methods shall be selected and justified."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","5.1e","Recommendation","ECSS-E-ST-35-06_0200392",1,"Unchanged","Cleaning should be done by liquids.\n    ","NOTE Liquids have a large dirt carrying capacity"]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","5.3.3.2d","Requirement","ECSS-E-ST-35-06_0200168",1,"Unchanged","The neutralization process shall use water complying with ISO 14951-10, Type HP, as final rinsing fluid."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","5.5.2c","Requirement","ECSS-E-ST-35-06_0200189",1,"Unchanged","Gas specified in 5.5.2a and 5.5.2b shall be filtered through a filter with dp £ 2 mm."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","5.5.3.2c","Requirement","ECSS-E-ST-35-06_0200194",1,"Unchanged","The reliability sample and the segment of production that it represents shall be identified, as specified by the customer."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","5.5.5.4b","Requirement","ECSS-E-ST-35-06_0200215",1,"Unchanged","Once the liquids have been evaporated from the hardware, the heating shall be discontinued and the oven is slowly filled with a filtered gas in conformance with 5.5.5.2a.2."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","6.2.3b","Requirement","ECSS-E-ST-35-06_0200241",1,"Unchanged","The standard test sample shall be 1 l of test liquid per m2 of critical surface area. \n    ","NOTE This is to ensure that all critical surfaces are being flushed. "]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","6.3.3b","Requirement","ECSS-E-ST-35-06_0200266",1,"Unchanged","Hardware replacement shall take place under pressurant gas purge.\n    ","NOTE Typical over-pressures range from 0,01 MPa to 0,05 MPa."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","6.4.4c","Requirement","ECSS-E-ST-35-06_0200282",1,"Unchanged","For repeated dryness verification of a hardware configuration a procedure shall be qualified and implemented in conformance with Annex B."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","7.5.1a","Requirement","ECSS-E-ST-35-06_0200292",1,"Unchanged","All plastic films of one lot shall have the cleanliness level verified prior to use."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","10.1a","Requirement","ECSS-E-ST-35-06_0200317",1,"Unchanged","The test procedure and total volume of test fluid necessary to flush the cleansed item or items shall be ascertained in accordance with Method I (clause 11.1.2 Method I “Liquid Flush Test”)."]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","11.1.4a","Requirement","ECSS-E-ST-35-06_0200338",1,"Unchanged","Systems or components which are not allowed to be flushed with liquids shall be cleaned by purging with gas as follows:\n    1. in conformance with clause 5.5.2.\n    2. filtered through a 2µm filter.\n    3. for components with a critical area £ 0,1 m2, an amount of gas equivalent to 100 l at 0,1 MPa and 293 K (standard conditions) with a minimum flow rate of 10 l/min (standard conditions).\n    4. for large subsystems or systems a minimum of 1000 l gas (standard conditions) with a minimum flow rate of 100 l/min (standard conditions).\n    5. for components and small subsystems with a critical area > 0,1 m2, 1000 l/m2 of critical surface area using gas with a flow rate of 100 l/min (standard conditions) to 1000 l/min (standard conditions).\n    6. the flow rate is less than the maximum allowable flow rate specified for the hardware.\n    7. the static pressures does not exceed the operating limits of the hardware.\n    8. the gas sample is counted for particles using:\n        (a) ECSS-E-ST-35-06 clause 12.1 with a gridded membrane filter of £ 2 mm, or\n        (b) a calibrated automatic gas particle counter.\n    9. repeated sampling is performed until two successive readings comply with the required level in conformance with clause 4.4.1, Table 4-1. "]
["ECSS-E-ST-35-06C Rev.2","ECSS - Current v0.9","C.2.1<2>a","Requirement","ECSS-E-ST-35-06_0200368",1,"Unchanged","The visual inspection results part shall contain:\n    1. Check box for requirement application\n    2. Identification of procedure used\n    3. Specification of requirement:\n        (a) Specific visual inspection requirement (GC) regarding manufacturing (e.g. burrs removed, surface finish applied)\n        (b) Visually clean (VC)\n        (c) Ultraviolet light (VC+UV)\n    4. Date of tests."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.1.3e","Requirement","ECSS-E-ST-40-07_1440018",1,"Created","Trailing delimiters shall be allowed in path strings."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.3.2a","Requirement","ECSS-E-ST-40-07_1440040",1,"Created","All SMP Components which contain the implementation of the simulations functional behaviour shall implement the IModel interface as per IModel.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.4.1a","Requirement","ECSS-E-ST-40-07_1440045",1,"Created","All SMP Components which are referencing other components shall implement the IAggregate interface as per IAggregate.h in [SMP_FILES]. ","NOTE\tThe IReference interface is the referencing mechanism used by the aggregation interface.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.6.2b","Requirement","ECSS-E-ST-40-07_1440071",1,"Created","The IEventSource Subscribe method shall add the given event sink to the list of subscribed event sinks, with the following argument and behaviour: \n1.\tArgument:\n(a)\t“eventSink” giving the reference to the event.\n2.\tBehaviour:\n(a)\tIf the given event sink is already subscribed to the event source, it throws an EventSinkAlreadySubscribed exception as per EventSinkAlreadySubscribed.h in [SMP_FILES];\n(b)\tIf the primitive type kind of the argument expected by the event sink is not semantically equivalent to the one of the event source as per Table 5-3, it throws an InvalidEventSink exception as per InvalidEventSink.h in [SMP_FILES].","NOTE\tAny event sink can only be subscribed once to each event source.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.8.1h","Requirement","ECSS-E-ST-40-07_1440092",1,"Created","The IDynamicInvocation GetOperations method shall return a collection of the invokable operations of the component as per OperationCollection in IOperation.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.11.2a","Requirement","ECSS-E-ST-40-07_1440117",1,"Created","All SMP Fields which represent a structured data shall implement the IStructureField interface as per IStructureField.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.11.5c","Requirement","ECSS-E-ST-40-07_1440131",1,"Created","The IField IsState method shall return true if the field State property is true, false otherwise."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.2.12.1b","Requirement","ECSS-E-ST-40-07_1440145",1,"Created","All SMP models and services shall use the predefined LogMessageKinds as defined in Table 5-4 for messages of message type Information, Event, Warning, Error or Debug ."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.3c","Requirement","ECSS-E-ST-40-07_1440171",1,"Created","The Scheduler shall allow to specify the cycle time between each call for cyclic Events with the following behaviour:\n1.\tFor non-cyclic Events, the cycle time parameter is stored, but not used;\n2.\tFor cyclic Events, the cycle time is a positive duration;\n3.\tFor cyclic Events, an InvalidCylceTime exception as per Services/InvalidCycleTime.h in [SMP_FILES] is thrown if the cycle time is negative or zero.","NOTE\tThe cycle time can become relevant if a subsequent call to SetEventCount is received before the Event is removed from the scheduler.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.5a","Requirement","ECSS-E-ST-40-07_1440202",1,"Created","The simulation environment shall provide a component implementing the IResolver interface as Services/IResolver.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.7h","Requirement","ECSS-E-ST-40-07_1440219",1,"Created","The ISimulator Run method shall change the state from Standby to Executing as per following procedure:\n1.\tIf the simulation is not in Standby state, then it returns and no action is taken;\n2.\tIf Run method is called during the execution of the global event SMP_LeavingStandby, then it returns and no action is taken;\n3.\tIf Run method is called during the execution of the global event SMP_EnterStandby, then it returns and no action is taken;\n4.\tIf the simulation is in Standby state, it issues the global event “SMP_LeavingStandby” via the Event Manager;\n5.\tAfter returning from the SMP_LeavingStandby global event, it changes the simulation state to “Executing” state;\n6.\tAfter entering Executing state, it issues the global event “SMP_EnterExecuting” via the Event Manager."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.7cc","Requirement","ECSS-E-ST-40-07_1440240",1,"Created","The ISimulator GetFactories method shall return a collection of all registered facories as per FactoryCollection in IFactory.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.9.1k","Requirement","ECSS-E-ST-40-07_1440265",1,"Created","The IPublication GetField method shall return an interface to a field, with the following argument and behaviour:\n1.\tArgument:\n(a)\t“fullName“ giving the path relative to the component.\n2.\tBehaviour:\n(a)\tIf no field exists with the given fully qualified name, it throws an InvalidFieldName exception as per InvalidFieldName.hin [SMP_FILES];\n(b)\tIf the field matching the given fully qualified name has a simple type, it returns an ISimpleField instance;\n(c)\tIf the field matching the given fully qualified name is an Array Field, it returns an IArrayField instance;\n(d)\tIf the field matching the given fully qualified name is a Structure Field, it returns an IStructureField instance.","NOTE\tThe path relative to the component is constructed as per clause 5.1.3. Examples:\n·\tMyStructuredField.InnerField\n·\tMyArrayField[2]\n·\tMyStructuredField.ArrayInnerField[2]\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.10.1k","Requirement","ECSS-E-ST-40-07_1440284",1,"Created","The ITypeRegistry AddClassType method shall return the interface to a new Class type that allows adding fields, with the following arguments and behaviour:\n1.\tArguments:\n(a)\t“name” giving name of the registered type;\n(b)\t“description” giving description of the registered type;\n(c)\t“uuid” giving the universally unique identifier of the base class.\n2.\tBehaviour:\n(a)\tIf another type with the same uuid already is registered, it throws a TypeAlreadyRegistered exception as per TypeAlreadyRegistered.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.3.10.5a","Requirement","ECSS-E-ST-40-07_1440292",1,"Created","The simulation environment shall provide a class implementing the IArrayType interface as per Publication/IArrayType.h in [SMP_FILES]."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.4.1.2.2i","Requirement","ECSS-E-ST-40-07_1440317",1,"Created","The type for an AttributeType shall point to a ValueType."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.4.1.2.4e","Requirement","ECSS-E-ST-40-07_1440331",1,"Created","The Type link of a Container shall point to a Reference Type."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","5.4.1.2.12d","Requirement","ECSS-E-ST-40-07_1440364",1,"Created","The Type link of an EventSink shall point to an EventType."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.2d","Requirement","ECSS-E-ST-40-07_1440391",1,"Created","Header files shall avoid circular dependencies by using forward declaration."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.4.4b","Requirement","ECSS-E-ST-40-07_1440406",1,"Created","The access specifier of the Association member variable shall be defined by the mapping of the Visibility attribute.","NOTE\tSee clause 6.1.3 for details on the mapping of Visibility attributes.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.4.6e","Requirement","ECSS-E-ST-40-07_1440421",1,"Created","The ByPointer 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 of the type includes the ‘*’ specifier;\n2.\tIf not set, then the C++ mapping of the type includes the specifier corresponding to the type referenced in the Type attribute as per Table 6-6;\n3.\tIf set to “false”, then the C++ mapping of the type does not include the ‘*’ specifier."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.4.10d","Requirement","ECSS-E-ST-40-07_1440448",1,"Created","If the EventType of an EventSource has an EventArgs, the implementation of the Emit method of the Smp::IEventSource interface shall expect to pass an “arg” parameter of simple type as defined by the type of the EventArgs. ","NOTE\tSee clause 5.2.6.2 for the details of the Emit method of the Smp::IEventSource interface.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.6.1b","Requirement","ECSS-E-ST-40-07_1440469",1,"Created","The value of universally unique identifier (UUID) variables shall be defined as per “Uuid” template in Table 6-2."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.1.7.1d","Requirement","ECSS-E-ST-40-07_1440492",1,"Created","The access specifier of class constructors and destructors within the C++ class a type is mapped to shall be defined by the mapping of the type Visibility attribute.","NOTE\tSee clause 6.1.3 for details on the mapping of Visibility attributes.\n"]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.2.3b","Requirement","ECSS-E-ST-40-07_1440517",1,"Created","The Static Library shall contain an Initialise method as per the “Static Initialise” template in Table 6-8."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","6.2.3g","Requirement","ECSS-E-ST-40-07_1440522",1,"Created","The Finalise function shall call the Finalise$Package.Name$ ( ) function."]
["ECSS-E-ST-40-07C","ECSS - Current v0.9","C.2.1a","Requirement","ECSS-E-ST-40-07_1440540",1,"Created","The suffix for configuration files shall be “smpcfg”."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","4.3.1.3b","Requirement","ECSS-E-ST-20-01_1450022",1,"Created","As a minimum, the failure modes shall include the following:\n1.\tfailed equipment \n2.\thot switching \n3.\toverdrive scenario \n4.\tunexpected thermal variations\n5.\tunexpected full or partial RF power reflection\n6.\tunexpected increase of input power"]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","4.7.3.1c","Requirement","ECSS-E-ST-20-01_1450054",1,"Created","Any deviation from Table 4-8 shall be proposed by the supplier and agreed with the customer."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","5.3.2.2.4f","Permission","ECSS-E-ST-20-01_1450080",1,"Created","Different analysis methodologies may be used in agreement with the customer."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","5.3.2.3.3b","Requirement","ECSS-E-ST-20-01_1450087",1,"Created","A convergence study of the mesh density and of the initial number of electrons shall be performed until the Multipactor threshold is stabilized."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","6.1a","Requirement","ECSS-E-ST-20-01_1450108",1,"Created","Airborne particulate cleanliness class 8 as per ISO 14644-1 or better conditions, shall be maintained throughout the equipment or component assembly, test, delivery and post-delivery phases."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","6.4.3.1b","Permission","ECSS-E-ST-20-01_1450129",1,"Created","If a single carrier test is not possible, a test with a multi-carrier signal, subjected to a frequency multiplex with CW carriers located in accordance with the operational frequency plan and with free-running phase per carrier may be performed under the condition that the test margins and test conditions, including the duration, are agreed between supplier and customer."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","7.3.2a","Requirement","ECSS-E-ST-20-01_1450156",1,"Created","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"]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","8.3f","Requirement","ECSS-E-ST-20-01_1450180",1,"Created","The test bed validation as per requirement b.1 shall be performed at the same pressure and temperature conditions as for the equipment test."]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","8.5.4a","Requirement","ECSS-E-ST-20-01_1450201",1,"Created","If non-repeatable or ambiguous events or discharges have occurred, an investigation shall be performed in order to determine the root cause of the event, events or isolated discharge that was observed. ","NOTE\tThis investigation can include:\n·\tContinued testing at higher power levels or lower duty cycle, pending approval of the customer.\n·\tVenting of the chamber, followed by a repeated test.\n·\tValidation of the test bed, repeating one or more of the steps described in clause 8.3.\n·\tEvaluation of the conditions under which the event or discharge occurred. For example; Test witness getting close to the test bed, unexpected test bed shock, abrupt increment in temperature leading to a return loss change, fluctuations in the high power amplifier.\n·\tOther aspects that are motivated by the experience and knowledge of the equipment or component supplier, the test supplier or the customer.\n"]
["ECSS-E-ST-20-01C","ECSS - Current v0.9","9.2a","Requirement","ECSS-E-ST-20-01_1450206",1,"Created","If the manufacturing process or the material of any potential critical gap is changed, a representative SEY sample of the new equipment or component shall be used for SEY measurements.","NOTE\tAny change of manufacturing process and any change of materials can be traced by means of DPL and DML according to ECSS-Q-ST-70.\n"]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","5.2.1a","Requirement","ECSS-E-ST-10-04_0760008",2,"Normative Change","IGRF-12 [RN.29] shall be used as the Internal Geomagnetic Field Model.","NOTE \tAs a stand-alone model, the inputs required of the IGRF-12 are either position in geodetic coordinates, according to the reference ‘World Geodetic Service 84’ standard ellipsoid, or position in a geocentric system, with respect to the centre of the Earth and for which the reference Earth radius is 6 371,2 km. The coordinates are therefore geodetic or geocentric latitude in decimal degrees, longitude (same in both coordinate systems), altitude in km above the reference ellipsoid, or distance in km from the centre of the Earth. Time is input in decimal years, e.g. 2 007,5. It is recommended that geocentric data are used, to avoid errors or confusion in respect of the reference ellipsoid. \n"]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","6.2.3c","Requirement","ECSS-E-ST-10-04_0760023",2,"Normative Change","The values given in Table A-1 shall be used:\n1.\tfor applications that require a realistic sequence of index values for future predictions, for example orbital calculations using index-driven atmospheric models; \n2.\tfor a given specific phase of the respective solar activity cycle."]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","8.2.4b","Requirement","ECSS-E-ST-10-04_0760045",2,"Normative Change","For spacecraft charging assessments, Kp=9 shall be used to represent a worst case situation.","NOTE \tThis is because the plasmasphere is a moderating influence on spacecraft charging, and so the worst case is considered to be when the plasmasphere is small which occurs when geomagnetic activity is high.\n"]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","9.2.1.1d","Requirement","ECSS-E-ST-10-04_0760055",2,"Normative Change","The dates of Minima and Maxima that shall be used for solar cycles 1 to 24 and the algorithm for forecasting future Minima and Maxima are presented in Annex B.1 and Table B-2.","NOTE\tAs it is difficult to define the % of solar MIN and MAX to apply for missions not scheduled in Max or Min periods, a more conservative analysis can be obtained for all periods using AE8MAX for electron fluxes and AP8MIN for proton fluxes.\n"]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","9.3c","Requirement","ECSS-E-ST-10-04_0760081",1,"Informative Change","The uncertainties in results from the models shall be included in the risk assessment."]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","10.2.1c","Requirement","ECSS-E-ST-10-04_0760086",1,"Unchanged","The directional and velocity distributions of the space debris and meteoroid fluxes shall be included in the impact risk assessment."]
["ECSS-E-ST-10-04C Rev.1","ECSS - Current v0.9","10.2.2.2k","Requirement","ECSS-E-ST-10-04_0760157",1,"Created","The Divine-Staubach model [RD.108] shall be used with following input parameters:\n1.\tMass range 10-12 g to 1 g.\n2.\tInherent velocity distribution model.\n3.\tParticle density equal to:\n(a)\t2,0 g/cm3 for m < 10-6 g\n(b)\t1,0 g/cm3 for 10-6 g < m < 10-2 g\n(c)\t0,5 g/cm3 for 10-2 g < m"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","5.2.1b","Requirement","ECSS-E-ST-50-16_1490002",1,"Created","All Time-Triggered End-System shall be of either SM or SC type as specified in [SAE AS6802]."]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","6.2.2g","Requirement","ECSS-E-ST-50-16_1490029",1,"Created","The redundant frames transmitted on all ports shall always be the same except the MAC source address where different interface ID fields are assigned at each port and the FCS."]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","6.2.6c","Requirement","ECSS-E-ST-50-16_1490055",1,"Created","In reception, if a TT frame is received outside its scheduled time window, the frame shall be discarded.","NOTE\tFor the calculation of the acceptance window duration, refer to guidelines provided in Clause 7.5.8.\n"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","6.2.8a","Requirement","ECSS-E-ST-50-16_1490071",1,"Created","The Switch shall support both of the following routing scheme: \n1.\tStatic Best-Effort routing according to a static Best-Effort routing table as part of the configuration \n2.\tDynamic Best-Effort routing according to a dynamic Best-Effort routing table created via address learning according to RFC 826"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","7.2.3.2d","Requirement","ECSS-E-ST-50-16_1490085",1,"Created","A Switch shall specify the number of SW_TT_TX_FRAMES Time-Triggered frames it is capable to transmit."]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","7.2.4.2h","Requirement","ECSS-E-ST-50-16_1490110",1,"Created","An End-System shall specify the different ES_TT_TX_PERIOD it supports. "]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","7.5.2d","Recommendation","ECSS-E-ST-50-16_1490147",1,"Created","Each node should update the pcf_transparent_clock field of PCF with the appropriate (regarding the physical port used and the way of the transmission) configurable value of external delay (as defined in [SAE AS6802] §5.3).","NOTE\tThat allows to reduce again the uncertainty on the PCF reception as presented in Figure 7-6.\n"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","8.2.3d","Requirement","ECSS-E-ST-50-16_1490173",1,"Created","In transmission, in the UDP structure, the Checksum field shall be set to 0.","NOTE\tThe checksum field is not used in UDP.\n"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","8.4.3.1d","Recommendation","ECSS-E-ST-50-16_1490195",1,"Created","In reception, if a frame has to be discarded because the receiving buffer was full, the MIB counter tteDropNoMem counter should be incremented. "]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","8.4.3.2m","Recommendation","ECSS-E-ST-50-16_1490216",1,"Created","In a Switch, the sub-entry called “ErrorN” should contain at least the following fields to describe the error it is reporting:\n1.\tErrorType - containing the type of error\n2.\tErrorField - containing the value of the field identified as faulty\n3.\tErrorOrigin - containing the MAC address of the originator of the faulty frame\n4.\tErrorTimeStamp - containing the date of the failure"]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","8.4.3.2q","Recommendation","ECSS-E-ST-50-16_1490220",1,"Created","If an ICMP frame length of the Switch is greater than 64 bytes, the frame should be discarded and the MIB counter ICMProtocolInError be incremented."]
["ECSS-E-ST-50-16C","ECSS - Current v0.9","9.2.2e","Requirement","ECSS-E-ST-50-16_1490247",1,"Created","It shall be checked that the network’s redundancy management works as foreseen in the System’s specification."]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.2.5.3a","Requirement","ECSS-E-ST-50_0970021",2,"Normative Change","The supplier shall provide a verification test report detailing the results of the execution of all verification tests, in conformance with the Verification report DRD in Annex F of ECSS-E-ST-10-02.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.5.2a","Requirement","ECSS-E-ST-50_0970043",2,"Normative Change","The design of the space communication system shall enable essential telemetry to be acquired from critical monitoring points and transmitted to the ground, even when only one of the redundant parts of the other systems, including the CDMU, is operational.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.5.7a","Requirement","ECSS-E-ST-50_0970238",1,"Created","The space communication system shall provide telemetry authentication and encryption services when the security requirements cannot be met by other means. \n","NOTE \tAuthentication and encryption can be provided, together or separately, at the upper layers, but it can also be provided at the Protocol sub layer of the Data Link layer e.g via the Space Data Link Security (SDLS) option provided in ECSS-E-AS-50-22 and ECSS-E-AS-50-23.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.6.11.5a","Requirement","ECSS-E-ST-50_0970069",1,"Unchanged","Uplink budget calculations shall be based on a BER of 10-5 at the input to the telecommand decoder.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.6.14.6a","Requirement","ECSS-E-ST-50_0970094",2,"Normative Change","The space link shall provide a time correlation capability that enables the time maintained on the spacecraft, the on-board time, to be correlated with the time maintained on the ground.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","5.8.2a","Requirement","ECSS-E-ST-50_0970115",2,"Normative Change","The ground network shall ensure that all items of data acquired from the spacecraft are uniquely labelled so that the parameter name, the parameter sampling time, and the time received on ground can be determined.\n"]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","A.2.1<7.1>b","Requirement","ECSS-E-ST-50_0970133",1,"Unchanged","The list specified in <7.1>a shall include the communication system requirements that address the following major system elements:\n1.\tfunctional;\n2.\tperformance;\n3.\treliability;\n4.\tavailability;\n5.\tinterface;\n6.\tdesign (implementation);\n7.\tmaintainability;\n8.\tsecurity."]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","B.2.1<9>d","Requirement","ECSS-E-ST-50_0970158",1,"Unchanged","The CSBD shall describe the technical approach to monitoring the health and performance of the communication system."]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","D.2.1<1>a","Requirement","ECSS-E-ST-50_0970179",1,"Unchanged","The CSVP shall contain a description of the purpose, objective, content and the reason prompting its preparation."]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","E.2.1<4>b","Requirement","ECSS-E-ST-50_0970197",1,"Unchanged","As a minimum, the architectural design of the communication system shall:\n1.\tlist each major component of the communication system,\n2.\tdescribe the function and performance of each major component in terms of top level requirements,\n3.\tlist and broadly describe all of the internal interfaces (i.e. interfaces between components of the communication system), and\n4.\tlist and broadly describe all of the external interfaces (i.e. interfaces between external entities and components of the communication system)."]
["ECSS-E-ST-50C Rev. 1","ECSS - Current v0.9","F.2.2a","Permission","ECSS-E-ST-50_0970233",1,"Unchanged","This DRD imposes no constraints on the tools used to elaborate the detailed design, and some elements of the detailed design, that can only be viewed with the aid of the tools used in the elaboration of the design, may be accepted."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","5.2b","Requirement","ECSS-E-ST-32-01_0810007",1,"Unchanged","The fracture control plan shall be subject to approval by the customer."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","6.2.1b","Requirement","ECSS-E-ST-32-01_0810020",2,"Normative Change","For the damage tolerance evaluation of PFCI, one of the following design principles shall be used in conformance with 6.3:\n1.\tSafe life, or\n2.\tFail-safe, or\n3.\tLow-risk fracture","NOTE\t1\tAn overview of the fracture control evaluation procedure, including damage tolerance design approaches, classification of Potential Fracture Critical Items and the relevant documentation is illustrated in Figure 6-2.\nNOTE\t2\tAnother way to implement damage tolerance is containment. Containment verification is considered a fracture control activity (see clause 6.3.4). The container (or restraint) is a PFCI (see 6.1f). Contained (or restrained) items are however not considered PFCI (see Figure 6-1).\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","6.3.5.3.2a","Requirement","ECSS-E-ST-32-01_0810052",2,"Normative Change","One of the following criteria shall be met:\n1.\tLow-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\n2.\tLow-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 the following assumed initial cracks  do not grow to failure in less than four complete service lifetimes.\n(a)\tFor items of more than 3mm thickness or diameter, surface cracks of a=3 mm depth and 2c=6 mm length and corner cracks of a=c=3 mm radius from holes and edges, \n(b)\tFor items of less than 3 mm thickness or diameter, through cracks of 2c=6 mm length and edge cracks from holes and edges of c=3 mm length.","NOTE\tFor the definition of the dimensions a and c see Figure 7-1, Figure 7-2 and Figure 7-3.\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","7.2.5c","Requirement","ECSS-E-ST-32-01_0810077",1,"Unchanged","Mean value of threshold stress intensity range (DKth) shall be used."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","7.2.5h","Requirement","ECSS-E-ST-32-01_0810082",1,"Informative Change","For those materials where a significant reduction of the KC for thin sheets is observed, the reduced value shall be used in the analysis.","NOTE\tThis reduction of fracture toughness is not automatically accounted for in the ESACRACK software.\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","7.3c","Requirement","ECSS-E-ST-32-01_0810104",1,"Unchanged","The material properties used for the critical crack size calculation shall be in conformance with 7.2.5."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","8.2.6b","Requirement","ECSS-E-ST-32-01_0810125",1,"Unchanged","If provision 8.2.6a is not met, hazardous fluid containers shall:\n    1. Have safe-life against rupture and leakage.\n    2. Be treated and certified the same as pressure vessels when the contained fluid has a delta pressure greater than one atmosphere."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","8.4.3.2a","Requirement","ECSS-E-ST-32-01_0810145",1,"Informative Change","The events that can cause mechanical damage during the service life, shall be identified and documented in the fracture control analysis report.","NOTE\t1\tThe service life includes the following phases:\n·\tHandling,\n·\tTest,\n·\tTransportation,\n·\tIn-service use, \n·\tMaintenance, \n·\tThe manufacturing phase, which are not covered by NDT.\nNOTE\t2\tThe following are examples of credible events:\n·\tTool drop\n·\tBumping or falling during handling\n·\tScratch during assembly.\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","8.4.4.3e","Requirement","ECSS-E-ST-32-01_0810167",1,"Unchanged","For a low-risk fracture item the strain at the limit load shall be below the damage tolerance threshold strain. "]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","8.6b","Requirement","ECSS-E-ST-32-01_0810176",1,"Informative Change","The proof test factor shall be derived by means of fracture mechanics analysis, but not be less than 1,1. ","NOTE\tRotating hardware not considered as rotating machinery in conformance with 3.2.32 is treated as any structural item.\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","9b","Requirement","ECSS-E-ST-32-01_0810195",1,"Unchanged","Where validated properties for analysis are not available, or available properties are not validated by standard or other test procedures agreed with the customer, the statistical basis for average and minimum values shall be established by tests."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","10.3.2f","Requirement","ECSS-E-ST-32-01_0810217",2,"Normative Change","Other non-metallic items shall be non-destructive tested and proof tested in conformance with clause 8.5."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","10.4.3.2b","Requirement","ECSS-E-ST-32-01_0810249",2,"Deleted","<<deleted (moved to ECSS-Q-ST-70-15)>>"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","10.5.1a","Requirement","ECSS-E-ST-32-01_0810265",2,"Deleted","<<deleted (moved to ECSS-Q-ST-70-15)>>"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","10.7.2.1.1a","Requirement","ECSS-E-ST-32-01_0810290",1,"Informative Change","The detected defect shall be verified as crack-like defect, and a fracture mechanics analysis or test performed to verify the acceptability of this defect.","NOTE\tOnly 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.\n"]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","10.7.2.1.2c","Requirement","ECSS-E-ST-32-01_0810296",1,"Unchanged","The fatigue test specified in 10.7.2.1.2b shall demonstrate limit load capability after application of the complete load spectrum 6 times in sequence."]
["ECSS-E-ST-32-01C Rev. 2","ECSS - Current v0.9","11.2.2.8c","Permission","ECSS-E-ST-32-01_0810356",1,"Created","X-ray testing of fusion welded joints may also be omitted before proof test if all of the following requirements are met:\n1.\tMaterial selection is limited to materials, which are known to be well weldable.\n2.\tIt is demonstrated that welding verification:\n(a)\twas performed in accordance with clause 11 of ECSS-Q-ST-70-39, including X-ray testing and destructive testing of verification samples, or\n(b)\tis based on large heritage of the following: identical material, comparable thickness, and fusion depth, comparable weld method, jigs, tooling and parameters,. without failure during or after proof testing, including X-ray testing of sufficient samples.\n3.\tIf X-ray testing of the flight hardware is omitted or cannot be performed, in addition to other design and process control measures implemented to ensure robustness of the hardware, X-ray testing is required on accompanying samples, that are welded using parameters and a setup as close as possible to the flight hardware for representativeness, to demonstrate acceptance criteria according to the weld specification, to the extent and with margin agreed with the customer.\n4.\tA minimum proof pressure test factor of 1,5 is applied, while also fulfilling 8.2.1b.\n5.\tIf flaw growth due to cyclic or sustained loads cannot be neglected, safe life is demonstrated, where the potential crack extension is covered by the difference between critical crack size during proof test and critical crack size during operation, or it is based on a conservative envelope of credible weld defects agreed with the customer:","NOTE\t1\tacp + Da < aco\n\twhere: \n\tacp \t= critical crack size during proof test\n\taco\t= critical crack size during operation\n\tDa\t= crack extension during dimensioning life\nNOTE\t2\tVisual inspection of all flight welds is always requested by ECSS-Q-ST-70-39.\nNOTE\t3\tto item 1: Examples for well weldable materials are: \n(a)\tTi-6Al-4V\n(b)\tTi-3Al-2.5V\n(c)\tTi-6Al-4V/Ti-3Al-2.5V dissimilar weld\t\n(d)\tAA2219\n(e)\tAA6XXX\n(f)\tAA5XXX\n(g)\tAISI type stainless steels\n\tExamples of alloys which are fusion weldable only under precautions and with limitations are the standard AA7XXX alloys and AA2XXX aluminum lithium alloys.\nNOTE\t4\tto item 3: A margin against the size specified in acceptance criteria that would apply to fully inspected flight welds is requested because flight hardware that is not inspected can contain worse imperfections than the inspected accompanying samples.\nNOTE\t5\tto item 3: Examples of design and process control measures that help to ensure robustness of the hardware are tight tolerances and generous width of electron beam and laser welds as well as process control means to verify accurate weld path.\nNOTE\t6\tto item 3: Acceptance criteria are defined for all credible defect types, like porosity (individual, clustered), inclusions, geometrical imperfections (including incomplete fusion, if part of the weld design), and are relevant to the dimensions relevant to the transfer of load. Detailed requirements for acceptance criteria for flaws other than crack-like defects are not within the scope of this ECSS standard.\nNOTE\t7\tto item 4: Examples of potential defects in welds  porosity, inclusions, geometrical imperfections.\nNOTE\t8\tto item 4: Requirement 8.2.1b limits the magnitude of loads other than pressure.\nNOTE\t9\tto item 5: Sharp features, like lack of fusion, are considered as crack like, unless covered conservatively in another manner agreed with the customer.\nNOTE\t10\tto item 5: The user is reminded that the standards like ECSS-E-ST-32 and ECSS-E-ST-32-02 require the hardware to be designed to sustain the proof loading without detrimental deformation, i.e. without large scale yielding.\nNOTE\t11\tto item 5: The crack screening proof test approach described above will take into account the requirements and guidelines of clause 10.4.2.3 if not agreed otherwise with the customer.\nNOTE\t12\tto item 5: Customer approval is required in 11.2.2.8c.5 for welds not screened by proof testing because it is normally desirable to avoid the situation where flaw growth due to cyclic or sustained loads cannot be neglected for welds that will not be inspected, especially in, for example welds, that contain a lack of fusion at the weld root by design which are generally considered non-structural.\n"]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","4.2.11.2d","Requirement","ECSS-E-ST-20-07_0080026",2,"Normative Change","The DC resistance between the equipment bonding stud and the local structure grounding point shall be less than 5 mW."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.2.2c","Requirement","ECSS-E-ST-20-07_0080047",1,"Unchanged","The RF absorber shall be placed above, behind, and on both sides of the EUT, and behind the radiating or receiving antenna as shown in Figure 5-1."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.3.3a","Requirement","ECSS-E-ST-20-07_0080062",1,"Unchanged","When the EUT is installed on a conductive composite ground plane, the surface resistivity of the actual installation shall be used."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.6.6.2d","Requirement","ECSS-E-ST-20-07_0080090",1,"Unchanged","The cable arrangement shall be such that it satisfies the following conditions:\n1.\tAt least the first 2 m (except for cables that are shorter in the actual installation) of each interconnecting cable associated with each enclosure of the EUT are run parallel to the front boundary of the setup.\n2.\tRemaining cable lengths are routed to the back of the setup and placed in a zigzagged arrangement."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.6.6.2i","Recommendation","ECSS-E-ST-20-07_0080276",1,"Created","For signal cable bundles, the overall shield, if present, and the individual shields should be bonded to the test set-up boundary to the EGSEs, either to the relevant edge of the metallic ground plane or to the access panel between the control room and the test chamber."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.9.3d","Requirement","ECSS-E-ST-20-07_0080124",1,"Unchanged","For equipment that operates, such that potential emissions are produced at only infrequent intervals, times for frequency scanning shall be increased such than any emission is captured."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.2.10.1g","Requirement","ECSS-E-ST-20-07_0080280",1,"Created","Stepped scans shall dwell, exclusive of test equipment settling time, at each tuned frequency for the greater of one second or the EUT response time, within the limit of ten seconds."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.3.3a","Permission","ECSS-E-ST-20-07_0080266",2,"Normative Change","If the spacecraft is not powered during launch, EMC with the launch system need not be verified by test."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.4.4.5a","Requirement","ECSS-E-ST-20-07_0080177",1,"Unchanged","In addition to 5.2.9.4, data presentation shall be a graphic output of current versus time displaying the transient characteristics with following conditions:\n1.\tamplitude resolution within 3 % of the applicable limit,\n2.\ttime base resolution within 10 % of rise time for measurement of rise and fall slopes.","NOTE \tRise time is the duration between 10 % and 90 % of peak-to-peak amplitude\n"]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.4.6.4d","Requirement","ECSS-E-ST-20-07_0080195",1,"Unchanged","The EUT shall be tested by using the measurement path of Figure 5-13 and by determining the radiated emissions from the EUT and its associated cabling as follows:\n1.\tTurn on the EUT and wait until it is stabilized.\n2.\tScan the measurement receiver for each applicable frequency range, using the bandwidths and minimum measurement times in 5.2.9.1\n3.\tOrient the antennas for both horizontally and vertically polarized fields.\n4.\tRepeat steps 5.4.6.4d.2 and 5.4.6.4d.3 for each antenna position determined under 5.4.6.3c, 5.4.6.3d, and 5.4.6.3e."]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.4.8.2a","Requirement","ECSS-E-ST-20-07_0080202",2,"Normative Change","The test equipment shall be as follows:\n1.\tSignal generator with amplitude or pulse modulation capability,\n2.\tpulse generator, 1 kHz – 100 kHz, adjustable duty cycle,\n3.\tpower amplifier, 50 kHz – 100 MHz,\n4.\tcurrent injection probe, 50 kHz – 100 MHz,\n5.\tcurrent measurement probe, 50 kHz – 100 MHz,\n6.\tone or two calibration fixture(s) (jigs) defined in 5.2.8.3,\n7.\tmeasurement receivers or spectrum analysers,\n8.\twaveform recording device,\n9.\t50 W coaxial load,\n10.\tLISN defined in 5.2.4,\n11.\tpower meter (optional),\n12.\tdirectional coupler.","NOTE \tto 7: In clauses 5.4.8.3 to 5.4.8.4, “measurement receiver” means “measurement receiver or spectrum analyser”.\n"]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.4.11.3d","Requirement","ECSS-E-ST-20-07_0080221",2,"Normative Change","For the calibration of the electric field, performed in the absence of the EUT, LISN and test harness, the setup shall be as follows:\n1.\tPlace the transmit antenna at each of the positions planned for EUT testing, as specified in 5.4.11.3e.\n2.\tPlace the electric field sensor directly opposite the transmit antenna as shown in Figure 5-30 at  30 cm above the ground plane.","NOTE \tAn illustration of the setup is given in Figure 5-29.\n"]
["ECSS-E-ST-20-07C Rev. 2","ECSS - Current v0.9","5.4.14.2a","Requirement","ECSS-E-ST-20-07_0080309",1,"Created","The test equipment shall be as follows:\n1.\tESD generator as specified in the IEC 61000-4-2, with 150 pF capacitance and 330 Ω discharge resistance, and contact discharge tip.\n2.\tESD current target, input resistance 2 ± 5% Ω, as specified in the IEC 61000-4-2.\n3.\tAttenuator, 20 dB.\n4.\tCoaxial cable, 50 Ω impedance, length ≤ 1 metre.\n5.\tDigital oscilloscope: 50 Ω input impedance, analogue bandwidth ≥ 1 GHz, real time sampling rate ≥ 5 GSa/s, with pre-triggering capability."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","4.3.2.2b","Requirement","ECSS-E-ST-10-03_0750015",2,"Normative Change","The TRR shall address the following topics:\n1.\ttest documentation availability and suitability, including: \n(a)\tapproved AIT Plan,\n(b)\tapproved test specification,\n(c)\ttest predictions (when relevant),\n(d)\tapproved test procedures (including contingency and emergency procedures),\n(e)\tapproved measurement point plan,\n(f)\tapproved test facility readiness report,\n(g)\tapproved test schedule, and\n(h)\tacceptance data package of lower level items.\n2.\titem under test configuration;\n3.\ttest configuration/set-up;\n4.\tinspection status report of KIP, MIP, or both;\n5.\ttest facility, environmental conditions, test instrumentations, calibration, maintenance status; \n6.\tcleanliness condition, hazard and safety;\n7.\tground support equipment (GSE) and infrastructures;\n8.\tstatus of nonconformances that affect the item under test, its associated GSE, or the test facility;\n9.\twaivers status, and deviations;\n10.\tpersonnel qualification and availability;\n11.\tresults from test rehearsal using the test facility with or without the item under test, when relevant;\n12.\ttest pass/fail criteria completeness;\n13.\tassignment of responsibilities;\n14.\ttest schedule.","NOTE\t1\tFor 4.3.2.2b.1(f), the content of the facility readiness report is defined in ECSS-Q-ST-20-07.\nNOTE\t2\tThe level of details according to which each topic is addressed, is different for the general test programme TRR than for each block test TRR. \n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","4.3.4a","Requirement","ECSS-E-ST-10-03_0750036",1,"Unchanged","Any failure or anomaly during testing shall be recorded."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","4.4.2b","Requirement","ECSS-E-ST-10-03_0750051",2,"Normative Change","For the purpose of 4.4.2a, test input tolerances shall account for the uncertainty budget and confidence level of the measurement instrument(s) and test equipment used to control and monitor the test parameters.","NOTE\t1\tJCGM 100 series, EA-4/16 and EA-4/02 guidelines and ISO/IEC 17025 general requirements can be used to build up the measurement uncertainty budgets.\nNOTE\t2\tThe test input tolerances specified in Table 4‑1 are the allowable ranges within which the test parameters, as measured, can vary.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","4.5.2b","Requirement","ECSS-E-ST-10-03_0750063",1,"Unchanged","Qualification testing shall be conducted on dedicated qualification models except when using protoflight approach."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","4.6.5b","Requirement","ECSS-E-ST-10-03_0750086",1,"Unchanged","Additional testing of qualification space segment element or equipment subsequently selected for flight shall be compatible with the residual life.","NOTE \tThis is done when the customer considers the risk acceptable.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.1.1j","Requirement","ECSS-E-ST-10-03_0750111",1,"Unchanged","When accessible, protection functions shall be tested.","NOTE \tExample of protection function are over-voltage, and over-current.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.2.3f","Requirement","ECSS-E-ST-10-03_0750135",1,"Unchanged","For space segment equipment which is designed to be re-flown, the qualification test duration per axis shall be in conformance with Table 5‑2 plus 50 seconds per additional flight."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.2.7d","Requirement","ECSS-E-ST-10-03_0750472",1,"Unchanged","The background noise shall be measured, including each individual contribution from EGSE, MGSE, FGSE.","NOTE \tExample of FGSE: pumps.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.2.8d","Requirement","ECSS-E-ST-10-03_0750475",1,"Unchanged","The background noise shall be measured, including each individual contribution from EGSE, MGSE, FGSE.","NOTE \tExample of FGSE: pumps.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.4.1a","Requirement","ECSS-E-ST-10-03_0750175",2,"Normative Change","Both thermal vacuum test and thermal test at mission pressure shall be performed for space segment equipment that operate under a non-vacuum environment after having been exposed to vacuum.","NOTE\t1\tFor example, in the case of a planetary mission within an atmosphere, the space segment equipment is tested in vacuum and in the mission atmosphere pressure.\nNOTE\t2\tAt space segment equipment level, the version C of ECSS-E-ST-10-03 does not consider a thermal test at room pressure (also called \"thermal cycling\", by example, in US standards and in the version A of ECSS-E-ST-10-03).\nNOTE\t3\tAt space segment equipment level, clause 5.5.4.4 of ECSS-E-HB-10-03 gives guidelines for assessment of alternative thermal testing approaches using room pressure temperature cycling tests.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","5.5.5.1a","Requirement","ECSS-E-ST-10-03_0750202",1,"Unchanged","The EMC test shall be performed in conformance with ECSS-E-ST-20-07 clause 5."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.1f","Requirement","ECSS-E-ST-10-03_0750223",1,"Unchanged","Any unusual or unexpected behaviour shall be evaluated to determine the existence of any trend potentially leading to anomaly or failure situation."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.1.2.3h","Requirement","ECSS-E-ST-10-03_0750248",1,"Unchanged","Autonomous lockout or shutdown sequences shall be verified to ensure that they do not adversely affect other system operations during or subsequent to the intended lockout or shutdown."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.1.3d","Requirement","ECSS-E-ST-10-03_0750256",1,"Unchanged","Performance tests shall be performed after the end of the environmental test programme."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.2.2a","Requirement","ECSS-E-ST-10-03_0750274",1,"Unchanged","The modal survey shall be conducted on a structural representative model in conformance with ECSS-E-ST-32-11."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.2.7e","Requirement","ECSS-E-ST-10-03_0750299",1,"Unchanged","Space segment element equipped with apogee or retro motors shall be tested for the vibration environment generated by the motor if\n1.\tthe environment is not enveloped by the launch boost environment; or\n2.\tthe configuration during the apogee or retro motor burn is different from the launch configuration."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.2.10a","Requirement","ECSS-E-ST-10-03_0750323",2,"Normative Change","During performance test on a space segment element, the effect of each potential source of micro-vibration shall be tested separately by comparing tests with and without perturbation.","NOTE\t1\tcombined effects of several contributors can also be tested.\nNOTE\t2\tEffect of a source of micro-vibrations can also depend on the operating mode (e.g. reaction wheel speed) and/or test configuration (e.g. gravity orientation effect).\nNOTE\t3\tSusceptibility of the space segment element performance can also depend on the operating mode (e.g. integration time).\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.4.1f","Requirement","ECSS-E-ST-10-03_0750339",1,"Unchanged","The equipment power ON/OFF status, throughout the test (including transitions), shall be defined in the test specification."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","6.5.5.5a","Requirement","ECSS-E-ST-10-03_0750364",1,"Unchanged","The magnetic field measurement shall be performed in a dedicated facility featuring Earth field compensation."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","7e","Requirement","ECSS-E-ST-10-03_0750382",1,"Unchanged","Pre-launch functional tests shall be performed to verify that no damage or performance degradation of the space segment element and its constituents has occurred during shipment or handling.","NOTE \tVerification of redundancy is included.\n"]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","A.2.1<6>b","Requirement","ECSS-E-ST-10-03_0750399",2,"Normative Change","The AIT Plan shall describe the logistics and list the major transportations."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","B.2.1<8>a","Requirement","ECSS-E-ST-10-03_0750413",1,"Unchanged","The TSPE shall describe the test activity flow and the associated requirements."]
["ECSS-E-ST-10-03C Rev.1","ECSS - Current v0.9","C.2.1<13>b","Requirement","ECSS-E-ST-10-03_0750434",1,"Unchanged","The TPRO shall describe QA and PA aspects applicable to the test."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.1.3b","Requirement","ECSS-E-ST-20_0020008",1,"Unchanged","All executable commands shall be explicitly acknowledged by telemetry."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.2.1.1w","Requirement","ECSS-E-ST-20_0020043",2,"Unchanged","The spacecraft electrical system shall be single failure tolerant for unmanned mission and double failure tolerant for manned mission."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.2.1.2.3v","Requirement","ECSS-E-ST-20_0020449",1,"Created","In case flexible connections are used, i.e. flex PCBs, the applicable requirements of clause 8 of ECSS-Q-ST-70-12 shall be applied."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.2.1.2.3aa","Permission","ECSS-E-ST-20_0020454",1,"Created","The electrical diagrams, layout and assembly drawings providing the information of the critical lines or nets may be part of the relevant analysis report."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.2.3n","Requirement","ECSS-E-ST-20_0020062",2,"Unchanged","<<deleted>>"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","4.3.2c","Requirement","ECSS-E-ST-20_0020087",1,"Unchanged","FMECA shall be performed and based on the failure modes previously defined at component level."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.5.2g","Requirement","ECSS-E-ST-20_0020111",3,"Normative Change","In all configurations, stowed and deployed, the solar array , deployable and body mounted, and spacecraft structure shall be insulated from each other, disregarding the bleed resistor.","NOTE\t1\tExamples of such structural parts of the SA panel are hold-down mechanisms, yokes, hinges and CCL (Closed Cable Loop).\nNOTE\t2\tTypical value of insulation is in the order of 100 MΩ, and typical bleed resistor is in between 2 kΩ to 20 kΩ.\n"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.5.3c","Requirement","ECSS-E-ST-20_0020124",2,"Unchanged","I(V) solar cells characteristics shall be computed in BOL and EOL conditions at maximum and minimum operating temperatures according to the mission profile."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.5.4b","Requirement","ECSS-E-ST-20_0020134",2,"Unchanged","The design of the insulation barriers between adjacent wires, connector pins and slip rings shall be such that no discharge phenomena can occur."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.6.3e","Requirement","ECSS-E-ST-20_0020154",2,"Unchanged","<<deleted>>"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.7.2j","Recommendation","ECSS-E-ST-20_0020402",1,"Unchanged","Fuses should be avoided to maintain the quality of the bus.","NOTE \tThe rationale for requirement 5.7.2h to 5.7.2j is the following:\n\tIn order to be advantageous over an unregulated scheme, a regulated bus ensures a good regulation quality at the regulation point, including when the various loads on the bus are changing. The regulated bus is designed to ensure that normal transients including interdomain are within 5% all included. Abnormal transients are more than twice the normal transients; the load is then designed to operate nominally in normal transients and sustain without damage abnormal transients.\n"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.7.5a","Requirement","ECSS-E-ST-20_0020204",2,"Unchanged","For converters and regulators in closed loop control, the phase margin shall be at least 50° and the gain margin 6 dB for worst case end–of–life conditions with representative loading."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.8.1j","Requirement","ECSS-E-ST-20_0020225",2,"Unchanged","Equipment connected to independent, redundant power buses not protected at the source shall ensure that:\n1.\tfor unmanned missions, no single failure causes the loss of more than one power bus;\n2.\tfor manned missions, two failures do not cause the loss of more than one power bus."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.9a","Requirement","ECSS-E-ST-20_0020242",2,"Unchanged","The design of electrical subsystems and payloads shall conform to ECSS-Q-ST-40. "]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","5.10e","Requirement","ECSS-E-ST-20_0020247",1,"Unchanged","The design of high voltage equipment shall be such that worst case DC and AC field strengths are less than half of the values for which breakdown can occur."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","6.3.4.2a","Requirement","ECSS-E-ST-20_0020268",1,"Unchanged","The spacecraft charging protection programme shall include the preparation and maintenance of an analysis plan, and the preparation and maintenance of a test plan.","NOTE \tThe objective of the programme is to ensure that the space vehicle is capable of operating in the specified space plasma charging environment and its energetic electron content without degradation of the specified space vehicle capability and reliability and without changes in operational modes, location, or orientation. \n"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","7.2.1.2.1a","Requirement","ECSS-E-ST-20_0020293",1,"Unchanged","All antenna terms used in all documentation (DDF, DJF, Test Report, Test Procedures, ICD and EIDP) shall follow the definitions found in IEEE 145:1993 ”Antenna Terms”."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","7.2.2.3.2b","Requirement","ECSS-E-ST-20_0020314",1,"Unchanged","The reflective and transmissive properties (losses, depolarisation, diffusivity) of the materials and composites used for polarisation and frequency selective reflectors shall be quantified and their impact on antenna performances assessed."]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","7.2.2.3.5d","Requirement","ECSS-E-ST-20_0020328",1,"Unchanged","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"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","7.2.3.2a","Requirement","ECSS-E-ST-20_0020345",1,"Unchanged","Electromagnetic interactions among the antenna and the surrounding spacecraft structure and appendages shall be quantified starting from Phase B, as a minimum, and their impact on antenna performances assessed.","NOTE \tThe field radiated or received by the antenna interacts with the surrounding environment. Interactions with the spacecraft structure and appendages usually have a direct impact on the antenna performances.\n"]
["ECSS-E-ST-20C Rev.2","ECSS - Current v0.9","A.2.1a","Requirement","ECSS-E-ST-20_0020365",1,"Unchanged","The EMC control plan shall contain a description of the purpose, objective, content and the reason of prompting its preparation."]
["ECSS-M-ST-10-01C","ECSS - Current v0.9","5.3.1a","Requirement","ECSS-M-ST-10-01_0310010",1,"Created","The review authority shall approve the review procedure and in particular:\n    1. the objectives of the review according to ECSS-M-ST-10 requirements;\n    2. the review team composition;\n    3. the execution of the review."]
["ECSS-M-ST-10-01C","ECSS - Current v0.9","5.4a","Requirement","ECSS-M-ST-10-01_0310027",1,"Created","Prior to starting the review, fulfilment of the review prerequisites defined in the procedure shall be confirmed by the customer and agreed by the review team leader.\n    NOTE See also 5.3.4b."]
["ECSS-M-ST-10-01C","ECSS - Current v0.9","B.2.1a","Requirement","ECSS-M-ST-10-01_0310052",1,"Created","A RID shall contain at least the following information:\n    1. Issue raised and reference of the applicable document violated\n    2. Originator recommendation to resolve the issue\n    3. Classification in major or minor\n    4. Endorsement of the RID by the review team\n    5. Response from the supplier\n    6. Concurrence (or not) of the review team with the supplier response\n    7. Identification of action items\n    8. Confirmation of RID status or close-out reference\n    9. Any attached document supporting the issue.\n        NOTE An example of a RID form is provided in Figure B-1."]
["ECSS-M-ST-10C Rev. 1","ECSS - Current v0.9","5.2.2.1b","Requirement","ECSS-M-ST-10_0010023",1,"Created","Each customer and supplier in the customer-supplier chain shall implement and maintain the project reporting an action monitoring systems."]
["ECSS-M-ST-10C Rev. 1","ECSS - Current v0.9","5.2.3.3b","Requirement","ECSS-M-ST-10_0010042",1,"Created","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."]
["ECSS-M-ST-10C Rev. 1","ECSS - Current v0.9","5.3e","Requirement","ECSS-M-ST-10_0010050",1,"Created","The identification shall remain unchanged during the product lifetime, unless a modification causes discontinuation of interchangeability."]
["ECSS-M-ST-10C Rev. 1","ECSS - Current v0.9","A.2.1<7>a","Requirement","ECSS-M-ST-10_0010075",1,"Created","The PMP shall describe the cost and schedule management approach, as defined in ECSS-M-ST-60."]
["ECSS-M-ST-10C Rev. 1","ECSS - Current v0.9","B.2.1<3>e","Requirement","ECSS-M-ST-10_0010089",1,"Created","When recurrent products from previous space projects are used, they shall be identified in the tree structure."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.1.2c","Requirement","ECSS-M-ST-40_0320023",1,"Created","The configuration item list shall be provided at the PDR for customer approval."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.1.6f","Requirement","ECSS-M-ST-40_0320044",1,"Created","The system shall be able to generate any current, baseline or past version of the file. "]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.1.6k","Requirement","ECSS-M-ST-40_0320049",1,"Created","Digital data media shall be identified by the following:\n    1. CI identifier\n    2. File names\n    3. Version and issue\n    4. Date of generation\n    5. Generating entity\n    6. Total number of delivered media per information set (1 of ...)."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.2.6b","Requirement","ECSS-M-ST-40_0320072",1,"Created","The supplier shall request unplanned departures from requirements or design using a request for waiver in conformance with Annex J, request for waiver DRD."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.4.1c","Requirement","ECSS-M-ST-40_0320096",1,"Created","At CDR, the design definition shall be verified against the relevant design documentation."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.7.2.4b","Requirement","ECSS-M-ST-40_0320121",1,"Created","Configuration management requirements shall be taken into account for documents that are part of a configuration baseline."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","5.3.7.3.3d","Requirement","ECSS-M-ST-40_0320144",1,"Created","A Log-File of the processing steps of approval shall be generated automatically by the information system. "]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","A.2.1<4.1>b","Requirement","ECSS-M-ST-40_0320168",1,"Created","The configuration management plan shall introduce the following, as a minimum:\n    1. configuration identification;\n    2. configuration control;\n    3. configuration status accounting;\n    4. configuration audits and reviews;\n    5. interface control;\n    6. supplier control."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","A.2.1<4.3>a","Requirement","ECSS-M-ST-40_0320173",1,"Created","The configuration management plan shall describe the configuration control process and data for implementing changes to the configuration items and identify the records to be used for tracking and documenting the sequence of steps for each change."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","A.2.1<5.3>b","Requirement","ECSS-M-ST-40_0320194",1,"Created","The configuration management plan shall describe the handling of legacy documentation and \"off-the-shelf\" documentation."]
["ECSS-M-ST-40C Rev. 1","ECSS - Current v0.9","E.2.1<9>a","Requirement","ECSS-M-ST-40_0320226",1,"Created","The SCF shall describe how to install the software configuration item version, its means and procedures necessary to install the product and to verify its installation. "]
["ECSS-M-ST-60C","ECSS - Current v0.9","7.2a","Requirement","ECSS-M-ST-60_0300008",1,"Created","The supplier shall identify from the risk register, established in conformance with ECSS-M-ST-80, those risk elements of explicit relevance to Cost and Schedule management."]
["ECSS-M-ST-60C","ECSS - Current v0.9","9.2.1c","Requirement","ECSS-M-ST-60_0300029",1,"Created","The supplier shall provide a project cost estimating report in conformance with Annex G, Cost estimate report DRD."]
["ECSS-M-ST-60C","ECSS - Current v0.9","9.2.5a","Requirement","ECSS-M-ST-60_0300036",1,"Created","The supplier shall propose a Price Variation Mechanism to be applied during execution of the work."]
["ECSS-M-ST-60C","ECSS - Current v0.9","9.3.7a","Requirement","ECSS-M-ST-60_0300056",1,"Created","In the case of a cost reimbursement contract, the customer shall have the right to audit, either itself or through an authorized representative (relevant national authority or international organization), the claimed expenses against the internal company accounts, in conformance with ECSS-M-ST-10."]
["ECSS-M-ST-60C","ECSS - Current v0.9","F.2.1<3.3>a","Requirement","ECSS-M-ST-60_0300081",1,"Created","The cost estimating plan shall:\n    1. describe the process for acquiring, processing and maintaining reference data for developing models,\n    2. address how the input data is gathered, and\n    3. explain how clarification interviews of specialists are carried out"]
["ECSS-M-ST-60C","ECSS - Current v0.9","H.2.1<2>a","Requirement","ECSS-M-ST-60_0300105",1,"Created","The milestone table shall include:\n    1. Milestone number and nature of payment (advance payment, progress payment, final payment)\n    2. Milestone definition\n    3. Milestone achievement date (indicative information)\n    4. Milestone amount"]
["ECSS-M-ST-60C","ECSS - Current v0.9","L.2.1<2>a","Requirement","ECSS-M-ST-60_0300121",1,"Created","The OBCP (respectively CBCP) shall list the applicable and reference documents supporting the generation of the document, such as the applicable business agreements, minutes of meeting, complete list of the agreed CCNs taken into account."]
["ECSS-M-ST-80C","ECSS - Current v0.9","A.2.1<5>a","Requirement","ECSS-M-ST-80_0340022",1,"Created","The risk management policy document shall provide an overview of the risk management approach, to include the status of the risk management effort, and a description of the project risk management strategy consistently deriving from the project’s objectives."]
["ECSS-M-ST-80C","ECSS - Current v0.9","B.2.1<7>a","Requirement","ECSS-M-ST-80_0340043",1,"Created","The risk management plan shall describe how the risk management process is implemented."]
["ECSS-M-ST-80C","ECSS - Current v0.9","C.2.1<4>a","Requirement","ECSS-M-ST-80_0340059",1,"Created","The assessment report shall describe how the risks in question were identified, which inputs, method, tool(s) were used, and which people were involved. "]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.2.2a","Requirement","ECSS-Q-ST-20_0380008",1,"Unchanged","The supplier shall implement a nonconformance control system in conformance with ECSS-Q-ST-10-09."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.2.6i","Requirement","ECSS-Q-ST-20_0380030",1,"Unchanged","The supplier shall identify inspection, measuring and test equipment with a suitable indicator or approved identification record to show the calibration status."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.3.1.1a","Requirement","ECSS-Q-ST-20_0380051",2,"Unchanged","The supplier shall ensure that the product is designed such that it can be produced with the specified level of quality. "]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.3.2.4.3a","Requirement","ECSS-Q-ST-20_0380070",1,"Unchanged","The product used for qualification testing shall be produced in accordance with a full and clearly identified manufacturing and inspection file. "]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.4.4.4a","Requirement","ECSS-Q-ST-20_0380094",1,"Unchanged","The supplier shall maintain receiving inspection records to ensure traceability and the availability of historical data to monitor supplier performance and quality trends."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.5.1e","Requirement","ECSS-Q-ST-20_0380099",2,"Unchanged","The QA organization shall review and approve such documents, and any modifications thereof, to ensure that they include or refer to:\n1.\tIdentification of the item to be manufactured or equipment to be used.\n2.\tConfiguration data, including parts lists, drawings, changes and specifications.\n3.\tIdentification of the production and inspection equipment to be used for the manufacturing, assembly and integration of the item.\n4.\tIdentification of critical characteristics.\n5.\tDetailed definition, by description or reference, of manufacturing, assembly, integration, inspections and test operations to be performed, and special conditions to be maintained.\n6.\tProvisions for inspections and tests to be witnessed by customer representative.\n7.\tAccept or reject criteria (with tolerances) and workmanship standards.\n8.\tDetails of sampling inspection procedures to be used, if any.\n9.\tDetailed procedures for the activities to be performed.","NOTE \t1\tExamples for item 3, of production and inspection equipment are tools, jigs and fixtures.\nNOTE \t2\tCritical characteristics, for item 4, are defined in ECSS-Q-ST-30.\n"]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.5.6.1d","Requirement","ECSS-Q-ST-20_0380119",2,"Unchanged","The approval shall be marked in conformance with 5.2.4, and recorded."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.5.9.1a","Requirement","ECSS-Q-ST-20_0380144",1,"Unchanged","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."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.6.4f","Requirement","ECSS-Q-ST-20_0380167",1,"Unchanged","Testing shall be subject to the requirements for the control of hazardous operations.","NOTE\tDefinition of hazardous operations is given in ECSS-Q-ST-40.\n"]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.7.3g","Requirement","ECSS-Q-ST-20_0380182",2,"Unchanged","For the delivery a certificate of conformity, in conformance with Annex D, shall be made available and signed by the supplier.","NOTE\tCertificate of Conformity is also known as Declaration of Conformity.\n"]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","5.8.3.1b","Requirement","ECSS-Q-ST-20_0380193",2,"Normative Change","Procurement documents shall identify validation and receiving inspection requirements, and conform to the requirements in clause 5.4.2."]
["ECSS-Q-ST-20C Rev.2 Corr.1","ECSS - Current v0.9","C.2.1a","Requirement","ECSS-Q-ST-20_0380215",1,"Unchanged","The logbook cover page shall contain the following:\n1.\tgeneral information,\n2.\tcontents,\n3.\tapprovals of the relevant authorities (QA, PA, PM), and\n4.\tcustomer acceptance (if required by the business agreement).","NOTE\tAn example of a logbook cover page is given in Annex E.\n"]
["ECSS-Q-ST-70-54C","ECSS - Current v0.9","5.2.1c","Requirement","ECSS-Q-ST-70-54_1360012",1,"Created","The geometry of the witness plates shall be simplified to allow quantitative analysis by the selected techniques.","NOTE \tWitness plates can be installed in different hardware.\n"]
["ECSS-Q-ST-70-54C","ECSS - Current v0.9","5.2.7.1b","Requirement","ECSS-Q-ST-70-54_1360036",1,"Created","An overall cleaning efficacy shall be determined comprising all process steps specified in clause 5.2.7.1a."]
["ECSS-Q-ST-10-04C","ECSS - Current v0.9","5.1.1e","Requirement","ECSS-Q-ST-10-04_0180005",1,"Created","The supplier shall define evaluation points for assessing the implementation of critical-item control measures."]
["ECSS-Q-ST-10-04C","ECSS - Current v0.9","5.2.4.4a","Requirement","ECSS-Q-ST-10-04_0180030",1,"Created","The supplier shall implement the CI control strategy by applying the selected implementation methods."]
["ECSS-Q-ST-10-04C","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-10-04_0180051",1,"Created","This list shall uniquely identify the critical item."]
["ECSS-Q-ST-10-04C","ECSS - Current v0.9","A.2.1<6>a","Requirement","ECSS-Q-ST-10-04_0180057",1,"Created","This list shall contain the description of the cause which makes this item critical."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.2.1.3d","Requirement","ECSS-Q-ST-20-10_1120021",1,"Created","The supplier shall identify all the OTS item functions which can lead to negative effects."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.3.2.1.4b","Requirement","ECSS-Q-ST-20-10_1120042",1,"Created","The supplier shall verify the capability to switch-off the item in all conditions, considering also the case of internal item battery provision."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.3.2.1.9a","Requirement","ECSS-Q-ST-20-10_1120055",1,"Created","The supplier shall get data on the actual OTS item derating factors and on its proven heritage, and assess if OTS item derating is critical with respect to the mission requirements."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.3.2.3.2d","Requirement","ECSS-Q-ST-20-10_1120073",1,"Created","The supplier shall be able to track the supply chain back to the manufacturer of the OTS item."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.4.3.2a","Requirement","ECSS-Q-ST-20-10_1120094",1,"Created","The supplier shall verify the OTS item electrical requirements in accordance with ECSS-E-ST-20."]
["ECSS-Q-ST-20-10C","ECSS - Current v0.9","5.6.1.2c","Requirement","ECSS-Q-ST-20-10_1120123",1,"Created","The supplier shall check that the number of OTS items purchased in the same lot conform to the project needs and with the obsolescence strategy of the manufacturer."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","4.1e","Requirement","ECSS-Q-ST-30-02_0390005",1,"Created","All recommendations which result from the FMEA shall be evaluated, dispositioned and documented as part of the Dependability Recommendations in conformance with ECSS-Q-ST-30, clause 5.7)"]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","4.6b","Requirement","ECSS-Q-ST-30-02_0390026",1,"Created","The failure effects resulting from each failure mode shall be determined at the level of the item under investigation (local effect) and at the level of the product under analysis (end effect)."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","5.2n","Requirement","ECSS-Q-ST-30-02_0390051",1,"Created","The CN shall be calculated as the product of the ranking assigned to each factor: CN = SN x PN."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","6.5b","Requirement","ECSS-Q-ST-30-02_0390069",1,"Created","The FMEA/FMECA shall allow to verify that the design fulfil the dependability and safety requirements, allocated to all of the project levels (system, subsystem and lower levels) in phase B. "]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","7.2a","Requirement","ECSS-Q-ST-30-02_0390078",1,"Created","The HSIA shall be performed concurrently with the FMEA/FMECA to influence the hardware design and the software requirements."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","8.6.2a","Requirement","ECSS-Q-ST-30-02_0390104",1,"Created","An actionee and a due date shall be entered for the implementation. "]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","A.2.1<6>a","Requirement","ECSS-Q-ST-30-02_0390117",1,"Created","The FMEA/FMECA report shall include block diagrams and schematics to assist in describing the product, provide schematic diagrams, functional block diagrams and reliability block diagrams (RBDs) to a level consistent with the depth of the analysis and with design maturity.\n    NOTE Functional tree is also useful to describe functional relationships."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","D.2.1<4>a","Requirement","ECSS-Q-ST-30-02_0390151",1,"Created","The HSIA form shall contain a summary of failure mode description."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","F.2.1<7>a","Requirement","ECSS-Q-ST-30-02_0390176",1,"Created","The Process FMECA worksheet shall contain the description of the existing means and methods by which the effects can be detected."]
["ECSS-Q-ST-30-02C","ECSS - Current v0.9","F.2.1<8>a","Requirement","ECSS-Q-ST-30-02_0390177",1,"Created","The Process FMECA worksheet shall contain the description of the existing preventive or compensatory provisions to prevent the failure mode, to reduce its effects, or to reduce its probability of occurrence."]
["ECSS-Q-ST-30-09C","ECSS - Current v0.9","5.2.5a","Requirement","ECSS-Q-ST-30-09_0400017",1,"Created","In the specific case that the availability is specified by an outage distribution and duration, and if a maximum duration is specified, a probability of exceeding this duration shall be associated.\n    NOTE 1 This can apply at subsystem level when a short service interruption is masked or filtered by the upper level function.\n    NOTE 2 For example, typically a GPS receiver temporary outage is tolerated by a navigation model. For this type of application, numerous short outages would be preferable to a few long ones."]
["ECSS-Q-ST-30-09C","ECSS - Current v0.9","7.2.1a","Requirement","ECSS-Q-ST-30-09_0400042",1,"Created","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)."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","4.1.2c","Requirement","ECSS-Q-ST-60-02_0450004",1,"Created","In case of major problems, the development team, as allocated in the development plan (see 4.3.1), shall directly report to the component advisory board as defined in ECSS-Q-ST-60."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","5.3.3.2a","Requirement","ECSS-Q-ST-60-02_0450022",1,"Created","As a tool of the quality assurance system (see clause 6.3) a risk analysis shall be performed that identifies potential risk items and assigns preventive measures and contingency plans."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","5.5.2c","Permission","ECSS-Q-ST-60-02_0450202",1,"Created","For FPGAs and analog designs, a combined DDR and CDR meeting may be justified. \n    NOTE In these cases also the corresponding output reports can be merged together."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","5.5.3d","Requirement","ECSS-Q-ST-60-02_0450056",1,"Created","Implement the specified radiation hardening concept by design and during synthesis."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","5.6.3a","Requirement","ECSS-Q-ST-60-02_0450077",1,"Created","As a minimum the following tasks shall be performed and documented in a layout verification report:\n    1. layout design rule check (DRC);\n    2. electrical rule check (ERC), check cross-talk sensitivity, if required by customer;\n    3. extract a netlist from the layout given in terms of IDMP;\n    4. verify that the gate-level netlist is consistent with the layout by performing a layout versus schematic (LVS) comparison, i.e. a netlist comparison check (NCC) between the post-layout netlist and the layout (IDMP) extracted netlist;\n    5. verify that the post-layout netlist is consistent in terms of functionality with the pre-layout netlist by simulation and formal methods;\n    6. extract the parasitic information;\n        NOTE This delivers capacitance, resistance and inductivity values (only deep sub-micron technology), from which the actual delays are calculated for digital designs.\n    7. perform comprehensive post-layout verification according to the verification plan;\n        NOTE This is mostly accomplished by back-annotated simulations and timing analysis\n    8. check the resulting clock skew and latency; \n        NOTE This is not applicable for FPGA designs.\n    9. check relevant timing of I/Os; \n    10. check the power distribution on the chip; \n        NOTE This is not applicable for FPGA designs.\n    11. perform transition check and load check on the nets inside the ASIC;\n    12. characterize ASIC and FPGA timing performances, \n        NOTE For example: max clock frequency, clock duty cycle, set-up and hold times for all inputs and propagation delays for all outputs."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","5.8.3e","Requirement","ECSS-Q-ST-60-02_0450108",1,"Created","The suppler shall ensure the storage of the complete design database during the lifetime of the product, including associated data, documentation, pattern generation files, test program(s) and mask sets used."]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","6.1f","Requirement","ECSS-Q-ST-60-02_0450128",1,"Created","All technology independent CAD tools to be employed during the development shall be mature and fit for their purpose. "]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","7.1e","Requirement","ECSS-Q-ST-60-02_0450149",1,"Created","Block diagrams, control flow charts, timing diagrams and other figures shall be introduced where beneficial for the understanding of the text. "]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","7.3.1.2b","Requirement","ECSS-Q-ST-60-02_0450155",1,"Created","All intermediate design data shall be reproducible to assist possible iterations. "]
["ECSS-Q-ST-60-02C","ECSS - Current v0.9","A.2.1c","Requirement","ECSS-Q-ST-60-02_0450180",1,"Created","Initiation of the definition phase for the ASIC and FPGA developments."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","5.2.2a","Requirement","ECSS-Q-ST-60-05_0160005",1,"Created","A supplier wishing to use (or manufacture) hybrid circuits from a production line that has not been approved by the approving authority shall:\n    1. justify its requirements to the customer (especially if this involves developing a new circuit), and \n    2. satisfy the validation conditions described in Clause 6."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","7.1.2b","Requirement","ECSS-Q-ST-60-05_0160030",1,"Created","When selecting the technology in conformance with 7.1.2a.1, the technology shall be as specified in the PID and described in the hybrid technology identification form (HTIF) specified in Annex A."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","7.3.4d","Permission","ECSS-Q-ST-60-05_0160239",1,"Created","The customer may reject the case for a recurrent circuit if the information supplied is considered to be inadequate."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","8.3.3.2.3a","Requirement","ECSS-Q-ST-60-05_0160077",1,"Created","User LAT shall be performed either on actual MMICs or on TCVs (technological characterization vehicles present on the same wafer of the MMICs) providing that these TCV dies are designed in conformance with the design manual of the MMIC foundry."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","8.4b","Requirement","ECSS-Q-ST-60-05_0160082",1,"Created","The hermetically encapsulated components to be used on hybrids shall be procured in conformance with component selection requirements of ECSS-Q-ST-60, or fully tested and screened in conformance with a procedure that is agreed upon by the approving authority during capability approval, and specified in the PID."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","10.3.2d","Requirement","ECSS-Q-ST-60-05_0160114",1,"Created","If an infrared microscope is used, the circuit shall be coated to obtain a uniform emissivity factor from the metallization surfaces. \n    NOTE This test is destructive."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","10.3.9b","Requirement","ECSS-Q-ST-60-05_0160130",1,"Created","If another temperature is selected, the burn-in duration shall be adjusted in conformance with MIL-STD-883 method 1015."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","10.5.2f","Requirement","ECSS-Q-ST-60-05_0160151",1,"Created","It shall be demonstrated that the reliability of the remaining elements is not impacted."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","12.2.1.4a","Requirement","ECSS-Q-ST-60-05_0160176",1,"Created","For a manufacturer pending capability approval, the lot(s) produced and approved in conformance with the procedure described above shall not be delivered to the project until the approving authority has approved the production line."]
["ECSS-Q-ST-60-05C Rev. 1","ECSS - Current v0.9","14a","Requirement","ECSS-Q-ST-60-05_0160196",1,"Created","DPA test sequence depends on the technology and shall be performed in conformance with the following methods: \n    1. External visual inspection, MIL-STD-883 Method 2009.8.\n    2. X-rays (if soldered items or gold wires are present), MIL-STD-883 Method 2012.\n    3. SAM inspection, MIL-STD-883 Method 2030.\n    4. Seal test, MIL-STD-883 Method 1014 Condition A2 - Condition C.\n    5. PIND test, MIL-STD-883 Method 2020 Condition A.\n    6. Internal visual inspection, MIL-STD-883 Method 2017 Class K, MIL-STD-883 Method 2010 Condition A, MIL-STD-750 Method 2072, MIL-STD-750 Method 2073, MIL-STD-883 Method 2032.\n    7. MIL-STD-750 Method 2073.\n    8. SEM inspection, MIL-STD-883 Method 2018 (Provide photos of typical assemblies and possible anomalies).\n    9. Bond pull test, MIL-STD-883 Method 2011 Condition D (Pull all wires).\n    10. Die shear test, MIL-STD-883 Method 2019 (Shear all chips)."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","4.2a","Requirement","ECSS-Q-ST-60-12_0190001",1,"Created","The following steps involved in procuring MMICs for Space applications shall be followed:\n    1. Process selection, in conformance with clause 5.\n    2. Allocation of responsibilities, in conformance with clause 6.\n    3. MMIC design, in conformance with clause 7.\n    4. Application approval, in conformance with clause 8\n    5. Procurement and LAT specifications, in conformance with clause 9.\n    6. Die form procurement sequences, in conformance with clause 10."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","5.1.2b","Requirement","ECSS-Q-ST-60-12_0190006",1,"Created","The MMIC design shall be analysed and validated in terms of application domain compared to the qualification domain and space application requirements.\n    NOTE The qualification domain is documented in terms of the following boundaries with respect to any potential failure mode identified on the process:\n        · The physical design and procedures that are closely related to the manufacturing process (no major process change identified since the evaluation testing).\n        · The electrical design in term of extreme limits (thermal, DC and RF parameters).\n        · Function (e.g. oscillator, gain block), and application (e.g. small signal, pulsed, high drive).\n        · The performances, the reliability figures, and the environmental resistance."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","7.2.8d","Requirement","ECSS-Q-ST-60-12_0190042",1,"Created","The analysis specified in requirement 7.2.8a shall also include the effect of feedback paths caused by the following: \n    1. the biasing elements (on and off-die);\n    2. the final packaging;\n    3. the effects of process variations, temperature, and slight changes of biasing conditions."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","7.2.10b","Recommendation","ECSS-Q-ST-60-12_0190230",1,"Created","A hierarchical design should be used. "]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","7.3.6a","Requirement","ECSS-Q-ST-60-12_0190078",1,"Created","The designer shall provide the derating for each passive or active element, calculated from the manufacturer maximum rating. "]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","8.1b","Requirement","ECSS-Q-ST-60-12_0190099",1,"Created","Dedicated test flow and test procedures shall be implemented in conformance with requirements in clause 8.2."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","9b","Requirement","ECSS-Q-ST-60-12_0190107",1,"Created","A MMIC lot acceptance specification for user LAT shall be issued by the supplier in conformance with Annex F."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","10.2.4.4b","Requirement","ECSS-Q-ST-60-12_0190130",1,"Created","The assembly test sequence shall be performed by sampling rejected dies (assembled using the manufacturer process) from the wafers manufactured, and includes the following:\n    1. A bond pull test on 10 wires as per MIL-STD-883 method 2011.No failures allowed.\n    2. A die shear test on 2 parts as per MIL-STD-883 method 2019.No failure allowed."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","10.3.2g","Requirement","ECSS-Q-ST-60-12_0190151",1,"Created","The shear test on mounted dies shall be according to MIL-STD-883 method 2019 on 4 dies. No failure allowed."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","10.4.3f","Requirement","ECSS-Q-ST-60-12_0190175",1,"Created","If the parts are epoxy die attached, the same restrictions as given in requirement 10.4.2f shall apply and the calculations for the duration of the test shall be based on the same acceleration factor."]
["ECSS-Q-ST-60-12C","ECSS - Current v0.9","10.5d","Requirement","ECSS-Q-ST-60-12_0190202",1,"Created","Any relevant failures (see requirement 10.5f) observed in assembly tests shall be included in a nonconformance sheet and the problem subjected to a review. "]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.1.2.1c","Recommendation","ECSS-Q-ST-70-01_0500258",1,"Created","The CRS should be prepared in collaboration with users and engineers from the different disciplines.\n    NOTE Users can be, for example, experimenters or scientists."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.1.4a","Requirement","ECSS-Q-ST-70-01_0500010",1,"Created","As part of the C&CCP (see Annex B), particulate and molecular contamination predictions shall be established.\n    NOTE Contamination predictions are done in order to estimate the expected on ground and in-orbit molecular and particulate contamination levels."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.2.2.2c","Requirement","ECSS-Q-ST-70-01_0500043",1,"Created","When an exposure of sensitive and critical elements cannot be avoided, the exposure time and conditions shall be recorded."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.2.3.1c","Requirement","ECSS-Q-ST-70-01_0500057",1,"Created","The potential contamination during launch preparation shall be also controlled.\n    NOTE This can be done through the C&CCP or through specific launch base procedures approved by the project."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.3.1.5b","Requirement","ECSS-Q-ST-70-01_0500082",1,"Created","Accuracy and repeatability of instrumentation shall be demonstrated."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.3.1.5j","Requirement","ECSS-Q-ST-70-01_0500090",1,"Created","Air monitoring of class ISO 8 or better shall be achieved by means of light scattering equipment."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.3.1.9d","Requirement","ECSS-Q-ST-70-01_0500109",1,"Created","Pressure in all areas shall be monitored continuously\n    NOTE In order to take timely corrective actions in case of a pressure drop."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.3.1.13g","Requirement","ECSS-Q-ST-70-01_0500130",1,"Created","Barriers or similar means separating clean and not clean zones inside the airlock shall be placed.\n    NOTE Similar means can be tacky mats."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.4.1.1b","Requirement","ECSS-Q-ST-70-01_0500155",1,"Created","The choice of the cleaning method shall be determined by the following criteria: \n    1. The type of contaminants to be removed.\n    2. The physical or chemical nature of the item to be cleaned.\n    3. The actual on ground phase.\n        NOTE 1 Examples are provided in Annex M for removal of both particulate and molecular contamination.\n        NOTE 2 The cleaning of some parts is particularly important during the course of manufacture or before processing (e.g. prior to bonding, painting, vacuum, coating, welding and soldering).\n        NOTE 3 Any detrimental effect of cleaning is evaluated as well as the order of the defined cleaning methods.\n        NOTE 4 For those items that are too delicate to withstand cleaning, preventive contamination control is of the utmost importance."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.4.2.3a","Requirement","ECSS-Q-ST-70-01_0500172",1,"Created","Molecular contamination shall be monitored through visual inspection and quantitative methods directly on the surface (including witnesses) or indirectly after transfer of contaminants.\n    NOTE 1 Surfaces can be examined by the same visual inspection methods as for particulate contamination. Experience with Micro-VCM tests has shown that, generally, levels of organic contamination above 1 ´ 10-6 g/cm2 can already be visible to the naked eye. By wet wiping of a portion of the surface or after evaporation of a droplet of a substrate compatible solvent, a contamination can be revealed by contrast. \n    NOTE 2 A surface of a known area is wiped with a clean tissue, the tissue is subjected to extraction with chloroform of spectral grade, and the residue of the chloroform is analysed by infrared techniques in accordance with ECSS-Q-ST-70-05. This method, applied to a wiped area of 100 cm2, permits detection of organic contamination levels down to 3 10-9 g/cm2. The results of this method depend very much on the surface roughness, on the type of tissue and on the solvent used. Particular attention is paid to the compatibility between solvent and surface.\n    NOTE 3 A surface of a known area is rinsed with a solvent and the residue is weighed after evaporation according to ASTM-E1235M-95.. The accuracy and detection limit of this method depend greatly upon the sensitivity of the balance, the substrate water absorption, the washing efficiency and the solvent background. The NVR measurement is expressed in mass per unit area and the residue can be used for further analyses). Direct measurements can be made in situ using quartz crystal microbalances (QCM).\n    NOTE 4 Further analyses can be performed to characterize molecular contamination (e.g. gas chromatography, mass spectrometry, ultra-violet degradation, SEM)."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","5.4.4d","Requirement","ECSS-Q-ST-70-01_0500202",1,"Created","Storage areas shall provide adequate protection to the package and the product for the intended storage period."]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","A.2.1<4>a","Requirement","ECSS-Q-ST-70-01_0500227",1,"Created","The CRS shall specify all cleanliness requirements allocated to the major integration and testing phases. "]
["ECSS-Q-ST-70-01C","ECSS - Current v0.9","B.2.1<6>b","Requirement","ECSS-Q-ST-70-01_0500240",1,"Created","References for internal procedures dedicated to area or facilities verification, control and maintenance shall be included."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.1a","Requirement","ECSS-Q-ST-70-02_0510001",1,"Created","For those materials that are subjected, during the mission, to temperature above 125 °C for short period of time (in the order of hours) or above 50 °C for an extended period of time (in the order of weeks or above), dedicated tests shall be performed at conditions representative of the real application (i.e. higher temperature tests). "]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.2.4.2a","Requirement","ECSS-Q-ST-70-02_0510026",1,"Created","The apparatus shall consist of an insert located in a common-type vacuum system suitably dimensioned with respect to the insert, able to accommodate the necessary feedthroughs."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.3.2.2e","Requirement","ECSS-Q-ST-70-02_0510047",1,"Created","During the test, the supplier shall place collector plates in front of each cup. "]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.4b","Requirement","ECSS-Q-ST-70-02_0510073",1,"Created","The supplier shall report the results in a micro VCM datasheet form in conformance with Annex C.\n    NOTE The outgassing data are given down to 0,01 % for normal tests, and for tests with increased sensitivity these figures can be one order of magnitude lower."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.7.2.2a","Requirement","ECSS-Q-ST-70-02_0510098",1,"Created","The customer shall inspect the following parts of the Micro-VCM apparatus:\n    1. internal dimensions, view factor (sample compartment to collector plates) and cross contamination protection;\n    2. pumping system and associated monitoring equipment;\n    3. temperature regulation of sample and collector plates and associated monitoring equipment;\n    4. thermal contact of the temperature sensors."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","5.7.2.2b","Requirement","ECSS-Q-ST-70-02_0510099",1,"Created","The customer shall inspect the following associated equipment:\n    1. precision balance (reading to 1 mg);\n    2. temperature and relative humidity in the balance room is controlled to obtain the required accuracy and reproducibility;\n    3. room for sample pre- and post conditioning;\n    4. vacuum oven for bakeout of collector plates;\n    5. clean sample preparation room;\n    6. infrared apparatus (optional)."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-70-02_0510120",1,"Created","The materials identification card shall contain the following information:\n    1. Trade name and number\n    2. Manufacturer\n    3. Type of product\n    4. Chemical nature\n    5. Processing details."]
["ECSS-Q-ST-70-02C","ECSS - Current v0.9","D.2.1<8>a","Requirement","ECSS-Q-ST-70-02_0510150",1,"Created","The report shall contain details of failure mode."]
["ECSS-Q-ST-70-03C","ECSS - Current v0.9","5.4.2a","Requirement","ECSS-Q-ST-70-03_0520019",1,"Created","An electrical contact shall be employed for each part to be anodized."]
["ECSS-Q-ST-70-03C","ECSS - Current v0.9","5.5.2e","Requirement","ECSS-Q-ST-70-03_0520036",1,"Created","Mechanical damage shall be avoided by packing the polyethylene- or polypropylene-wrapped work-pieces in clean, dust- and lint-free material."]
["ECSS-Q-ST-70-04C","ECSS - Current v0.9","5.1.1b","Requirement","ECSS-Q-ST-70-04_0530002",1,"Created","ECSS-Q-ST-20 shall be made applicable in the request for thermal cycling test."]
["ECSS-Q-ST-70-04C","ECSS - Current v0.9","5.1.2.1b","Requirement","ECSS-Q-ST-70-04_0530007",1,"Created","Air used for ventilation shall be nominally filtered to prevent contamination of the sample."]
["ECSS-Q-ST-70-04C","ECSS - Current v0.9","5.2.2.4c","Requirement","ECSS-Q-ST-70-04_0530032",1,"Created","Coated surfaces shall be shielded from contact by using polyethylene or polypropylene bags or sheets. "]
["ECSS-Q-ST-70-04C","ECSS - Current v0.9","C.2.1a","Requirement","ECSS-Q-ST-70-04_0530058",1,"Created","The thermal cycling test report shall include or refer to the following information:\n    1. description of the purpose, objective, content and the reason prompting its preparation,\n    2. description of the thermal cycling test facility,\n    3. description of the item to be tested or a reference to the document containing its identification characteristics,\n        NOTE For example: request for thermal cycling test.\n    4. calibration tools,\n    5. the actual thermal cycling test procedures or a reference to the document containing the description of the test procedure (e.g. thermal cycling test specifications and procedures DRD),\n    6. the test results,\n    7. discussion about the test results,\n    8. conclusion and recommendations."]
["ECSS-Q-ST-70-06C","ECSS - Current v0.9","5.1.3.2c","Requirement","ECSS-Q-ST-70-06_0550021",1,"Created","The supplier shall evaluate the integrated irradiance of the source outside of the lL to lH wavelength range.\n    NOTE This additional irradiance can contribute to degradation and additional heating of the samples."]
["ECSS-Q-ST-70-06C","ECSS - Current v0.9","5.2.2e","Requirement","ECSS-Q-ST-70-06_0550042",1,"Created","Samples shall be stored in a clean area."]
["ECSS-Q-ST-70-06C","ECSS - Current v0.9","B.2.1<2>e","Requirement","ECSS-Q-ST-70-06_0550068",1,"Created","The test procedure for controlling and monitoring the contamination shall contain the following information:\n    1. contamination check methods used during tests,\n    2. contamination results."]
["ECSS-Q-ST-70-06C","ECSS - Current v0.9","B.2.1<5>a","Requirement","ECSS-Q-ST-70-06_0550073",1,"Created","The source characterization information shall contain:\n    1. operational conditions (operating range, maximum ratings),\n    2. energies, spectral range,\n    3. deviation between the Solar Spectrum and the source,\n    4. dose rates/ instantaneous doses/ total dose (taking into account energy distribution),\n    5. selected acceleration factors,\n    6. size and uniformity of irradiated surface, used method to cover large surfaces (optics, sweeping plates, diffusion window),\n    7. ageing of the source."]
["ECSS-Q-ST-70-09C","ECSS - Current v0.9","4.1.3.2a","Requirement","ECSS-Q-ST-70-09_0580014",1,"Created","The ambient conditions for the process and work areas shall be (22 ± 3) °C with a relative humidity of (55 ± 10) % unless otherwise stated."]
["ECSS-Q-ST-70-09C","ECSS - Current v0.9","B.2.1c","Requirement","ECSS-Q-ST-70-09_0580039",1,"Created","The review report shall describe the mutual comparability evaluation (testing)."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.1.2a","Requirement","ECSS-Q-ST-70-18_0620008",1,"Created","The supplier shall have an assembly area which has a controlled environment that limits entry of contamination."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.2.3c","Requirement","ECSS-Q-ST-70-18_0620045",1,"Created","The supplier shall label the solvents and maintain them in a clean and uncontaminated condition."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.2.4b","Requirement","ECSS-Q-ST-70-18_0620050",1,"Created","The supplier shall procure semi-rigid cable with outer conductor diameter standardized as either 0,085 inches or 0,141 inches (±0,001 inches) and fabricated from copper.\n    NOTE The outer conductor can be finished with silver plating."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.3.5.2c","Requirement","ECSS-Q-ST-70-18_0620080",1,"Created","The supplier shall place the entire cable in the thermal cycling arrangement."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.4.2e","Requirement","ECSS-Q-ST-70-18_0620097",1,"Created","The supplier shall pretin the cable’s outer and inner conductors."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.5.1.1.2e","Requirement","ECSS-Q-ST-70-18_0620122",1,"Created","After the solder has solidified and cooled, the supplier shall clean the joint with one of the solvent cleaners specified in clause 5.2.3."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.5.2b","Requirement","ECSS-Q-ST-70-18_0620143",1,"Created","The supplier shall submit these procedures for customer acceptance.\n    NOTE This acceptance can involve a customer audit of the facilities and procedures used for assembling the cables and connectors."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.6.1k","Requirement","ECSS-Q-ST-70-18_0620162",1,"Created","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."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.8.4a","Requirement","ECSS-Q-ST-70-18_0620190",1,"Created","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."]
["ECSS-Q-ST-70-18C","ECSS - Current v0.9","5.8.7a","Requirement","ECSS-Q-ST-70-18_0620195",1,"Created","The supplier shall employ trained and competent personnel for all soldering and crimping operations and inspections."]
["ECSS-Q-ST-70-20C","ECSS - Current v0.9","5.4.1a","Requirement","ECSS-Q-ST-70-20_0630023",1,"Created","The supplier shall establish an evaluation report in conformance with Annex A"]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.1.1a","Requirement","ECSS-Q-ST-70-21_0640001",1,"Created","The supplier shall isolate hazardous substances, items and operations from other activities."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.2.2.2f","Requirement","ECSS-Q-ST-70-21_0640026",1,"Created","If the spacecraft substrate is not available, the coatings shall be applied to 300 mm x 60 mm x 0,075 mm aluminium panels."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.2.2.4c","Requirement","ECSS-Q-ST-70-21_0640031",1,"Created","Internal lighting shall be installed."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.2.3.1a","Requirement","ECSS-Q-ST-70-21_0640054",1,"Created","The supplier shall use this procedure to determine the concentration limit of oxygen (Clim) during the combustion of candidate materials.\n    NOTE This test is based on RKK Energia test method ZZU.0336.028."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.2.4.2d","Requirement","ECSS-Q-ST-70-21_0640078",1,"Created","The supplier shall clean the specimens of foreign matter and residue, using a method compatible with the insulation being tested."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.1.2.4.12a","Recommendation","ECSS-Q-ST-70-21_0640156",1,"Created","The supplier should run the pre-test procedure as described in annex B.3.1."]
["ECSS-Q-ST-70-21C","ECSS - Current v0.9","5.2.3a","Requirement","ECSS-Q-ST-70-21_0640122",1,"Created","The supplier shall calibrate any measuring equipment to traceable reference standards."]
["ECSS-Q-ST-70-22C","ECSS - Current v0.9","4.1.2.1a","Requirement","ECSS-Q-ST-70-22_0170003",1,"Created","For procurement specifications and purchase orders, the date of manufacture, storage conditions and shelf-life of the products shall be declared."]
["ECSS-Q-ST-70-22C","ECSS - Current v0.9","4.2.2b","Requirement","ECSS-Q-ST-70-22_0170024",1,"Created","Any suspected or actual equipment failure shall be recorded as a project nonconformance report according to the NCR DRD in ECSS-Q-ST-10-09.\n    NOTE This is to ensure that previous results are examined to ascertain whether or not re-inspection and retesting is necessary."]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.1.1a","Requirement","ECSS-Q-ST-70-28_0150001",1,"Created","The supplier shall define and implement procedures to control hazards to personnel, equipment or materials."]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.6.1b","Requirement","ECSS-Q-ST-70-28_0150029",1,"Created","It shall be verified that no damage occurs to the printed wiring assembly by cutting around the area to be repaired."]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.9.2b","Requirement","ECSS-Q-ST-70-28_0150048",1,"Created","The maximum wire diameter shall not be greater than two thirds of the width of the conductor."]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.13.1b","Requirement","ECSS-Q-ST-70-28_0150073",1,"Created","If the wire is shaped to by-pass a component, the wire shall have additional fixing at each bend."]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.14.1.2a","Requirement","ECSS-Q-ST-70-28_0150080",1,"Created","The supplier shall extend the leads for an equal distance on each side of the component by means of the lap joint method defined in Annex H or the wraparound method of clause “Turret and straight pin terminals” of ECSS-Q-ST-70-08. "]
["ECSS-Q-ST-70-28C","ECSS - Current v0.9","4.17.1b","Requirement","ECSS-Q-ST-70-28_0150100",1,"Created","No more than two leads shall be cropped or insulated on each side of a 14-lead DIL package"]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","5.1b","Requirement","ECSS-Q-ST-40_0440002",1,"Unchanged","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 ","NOTE \t1\tFor tailoring, refer to clause 1.\nNOTE \t2\tThe 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.\nNOTE \t3\tAs support to tailoring, informative Annex F provides a guideline for determining the applicability of this standard depending on the type of project.\n"]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","5.6a","Requirement","ECSS-Q-ST-40_0440023",1,"Unchanged","The safety critical items shall be part of the project's overall critical items control programme as specified in ECSS-Q-ST-10-04."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","5.7.1.6a","Requirement","ECSS-Q-ST-40_0440039",1,"Unchanged","Safety analysis shall evaluate all disposal operations and associated hazards. "]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","5.11.2d","Requirement","ECSS-Q-ST-40_0440070",1,"Unchanged","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."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.3.3.4.4b","Requirement","ECSS-Q-ST-40_0440095",2,"Normative Change","The safety devices, specified in 6.3.3.4.4a, shall not be dependent on human performance."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.3.6a","Requirement","ECSS-Q-ST-40_0440108",1,"Unchanged","Safety monitoring, display, alarm and safing capabilities shall be incorporated for manned space systems."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.3.6p","Requirement","ECSS-Q-ST-40_0440123",1,"Unchanged","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."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.4.1k","Requirement","ECSS-Q-ST-40_0440322",1,"Created","The criticality of a function implemented in the space system shall be assigned in accordance with the severity of identified hazardous events it can cause, following the categories defined in Table 6-2.","NOTE \tHazardous events can result from a function not executed or executed degraded, incorrectly, untimely, out of the specified time interval, out of sequence or inadvertently.\n"]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.5.3a","Requirement","ECSS-Q-ST-40_0440168",1,"Unchanged","The system shall provide failure tolerance and redundancy status information of safety-critical functions."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.6.1e","Requirement","ECSS-Q-ST-40_0440183",1,"Unchanged","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."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.6.3.6b","Requirement","ECSS-Q-ST-40_0440209",1,"Unchanged","All GSE shall conform to the ‘Essential Health & Safety Requirements’ of all applicable EU ‘New Approach directives’. "]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","6.6.3.6c","Requirement","ECSS-Q-ST-40_0440210",1,"Unchanged","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’."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","7.5.3a","Requirement","ECSS-Q-ST-40_0440230",1,"Informative Change","Safety risk assessment shall \n1.\tcomprise the identification, classification and ranking of safety risks and their contributors,\n2.\tbe based on deterministic hazard analysis by combining the consequence severity and the likelihood of occurrence of the consequence,\n3.\tbe used to facilitate effective and efficient safety risk reduction and control, \n4.\tsupport project risk management as defined in ECSS-M-ST-80, \n5.\tassess compliance with probabilistic safety targets.","NOTE \t1\tThe estimation of event likelihoods is based on the use of different sources of data i.e.: \n·\tprevious experience on the particular system (i.e. measured or observed directly relevant test or experience data), \n·\tdata from other systems or projects (i.e. extrapolation from generic data, similarity data, or physical models), and \n·\texpert judgment (i.e. direct estimation of likelihoods by domain specialists).\nNOTE \t2\tThe determination of likelihood is not a mean to downgrade the criticality of function.\n"]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","8.2.2a","Requirement","ECSS-Q-ST-40_0440261",1,"Unchanged","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."]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","8.4.2b","Requirement","ECSS-Q-ST-40_0440282",1,"Unchanged","Safety-critical function qualification testing shall include the determination of performance margins considering worst case combinations of induced and natural environments and operating conditions. "]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","C.2.1<6>a","Requirement","ECSS-Q-ST-40_0440307",1,"Unchanged","The input of \"yes\" or \"no\" shall indicate whether the verification has to be performed independently (in accordance with 8.4.5b). "]
["ECSS-Q-ST-40C Rev.1","ECSS - Current v0.9","D.2.1<2>a","Requirement","ECSS-Q-ST-40_0440316",1,"Unchanged","The safety analysis report shall identify the following general information:\n1.\tthe project documentation identification number, the title of the safety analysis  report, date of release and release authority;\n2.\tthe project phase;\n3.\tidentification of which organizational entity prepared the document;\n4.\tinformation regarding the approval of the document;\n5.\ta statement of effectivity identifying which other documents have been cancelled and replaced in whole or in part."]
["ECSS-Q-ST-70-29C","ECSS - Current v0.9","4.1.1.5a","Requirement","ECSS-Q-ST-70-29_0650016",1,"Created","The supplier shall test assembled articles in the condition in which it was received."]
["ECSS-Q-ST-70-29C","ECSS - Current v0.9","4.2.5a","Requirement","ECSS-Q-ST-70-29_0650041",1,"Created","All carrier gases used shall be of purity not less than 99,99 %.\n    NOTE For example Helium or Hydrogen.\n1. Table 4-1\n2. The GC/MS parameters are such that 100 picograms of Methyl Stearate injected on to the GC capillary column gives a signal to noise ratio of 50:1, for a MS source on the molecular ion at m/z 298."]
["ECSS-Q-ST-70-29C","ECSS - Current v0.9","A.2.1<4>a","Requirement","ECSS-Q-ST-70-29_0650066",1,"Created","The report shall contain the following information:\n    1. Result of analysis\n    2. Projected spacecraft volume."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.1.4a","Requirement","ECSS-Q-ST-70-30_0120023",1,"Created","Materials, tools and techniques, which are planned to be used shall be reviewed with respect to design needs, to ensure conformance to customer requirements and as a means of identifying any pending process qualification. "]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.2.1.2e","Requirement","ECSS-Q-ST-70-30_0120048",1,"Created","Annealed copper shall not be continually operated for long periods above 90 °C, owing to the likelihood that excessive wire stress relaxation affects the reliability of the wrap connection."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.2.2.3a","Requirement","ECSS-Q-ST-70-30_0120069",1,"Created","Terminal posts shall be durable enough to withstand being unwrapped and re-wrapped and still conform with the test requirements in clause 5.4.\n    NOTE Annex A.2 describes the rework procedure."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.3.2.1c","Requirement","ECSS-Q-ST-70-30_0120083",1,"Created","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."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.3.4c","Requirement","ECSS-Q-ST-70-30_0120096",1,"Created","Disturbed joints shall be rejected and replaced."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.4.5b","Requirement","ECSS-Q-ST-70-30_0120121",1,"Created","The wrapped connection shall show evidence on every turn, except the first and last, of a gas-tight surface equal to or greater than 75 % of the corners of the terminal post in contact with the bare conductor. \n    NOTE This means, either 3 or 4 terminal post corners per turn of bare conductor are gas-tight."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.6.1a","Requirement","ECSS-Q-ST-70-30_0120151",1,"Created","The supplier shall conform with the quality assurance requirements defined in ECSS-Q-ST-20."]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.6.6a","Requirement","ECSS-Q-ST-70-30_0120168",1,"Created","Visual standards consisting of satisfactory work samples or visual aids which clearly illustrate the quality characteristics of wire-wrap connections shall be prepared and available to each operator and inspector. "]
["ECSS-Q-ST-70-30C","ECSS - Current v0.9","5.6.7d","Requirement","ECSS-Q-ST-70-30_0120173",1,"Created","The certification of personnel shall be based upon objective evidence of wire wrap quality, resulting from test and inspection of the wrap joints. "]
["ECSS-Q-ST-70-36C","ECSS - Current v0.9","5.2.3.3a","Requirement","ECSS-Q-ST-70-36_0670012",1,"Created","Alloys and tempers listed in Table 5-2 shall only be considered for use when a suitable alloy cannot be found in Table 5-1."]
["ECSS-Q-ST-70-36C","ECSS - Current v0.9","C.2.1<6>a","Requirement","ECSS-Q-ST-70-36_0670030",1,"Created","The SCEF shall contain the number of identical parts."]
["ECSS-Q-ST-70-37C","ECSS - Current v0.9","5.1d","Requirement","ECSS-Q-ST-70-37_0680004",1,"Created","The test shall be performed at a temperature of 23 °C ±4 °C"]
["ECSS-Q-ST-70-37C","ECSS - Current v0.9","5.2.2.3e","Requirement","ECSS-Q-ST-70-37_0680025",1,"Created","The supplier shall radius the edges of flat specimens by abrasion using fine silicon carbide paper with a grade of 1200."]
["ECSS-Q-ST-70-37C","ECSS - Current v0.9","5.3.1a","Requirement","ECSS-Q-ST-70-37_0680043",1,"Created","For unwelded specimen, the supplier shall calculate the stress-corrosion test load from the average 0,2 % proof stress value provided by the three specimens tensile tested initially."]
["ECSS-Q-ST-70-37C","ECSS - Current v0.9","5.4.1a","Requirement","ECSS-Q-ST-70-37_0680056",1,"Created","The supplier shall retain the quality records for ten years or in accordance with project business agreement requirements.\n    NOTE Example of such quality records are log sheets."]
["ECSS-Q-ST-70-45C","ECSS - Current v0.9","5.2.2c","Requirement","ECSS-Q-ST-70-45_0690006",1,"Created","For specimens with a transverse weld, the specimen gauge length shall be equal or greater than the weld heat affected zone (HAZ).\n    NOTE 1 When testing specimens with a transverse weld, note that the strain distribution within the HAZ varies as a function of the distance from the weld centre line. This implies that elongation varies as a function of the gauge length. \n    NOTE 2 Weldments are characterized by non-uniformity in tensile properties."]
["ECSS-Q-ST-70-45C","ECSS - Current v0.9","5.5.1c","Requirement","ECSS-Q-ST-70-45_0690031",1,"Created","Accuracy and resolution of selected crack length measurement methods shall be assessed before testing.\n    NOTE Measurement methods are optical, direct current potential drop technique and compliance methods."]
["ECSS-Q-ST-70-45C","ECSS - Current v0.9","5.12.1c","Requirement","ECSS-Q-ST-70-45_0690058",1,"Created","The supplier shall establish and implement quality control actions and inspections to provide evidence of conformity to test requirements. \n    NOTE Quality control actions and inspections for test activities carried out by sub-contracted laboratories are under the responsibility of the supplier."]
["ECSS-Q-ST-70-45C","ECSS - Current v0.9","A.2.2b","Requirement","ECSS-Q-ST-70-45_0690078",1,"Created","The descriptive modifier shall be selected to clearly identify the applicable product.  \n    NOTE 1 For example: “Measurement of fracture toughness of AA 7175-T7351 plate - Request for mechanical testing of materials”\n    NOTE 2 For example: “Fatigue crack propagation behaviour of Ti-6Al-4V STA sheet at different stress ratios - Request for mechanical testing of materials”."]
["ECSS-Q-ST-70-45C","ECSS - Current v0.9","B.2.2b","Requirement","ECSS-Q-ST-70-45_0690083",1,"Created","The descriptive modifier shall be selected to clearly identify the applicable product.  \n    NOTE 1 For example: “Measurement of fracture toughness of AA 7175-T7351 plate - Request for mechanical testing of materials”\n    NOTE 2 For example: “Fatigue crack propagation behaviour of Ti-6Al-4V STA sheet at different stress ratios - Request for mechanical testing of materials”."]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.1.2d","Requirement","ECSS-Q-ST-70-46_0700007",1,"Created","Materials for threaded fasteners shall be corrosion resistant "]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.1.8b","Requirement","ECSS-Q-ST-70-46_0700032",1,"Created","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. "]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.2.5b","Requirement","ECSS-Q-ST-70-46_0700057",1,"Created","Fasteners when visually examined at a magnification of between ´10 and ´50 shall exhibit a continuous grain flow in the head area and head-to-shank transition zone. "]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.3.2.2a","Requirement","ECSS-Q-ST-70-46_0700075",1,"Created","Hardness tests on fasteners shall be carried out on the circular surface at the end of the threaded portion of the fastener shank after removing any surface coating. "]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.3.5.3e","Requirement","ECSS-Q-ST-70-46_0700104",1,"Created","Fatigue strength values shall be determined in the finite life range (failure of all test pieces before a predetermined number of stress cycles is reached) and in the transition range where, up to a predetermined number (typically 5 ´ 106 to 5 ´ 107) of stress cycles, failure as well as non-failure occurs. "]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.4.2.3c","Requirement","ECSS-Q-ST-70-46_0700125",1,"Created","The supplier shall define the batch acceptability criteria in terms of:\n    1. acceptance quality limit (AQL), if the batch-by-batch inspection method is selected, or\n    2. limiting quality (LQ), if the isolated batch inspection is selected."]
["ECSS-Q-ST-70-46C Rev. 1","ECSS - Current v0.9","4.4.2.4a","Requirement","ECSS-Q-ST-70-46_0700130",1,"Created","In the case where the number of nonconforming units is greater than the acceptance level specified in the customer specification document for threaded fasteners, the supplier shall reject the batch. "]
["ECSS-Q-ST-70-53C","ECSS - Current v0.9","5.1.3.1a","Requirement","ECSS-Q-ST-70-53_0990010",1,"Created","The test procedures shall address the test conditions, control and monitoring of:\n    1. Process parameters for sterilization.\n        NOTE Required process parameters for dry heat sterilization are described in ECSS-Q-ST-70-57, and for vapour phase (e.g. hydrogen peroxide) sterilization are described in ECSS-Q-ST-70-56.\n    2. SAL.\n    3. Contamination."]
["ECSS-Q-ST-70-53C","ECSS - Current v0.9","5.2.3b","Requirement","ECSS-Q-ST-70-53_0990030",1,"Created","For mechanical testing or other forms of destructive analysis, representative samples for the hardware shall be supplied for comparison of results before and after sterilization."]
["ECSS-Q-ST-70-53C","ECSS - Current v0.9","C.2.1b","Requirement","ECSS-Q-ST-70-53_0990055",1,"Created","Test records shall be made available in electronic form for incorporation in a database defined by the customer, and contain as a minimum the following:\n    1. Manufacturer.\n    2. Traceable identification numbers for sterilised items.\n        NOTE For example: batch number, serial number.\n    3. Sample description (type of application, size, colour, number of samples).\n    4. Material name (trade name).\n    5. Chemical nature.\n    6. Thermal history / process parameters (for general materials property field).\n    7. Intended application.\n    8. Sterilization method, apparatus/facility, date.\n    9. Nominal/measured sterilization parameters (e.g. temperature, radiation dose, gas concentration).\n    10. Pre and post conditioning/storage parameters.\n    11. Pre- and post sterilization values of test parameters defined in 5.2 including date of tests.\n    12. Occurrence of NCRs.\n    13. Copy of the final inspection documentation (attached docs in new tab).\n    14. Copy of test reports (attached docs in new tab)."]
["ECSS-Q-ST-70-55C","ECSS - Current v0.9","5.4.1a","Requirement","ECSS-Q-ST-70-55_1030023",1,"Created","The test records of the microbiological examination shall be retained for, at least, ten years or in accordance with customer requirements."]
["ECSS-Q-ST-70-55C","ECSS - Current v0.9","5.4.2b","Requirement","ECSS-Q-ST-70-55_1030027",1,"Created","The supplier shall submit the test report to the customer for approval."]
["ECSS-Q-ST-70-58C","ECSS - Current v0.9","5.2.3.1c","Requirement","ECSS-Q-ST-70-58_1040016",1,"Created","The layout of equipment shall provide for ergonomics that optimize comfort and movement of operators."]
["ECSS-Q-ST-70-58C","ECSS - Current v0.9","5.2.5.1a","Requirement","ECSS-Q-ST-70-58_1040037",1,"Created","A sampling plan shall be developed through the formal system (i.e., in the commissioning phase), and documented in conformance with Annex A."]
["ECSS-Q-ST-70-58C","ECSS - Current v0.9","5.2.7c","Requirement","ECSS-Q-ST-70-58_1040052",1,"Created","Only personnel with the appropriate level of training and medical clearance shall access the bioburden controlled environments, including. personnel for cleaning and maintenance."]
["ECSS-Q-ST-70-13C Rev. 1","ECSS - Current v0.9","5.1.2.3c","Requirement","ECSS-Q-ST-70-13_0610018",1,"Unchanged","The supplier shall shield coated surfaces from contact by using polyethylene or polypropylene bags or sheets."]
["ECSS-Q-ST-70-13C Rev. 1","ECSS - Current v0.9","5.2.1.1a","Requirement","ECSS-Q-ST-70-13_0610039",1,"Unchanged","The supplier shall locate the test sample on the sample holder in conformance with the requirements stated in clause 5.1.4.3."]
["ECSS-Q-ST-70-13C Rev. 1","ECSS - Current v0.9","5.3e","Requirement","ECSS-Q-ST-70-13_0610050",1,"Unchanged","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."]
["ECSS-Q-ST-70-13C Rev. 1","ECSS - Current v0.9","A.2.1f","Requirement","ECSS-Q-ST-70-13_0610066",1,"Unchanged","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."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.1.1.4h","Requirement","ECSS-Q-ST-70-50_1140017",1,"Created","Excess tape not attached to the membrane filter shall be removed using scissors or a scalpel."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.1.2.6h","Requirement","ECSS-Q-ST-70-50_1140041",1,"Created","After exposure, the container shall be closed in-situ."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.1.3.5.2a","Requirement","ECSS-Q-ST-70-50_1140058",1,"Created","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."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.3.2g","Requirement","ECSS-Q-ST-70-50_1140084",1,"Created","The use of statistical sampling shall be agreed between the supplier and the customer prior to the measurement."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.3.5b","Requirement","ECSS-Q-ST-70-50_1140088",1,"Created","The statistical sampling shall be performed by using a mask or grid which contains a number of unit areas as described in 5.3.5c.\n    ","NOTE An example is provided in Figure 5-3."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","5.4.9e","Requirement","ECSS-Q-ST-70-50_1140117",1,"Created","If existing tables, cupboards, cabinets, racks or equipment surfaces are used to put the sensor on, the surface shall be pre-cleaned using non-shedding and lint-free wipes, wetted by immersion in spectral grade methanol, ethanol or IPA, to approximately 1 m2 around the location."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","6.2i","Requirement","ECSS-Q-ST-70-50_1140127",1,"Created","Heat generated by high intensity fibre optic light sources shall not damage temperature sensitive items."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","6.3.2.3b","Requirement","ECSS-Q-ST-70-50_1140144",1,"Created","The article shall be manipulated with respect to the illumination source in order to maximise the contrast between the surface and any in-homogeneities."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","C.2.1<1>a","Requirement","ECSS-Q-ST-70-50_1140168",1,"Created","The report shall contain the name, organization and address of the requesting authority."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","C.2.1<5>a","Requirement","ECSS-Q-ST-70-50_1140172",1,"Created","The report shall contain the name and class of the facility where the measurements have been performed."]
["ECSS-Q-ST-70-50C","ECSS - Current v0.9","D.2.1<11>a","Requirement","ECSS-Q-ST-70-50_1140195",1,"Created","The report shall contain a description of the area in which the inspection has taken place."]
["ECSS-Q-ST-60-15C","ECSS - Current v0.9","5.1t","Requirement","ECSS-Q-ST-60-15_1150021",1,"Created","For geostationary orbit, RVT on flight lot shall be performed if flight model part diffusion lot number is different from tested part diffusion lot number and tested parts date code is 4 years older than flight model part date code."]
["ECSS-Q-ST-60-15C","ECSS - Current v0.9","5.2t","Requirement","ECSS-Q-ST-60-15_1150045",1,"Created","TNID analysis shall be documented in the equipment radiation analysis report in conformance with the DRD in Annex B."]
["ECSS-Q-ST-60-15C","ECSS - Current v0.9","5.3o","Requirement","ECSS-Q-ST-60-15_1150071",1,"Created","Proton SEE test data shall satisfy requirement 5.3f to be acceptable."]
["ECSS-Q-ST-60-15C","ECSS - Current v0.9","A.2.1<3>c","Requirement","ECSS-Q-ST-60-15_1150096",1,"Created","Trapped and solar protons shielded (e.g. behind 1 g/cm2 of Al) fluxes versus energy spectra shall be presented with figures and tables."]
["ECSS-Q-ST-70-56C","ECSS - Current v0.9","5.2.2b","Requirement","ECSS-Q-ST-70-56_1230008",1,"Created","The bioburden of the product shall be measured in conformance with requirements from the ECSS-Q-ST-70-55 before the bioburden reduction process is applied."]
["ECSS-Q-ST-70-56C","ECSS - Current v0.9","5.3.1.1c","Requirement","ECSS-Q-ST-70-56_1230021",1,"Created","D-value for surface bioburden reduction under controlled ambient conditions shall be 200 (mg/L)sec.","NOTE Example: to calculate the Ct-value necessary for a 5 order of magnitude bioburden reduction in a controlled ambient environment, the D-value in requirement 5.3.1.1c is multiplied by a factor of 5, i.e. 200 (mg/L)sec time 5 = 1000 (mg/L)sec."]
["ECSS-Q-ST-70-56C","ECSS - Current v0.9","5.4i","Requirement","ECSS-Q-ST-70-56_1230039",1,"Created","Any nonconformance shall be recorded in an NCR in compliance with requirements from the clause 5.1 of the ECSS-Q-ST-10-09. "]
["ECSS-Q-ST-70-57C","ECSS - Current v0.9","5.3.1.1e","Requirement","ECSS-Q-ST-70-57_1240017",1,"Created","Temperature dependent D-values in minutes for 2 to 3 order of magnitude encapsulated bioburden and surface and mated bioburden reduction under uncontrolled humidity conditions shall be calculated by multiplying the D-values from equation [5-1] or [5-2] with a factor of 10.","NOTE Example: to calculate the time to achieve a 3 order of magnitude surface (or mated, or encapsulated) bioburden reduction under uncontrolled humidity conditions at 120 °C means to use equation [5-1] with T=120 °C to calculate the D120 value (= 52 minutes); D120 (52 minutes) times 3 is the time necessary for a 3 order of magnitude reduction for surface bioburden under dry conditions (= 156 minutes); 156 minutes times 10 = 1560 minutes (26 hours) is the time required to achieve a 3 order of magnitude surface/mated/ encapsulated bioburden reduction under uncontrolled humidity conditions at 120 °C."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","5.2i","Requirement","ECSS-Q-ST-70-12_1200006",1,"Created","The PCB manufacturer shall issue to the supplier a MRR checklist, which is part of the PCB manufacturing dossier, in conformance with the DRD in the Annex B.\nNOTE \tAn example of a MRR checklist is given in Annex G."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","7.1.2b","Requirement","ECSS-Q-ST-70-12_1200022",1,"Created","In case the thickness of the copper cladding on the laminate is asymmetric, this asymmetric build-up of the PCB shall be recorded as a Review Item in the PCB definition dossier. \nNOTE \t17/70 copper thickness is more risky than 17/35 or 35/70 copper thickness. The presence of fine pitch tracks in combination with asymmetric copper further increases the difficulty to process."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","7.1.2g","Requirement","ECSS-Q-ST-70-12_1200024",1,"Created","In case the total as-designed thickness of copper is above 700 µm, this shall be recorded as a Review Item in the PCB definition dossier.\nNOTE \tHigh layer count in combination with thick copper layers can have significant impact on manufacturability and long-term reliability."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","7.3.5a","Requirement","ECSS-Q-ST-70-12_1200041",1,"Created","Except the case specified in the requirement 11.5.6a, the aspect ratio of vias on a rigid and rigid-flex PCB shall be ≤ 7.\nNOTE \t1\tThere is no additional requirement for the minimum diameter of plated via in case the diameter conforms to the aspect ratio of ≤ 7.\nNOTE \t2\tRequirement 11.5.6a specifies aspect ratio for AAD with 1 mm pitch on HDI PCBs."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","7.4.5a","Requirement","ECSS-Q-ST-70-12_1200055",1,"Created","Except the case specified in the requirement 11.5.5a, the track width and spacing for fine pitch on internal layers shall be in conformance with the as-manufactured dimensions specified in Table 7-5.\nNOTE \tRequirement 11.5.5a specifies track width and spacing for impedance controlled routing to AAD with 1 mm pitch on HDI PCBs ."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","7.6d","Recommendation","ECSS-Q-ST-70-12_1200411",1,"Created","Copper layers should be placed symmetrically within the build-up.\nNOTE \tThis is done to limit warp and twist."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","8.3.4c","Recommendation","ECSS-Q-ST-70-12_1200417",1,"Created","In case a copper plane is used in a flex PCB, a grid with openings should be implemented as specified in the Figure 7-3.\nNOTE \tThe purpose of the openings is to improve adhesion of the cover layer, desorption of humidity and flexibility of the PCB. A grid can be 0,4 mm lines at a pitch of 0,6 mm and at 45° angle. It is preferable to have the grid offset between layers. In this case, the electrical and thermal resistance increases by a factor of approximately x2,5 compared to a solid plane."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","8.4m","Recommendation","ECSS-Q-ST-70-12_1200424",1,"Created","The distance of tracks or reinforcement strip to the edge of the board should be ≥ 1,0 mm."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","8.6.2a","Requirement","ECSS-Q-ST-70-12_1200110",1,"Created","The radius on a flex PCB having 50 µm laminate thickness and 35 µm double sided copper thickness and including cover layer shall be ≥ 12x total thickness of the flex for a static application.\nNOTE \tIn the Figure 8-4 R is the bending radius of a flex PCB"]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","8.7.6b","Requirement","ECSS-Q-ST-70-12_1200127",1,"Created","Bending shall only occur on the etched track."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","10.2a","Requirement","ECSS-Q-ST-70-12_1200149",1,"Created","Design with heat sink shall be recorded as a Review Item in the PCB definition dossier."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","10.4.2e","Requirement","ECSS-Q-ST-70-12_1200169",1,"Created","The copper foil shall be procured in conformance with the requirements from the IPC-4562.\nNOTE \tTypes of copper foil types commonly used are: HTE grade 3, and JTC grade 1."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","11.4.1e","Permission","ECSS-Q-ST-70-12_1200442",1,"Created","On microvia layers, the external and internal copper layers may be designed using basic copper thickness of 9 or 12 µm, in case the following conditions are met:\n1.\tthe peel strength is measured on the test coupon to be ≥ 12 N/cm,\n2.\ta carrier on the foil is used during manufacturing, and\n3.\tit is recorded as a Review Item in the PCB definition dossier.\nNOTE \t1\tThe copper thickness defined in requirement 11.4.1d is in conformance with the requirement 7.1.2c. The copper thickness defined in requirement 11.4.1e is a deviation from the requirement 7.1.2c. \nNOTE \t2\tThe benefit of reduced copper thickness is to improve etching accuracy of fine features. To ensure an insulation of 60 µm between layers it can be beneficial to use thin copper on the internal microvia layer to avoid planarization processes.\nNOTE \t3\tThe potential lower peel strength of thin copper foil is a risk factor for manufacture, which is mitigated by the coupon measurement. \nNOTE \t4\tThin copper foil is more fragile, therefore a rigid carrier is used during manufacture. When the core surface is non-planar, it is possible the rigid carrier does not conform well to the non-planar prepreg causing lack of adhesion or deformation of the copper foil. The following features can cause non-planarity of the core surface: rigid-flex constructions, high via density, high track density, high copper thickness, use of no-flow prepreg."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","11.4.1j","Requirement","ECSS-Q-ST-70-12_1200193",1,"Created","For voltages >30V microvia layers shall not have superimposed conductors.\nNOTE \tThis is done to ensure that insulation in Z direction is in conformance with the Table 13-3."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","11.5.3a","Recommendation","ECSS-Q-ST-70-12_1200448",1,"Created","External layers should not include tracks.\nNOTE \tThis is in particular important for critical tracks."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","12.4a","Recommendation","ECSS-Q-ST-70-12_1200458",1,"Created","The thickness of RF PCB as-designed should be ≤ 3 mm."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.6.2d","Recommendation","ECSS-Q-ST-70-12_1200468",1,"Created","The temperature of tracks should be ≤ 85 °C.\nNOTE \tThe increment of 10 °C is based on a temperature of the PCB substrate of 85 °C, in which case the tracks can heat to 95 °C due to self-heating. The self-heating of tracks up to 10°C compared to the substrate, regardless of overall substrate temperature, is based on heritage."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.8.2d","Requirement","ECSS-Q-ST-70-12_1200257",1,"Created","The insulation distance as function of voltage of the as-manufactured PCB shall be in compliance with values specified in Table 13-3 and Table 13-4.\nNOTE \t1\tThe insulation distances also depends on manufacturing capability and tolerances as specified in clause 13.8.1 and specified in Table 7-4 and Table 7-5.\nNOTE \t2\tThe Table 13-3 and Table 13-4 cover any elevation. Withstanding voltage between two tracks in air at 87% relative humidity is 1600 V/mm. It is considered that breakdown or arcing cannot occur below this field strength as indicated in the paper by D. P Cullen and G O’Brien (see bibliography)."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.8.3b","Requirement","ECSS-Q-ST-70-12_1200267",1,"Created","The spacing of conductors on flex laminate in the flex section shall be in conformance with values for X,Y internal specified in the Table 13-4.\nNOTE \tConductors on flex laminate in flex section are covered by cover layer. "]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.9.3.3a","Recommendation","ECSS-Q-ST-70-12_1200478",1,"Created","Critical tracks as specified in the requirement 13.9.2a should not be routed on external layers. \nNOTE \tThis is also recommended for non-critical track in conformance with requirements from the clause 7.4.3a."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.11.5c","Requirement","ECSS-Q-ST-70-12_1200300",1,"Created","In multidrop configuration with one driver and several receivers the driver shall be at one end of the line and the termination at the other end."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","13.13.3b","Recommendation","ECSS-Q-ST-70-12_1200500",1,"Created","Ground planes should be used for non-critical analog circuitries specified in the requirement 13.13.2.1a.\nNOTE \t\tGround planes shield signals from pickup noise."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","14.3.3c","Requirement","ECSS-Q-ST-70-12_1200328",1,"Created","The location of the devices shall be such that each solder connection can be visually inspected."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","14.5.6a","Requirement","ECSS-Q-ST-70-12_1200350",1,"Created","The pad design for components of type LCC shall be in conformance with the as-manufactured values specified in the Table 14-9, except for the case specified in 14.5.2c.\nNOTE \t1\tAn illustration is given in Figure 14-11.\nNOTE \t2\tLCC means leadless chip carrier."]
["ECSS-Q-ST-70-12C","ECSS - Current v0.9","A.2.2a","Requirement","ECSS-Q-ST-70-12_1200370",1,"Created","The format of the data of the PCB definition dossier shall be agreed between supplier and PCB manufacturer."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.1j","Requirement","ECSS-Q-ST-20-07_0370010",1,"Created","The quality and safety management system of the space test centre, or its parent organization, shall be implemented and maintained to allow external and internal revisions or audits by customer or external authorities."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.3.3c","Requirement","ECSS-Q-ST-20-07_0370022",1,"Created","Top management shall ensure that space test centre personnel are free from undue pressures, conflict of interest or influences that can affect the quality of their work."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.5.1a","Requirement","ECSS-Q-ST-20-07_0370043",1,"Created","The space test centre shall ensure that all processes are carried out under controlled conditions using test facilities, measuring equipment, servicing equipment and environmental conditions meeting all process requirements.","NOTE \t1\tThe use of unsuitable test facilities, equipment and environmental conditions can for example lead to invalid test results.\nNOTE \t2\tMeasuring equipment includes hardware and software."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.5.3e","Requirement","ECSS-Q-ST-20-07_0370057",1,"Created","The cleanliness levels shall be specified for molecular contamination in terms of surface contamination."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.6.3n","Requirement","ECSS-Q-ST-20-07_0370093",1,"Created","The calibration records shall contain as a minimum the measurement results, the measurement uncertainty or a statement of compliance with an identified specification."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.7.2b","Requirement","ECSS-Q-ST-20-07_0370114",1,"Created","The space test centre shall maintain records of all requirements review."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.7.3d","Requirement","ECSS-Q-ST-20-07_0370119",1,"Created","The planning shall demonstrate the compatibility of the design of the test processes with the infrastructure, the test facilities, the test execution, and the applicable test procedures."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.7.4.4c","Requirement","ECSS-Q-ST-20-07_0370138",1,"Created","Access control to the storage area shall be established to provide as a minimum the same security level as in working areas."]
["ECSS-Q-ST-20-07C","ECSS - Current v0.9","5.9.2b","Requirement","ECSS-Q-ST-20-07_0370166",1,"Created","The space test centre management shall periodically review its safety policy."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","4.2g","Requirement","ECSS-Q-ST-20-08_1170008",1,"Created","Test or stimulus points shall be accessible without the need to disconnect or deroute flight harness of an item of equipment."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","5.3g","Requirement","ECSS-Q-ST-20-08_1170026",1,"Created","De-storage activities shall be agreed with the customer prior the storage phase, and included in the Storage Plan, in conformance with DRD from the Annex A."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","6.2.1a","Requirement","ECSS-Q-ST-20-08_1170054",1,"Created","All GSE fixing points shall be able to be visually inspected.","NOTE \tThis requirements imply that attachment parts necessary to secure the flight hardware are clearly visible by design."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","6.2.3b","Requirement","ECSS-Q-ST-20-08_1170059",1,"Created","This analysis report specified in the requirement 6.2.3a shall be delivered by MGSE design authority to every MGSE user."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","6.3.2g","Requirement","ECSS-Q-ST-20-08_1170079",1,"Created","Hardware configuration shall be verified to be compliant with the handling constraint.","NOTE \tFor example, mechanical and electrical configuration can be checked, search for loose part."]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","7.5f","Requirement","ECSS-Q-ST-20-08_1170107",1,"Created","The dispatch of products shall be documented. "]
["ECSS-Q-ST-20-08C","ECSS - Current v0.9","7.8.2d","Requirement","ECSS-Q-ST-20-08_1170133",1,"Created","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)"]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","6.2.1e","Permission","ECSS-Q-ST-70-39_1280238",1,"Created","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. "]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","7.2h","Requirement","ECSS-Q-ST-70-39_1280037",1,"Created","All maintenance operations of welding equipment shall be documented.","NOTE\tFor example, in the Maintenance Book."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","7.3.1c","Requirement","ECSS-Q-ST-70-39_1280040",1,"Created","Weld start and runoff tabs, when used, shall be of the same alloy as the base metal alloy being joined."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","8.1.4c","Requirement","ECSS-Q-ST-70-39_1280063",1,"Created","The applicable welding position shall be in accordance with ISO 6947:2011."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","9.1.1a","Requirement","ECSS-Q-ST-70-39_1280081",1,"Created","The production of weld joints and test joints shall be inspected to demonstrate that the construction, physical dimensions, identification, and production records are in conformance with the engineering drawing and the requirements from clause 9. "]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","9.2.1e","Requirement","ECSS-Q-ST-70-39_1280109",1,"Created","For fusion welds, every cross-section shall be documented by pictures and show the following features of the weld:\n1.\tPenetration and depth of the weld seam,\n2.\tMisalignment,\n3.\tMicrostructural features of the weld zone,\n4.\tIncomplete fusion,\n5.\tHeat affected zone, and\n6.\tParent material(s)."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","11.1.3a","Requirement","ECSS-Q-ST-70-39_1280137",1,"Created","For all welding processes from safety class 3, two samples shall be produced and subjected to visual inspection."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","11.5f","Requirement","ECSS-Q-ST-70-39_1280158",1,"Created","Re-inspection of all repair weld areas shall be performed using the same methods and requirements as the original weld."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","12.2.1e","Requirement","ECSS-Q-ST-70-39_1280170",1,"Created","During test or final assembly of the piece parts, the cleanliness requirements of clauses 7.3.4c and 8.1.5 shall apply."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","13.2.1b","Requirement","ECSS-Q-ST-70-39_1280191",1,"Created","Reference samples shall be stored in conformance with life duration of the mission.","NOTE\tExamples of reference samples includes alpha and beta samples."]
["ECSS-Q-ST-70-39C","ECSS - Current v0.9","A.2.1<1.6>a","Requirement","ECSS-Q-ST-70-39_1280212",1,"Created","In case pre-heating is applied, the temperature, and the time at temperature, shall be included in the WPS.","NOTE\tThis includes a description of any other instructions related to the heat treatment."]
["ECSS-Q-ST-10C Rev.1","ECSS - Current v0.9","5.1.1.1c","Requirement","ECSS-Q-ST-10_0360003",1,"Unchanged","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."]
["ECSS-Q-ST-10C Rev.1","ECSS - Current v0.9","5.1.1.2b","Requirement","ECSS-Q-ST-10_0360006",1,"Unchanged","The supplier shall define and document the responsibilities and the interfaces of the PA functions, either external or internal, involved in a project."]
["ECSS-Q-ST-10C Rev.1","ECSS - Current v0.9","5.2.1j","Requirement","ECSS-Q-ST-10_0360027",1,"Unchanged","The PA manager shall ensure that a Qualification Status List of the programme items is maintained in conformance with Annex B."]
["ECSS-Q-ST-10C Rev.1","ECSS - Current v0.9","5.2.9a","Requirement","ECSS-Q-ST-10_0360048",1,"Unchanged","The supplier shall notify its customer of preliminary information on failures or problems that can result in an alert.","NOTE \t1\tThe above is applicable to failure or problems detected by the supplier or by one of his lower tier suppliers.\nNOTE \t2\tThe above is only applicable to failures or problems meeting all of the following criteria:\n·\tThe item with the observed failure or problem has multiple applications, which can have implications for more than one project, thus requiring prompt action.\n·\tThe failure or problem has occurred in the application of an item within the specified design and usage limitations. \n·\tFailures or problems due to usage within reasonably expected limits of performance, but where these limits were not specified precisely.\n·\tA preliminary investigation has provided evidence of the root cause of the failure or problem.\n·\tFailure or problems are confirmed not to be of a random nature.\n"]
["ECSS-Q-ST-10C Rev.1","ECSS - Current v0.9","A.2.2b","Permission","ECSS-Q-ST-10_0360073",1,"Created","The response to this DRD may be performed by reference to separate discipline plans addressing some of the above clauses of this DRD."]
["ECSS-Q-ST-70-14C","ECSS - Current v0.9","5.5.1e","Requirement","ECSS-Q-ST-70-14_1340029",1,"Created","The process parameters specified in the requirement 5.5.1d shall be defined in the process specification."]
["ECSS-Q-ST-70-14C","ECSS - Current v0.9","5.6.5a","Requirement","ECSS-Q-ST-70-14_1340050",1,"Created","Copper plating shall be applied in accordance with specification identified in the DPL specified in the DRD of Annex C from ECSS-Q-ST-70.","NOTE \tSAE AMS2418 or ASTM B734 are internationally recognised standards describing copper plating.\n"]
["ECSS-Q-ST-70-14C","ECSS - Current v0.9","5.9.1a","Requirement","ECSS-Q-ST-70-14_1340061",1,"Created","All design and verification shall include the surface treatments or features on a flight hardware.","NOTE \tA flight hardware can have regions with difficult geometries for coating systems. For example holes through or blind, abrupt change of geometry, sharp edges and crevices.\n"]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","5.1.4.2a","Requirement","ECSS-Q-ST-80_0720008",1,"Unchanged","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."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","5.2.7.1a","Requirement","ECSS-Q-ST-80_0720032",1,"Unchanged","Quality models shall be used to specify the software quality requirements.\n","EXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","5.6.1.2a","Requirement","ECSS-Q-ST-80_0720053",1,"Unchanged","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]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.2.1.2a","Requirement","ECSS-Q-ST-80_0720074",1,"Unchanged","All plans shall be finalized before the start of the related activities.\n","EXPECTED OUTPUT: Software project plans [MGT, MF, DJF]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.2.3.7a","Requirement","ECSS-Q-ST-80_0720099",1,"Unchanged","Unit and integration testing shall be (re-)executed on non-instrumented code."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.2.4.4a","Requirement","ECSS-Q-ST-80_0720104",1,"Unchanged","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]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.2.7.9a","Requirement","ECSS-Q-ST-80_0720141",1,"Unchanged","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]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.3.1.1a","Requirement","ECSS-Q-ST-80_0720151",1,"Unchanged","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."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.3.5.1a","Requirement","ECSS-Q-ST-80_0720176",1,"Informative Change","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    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.","NOTE \tFor examples for item 1 are: functional, boundary, performance, and usability tests.\nEXPECTED OUTPUT: Software product assurance plan [PAF, SPAP; PDR, CDR]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.3.5.21a","Requirement","ECSS-Q-ST-80_0720197",1,"Unchanged","The supplier shall review the test documentation to ensure that it is up to date and organized to facilitate its reuse for maintenance."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","6.3.5.30a","Requirement","ECSS-Q-ST-80_0720206",1,"Unchanged","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]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","7.1.1a","Requirement","ECSS-Q-ST-80_0720228",1,"Unchanged","The software quality requirements (including safety and dependability requirements) shall be derived from the requirements defined at system level.","EXPECTED OUTPUT: The following outputs are expected:\n          a.Requirement baseline [RB, SSS; SRR];\n          b.Technical specification [TS, SRS; PDR]."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","7.3.2a","Requirement","ECSS-Q-ST-80_0720249",1,"Unchanged","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. "]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","B.2.1<5.6>a","Requirement","ECSS-Q-ST-80_0720274",1,"Unchanged","The SPAP shall describe the contribution of the software product assurance function to the project risk management."]
["ECSS-Q-ST-80C Rev.1","ECSS - Current v0.9","C.2.1<2>a","Requirement","ECSS-Q-ST-80_0720300",1,"Unchanged","The SPAMR shall list the applicable and reference documents to support the generation of the document."]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","4.4a","Requirement","ECSS-Q-ST-30_0410010",1,"Unchanged","As part of the risk management process implemented on the project, the Dependability engineer shall be responsible for identifying and reporting dependability associated risks.","NOTE \tECSS-M-ST-80 describes the risk management process.\n"]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","5.3.2c","Requirement","ECSS-Q-ST-30_0410034",1,"Unchanged","For analyses lower than system level, the severity due to possible failure propagation shall be identified as level 1 for dependability. ","NOTE \tFor example, for analysis at subsystem, and equipment level\n"]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","5.4.1b","Requirement","ECSS-Q-ST-30_0410125",1,"Created","The classification of the functions, as per requirement 5.4.1a, shall be submitted to the customer for approval.","NOTE \tThe function criticality is documented by FMEA, i.e. by the attributed severity category assigned to the consequences of the functional failure.\n"]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","5.5a","Requirement","ECSS-Q-ST-30_0410047",1,"Unchanged","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. "]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","6.4.2.1b","Requirement","ECSS-Q-ST-30_0410072",1,"Unchanged","The reliability data sources and methods used in reliability predictions shall be as specified by the customer. "]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","6.4.4e","Requirement","ECSS-Q-ST-30_0410102",1,"Unchanged","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"]
["ECSS-Q-ST-30C Rev.1","ECSS - Current v0.9","E.2.2a","Permission","ECSS-Q-ST-30_0410142",1,"Created","The reliability prediction may be linked as either an input source or an output to other dependability analyses.","NOTE \tExamples of such analyses are:\n·\tFMEA, FMECA and Fault tree analysis: reliability prediction is an input (providing failure rates for dedicated items) but FMEA, FMECA and Fault tree analysis also provide inputs for the reliability prediction,\n·\tPart stress analysis provides inputs for failure rate calculation,\n·\tInputs for availability analysis.\n"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.1.1.4a","Requirement","ECSS-Q-ST-70-26_0130011",1,"Unchanged","The supplier shall ensure adequate illumination conditions of the crimp workstations."]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.1.2.1c","Requirement","ECSS-Q-ST-70-26_0130016",2,"Normative Change","Tools shall be sealed on one setting value in case of variable settings tools."]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.1.2.4a","Requirement","ECSS-Q-ST-70-26_0130032",2,"Normative Change","The supplier shall provide the equipment specified in Table 5-1 necessary for verification activities specified in clause 5.4.3. "]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.2.4h","Requirement","ECSS-Q-ST-70-26_0130170",1,"Created","The use of potting, to ensure insulation at the rear of connectors with removable contacts, shall not be used except when authorized by the customer through RFA.","NOTE \tThe use of potting on these types of connectors can violate specification from manufacturer and can invalidate the qualification status of the connector itself.\n"]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.3.1a","Requirement","ECSS-Q-ST-70-26_0130076",2,"Normative Change","All crimp configurations shall be qualified in compliance with requirements from clause 5.3.2."]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.3.4.2b","Requirement","ECSS-Q-ST-70-26_0130184",1,"Created","The average tensile strength at the operating point, as per 5.3.4.2a.1, shall be higher or equal to the result obtained in 5.3.4.2a.2 and in compliance with 5.4.3."]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.4.4f","Requirement","ECSS-Q-ST-70-26_0130101",1,"Unchanged","This section shall then be polished with successively finer grades of diamond paste down to 1 µm. "]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.5.1a","Requirement","ECSS-Q-ST-70-26_0130105",1,"Unchanged","The supplier shall install a Quality Assurance (QA) function in conformance with the requirements as defined in ECSS-Q-ST-20. "]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.5.4.2c","Requirement","ECSS-Q-ST-70-26_0130125",2,"Normative Change","The following acceptance criteria shall be met; \n1.\tWire insulation is not damaged by the crimping operation;\n2.\tThe conductor is visible in the inspection hole when an inspection hole is provided; in the case of lugs and splices the free end of the conductor is visible at the exit point;\n3.\tThe crimp barrel has no unintentional sharp edges, peeled metal, burrs, cracked platings or cuts after crimping;\n4.\tAll functional parts, including all retention clips or locking devices, are operational after the crimp has been made;\n5.\tNo tarnished or corroded crimped item are present;\n6.\tNo misplaced crimps, as determined by marks found on areas not designed to take crimping, are present \n7.\tNo undercrimps or overcrimps are present;\n8.\tThe detection of an under crimp or over crimp shall cause the stop of manufacturing as follows:\n(a)\toperations at that work place , \n(b)\trejection of all production crimps made since the last verification or pull test, \n(c)\tinvestigation of tools, wire and crimp item to determine the cause of failure.\n9.\tNo bent contacts are present.\n10.\tWire strands are not damaged as a result of the crimping operation.\n11.\tThe insulation clearance complies with the requirements 5.2.4d and 5.2.4e."]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.5.6.2d","Requirement","ECSS-Q-ST-70-26_0130144",2,"Normative Change","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), "]
["ECSS-Q-ST-70-26C Rev.1 Corr.1","ECSS - Current v0.9","5.6a","Requirement","ECSS-Q-ST-70-26_0130157",2,"Normative Change","The supplier shall produce documentation for: \n1.\tProcess identification, in a PID or a specific internal procedure and RFA,\n2.\tInspection,\n3.\tTraceability,\n4.\tTesting, both procedures and records,\n5.\tLogbooks, and\n6.\tCalibration."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","5.5f","Requirement","ECSS-Q-ST-70-60_1390019",1,"Created","The PCB manufacturer shall provide the completed survey for assessment of the PCB manufacturer’s capabilities in conformance with IPC-1710."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","5.9e","Requirement","ECSS-Q-ST-70-60_1390040",1,"Created","The PCB manufacturer shall provide the response to the audit checklist to the qualification authority at least one week prior to the date of the audit."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","5.9m","Requirement","ECSS-Q-ST-70-60_1390048",1,"Created","The final conclusion of the audit process shall be provided in the final audit report or minutes of meeting."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","5.13h","Recommendation","ECSS-Q-ST-70-60_1390731",1,"Created","Major process change notices should be submitted to the procurement authority for approval."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.2.6c","Requirement","ECSS-Q-ST-70-60_1390083",1,"Created","The PCB manufacturer and procurement authority shall review during the MRR as a minimum the following aspects:\n1.\tDesign review of PCB definition dossier including review items\n2.\tTraceability of any design modifications\n3.\tBuild-up\n4.\tPanelisation, placement of coupons and PCBs in the panel\n5.\tRisk assessment\n6.\tCompliance to ECSS-Q-ST-70-12\n7.\tCompliance to ECSS-Q-ST-70-60\n8.\tCompliance to PID recorded in PCB approval sheet part 2 from Annex G.2.1b.","NOTE \tFor the risk assessment, it is good practice to use a risk rating from 1 to 5. At a risk rating until 3 it is typical that the PCB manufacturer endorse the responsibility of the risk. At a risk rating of 4 or 5 it is typical that the procurement authority endorses the responsibility of the risk. At a risk rating from 3 to 5 it is good practice to involve the project for acceptance of the risk, because there can be a potential schedule impact.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.3j","Requirement","ECSS-Q-ST-70-60_1390094",1,"Created","In-process control by IST testing shall be in conformance with clause 9.5.5.2.1."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.7.2e","Recommendation","ECSS-Q-ST-70-60_1390743",1,"Created","Local measures for cleanliness at the lay-up area should include the following:\n1.\tlaminar flow bench;\n2.\tde-ionisation equipment;\n3.\tlocal monitoring of particulate contamination;\n4.\tlocal cleanliness class 6 or better, in accordance with ISO-14644-1:2015."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.7.2j","Requirement","ECSS-Q-ST-70-60_1390126",1,"Created","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"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.10.2m","Permission","ECSS-Q-ST-70-60_1390753",1,"Created","Nodules that reduce the diameter of PTH to below the requirement may be removed in case all the following conditions are met:\n1.\tThe nodules are caused by fibres connecting to only 1 side of the hole wall;\n2.\tThe nodules are removed by applying slight mechanical force by probing with a gauge;\n3.\tThe integrity of the hole wall after repair is not compromised;\n4.\tThe integrity of the hole wall after repair is verified by inspection by the PCB manufacturer using a prismatic ocular;\n5.\tSnPb is not reflowed after removal of nodule;\n6.\tThe number of repairs of nodules does not exceed 2 per PCB."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.12e","Requirement","ECSS-Q-ST-70-60_1390163",1,"Created","Baking of PCBs prior to soldering, after short or long storage, shall be performed in conformance with requirements 9.2.2a and 9.2.2b."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","6.14p","Requirement","ECSS-Q-ST-70-60_1390179",1,"Created","In case of non-compliance of a technology parameter to the PID, a delta qualification plan shall be submitted to the customer in conformance with requirement 6.14q.","NOTE \tClause 7.6 specifies the requirements of tests, inspections and specimen for delta qualification.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","7.6f","Requirement","ECSS-Q-ST-70-60_1390204",1,"Created","In case delta qualification is initiated in the context of a space project, the procurement authority shall handle it through an RFA, in conformance with clause 7.7."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","7.7.2p","Requirement","ECSS-Q-ST-70-60_1390215",1,"Created","In case suppliers use IPC standards as PCB procurement specification, all the following conditions shall be met:\n1.\tThe project qualification is performed using group 6 in conformance with clause 7.7.2.\n2.\tThe PCB design is in conformance with chapter 6.3 from IPC-2221B for electrical clearance.\n3.\tIPC-6012D and IPC-6012DS for space applications are used for rigid PCBs.\n4.\tIPC-6018C and IPC-6018CS for space applications are used for RF PCBs.\n5.\tIPC-6013D is used for flexible and rigid-flex PCB.\n6.\tPCB manufacturers are on the IPC QML or have passed a specific audit from the procurement authority to assess compliance to the IPC standards from conditions 3, 4 and 5.\n7.\tCoupons and PCBs of all panels are evaluated in conformance with clause 8.\n8.\tCoupon inspection is performed by a third-party lab for evaluation in conformance with IPC-A-600 and the applicable IPC standards from conditions 3, 4 and 5.","NOTE\t1\tFor requirement 7.7.2p.1 during the project qualification, any HDI technology or embedded film components are evaluated.\nNOTE\t2\tRequirement 7.7.2p.1 is in conformance with IPC-6011 clause 3.6 which specifies that the qualification assessment is as agreed between user and supplier (AABUS).\nNOTE\t3\tRequirement 7.7.2p.2 is particularly important in case double insulation is applicable. However, IPC-2221B is not necessarily meeting the requirements from ECSS-Q-ST-70-12 for double insulation. It is good practice to implement the additional risk mitigations for double insulation in conformance with the present standard and ECSS-Q-ST-70-12. In case the PCB design is not performed as per ECSS-Q-ST-70-12 as described in requirement 7.7.2p.2, it is good practice to provide a compliance matrix to insulation distance for double insulation from clause 13.9 of ECSS-Q-ST-70-12 and requirements 6.5c and 8.5c of ECSS-Q-ST-70-60.\nNOTE\t4\tFor requirement 7.7.2p.3 it is not good practice to use only IPC-6012D class 3, which represents a lower quality class.\nNOTE\t5 \tFor requirement 7.7.2p.5 it is good practice to use IPC-6013DS for space applications when this is issued.\nNOTE\t6\tThe evaluation from requirement 7.7.2p.7 includes the following:\n·\tcoupon evaluation includes IST testing in conformance with clause 9.5.5 when this is applicable to the technology,\n·\tcoupon evaluation includes three times solder bath float test and rework simulation, among others,\n·\tPCB visual inspection is performed using 10-40x magnification,\n·\tPCB evaluation includes high resistance electrical test with 1 GΩ insulation resistance threshold.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","8.2.2f","Requirement","ECSS-Q-ST-70-60_1390228",1,"Created","Coupon Bn shall include at least 3 holes per drilling sequence.","NOTE \tSee an example of 3 holes per drilling sequence for coupon Bn in Figure 8-2. The top layer is a different drill sequence than the bottom layer and therefore 3 holes are present in the coupon for both layers.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","8.2.4h","Requirement","ECSS-Q-ST-70-60_1390251",1,"Created","The microsection of the thermally stressed coupons for plated holes shall be submitted to microscopic inspection in as-polished condition.","NOTE \tThis is specified because micro-etch reveals the interface between plated copper layers. Therefore this is less efficient to evaluate any plating separation.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.2.3b","Requirement","ECSS-Q-ST-70-60_1390274",1,"Created","Plated copper tensile strength shall be ≥ 276 MPa."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.3.3.1a","Requirement","ECSS-Q-ST-70-60_1390289",1,"Created","Physical dimensions shall be measured for verification of the PCB definition dossier.","NOTE\t1\tIn addition to the specified measurement, the physical dimensions are also submitted to visual inspection in conformance with clause 9.3.2.\nNOTE\t2\tThe mechanical drawing is typically used to specify physical dimensions and tolerances of the PCB.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.3.3.3g","Requirement","ECSS-Q-ST-70-60_1390312",1,"Created","Twist shall be calculated as follows:\n1.\tTwist [%] = max distance [mm] / (2 x length of PCB diagonal [mm]) x 100"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.3.7.2l","Permission","ECSS-Q-ST-70-60_1390786",1,"Created","In case the first test fails between 0,1-1,0 GΩ, one further bake and re-test may be performed."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.3.8.2a","Requirement","ECSS-Q-ST-70-60_1390333",1,"Created","Resistive continuity testing shall be performed on final PCBs using flying probe equipment."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.4.3f","Requirement","ECSS-Q-ST-70-60_1390357",1,"Created","The test shall be carried out in conformance with test method 2.4.3.1c of IPC-TM-650 and paragraph 3.10.14 of IPC-6013D.","NOTE \tThe equipment can be similar to the automated equipment described in IPC-TM-650 2.4.3.1c. Alternatively the test can be performed using a manual equipment.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.4.6d","Requirement","ECSS-Q-ST-70-60_1390375",1,"Created","The composition of tin-lead shall be: Sn = 63 % ± 8 %","NOTE\t1\tLead-rich underplating of tin-lead finish can cause the content of tin in the final reflowed finish to be below the required 55 %.\nNOTE\t2\tAnalysis of SnPb coating can be measured coupon P from IPC-2221B.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.4.11.3b","Requirement","ECSS-Q-ST-70-60_1390389",1,"Created","The flux shall be type “ROL0” in conformance with table 6-2 of ECSS-Q-ST-70-08."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.5.2.5d","Requirement","ECSS-Q-ST-70-60_1390414",1,"Created","The specific magnification for microscopic inspection for each acceptance criteria shall be as specified in clause 10."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.5.3a","Requirement","ECSS-Q-ST-70-60_1390415",1,"Created","The test shall be carried out in conformance with condition A of test method 2.6.8e of IPC-TM-650."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.5.4.3l","Requirement","ECSS-Q-ST-70-60_1390436",1,"Created","Clauses 9.5.4.3i, 9.5.4.3j and 9.5.4.3k shall be repeated 10 times in total.","NOTE\t1\tThe wire is left inside the PTH.\nNOTE\t2\tThe acronym for the rework simulation is “RW”. This acronym refers to this test method which specifies 10 cycles. Thus, “RW” does not imply only 1 heat cycle.\nNOTE\t3\tThe worst-case combination of initial assembly, maximum number of repairs and maximum number of rework per component assembly can include a number of heat cycles that is higher than the 10 specified in this test method. \n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.5.5.4.2g","Requirement","ECSS-Q-ST-70-60_1390456",1,"Created","Failure threshold of resistance change shall be 4 % for microvias."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.5.5.5.2e","Recommendation","ECSS-Q-ST-70-60_1390826",1,"Created","The daisy-chain should include interconnection on all RF innerlayers."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.6.4c","Requirement","ECSS-Q-ST-70-60_1390485",1,"Created","For intralayer measurements the test voltage shall be applied between two adjoining, but not electrically connected conductors within the same layer with a total length of ≥ 25 mm.","NOTE \tInsulation distance between tracks or between layers is representative of the PCB, as specified in clause 15.2 of ECSS-Q-ST-70-12.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.7.2.2b","Requirement","ECSS-Q-ST-70-60_1390489",1,"Created","The sensitivity S of the pattern shall be calculated using the following formula:\n \nWhere:\nL: length of track\nN: number of gaps between tracks\nD: insulation distance","NOTE\t1\tThe unit of the sensitivity is “number of squares”. This is a dimensionless value representing the interface area, that is proportional to the sum of the length of parallel tracks and inverse proportional to the insulation distance. \nNOTE\t2\tThe pattern in Figure 9-10 uses 150 μm track width and 150 μm insulation distance over an area of 30 mm length and width. This results in 30/(0,15+0,15)=100 gaps N. Therefore the sensitivity S= 30 x 100 / 0,15 = 20000 number of squares.\n"]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.7.3.2g","Requirement","ECSS-Q-ST-70-60_1390511",1,"Created","The actual registration achieved on each coupon shall be included for the calculation of minimum insulation distances."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","9.8.3d","Requirement","ECSS-Q-ST-70-60_1390528",1,"Created","The duration at the maximum temperature of the profile shall be between 5 s and 10 s."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","10.2l","Requirement","ECSS-Q-ST-70-60_1390551",1,"Created","For the technological features tin-led thickness and composition, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-12. "]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","10.4b","Requirement","ECSS-Q-ST-70-60_1390615",1,"Created","For the technological feature conductor spacing, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-39."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","10.5i","Requirement","ECSS-Q-ST-70-60_1390650",1,"Created","For the technological feature aspect of pads for sculptured flex PCB, the acceptance criteria, the inspection samples and the measurement method shall be in conformance with Table 10-60."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","10.6.3d","Requirement","ECSS-Q-ST-70-60_1390688",1,"Created","Remaining insulation distance shall be the sum of insulation distances to conductors that are not affected by cracks."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","B.2.1.1b","Requirement","ECSS-Q-ST-70-60_1390694",1,"Created","The CoC shall cover the batch or a subset."]
["ECSS-Q-ST-70-60C Corr.1","ECSS - Current v0.9","C.2.2a","Requirement","ECSS-Q-ST-70-60_1390712",1,"Created","The qualification test report shall be maintained under configuration control."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","5.2.2.1b","Requirement","ECSS-Q-ST-10-09_0350012",1,"Unchanged","The responsibilities and authorities of each member shall be assigned."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","5.2.3.5a","Requirement","ECSS-Q-ST-10-09_0350041",1,"Unchanged","The responsible NRB shall identify and recommend the need for a waiver or deviation."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","5.5.1d","Requirement","ECSS-Q-ST-10-09_0350059",1,"Informative Change","The supplier shall provide the NCR status list as part of the periodic PA status report to the customer, in conformance with Annex B.","The nonconformance status list is usually generated from the nonconformance database."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","5.5.3b","Requirement","ECSS-Q-ST-10-09_0350064",1,"Informative Change","The nonconformance records shall be analysed to assess the existence of trends in the occurrence of nonconformances. ","1\tThis analysis aims at detecting conditions which can lead to new nonconformances and verify the effectiveness of the implementation of the corrective actions performed for previous nonconformances.\n2\tThe analysis of records aims at extracting lessons learned, useful for preventing the repetition of mistakes or reinforcing successful practices."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","6.3.2.2b","Requirement","ECSS-Q-ST-10-09_0350085",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","A.2.1<30>a","Requirement","ECSS-Q-ST-10-09_0350123",1,"Unchanged","The NCR shall summarize corrective actions agreed by customer NRB for major NCRs."]
["ECSS-Q-ST-10-09C Rev. 1","ECSS - Current v0.9","A.2.1<39>a","Recommendation","ECSS-Q-ST-10-09_0350148",1,"Created","The NCR should additionally contain the following information: \n    1. Related internal NCR\n    2. NCR title\n    3. Next higher assembly\n    4. Subsystem / Model reference \n    5. Identification of violated requirements \n    6. Customer notification (date and reference ) \n    7. Alert identification "]
["ECSS-Q-ST-70-17C","ECSS - Current v0.9","5.2j","Requirement","ECSS-Q-ST-70-17_1380014",1,"Created","Reduced test programme for qualification shall be agreed between customer and supplier."]
["ECSS-Q-ST-70-17C","ECSS - Current v0.9","5.6a","Requirement","ECSS-Q-ST-70-17_1380030",1,"Created","After the completion of each test, the coating shall be accepted when the following criteria are met: \n1.\tno visual degradation of the coating;\n2.\tno delamination or adherence loss;\n3.\tthickness conforms to requirements; \n4.\tperformance measurements comply with coating specification.","NOTE\t1\tDegradation can be colour change, cracks, pits.\nNOTE\t2\tAdditional microscope inspection can be used for suspected degradation.\nNOTE\t3\tSpecific acceptance criteria can also be defined for some tests.\nNOTE\t4\tFor some test steps, a partial set of measurements can be agreed with the customer, to save time and effort (see Annex D).\nNOTE\t5\tCoating specification is included in the qualification plan (see Annex A).\n"]
["ECSS-Q-ST-70-17C","ECSS - Current v0.9","6.6a","Requirement","ECSS-Q-ST-70-17_1380064",1,"Created","The abrasion resistance test for optical coatings shall be done in conformance with the requirements from ISO 9211-4:2012, Conditioning method 01, severity degree 01 "]
["ECSS-Q-ST-70-17C","ECSS - Current v0.9","6.7c","Requirement","ECSS-Q-ST-70-17_1380068",1,"Created","The radiation test shall be performed using fully flight representative substrates with known radiation characteristics for the mission environment."]
["ECSS-Q-ST-70-05C Rev.1","ECSS - Current v0.9","5.1.2.1b","Requirement","ECSS-Q-ST-70-05_0540009",1,"Unchanged","Air used for ventilation shall be filtered to prevent contamination of the work pieces."]
["ECSS-Q-ST-70-05C Rev.1","ECSS - Current v0.9","5.2.3.3e","Requirement","ECSS-Q-ST-70-05_0540031",1,"Unchanged","Depending on the chosen type of wiping process (wet or dry), the following steps shall be performed:\n1.\tFor a wet wipe process \n(a)\tFold with tweezers the pre-cleaned tissue in order to use it as a little \"sponge\";\n(b)\tWet with spectral grade IPA or chloroform;\n(c)\tHold the folded tissue with curved point tweezers;\n(d)\tStore the tissue after wiping, when the solvent is evaporated in the transport container.\n2.\tFor a dry wipe process, cover the foam or rubber tube with a standard filter paper and a pre-cleaned tissue."]
["ECSS-Q-ST-70-05C Rev.1","ECSS - Current v0.9","5.4.3.2a","Requirement","ECSS-Q-ST-70-05_0540056",1,"Informative Change","The calibration shall be performed covering the required concentration range.","NOTE \tTypical range is 5 ´ 10-8 g/cm2   to  5 ´ 10-6 g/cm2.\n"]
["ECSS-Q-ST-70-05C Rev.1","ECSS - Current v0.9","5.4.5.2b","Requirement","ECSS-Q-ST-70-05_0540077",1,"Informative Change","A training programme shall be developed, maintained and implemented.","NOTE \tThe training programme is set up to provide for excellence of workmanship and personnel skills as well as for thorough knowledge of the requirements detailed in this Standard.\n"]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.1.1b","Requirement","ECSS-Q-ST-70-31_0660002",1,"Unchanged","Depending on the specific project requirements, the paint applied shall fulfil part or all the acceptance criteria given in 4.4 of this Standard."]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.2.1c","Requirement","ECSS-Q-ST-70-31_0660011",1,"Unchanged","In addition, hazards to personnel, equipment, environment and materials shall be controlled and reduced to an acceptable risk.","NOTE \tHazard can be reduced by using protective clothing.\n"]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.2.4.3a","Requirement","ECSS-Q-ST-70-31_0660032",1,"Informative Change","Dependant on the specific requirements, the following utilities shall be available:\n1.\tAn oven capable of maintaining the workpiece in a clean environment and within ±5 °C of the required control temperature.\n2.\tAn ultrasonic bath.\n3.\tA fume cupboard used for handling toxic or irritating primers, paints, solvents or cleaning agents.\n4.\tA spray booth.","NOTE \tto item 2: A combined system can be used, in which ultrasonic cleaning can be followed by vapour cleaning.\n"]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.3.2b","Requirement","ECSS-Q-ST-70-31_0660057",1,"Unchanged","Paint shall be masked with pressure-sensitive tape, leaving no residue after removal or with clean non-absorbent paper."]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.3.6.1b","Requirement","ECSS-Q-ST-70-31_0660084",1,"Unchanged","For small areas (less than 2 cm x 2 cm), the repairing shall be done with a paint brush in a clean room."]
["ECSS-Q-ST-70-31C Rev.1","ECSS - Current v0.9","4.5.3a","Requirement","ECSS-Q-ST-70-31_0660104",1,"Unchanged","ECSS-Q-ST-10-09 shall apply."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.1b","Requirement","ECSS-Q-ST-70-71_1260002",1,"Unchanged","Alloys, heat treatments and coatings which minimize susceptibility to general corrosion, pitting, intergranular and stress corrosion cracking shall be used."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.8e","Requirement","ECSS-Q-ST-70-71_1260028",1,"Unchanged","The capability of the equipment to meet the specified requirements, processes, welding supplies and supplementary treatments selected by the supplier shall be demonstrated through qualification testing of welded specimens representing the materials and joint configuration of production parts."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.11a","Requirement","ECSS-Q-ST-70-71_1260049",1,"Unchanged","The surfaces on which the adhesives, coatings or varnishes are applied shall be clean and dry prior to their application."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.12l","Requirement","ECSS-Q-ST-70-71_1260073",1,"Unchanged","The supplier shall demonstrate that the selected Velcro-type tape does not release hooks or felt during assembly or disassembly."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.15i","Requirement","ECSS-Q-ST-70-71_1260094",1,"Unchanged","The supplier shall demonstrate that the cure procedures are performed such that the temperatures and pressures created during curing process do not damage the potting compound or the parts being potted."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.17g","Requirement","ECSS-Q-ST-70-71_1260109",1,"Unchanged","Material depolymerization due to vacuum exposure shall be assessed."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.18f","Requirement","ECSS-Q-ST-70-71_1260120",1,"Unchanged","For polymer-based materials, environmental exposure shall be assessed.","NOTE\tExamples of environmental exposure are: flammability requirements, electrical requirements, normal use temperature, abnormal use temperature excursions, chemical exposure and humidity levels.\n"]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.2.21c","Requirement","ECSS-Q-ST-70-71_1260145",1,"Unchanged","All applications using composite materials based on ceramic, carbon and glass compositions shall be reviewed and approved by the customer."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.3.6k","Requirement","ECSS-Q-ST-70-71_1260176",1,"Unchanged","The weld repair process and inspection shall be performed only under nonconformance review board approval."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.3.9.2a","Requirement","ECSS-Q-ST-70-71_1260192",1,"Unchanged","The supplier shall demonstrate that when anodizing processes are applied to thin foils, the perforation is prevented. "]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.3.12.5a","Requirement","ECSS-Q-ST-70-71_1260217",1,"Unchanged","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"]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.3.14b","Requirement","ECSS-Q-ST-70-71_1260222",1,"Unchanged","Solvents in inks shall not attack substrates."]
["ECSS-Q-ST-70-71C Rev.1","ECSS - Current v0.9","4.3.16b","Requirement","ECSS-Q-ST-70-71_1260241",1,"Unchanged","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"]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","4.2.3g","Requirement","ECSS-Q-ST-70_0490018",2,"Unchanged","The as­designed lists shall include the items from the baselines various design files, available for CDR."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","5.1.2a","Requirement","ECSS-Q-ST-70_0490034",2,"Informative Change","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","5.1.7e","Requirement","ECSS-Q-ST-70_0490214",1,"Informative Change","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","5.2.1a","Requirement","ECSS-Q-ST-70_0490059",2,"Informative Change","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","5.2.1b","Requirement","ECSS-Q-ST-70_0490060",2,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","5.5.2a","Requirement","ECSS-Q-ST-70_0490071",2,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","6.2a","Requirement","ECSS-Q-ST-70_0490098",2,"Unchanged","Mechanical parts shall be chosen from used for an identical application in other space programmes similar with respect to environment constraints and lifetime."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","6.5.4b","Requirement","ECSS-Q-ST-70_0490114",2,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","7.3b","Requirement","ECSS-Q-ST-70_0490139",2,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","7.6.2b","Requirement","ECSS-Q-ST-70_0490151",1,"Unchanged","When an evaluation is performed, the supplier shall provide \n1.\tan evaluation plan at PDR, and\n2.\tan evaluation report before CDR."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","7.6.3c","Requirement","ECSS-Q-ST-70_0490154",1,"Unchanged","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."]
["ECSS-Q-ST-70C Rev.2","ECSS - Current v0.9","B.2.2a","Requirement","ECSS-Q-ST-70_0490176",1,"Unchanged","The change record shall list the successive issues and their release dates since the first formal issue of the document."]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","ECSS - Current v0.9","4.2.3b","Requirement","ECSS-Q-ST-60-14_0470059",1,"Created","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"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","ECSS - Current v0.9","6.1.1d","Requirement","ECSS-Q-ST-60-14_0470021",1,"Unchanged","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"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","ECSS - Current v0.9","7.1.1a","Requirement","ECSS-Q-ST-60-14_0470068",1,"Created","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"]
["ECSS-Q-ST-60-14C Rev.1 Corr.1","ECSS - Current v0.9","7.5d","Requirement","ECSS-Q-ST-60-14_0470094",1,"Created","The relifing NCR, if any, signed and dated by the supplier, shall be delivered with the components.\n"]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","5.3.2c","Requirement","ECSS-Q-ST-30-11_0140004",2,"Normative Change","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.","NOTE \tIt is important to pay specific attention to breadboards and engineering models where parameter derating was not considered.\n"]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.2.1e","Recommendation","ECSS-Q-ST-30-11_0140180",1,"Created","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."]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.6.1b","Recommendation","ECSS-Q-ST-30-11_0140185",1,"Created","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."]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.14.2.1a","Requirement","ECSS-Q-ST-30-11_0140064",1,"Unchanged","Parameters of Diode (signal/switching, rectifier including Schottky, pin) shall be derated as per Table 6‑13."]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.19.2a","Requirement","ECSS-Q-ST-30-11_0140085",1,"Unchanged","Parameters of Integrated circuits from family-group code: 08-10, 08-20, 08-21, 08-29 to 08-42, and 08-80 shall be derated as per Table 6‑19."]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.23.2b","Requirement","ECSS-Q-ST-30-11_0140099",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.26.2.2a","Requirement","ECSS-Q-ST-30-11_0140114",2,"Normative Change","Parameters of Metal film semi-precision resistor (type RLR) shall be derated as per Table 6‑26."]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.32.4d","Requirement","ECSS-Q-ST-30-11_0140216",1,"Created","The harness designer shall make sure that the temperature of each component connected to the wire is compatible with the selected wire temperature Twire.","NOTE \tExamples of components connected to the wire are contacts, connectors, etc.\n"]
["ECSS-Q-ST-30-11C Rev.2","ECSS - Current v0.9","6.34.3c","Requirement","ECSS-Q-ST-30-11_0140159",1,"Unchanged","Maximum mating and de-mating cycles shall be limited to 50 cycles."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","5.1s","Requirement","ECSS-Q-ST-70-15_1470019",1,"Created","In the case of conflicting requirements, Clause 8 shall take precedence over Clause 6."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.1.2d","Requirement","ECSS-Q-ST-70-15_1470044",1,"Created","The testing object shall be accessible in that way, that the surface can be tested within a distance of 600 mm and with a viewing angle > 30°."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.1.3.2d","Recommendation","ECSS-Q-ST-70-15_1470049",1,"Created","Comparison catalogues should be controlled within the company documentation management system."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.3.2h","Requirement","ECSS-Q-ST-70-15_1470071",1,"Created","For parts that are shot peened, dry vapour blasted, machine polished or burnished in the testing area the qualification programme shall demonstrate that discontinuities are not closed by the surface processes.","NOTE\tExamples of surface treatments include: shot peened, dry vapour blasted, machine polished or burnished in the testing area.\n"]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.4.2b","Requirement","ECSS-Q-ST-70-15_1470096",1,"Created","Fastener holes shall be tested in accordance with SAE-ARP-4402:2013 or SAE-AS-4787:2013 or an equivalent standard approved by the customer."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.4.8.2a","Requirement","ECSS-Q-ST-70-15_1470117",1,"Created","Eddy current inspections shall be in accordance with ASTM E 426:2016, SAE-ARP-4402:2013, SAE-AS-4787:2013, or customer approved internal supplier specifications. "]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.5.8.2f","Requirement","ECSS-Q-ST-70-15_1470143",1,"Created","Pie gages shall not be used for measuring field intensities."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.6.4c","Requirement","ECSS-Q-ST-70-15_1470148",1,"Created","Each radiograph shall include the following identification: \n1.\tIdentification of the part;\n2.\tViewing number;\n3.\tDate of examination;\n4.\tNDT facility inspecting the part.","NOTE\tNumber of times that repairs were carried out is optional.\n"]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","6.7.4.1e","Requirement","ECSS-Q-ST-70-15_1470169",1,"Created","For discontinuities with randomly distributed orientations, automated phased-array or sampling phased-array testing shall be applied."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","8.2a","Requirement","ECSS-Q-ST-70-15_1470199",1,"Created","For the examination of wrought metals, forged and rolled, parts, the customer shall specify in consultation with Level 3:\n1.\tWho is certified to inspect wrought products\n2.\tThe NDT method to be used\n3.\tThe class and acceptance criteria\n4.\tThe aerospace quality standards to be applied, and their applicability\n5.\tThe added and modified requirements to these standards.","NOTE\t\tThe customer normally specifies in the purchase order or other contractual document, based on final piece part usage.\n"]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","8.5.2.5b","Requirement","ECSS-Q-ST-70-15_1470216",1,"Created","Examination specified in requirement 8.5.2.5a shall be performed in accordance with ASTM E 1814:2014, or EN ISO 15708-2:2019 and EN ISO 15708-4:2019."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","9.1.3a","Requirement","ECSS-Q-ST-70-15_1470241",1,"Created","NDT capability demonstration specimens shall be used for determining the detection capability for all Special fracture control NDT applications, as specified in clause 9.2.2.2 and requirement 9.2.1d."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","9.2.2.1f","Requirement","ECSS-Q-ST-70-15_1470267",1,"Created","For tight discontinuities as specified in 9.2.2.1e, Special fracture control NDT requirements shall apply as specified in the requirement 9.2.2.2. "]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","9.3.2.1b","Permission","ECSS-Q-ST-70-15_1470288",1,"Created","Analogy to knowledge of testing of metallic material may be used."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","9.3.2.3a","Requirement","ECSS-Q-ST-70-15_1470293",1,"Created","The capability of an NDT method to reliably detect the specified discontinuity size shall be demonstrated on test specimens with induced artificial discontinuities."]
["ECSS-Q-ST-70-15C","ECSS - Current v0.9","B.2.2b","Requirement","ECSS-Q-ST-70-15_1470314",1,"Created","The documents supporting the NDT Report shall be kept as agreed between customer and supplier."]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","6.3b","Requirement","ECSS-Q-ST-70-16_1460019",1,"Created","Date of the bonding process steps shall be recorded.\n"]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","7.8d","Requirement","ECSS-Q-ST-70-16_1460044",1,"Created","For the determination of design allowables the number of test items shall be agreed with the design authority."]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","7.12.2f","Requirement","ECSS-Q-ST-70-16_1460065",1,"Created","In addition to requirement 7.12.2b additional thermal cycles shall be performed to cover mission lifetime.\n","NOTE\t1\tThe additional thermal cycles are typically performed to simulate ageing effects (thermo-chemical, creep and fatigue phenomena).\nNOTE\t2\tThe additional thermal cycles can contain long term thermal endurance exposure, for example cruise phases of probes.\n"]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","8.3a","Requirement","ECSS-Q-ST-70-16_1460079",1,"Created","Procurement of all materials needed for adhesive bonding shall be in conformance with clause 5.6.1 of ECSS-Q-ST-70.\n","NOTE\tMaterials to be considered are for example raw materials, adhesives, filler materials, as well as adherends manufactured and pre-treated (for example plated, conversion coated) for bonding.\n"]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","8.7d","Requirement","ECSS-Q-ST-70-16_1460096",1,"Created","Selection of tooling and equipment shall conform to the requirements from clause 5.2.6 of ECSS-Q-ST-20.\n"]
["ECSS-Q-ST-70-16C","ECSS - Current v0.9","8.10e","Recommendation","ECSS-Q-ST-70-16_1460117",1,"Created","Visual standards of bonded joints such as photos, drawings or other visual aids and clearly illustrating the quality characteristics needed should be available to each inspector.\n","NOTE\t1\tThe visual standards can be examples of acceptable and unacceptable bond lines.\nNOTE\t2\tTypical defects can be reported in a defect catalogue.\n"]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","6.3b","Requirement","ECSS-Q-ST-70-80_1480016",1,"Created","The minimum content of the PMCR shall be in accordance with the DRD from Annex A."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","7.4.1b","Requirement","ECSS-Q-ST-70-80_1480034",1,"Created","The AMVP specified in 7.4.1a shall be agreed with the customer."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","7.5.4c","Requirement","ECSS-Q-ST-70-80_1480062",1,"Created","The test results of the witness specimens shall be incorporated in a Materials Properties Database (MPD), in accordance with clause 11.3.1."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","7.7.2c","Requirement","ECSS-Q-ST-70-80_1480067",1,"Created","If a machine pause is planned to occur during the hardware production phase, dedicated tests to characterise the properties of the interface zone shall be included in the AMVP."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","8.2.3.2c","Requirement","ECSS-Q-ST-70-80_1480086",1,"Created","The tensile specimens shall be evenly distributed in the build volume."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","9.3.2b","Requirement","ECSS-Q-ST-70-80_1480115",1,"Created","Only operators holding a valid qualification test certificate in accordance with requirement 9.3.2a shall perform operations on electron beam based powder bed fusion equipment."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","10.6.3b","Requirement","ECSS-Q-ST-70-80_1480140",1,"Created","The purity of nitrogen shall be at least 99,998 %."]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","11.5b","Permission","ECSS-Q-ST-70-80_1480154",1,"Created","Suppliers may be re-audited if major changes to the end-to-end manufacturing process are made.","NOTE\tAn example of an audit check list is proposed in Annex J.\n"]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","12.5.3.2d","Requirement","ECSS-Q-ST-70-80_1480187",1,"Created","The load ratio (R) shall be representative of the final application.","NOTE\tIn many cases, a stress ratio of -1 is representative of space applications, especially when the dominant load is caused by vibration.\n"]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","13.1a","Requirement","ECSS-Q-ST-70-80_1480188",1,"Created","With a test method proposed by the supplier and agreed with the customer, testing of powders shall include as a minimum:\n1.\tChemical composition, including light elements,\n2.\tParticle size distribution,\n3.\tDensity in both apparent and tapped conditions, and\n4.\tFlow properties.","NOTE\t1\tFor requirement 13.1a1: light elements can include carbon, hydrogen, oxygen, and nitrogen.\nNOTE\t2\tFor requirement 13.1a1: the chemical composition can be determined by energy-dispersive spectrometry (EDS) as per ISO 22309:2011 or ASTM E1508 or by atomic emission spectrometry for Aluminium alloys as per ASTM E3061:2017 and for titanium alloys as per ASTM E 2371:2013.\nNOTE\t3\tFor requirement 13.1a1: determination of hydrogen in titanium alloys can be done by inert gas fusion as per ASTM E 1447:2016. Determination of carbon in refractory and reactive metals can be done by combustion analysis as per ASTM E 1941:2016. Determination of oxygen in titanium alloys can be done by reduction-extraction methods as per ISO 4491-4:2019. Oxygen and nitrogen in titanium alloys can be determined by inert gas fusion as per ASTM E 1409:2013.\nNOTE\t4\tFor requirement 13.1a1: increased oxygen content can lead to reduced ductility of IN 718 at elevated temperatures. It is best practice to limit the oxygen content in the base material more strictly than this is done for conventional materials.\nNOTE\t5\tFor requirement 13.1a2: particle size distribution can be analyzed by sieve analysis as per ISO 4497:2020 or ASTM B214:2016, by laser diffraction in compliance with ISO 13320:2020 or ASTM B822:2017 or by image analysis in compliance with ISO 13322:2014.\nNOTE\t6\tFor requirement 13.1a3: the apparent density can be determined according to ISO 3923-1:2018 or ASTM B212:2017 (Funnel Method). The tap density can be determined according to ISO 3953:2011 or ASTM B527.\nNOTE\t7\tFor requirement 13.1a3: testing for porosity in powder particles is not required, but it can be performed by helium pycnometry in compliance with ASTM B923:2020, or through X-Ray CT scanning.\nNOTE\t8\tFor requirement 13.1a4: flow properties can be determined through the Hall Flowmeter test in compliance with ASTM B213:2020, ASTM B 964:2016, or ISO 4490:2018 and tap density as per ASTM B527:2020. Alternatively, “angle of repose” tests according to ISO 4324:1977 can also be used.\nNOTE\t9\tFor requirement 13.1a4: it is best practice to determine powder particle morphology and satellite build-up with an SEM as complementary information.\nNOTE\t10\tAluminium powders are known to pick up moisture, which can degrade flow properties or lead to significant gas porosity in the final AM part. It is best practice to control the humidity level in areas where AM powder is handled or stored. The test can be performed using one of the following methods: capacitive titration (Karl-Fischer) according to ISO 760:1978 or ASTM E203:2016, thermogravimetric according to ASTM E1131:2020, or with a humidity sensor.\n"]
["ECSS-Q-ST-70-80C","ECSS - Current v0.9","F.2.1a","Requirement","ECSS-Q-ST-70-80_1480213",1,"Created","The Hardware Production Report (HPR) shall contain the following information:\n1.\tReference to HFP\n2.\tWitness specimens test results\n3.\tNDT results\n4.\tReference to the shop traveller\n5.\tReference to Non-Conformance Reports (NCRs)\n6.\tReference to Requests for Waivers (RFWs)"]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.1.4g","Requirement","ECSS-Q-ST-60_0480017",2,"Unchanged","The “as built” DCL reflecting the actual EEE parts assembled into the flight hardware and their date code, shall be provided before TRR to the customer for review."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.2.2.3a","Requirement","ECSS-Q-ST-60_0480036",1,"Unchanged","Parts shall be chosen from the EPPL part I."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.2.3.1c","Requirement","ECSS-Q-ST-60_0480052",1,"Unchanged","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. "]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.2.4c","Requirement","ECSS-Q-ST-60_0480069",1,"Unchanged","The supplier shall maintain a system of traceability of the acceptance and approval of each component used in flight products."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.3.1a","Requirement","ECSS-Q-ST-60_0480072",1,"Unchanged","The supplier shall ensure that all procured components meet the programme requirements with respect to inspection, screening and tests."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.3.3g","Requirement","ECSS-Q-ST-60_0480449",2,"Deleted","<<deleted>>"]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.3.8e","Requirement","ECSS-Q-ST-60_0480109",1,"Unchanged","When RVT is performed in the frame of the project, the supplier shall send the related  report to the customer for information."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.5.4c","Requirement","ECSS-Q-ST-60_0480139",1,"Unchanged","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). "]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","4.6.6a","Requirement","ECSS-Q-ST-60_0480530",1,"Created","For connectors with removable contacts, contacts shall be procured from the same manufacturer as the connector in which they are mounted."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.1.6a","Requirement","ECSS-Q-ST-60_0480532",1,"Created","EEE components used in Engineering Qualification Model (EQM) shall be fit, form and function representative of the flight components and be from the same manufacturers."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.2.2.2a","Requirement","ECSS-Q-ST-60_0480180",1,"Unchanged","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. "]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.2.2.3i","Requirement","ECSS-Q-ST-60_0480196",1,"Unchanged","The Equipment Radiation Analysis document shall be submitted to the customer for approval.","NOTE \tMore detailed information about the above requirements is given in ECSS-E-ST-10-12 and ECSS-Q-ST-60-15.\n"]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.2.3.3a","Requirement","ECSS-Q-ST-60_0480210",1,"Unchanged","Constructional analysis shall be carried out on representative components. ","NOTE \tThe primary aim is to provide an early indication of a component’s constructional suitability for meeting the specified performances of the space project application.\n"]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.3.2b","Requirement","ECSS-Q-ST-60_0480228",1,"Unchanged","International specifications systems, new specifications or manufacturer’s datasheets under configuration shall be used by the supplier. "]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.3.4b","Requirement","ECSS-Q-ST-60_0480240",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.3.7d","Permission","ECSS-Q-ST-60_0480506",1,"Unchanged","If the parts have passed successfully a final CSI (or buy-off), the incoming inspection may be reduced to the following minimum:\n1.\tVerification of the manufacturer’s CoC,\n2.\tPacking checking,\n3.\tQuantity verification."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","5.4d","Requirement","ECSS-Q-ST-60_0480274",1,"Unchanged","As a minimum, the following areas shall be covered:\n1.\tControl of the environment in accordance with ESCC Basic Specification No. 24900.\n2.\tMeasures and facilities to segregate and protect components during receiving inspection, storage, and delivery to manufacturing. \n3.\tControl measures to ensure that electrostatic discharge susceptible components are identified and handled only by trained personnel using anti static packaging and tools."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.1.2.1a","Requirement","ECSS-Q-ST-60_0480302",1,"Unchanged","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."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.1.6b","Requirement","ECSS-Q-ST-60_0480542",1,"Created","If thermal vacuum tests are performed on the EQM, the EEE parts shall be material representative of the FM parts."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.2.2.4a","Requirement","ECSS-Q-ST-60_0480329",3,"Normative Change","The radiation requirements for EEE components are project specific."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.2.3.1j","Requirement","ECSS-Q-ST-60_0480349",2,"Unchanged","The supplier shall summarize the evaluation results in the evaluation report and send it to the customer for approval.","NOTE \tFor guidance for the assessment of the space environmental aspects refer to ECSS-E-ST-10-04 and ECSS E-ST-10-12.\n"]
["ECSS-Q-ST-60-13C Rev.1","ECSS - Current v0.9","6.3.1f","Requirement","ECSS-Q-ST-60-13_0460542",1,"Informative Change",null,"NOTE\tThe procurement of a single trace code per delivery lot should be preferred and encouraged.\n"]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.3.2d","Requirement","ECSS-Q-ST-60_0480369",1,"Unchanged","The content of any new specification shall be in conformance with the procurement specification DRD in Annex C."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.3.8c","Requirement","ECSS-Q-ST-60_0480389",1,"Unchanged","In such a case, a PAD in conformance with Annex D shall be issued and processed as per clause 6.2.4. "]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.4c","Requirement","ECSS-Q-ST-60_0480409",2,"Unchanged","On request, handling and storage procedures shall be sent to the customer for review."]
["ECSS-Q-ST-60C Rev. 3","ECSS - Current v0.9","6.6.4g","Requirement","ECSS-Q-ST-60_0480433",2,"Unchanged","The lot acceptance procedure, as defined in clause 6.3.5, shall be performed on devices coming from the flight lot/date code and programmed on the same kind of hardware tools and compatible software."]
["ECSS-Q-ST-60-13C Rev.1","ECSS - Current v0.9","8.2a","Requirement","ECSS-Q-ST-60-13_0460698",1,"Created"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.2a","Requirement","ECSS-Q-ST-70-61_1510008",1,"Created","The clean room shall be compliant to the requirements of clause 5.3.1 of ECSS-Q-ST-70-01."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.4.5a","Requirement","ECSS-Q-ST-70-61_1510038",1,"Created","All ESD-sensitive items shall be contained within ESD-protective containers for movement between and within ESD-protected areas. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.5.3a","Requirement","ECSS-Q-ST-70-61_1510060",1,"Created","Cutting edge profiles and cutter usage shall be in accordance with Figure 5-1."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.5.7c","Requirement","ECSS-Q-ST-70-61_1510082",1,"Created","Hot air blower shall be able to maintain and control a defined temperature."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.5.11b","Requirement","ECSS-Q-ST-70-61_1510107",1,"Created","The placement equipment used shall be of a type that:\n1.\tprevents component or board damages,\n2.\tindexes components with respect to the circuit and\n3.\taligns the component terminations with the board terminal areas."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","5.5.19c","Requirement","ECSS-Q-ST-70-61_1510129",1,"Created","The resolution of the X-ray equipment shall be able to detect solder balls having a diameter of 0,03 mm."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","6.1b","Requirement","ECSS-Q-ST-70-61_1510134",1,"Created","All materials remaining on the assembled board shall be specified in the bill of materials."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","6.4h","Requirement","ECSS-Q-ST-70-61_1510161",1,"Created","The following solvents shall be used for cleaning in soldering operations:\n1.\tethyl alcohol, 99,5 % pure by weight or 95 % pure by volume,\n2.\tisopropyl alcohol, 99 % pure,\n3.\tdeionized water at a maximum temperature of 40 °C is used for removing certain fluxes provided that the assembly is thoroughly dried directly after cleaning,\n4.\tany mixture of 6.4h.1, 6.4h.2 and 6.4h.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","6.7c","Requirement","ECSS-Q-ST-70-61_1510174",1,"Created","Wires shall be stripped of their insulation in accordance with clause 7.5.1."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","7.2.1d","Requirement","ECSS-Q-ST-70-61_1510208",1,"Created","Packaging and containers for ESD-sensitive components shall be in accordance with clause 5.4."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","7.5.2g","Requirement","ECSS-Q-ST-70-61_1510229",1,"Created","Plated wires where the base material is exposed other than at the cutting surface, shall not be used."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","7.6.1c","Requirement","ECSS-Q-ST-70-61_1510243",1,"Created","Solder alloy used for degolding and pretinning shall be Sn60, Sn62 or Sn63 solder."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","7.6.2g","Requirement","ECSS-Q-ST-70-61_1510261",1,"Created","The cross-sectional area of terminations shall not be reduced by dissolution into the solder bath below the minimum values of specification."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","7.6.4.2f","Requirement","ECSS-Q-ST-70-61_1510283",1,"Created","Solder shall not flow under insulation.","NOTE\tIt is good practice to use antiwicking tools to prevent the solder flow.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","8.2.1e","Requirement","ECSS-Q-ST-70-61_1510308",1,"Created","The component mounting shall be adapted so that the solder joints do not come in contact with the component body or welded area."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","8.2.6a","Requirement","ECSS-Q-ST-70-61_1510328",1,"Created","Stress relief for components with non-bendable leads mounted in contact with the PCB or adhesively bonded to the PCB shall use wire extensions according to Figure 8-4.","NOTE\tBending can damage components when lead diameters are large, or components have delicate seals or where lead-material composition makes bending impracticable.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","8.2.9a","Requirement","ECSS-Q-ST-70-61_1510362",1,"Created","PCB connectors shall be supplied with either:\n1.\tpre-formed leads supporting stress relief bends, or\n2.\tstraight, resin moulded connector."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","8.2.9f","Requirement","ECSS-Q-ST-70-61_1510367",1,"Created","Connector leads shall protrude through the board in accordance with clause 8.2.8.2."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.2.1a","Requirement","ECSS-Q-ST-70-61_1510408",1,"Created","The length of individual wires routed from a common cable to equally spaced terminals shall be uniform including wire ends and stress-relief bends.","NOTE\tUniform lengths prevent stress concentration in any one wire.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.3f","Permission","ECSS-Q-ST-70-61_1510416",1,"Created","More than one wire may be installed in a single slot of a terminal post provided that \n1.\tthe combined diameters of the wires are less than the height of the slot, and\n2.\tthe contour of each wire is visible.","NOTE\tit is good practice to solder one wire per slot\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.5a","Requirement","ECSS-Q-ST-70-61_1510444",1,"Created","Connections to hook terminals shall be as shown in Figure 9-5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.8c","Requirement","ECSS-Q-ST-70-61_1510468",1,"Created","Interconnection methods shall not use fluxed solder preforms within heat-shrinkable sleeves."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.8i","Requirement","ECSS-Q-ST-70-61_1510474",1,"Created","The sleeving shall be cut to a length that covers the finished soldered joint and extends over the remaining insulation of each conductor for a distance of 5 mm ±2 mm."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.9.4a","Requirement","ECSS-Q-ST-70-61_1510499",1,"Created","Conductors shall be secured to prevent disturbance during soldering and solidification using one, or a combination of, the following methods:\n1.\tA holding fixture that clamps the wires ensuring correct alignment.\n2.\tRings of heat-shrinkable sleeving positioned over the ends of the wire insulations, see Figure 9-8(b) and (c)."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","9.10f","Requirement","ECSS-Q-ST-70-61_1510521",1,"Created","Wire support shall be provided by staking, conformal coating or lacing."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.2.2d","Requirement","ECSS-Q-ST-70-61_1510547",1,"Created","Components shall not be stacked nor bridge the space between other components or terminals."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.2.5j","Requirement","ECSS-Q-ST-70-61_1510574",1,"Created","The soldering iron tip shall heat the joint area to the solder liquidus temperature in a time between 1 second and 2 seconds."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.3.3c","Requirement","ECSS-Q-ST-70-61_1510599",1,"Created","On the component side, the PCB pad shall show solder flow-through and a solder fillet between the lead and the pad for a minimum of 75 % of the circumference of the lead as illustrated in Figure 10-3.a"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.3.3h","Requirement","ECSS-Q-ST-70-61_1510604",1,"Created","The solder fillets for clinched leads shall meet the visual workmanship standards as illustrated in Figure E-2."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.4.9d","Requirement","ECSS-Q-ST-70-61_1510652",1,"Created","Assembly shall be inspected with X-ray according to criteria defined in requirement 12.4a when solder fillet is not visible."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.4.14c","Requirement","ECSS-Q-ST-70-61_1510677",1,"Created","Solder joints shall be inspected with X-ray according to criteria defined in requirement 12.4a.","NOTE\t1\tAs it is impossible to visually inspect solder joints to area array components, reliability of these components cannot be assured by inspection and rework. Even using X-Ray techniques, some types of defect are difficult to detect. Therefore, reliability of these solder joints can only be assured by robust process control. \nNOTE\t2\tExamples of typical area array components are shown in Figure 10-17.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","10.6a","Requirement","ECSS-Q-ST-70-61_1510700",1,"Created","Soldered joints shall be performed such to avoid Corona discharge."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","11.2a","Requirement","ECSS-Q-ST-70-61_1510732",1,"Created","Adhesive shall be selected in conformance with clause 6.11."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","12.1e","Requirement","ECSS-Q-ST-70-61_1510752",1,"Created","Additional magnification shall be used to resolve suspected anomalies or defects up to 40x."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.2.2c","Permission","ECSS-Q-ST-70-61_1510773",1,"Created","Approval Authority may request microsectioning."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.3c","Requirement","ECSS-Q-ST-70-61_1510779",1,"Created","The audit of the supplier’s assembly line shall be performed prior to the start of a verification programme."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.5i","Requirement","ECSS-Q-ST-70-61_1510795",1,"Created","The verification samples shall be assembled and tested according to agreed verification programme."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.5j","Requirement","ECSS-Q-ST-70-61_1510796",1,"Created","All test conditions shall be compliant with requirements from clause 14."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.6a","Requirement","ECSS-Q-ST-70-61_1510797",1,"Created","The verification report shall be in compliance with DRD from Annex B."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.6b","Requirement","ECSS-Q-ST-70-61_1510798",1,"Created","The verification report shall be made available to the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.6c","Requirement","ECSS-Q-ST-70-61_1510799",1,"Created","The supplier shall organise with the Approval Authority a final verification review.","NOTE\tThe assembly processes can be reviewed during the meeting to issue the PID. Verification of closure of the actions identified during the audit of the manufacturing line.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7a","Requirement","ECSS-Q-ST-70-61_1510800",1,"Created","Following the completion of the final verification review, the following documents shall be submitted to the Approval Authority:\n1.\tPID\n2.\tAssembly summary tables."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7b","Requirement","ECSS-Q-ST-70-61_1510801",1,"Created","The assembly summary tables shall be prepared by the supplier according to DRD from Annex D."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7c","Requirement","ECSS-Q-ST-70-61_1510802",1,"Created","In case of changes in assembly line impacting its approval, an audit shall be conducted to re-establish the approval as specified in clause 13.1.3.","NOTE\tA non-exhaustive list of changes that impact the Approval of the line is given in Table 13-1.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7d","Requirement","ECSS-Q-ST-70-61_1510803",1,"Created","A letter confirming the completion of a successful verification programme shall be sent to the contact person of the supplier from the Approval Authority, with the Assembly summary table in conformance with the DRD of Annex D.","NOTE\t1\tThe letter and the Assembly summary table provide evidence of the verification approval to a third party.\nNOTE\t2\tThe approval of verification applies to all space projects from the date of the approval until withdrawal.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7e","Requirement","ECSS-Q-ST-70-61_1510804",1,"Created","Reference to the Assembly summary table number shall be made on each Space project declared processes list."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7f","Requirement","ECSS-Q-ST-70-61_1510805",1,"Created","Assembly verification status of the electronic hardware shall be reviewed during assembly MPCB review.","NOTE\tA guideline to support MPCB review is: ESA-TECQTM-MO-1931 Issue 3 “Guideline for the review of Approval status of electronics assembly configurations during MPCB”.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7g","Permission","ECSS-Q-ST-70-61_1510806",1,"Created","Except for components covered by requirement 13.1.7j, verification may be omitted for components for which supplier can demonstrate their acceptance through previous verification heritage, listed in their approved summary table."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7h","Requirement","ECSS-Q-ST-70-61_1510807",1,"Created","Assembly sensitive components that have successfully passed the assembly verification in compliance with this standard, and are outside of what is defined in 3.2.2,shall not be considered as assembly sensitive component in the supplier PID. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7i","Requirement","ECSS-Q-ST-70-61_1510808",1,"Created","The supplier shall maintain a list of assembly sensitive components. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7j","Requirement","ECSS-Q-ST-70-61_1510809",1,"Created","Assembly sensitive components listed in the supplier PID shall be submitted to re-verification every four years to monitor the stability of the assembly."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.7k","Permission","ECSS-Q-ST-70-61_1510810",1,"Created","The re-verification of assembly sensitive components specified in the requirement 13.1.7j may be performed on limited verification programme with worst case configuration identified during initial verification provided acceptance of Approval Authority.","NOTE\t1\tOne substrate, one package per component type, three samples per component.\nNOTE\t2\tFor leadless components, mechanical testing can be omitted.\nNOTE\t3\tNon-destructive characterization can be proposed as alternative to microsection.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.1.8a","Requirement","ECSS-Q-ST-70-61_1510811",1,"Created","The approval status of the supplier shall be withdrawn if any of the following occurs:\n1.\tRepetitive supply problems and manufacturing defects,\n2.\tUndeclared changes of items listed in Table 13-1,\n3.\tNumerous non compliances to the PID.","NOTE\t1\tRenewed approval can be granted following a review of the discrepancies.\nNOTE\t2\tA repeat, or partial repeat of the verification programme can be requested by the Approval Authority.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1a","Requirement","ECSS-Q-ST-70-61_1510812",1,"Created","The approval of mounting and supporting of components, terminals and conductors, as specified in this standard, shall be applicable only to assemblies designed to continuously operate over the mission within the temperature limits of -55 °C to +85 °C at solder joint level."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1b","Requirement","ECSS-Q-ST-70-61_1510813",1,"Created","Compliance to environmental range within -55 °C to +85 °C at solder joint level for the mission shall be stated."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1c","Requirement","ECSS-Q-ST-70-61_1510814",1,"Created","The supplier shall demonstrate verification for each combination of substrate material type, PCB footprint, component type, soldering technique applied, staking and bonding, lead forming configuration, solder mask and conformal coating as used on FM.","NOTE\t1\tMaterial type groups as defined in Table 6-1 of ECSS-Q-ST-70-12.\nNOTE\t2\tVapour phase reflow, convection reflow, hot air and hand soldering are examples of different soldering techniques.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1d","Requirement","ECSS-Q-ST-70-61_1510815",1,"Created","Verification of area array components shall be performed in accordance with the requirements in clause 13.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1e","Permission","ECSS-Q-ST-70-61_1510816",1,"Created","Except for area array components which are covered by clause 13.3, verification may be performed with electrical testing procedure in compliance with clause 13.4."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1f","Requirement","ECSS-Q-ST-70-61_1510817",1,"Created","Verification of solderless assemblies shall be performed in compliance with clause 13.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1g","Permission","ECSS-Q-ST-70-61_1510818",1,"Created","Verification programme with reduced temperature range in accordance with clause 13.5 may be applied to reduce risk of failure during thermal cycling due to CTE mismatch between component and PCB.","NOTE\t1\tCeramic chip capacitors type II are highly prone to cracks in the ceramic. It has been demonstrated that the type of cracks and length of cracks seen in microsectioning at the top side are directly correlated to the temperature range during thermal cycling as well as the temperature gradient. It is therefore for this type of components recommended to perform verification programme with reduced temperature range from the beginning, not only after a previously failed verification programme.\nNOTE\t2\tFor chip capacitors it is good practice to perform the verification on the capacitance value used which has the thinnest cover plate and most densely packed dielectric planes. Cover plate is the distance between external surface. and first electrode.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1h","Requirement","ECSS-Q-ST-70-61_1510819",1,"Created","The verification shall be performed on at least 3 (three) components except for the assembly of sensitive components where 5 (five) components are used per configuration in the verification programme."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1i","Requirement","ECSS-Q-ST-70-61_1510820",1,"Created","When assembly sensitive component is listed in summary table, if the verification was performed with less than 5 (five) components, a new verification shall be performed."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1j","Requirement","ECSS-Q-ST-70-61_1510821",1,"Created","Verification of the assembly shall be performed with a nominal process and a repair process for each component.","NOTE\tManual process covers a range of processes such as hand soldering, hot gas station and IR station.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1k","Requirement","ECSS-Q-ST-70-61_1510822",1,"Created","The nominal process shall be representative of the FM manufacturing flow.","NOTE\tIf both collective and non-collective processes are used on FM, verification board is submitted to both processes also in verification.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1l","Requirement","ECSS-Q-ST-70-61_1510823",1,"Created","No rework shall be performed before MIP1 except for manually soldered components."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1m","Requirement","ECSS-Q-ST-70-61_1510824",1,"Created","Rework of components, other than manually soldered, shall be decided during the MIP1 "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1n","Requirement","ECSS-Q-ST-70-61_1510825",1,"Created","For chip components, more than 20 % of reworked soldered joints per component type and assembly configuration shall not be acceptable."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1o","Requirement","ECSS-Q-ST-70-61_1510826",1,"Created","For all components except those defined in requirement 13.2.1n, more than 10 % of reworked soldered joints per component type and assembly configuration shall not be acceptable."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1p","Permission","ECSS-Q-ST-70-61_1510827",1,"Created","Reworks outside of what is allowed in 13.2.1m and 13.2.1n may be accepted by Approval Authority.","NOTE\tSome packages due to their complexity can be more difficult to assemble without any rework.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1q","Requirement","ECSS-Q-ST-70-61_1510828",1,"Created","Any repair or modification, not compliant to ECSS-Q-ST-70-28, shall be submitted to a verification programme as agreed with the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1r","Requirement","ECSS-Q-ST-70-61_1510829",1,"Created","The supplier’s repair process using the nominal manual process including removing and replacing of 1 (one) of each type of mounted component shall be submitted to verification testing with the exception of AAD assembly verification for which a minimum of 2 (two) parts are being repaired.","NOTE\tThe supplier has the option to perform more than 1 (one) repair for each type of component.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1s","Requirement","ECSS-Q-ST-70-61_1510830",1,"Created","For each type of component, per configuration, the repair shall be performed on the largest component."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1t","Requirement","ECSS-Q-ST-70-61_1510831",1,"Created","For repair verification of collective assembled components, the repair shall be performed only on the components being assembled by manual soldering method, provided the same assembly configuration.","NOTE\tThe repair is required on the hand soldering process to keep a sample of 3 (three) or 5 (five) on the collective assembly configuration.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1u","Requirement","ECSS-Q-ST-70-61_1510832",1,"Created","Verification testing of commercial components shall be performed for each lot in conformance with this clause 13.2.1, except when requirement 13.8.1d can be met."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1v","Requirement","ECSS-Q-ST-70-61_1510833",1,"Created","Terminations to be microsectioned shall be connected to the internal PCB layers.","NOTE\tThe terminations to be microsectioned are described in Table 14-5.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1w","Requirement","ECSS-Q-ST-70-61_1510834",1,"Created","The verification sample shall be submitted to 2 (two) nominal soldering method reflows when reflow is performed on both PCB sides of the FM.","NOTE\tThe supplier has the option to flip the board for the second reflow.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1x","Requirement","ECSS-Q-ST-70-61_1510835",1,"Created","The verification programme shall be performed in accordance with Figure 13-1."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1y","Requirement","ECSS-Q-ST-70-61_1510836",1,"Created","A soldering log as specified in clause 13.2.4 shall be put in place for all soldering processes involved in a board manufacturing during verification programme."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1z","Requirement","ECSS-Q-ST-70-61_1510837",1,"Created","The soldering log shall be made available to the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1aa","Requirement","ECSS-Q-ST-70-61_1510838",1,"Created","The conditions associated with long term storage, extensive ground testing, mechanical stress after launch, high temperature application with or without thermal cycles shall be assessed by the supplier."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1bb","Requirement","ECSS-Q-ST-70-61_1510839",1,"Created","The environmental conditions of the mission including ground testing shall be covered by the environmental conditions of the verification programme."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1cc","Requirement","ECSS-Q-ST-70-61_1510840",1,"Created","For surface mounted components the total number of temperature cycles shall be 500, except for the cases defined in requirement 13.3.3g and requirement 13.4p."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1dd","Requirement","ECSS-Q-ST-70-61_1510841",1,"Created","For components mounted in plated through holes the total number of temperature cycles shall be 200."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1ee","Permission","ECSS-Q-ST-70-61_1510842",1,"Created","When mechanical bonding is underneath the component, microsectioning of one component may be performed after vibration and 50 thermal cycles to justify the integrity of the bonding.","NOTE\tThe component can be 1 (one), not the one repaired, of the 3 (three) assembled components which were cut out from the same verification board after the 50 thermal cycles.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1ff","Requirement","ECSS-Q-ST-70-61_1510843",1,"Created","Prior to start verification assembly the supplier shall organize a MRR with two weeks notification with the Approval Authority ","NOTE\t1\tThe PCB design is reviewed to check compliance with requirements from clause 13.1.5.\nNOTE\t2\tDuring the review, the Approval Authority can check that the verification programme is approved by all parties and that all actions are closed.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1gg","Requirement","ECSS-Q-ST-70-61_1510844",1,"Created","The supplier shall organise a MIP1 with two weeks notification, with the Approval Authority prior to any conformal coating.","NOTE\tThe Approval Authority can delegate the MIP1 to the supplier.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1hh","Requirement","ECSS-Q-ST-70-61_1510845",1,"Created","Prior to any environmental testing, the supplier shall organise with the Approval Authority a TRR with two weeks notification during which the MIP1 outputs and outstanding actions are reviewed.","NOTE\tThe Approval Authority can delegate the action review to the supplier.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1ii","Requirement","ECSS-Q-ST-70-61_1510846",1,"Created","The supplier shall organise with Approval Authority a MIP2 with two weeks notification at the completion of the environmental test. ","NOTE\tThe Approval Authority can delegate the MIP2 to the supplier.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.1jj","Requirement","ECSS-Q-ST-70-61_1510847",1,"Created","The supplier shall organize with the Approval Authority a final VR during which the environmental tests results are reviewed.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.2a","Requirement","ECSS-Q-ST-70-61_1510849",1,"Created","Any soldering configuration not covered by requirements from clauses 8.2, 9,10.2.6 and 10.3 or covered but for which assembly verification is requested shall be verified in accordance with clause 13.2.1."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.2b","Requirement","ECSS-Q-ST-70-61_1510850",1,"Created","A process specific verification programme shall be performed for through hole component assemblies with stress relief that are not compliant to clause 8.2."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3a","Requirement","ECSS-Q-ST-70-61_1510851",1,"Created","For components that are not assembly sensitive, the supplier shall provide 2 (two) assembled PCBs with at least 3 (three) components of each type per board and 1 (one) non-assembled PCB as reference."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3b","Requirement","ECSS-Q-ST-70-61_1510852",1,"Created","For assembly sensitive components, the supplier shall provide 2 (two) assembled PCBs with at least five components of each type per board and 1 (one) non-assembled PCB as reference."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3c","Requirement","ECSS-Q-ST-70-61_1510853",1,"Created","Each board shall have an identical layout and be from the same batch."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3d","Requirement","ECSS-Q-ST-70-61_1510854",1,"Created","The layout and component density shall be similar to that envisaged for FM boards."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3e","Requirement","ECSS-Q-ST-70-61_1510855",1,"Created","Warp and twist of all assembled PCBs shall be measured for wave soldering verification, according to clause 14.5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3f","Requirement","ECSS-Q-ST-70-61_1510856",1,"Created","Electrical continuity measurements shall be performed on wave soldered multilayer PCBs according to clause 14.7."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3g","Requirement","ECSS-Q-ST-70-61_1510857",1,"Created","One component of each type per board shall be submitted to repair."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.3h","Requirement","ECSS-Q-ST-70-61_1510858",1,"Created","More than 5 % of reworked soldered joints per component shall not be accepted."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.2.4a","Requirement","ECSS-Q-ST-70-61_1510859",1,"Created","The soldering log shall contain as a minimum the following data:\n1.\tBoard identification\n2.\tBoard technology description: materials, build up, ground planes\n3.\tSoldering process identification\n4.\tMain parameters for the soldering process\n5.\tList of identified defects\n6.\tNumber of reworks performed on each solder joint\n7.\tCalculation of percentage of defects\n8.\tInspectors observations\n9.\tAny miscellaneous remark of interest.","NOTE\tAn example of a soldering log for a wave process soldering is given in Figure 13-2.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.1a","Requirement","ECSS-Q-ST-70-61_1510860",1,"Created","The assembly verification of ceramic AADs shall be divided in the following 2 (two) steps, as shown in Figure 13-3.\n1.\tDemonstration of capability in accordance with clause 13.3.2, and\n2.\tDemonstration of electrical integrity in accordance with clause 13.3.3.","NOTE\t1\tOnce the capability samples show a satisfactory result the verification of AAD can commence.\nNOTE\t2\tCapability samples can be excluded from the programme if the supplier can demonstrate previous verification heritage.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.1b","Requirement","ECSS-Q-ST-70-61_1510861",1,"Created","The capability and verification samples shall be representative of the FM hardware.","NOTE\tFor example, PCB build-up and size, mechanical fixation, component packages.\nNOTE\tIt is recommended to have a successful IST test on PCB to avoid failing the assembly verification due to damaged PCB.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.1c","Requirement","ECSS-Q-ST-70-61_1510862",1,"Created","The PCB material, footprint, via technology used for the capability and verification samples shall be the same and interconnection similar as the ones used for the FM hardware.","NOTE\tHDI, blind via and buried via are different types of via technologies.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.1d","Requirement","ECSS-Q-ST-70-61_1510863",1,"Created","The verification shall be performed with daisy chain components to demonstrate a reliable electrical function of the PCB and the package interface throughout the environmental test campaign."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2a","Requirement","ECSS-Q-ST-70-61_1510865",1,"Created","The supplier shall manufacture and demonstrate that the 2 (two) capability samples are in conformance with the requirement 13.3.2i before the manufacture of the verification samples using daisy chain components can be initiated."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2b","Requirement","ECSS-Q-ST-70-61_1510866",1,"Created","2 (two) components shall be assembled with the nominal reflow process.","NOTE\tThe supplier can use daisy chain packages for the capability to have an early results of electrical monitoring during thermal cycles.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2c","Requirement","ECSS-Q-ST-70-61_1510867",1,"Created","One of the components from requirement 13.3.2b shall be removed and replaced with a new component using the repair process."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2d","Permission","ECSS-Q-ST-70-61_1510868",1,"Created","When nominal and repair processes are identical then the number of components, may be reduced to 1 (one) which is repaired","NOTE\tThe total number of components needed is 2 (two).\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2e","Requirement","ECSS-Q-ST-70-61_1510869",1,"Created","The components shall be inspected in conformance with requirements from the clause 10.4.14."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2f","Requirement","ECSS-Q-ST-70-61_1510870",1,"Created","The components shall be submitted to vibration testing in conformance with requirements from the clause 14.7."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2g","Requirement","ECSS-Q-ST-70-61_1510871",1,"Created","The components shall be submitted to shock testing in conformance with clause 14.9."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2h","Requirement","ECSS-Q-ST-70-61_1510872",1,"Created","The components shall be submitted to 500 thermal cycles in conformance with requirements from the clause 14.11."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.2i","Requirement","ECSS-Q-ST-70-61_1510873",1,"Created","After environmental tests completion, microsectioning of the components shall be performed to demonstrate PCB integrity in the AAD area with respect to:\n1.\tDamage to the component outside the procurement specification,\n2.\tDamages outside of what is allowed in clause 14.15.3.\n3.\tDamages outside of what is allowed in clause 14.16.","NOTE\tThe purpose of the capability samples is to show that the PCB and the component body are intact after the assembly and repair of AAD and environmental testing (vibration, mechanical shock and 500 temperature cycles). A crack in the columns or balls is not considered as reason for rejection.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3a","Requirement","ECSS-Q-ST-70-61_1510874",1,"Created","5 (five) components shall be assembled for each nominal assembly method and mounting configuration."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3b","Requirement","ECSS-Q-ST-70-61_1510875",1,"Created","2 (two) of the assembled components shall be removed and replaced with new components using the repair process."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3c","Permission","ECSS-Q-ST-70-61_1510876",1,"Created","When nominal and repair processes are identical then the number of components, may be reduced to 3 (three) out of which 2 (two) are repaired.","NOTE\tThe total number of components needed is 5 (five).\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3d","Requirement","ECSS-Q-ST-70-61_1510877",1,"Created","The components shall be inspected in conformance with requirements from the clause 10.4.14."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3e","Requirement","ECSS-Q-ST-70-61_1510878",1,"Created","The 5 (five) components shall be submitted to vibration testing in conformance with requirements from the clause 14.7."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3f","Requirement","ECSS-Q-ST-70-61_1510879",1,"Created","The 5 (five) components shall be submitted to shock testing in conformance with requirements in clause 14.9."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3g","Requirement","ECSS-Q-ST-70-61_1510880",1,"Created","The 5 (five) components shall be submitted to 1500 thermal cycles with temperature conditions in conformance with clause 14.11 and with continuous electrical monitoring in accordance with clause 14.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3h","Requirement","ECSS-Q-ST-70-61_1510881",1,"Created","Resistance measurement shall be done, at ambient, before and after any mechanical testing in accordance with clause 14.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.3.3i","Requirement","ECSS-Q-ST-70-61_1510882",1,"Created","After environmental testing the verification samples shall fulfil the acceptance criteria in accordance with clause 14.16."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4a","Permission","ECSS-Q-ST-70-61_1510883",1,"Created","Except for the cases specified in requirement 13.4b the supplier may propose assembly verification with electrical testing procedure as an alternative method."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4b","Requirement","ECSS-Q-ST-70-61_1510884",1,"Created","Leadless chip capacitors and leadless components with plane termination shall not be assembly verified through electrical testing procedure.","NOTE\tCapacitor and TO276 packages such as SMD05, SMD1, SMD2 and SMD5C, are excluded as the failure mechanism is crack in ceramic.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4c","Requirement","ECSS-Q-ST-70-61_1510885",1,"Created","Assembly verification with electrical testing procedure shall be performed in accordance with Figure 13-4 with samples for both capability verification with microsectioning and with electrical verification."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4d","Requirement","ECSS-Q-ST-70-61_1510886",1,"Created","Verification of capability shall be performed on at least one component except for the assembly sensitive components where 5 (five) components are assembled with nominal process. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4e","Requirement","ECSS-Q-ST-70-61_1510887",1,"Created","One of the components from requirement 13.4d shall be removed and replaced with a new component using the repair process providing the repair process is identical to the nominal assembly. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4f","Requirement","ECSS-Q-ST-70-61_1510888",1,"Created","If the repair procedure is different from the nominal assembly, a separate assembly verification with full number of capability as well as electrical verification samples shall be performed. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4g","Permission","ECSS-Q-ST-70-61_1510889",1,"Created","Capability samples may be excluded from the programme if capability can be demonstrated through previous verification heritage. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4h","Requirement","ECSS-Q-ST-70-61_1510890",1,"Created","Verification with electrical monitoring shall be performed on at least 32 components assembled for each assembly configuration with nominal process.","NOTE\t1\tMachine reflow, hand soldering are the examples of assembly method.\nNOTE\t2\tThe assembly of the capability and the electrical verification samples can be made on the same board.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4i","Requirement","ECSS-Q-ST-70-61_1510891",1,"Created","One of the components from requirement 13.4h, except for assembly sensitive components where it is 5 (five) components, shall be removed and replaced with new components using the repair process. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4j","Requirement","ECSS-Q-ST-70-61_1510892",1,"Created","All solder terminations shall be continuously electrically monitored throughout the temperature cycling"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4k","Requirement","ECSS-Q-ST-70-61_1510893",1,"Created","The electrical value of components for electrical monitoring shall be selected to be able to detect anomalies in the solder joint:\n1.\tfor resistor zero ohm or the lowest value in the procurement specification,\n2.\tfor other types, custom daisy chain."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4l","Permission","ECSS-Q-ST-70-61_1510894",1,"Created","In case of non-representative daisy chain component to FM one, the use of functional component may be proposed providing agreement of Approval Authority.","NOTE\tExample of such components are commercial components.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4m","Requirement","ECSS-Q-ST-70-61_1510895",1,"Created","For the capability samples microsectioning shall be performed in accordance with clause 14.14 after verification steps in accordance with Figure 13-1. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4n","Requirement","ECSS-Q-ST-70-61_1510896",1,"Created","If capability and electrical monitoring samples are on the same board they shall be separated before the microsectioning of the capability samples and before the environmental tests for the samples for electrical monitoring."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4o","Requirement","ECSS-Q-ST-70-61_1510897",1,"Created","The samples for electrical monitoring shall be submitted to vibration testing in conformance with requirements from clause 14.8 and shock testing in conformance with requirements in clause 14.9."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4p","Requirement","ECSS-Q-ST-70-61_1510898",1,"Created","The samples for electrical monitoring shall be submitted to 1500 thermal cycles in conformance with requirements in clause 14.11 and with continuous electrical monitoring in accordance with clause 14.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4q","Requirement","ECSS-Q-ST-70-61_1510899",1,"Created","Any failed component shall be subjected to failure analysis."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.4r","Requirement","ECSS-Q-ST-70-61_1510900",1,"Created","If the first failure occurs before the end of the 1500 thermal cycles, the number of cycles before the first failure shall be identified as the component assembly verification limitation."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.5a","Permission","ECSS-Q-ST-70-61_1510902",1,"Created","Verification programme with reduced temperature range may be applied to reduce risk of failure during thermal cycling due to CTE mismatch between component and PCB.","NOTE\t1\tThe majority of assembly sensitive components (see definition 3.2.2) has CTE mismatch between components and PCB as root cause of failure. Reduction of the temperature range and the temperature gradient can lower the risk of failure due to such root cause, but the thermal cycling will take a longer time. A case-by-case trade-off based on risk vs leadtime is necessary. \nNOTE\t2\tCeramic chip capacitors type II are highly prone to cracks in the ceramic. It has been demonstrated that the type of cracks and length of cracks seen in microsectioning at the top side are directly correlated to the temperature range during thermal cycling as well as the temperature gradient. It is therefore for this type of components recommended to perform verification programme with reduced temperature range from the beginning, not only after a previously failed verification programme.\nNOTE\t3\tFor ceramic chip capacitors it is good practice to perform the verification on the capacitance value used which has the thinnest cover plate and most densely packed dielectric planes.\nNOTE\t4\tIt is good practice to apply verification with reduced temperature range for leadless components with plane termination such as SMD0.5 to reduce the risk of cracks in the ceramic.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.5b","Requirement","ECSS-Q-ST-70-61_1510903",1,"Created","Verification programme with reduced temperature range shall follow the generic flow described in Figure 13-1, except for the temperature cycling conditions that are modified in compliance with clause 14.12."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.5c","Permission","ECSS-Q-ST-70-61_1510904",1,"Created","Components that have passed a successful verification with reduced temperature range in compliance with this clause may be added in the assembly summary tables as tailored verification, provided approval by the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.5d","Requirement","ECSS-Q-ST-70-61_1510905",1,"Created","Request for approval shall be submitted in each project where the component with tailored verification is used to justify that the verified temperature range covers the mission in which it is intended to be used."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6a","Requirement","ECSS-Q-ST-70-61_1510906",1,"Created","The verification of solderless process shall be performed on flight representative assembly configuration in accordance with Figure 13-5. ","NOTE\tRepresentative assembly configuration includes elements for thermal dissipation configuration.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6b","Requirement","ECSS-Q-ST-70-61_1510907",1,"Created","The verification tests shall be performed to show absence of degradation within the solderless interconnection part, PCB and component during all ground and in-orbit mission.","NOTE\tPossible degradations can be creeping of the spring, fretting degradation of the contact.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6c","Requirement","ECSS-Q-ST-70-61_1510908",1,"Created","6 (six) components shall be assembled with the same mechanical configuration as flight model."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6d","Requirement","ECSS-Q-ST-70-61_1510909",1,"Created","Mate/demate number shall permit to cover the application requirement with a margin of 4 in compliance with Table 4-4 of ECSS-E-ST-33-01."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6e","Requirement","ECSS-Q-ST-70-61_1510910",1,"Created","Minimum vibration levels shall be in compliance with requirement 14.8e."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6f","Requirement","ECSS-Q-ST-70-61_1510911",1,"Created","Shock test shall be performed in conformance with requirements from clause 14.9."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6g","Requirement","ECSS-Q-ST-70-61_1510912",1,"Created","Electrical monitoring shall be carried out according to clause 14.6 before and after mate/demate, and during vibration and shock tests, if the equipment is to be functional during launching phases."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6h","Requirement","ECSS-Q-ST-70-61_1510913",1,"Created","The samples for environmental testing shall be submitted to 500 thermal cycles with temperature conditions in conformance with clause 14.11 and with continuous electrical monitoring in accordance with clause 14.6. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6i","Requirement","ECSS-Q-ST-70-61_1510914",1,"Created","Damp heat test shall be performed for all applications in compliance with clause 14.10."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6j","Permission","ECSS-Q-ST-70-61_1510915",1,"Created","In case of long-term storage application, project specific requirements may apply instead of requirement 13.6i."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6k","Requirement","ECSS-Q-ST-70-61_1510916",1,"Created","Electrical continuity test according to clause 14.6 shall be performed to verify absence of degradation of the connection after damp heat test."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6l","Requirement","ECSS-Q-ST-70-61_1510917",1,"Created","Life test shall be performed in accordance with clause 14.13 and with continuous electrical monitoring in accordance with clause 14.6 to evaluate the spring reliability."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6m","Permission","ECSS-Q-ST-70-61_1510918",1,"Created","Life test may be omitted provided representative test were performed by the component manufacturer."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6n","Requirement","ECSS-Q-ST-70-61_1510919",1,"Created","Visual inspection criteria in compliance with clause 12 shall apply to interposer, component and PCB."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.6o","Requirement","ECSS-Q-ST-70-61_1510920",1,"Created","Microsections of interposer, component and PCB shall be done according to clause 14.15 in order to verify absence of plating damage at interposer level, component damage and laminate cracks or plating damage in the PCB.","NOTE\tMicrosectioning can be performed after dismounting of the assembly.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.7a","Requirement","ECSS-Q-ST-70-61_1510922",1,"Created","The supplier shall undertake a verification for any new configuration not covered by similarity rules in accordance with requirements from clause 13.8."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.7b","Requirement","ECSS-Q-ST-70-61_1510923",1,"Created","The delta verification shall be performed when changes are undertaken as specified in Table 13-1."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.7c","Permission","ECSS-Q-ST-70-61_1510924",1,"Created","For a process delta verification program, the number of samples may be tailored from the general requirements from clause 13.2, depending on the type of process changes made, subject to approval by the Approval Authority. ","NOTE\t1\tThe selection criteria are based on worst cases depending on the change of process to be verified.\nNOTE\t2\tFor PCB materials change, examples of worst cases are CTE mismatch, thermal dissipation, stiffness, glass transition temperature and copper peel strength.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.7d","Requirement","ECSS-Q-ST-70-61_1510925",1,"Created","For delta verification associated with process change the verification boards shall be designed such that they are representative of the new process."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.7e","Requirement","ECSS-Q-ST-70-61_1510926",1,"Created","A delta-verification programme in accordance with the DRD from Annex A shall be submitted for approval to the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.1a","Requirement","ECSS-Q-ST-70-61_1510928",1,"Created","Verification by similarity shall not be declared successful unless all the following conditions are met: \n1.\tSame substrate material type,\n2.\tSame solder mask,\n3.\tSame PCB finish,\n4.\tPCB footprint designed with same aspect ratios and same via technology of interconnection,\n5.\tRepresentative PCB build up\n6.\tSame solder material,\n7.\tSame flux\n8.\tSame solder process, and\n9.\tSame staking, bonding and conformal coating configuration.","NOTE\t1\tto item 1: Material type groups as defined in Table 6-1 of ECSS-Q-ST-70-12. \nNOTE\t2\tto item 1: Similarity for different materials belonging to the same type group is reviewed during assembly MPCB.\nNOTE\t3\tto item 1: See clause 13.7 for delta verification conditions, requirements and possible tailoring.\nNOTE\t4\tto item 4: Blind via in pads and microvias are different technologies of interconnection.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.1b","Permission","ECSS-Q-ST-70-61_1510929",1,"Created","Different solder masks may be used providing a risk assessment for the affected components.","NOTE\tExamples of factors to consider are materials, thickness, locations, if bonding or staking, compatibility with cleaning solvents.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.1c","Requirement","ECSS-Q-ST-70-61_1510930",1,"Created","Verification by similarity shall not apply to commercial components."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.1d","Permission","ECSS-Q-ST-70-61_1510931",1,"Created","Verification by similarity between different lots of commercial components may only be valid if a constructional analysis of the component is performed and confirms no changes in its construction."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.2a","Requirement","ECSS-Q-ST-70-61_1510932",1,"Created","Verification by similarity for PTH components requiring assembly verification, shall only be applied when all the following conditions are met:\n1.\tComponents are smaller than the verified Lmax, Wmax and Hmax,\n2.\tConstruction of the component is identical to that verified,\n3.\tAssembly configuration is the same,\n4.\tMaterials are identical,\n5.\tLead material is the same,\n6.\tLead section is the same, and\n7.\tPitch is smaller than the one verified \n8.\tEvidence that the PCB is not damaged for assembly with the same or smaller pitch.","NOTE\tAbsence of PCB damage can be demonstrated by successful verification on a different component with same small pitch \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.2b","Requirement","ECSS-Q-ST-70-61_1510933",1,"Created","Verification by similarity for a PTH shall be declared successful when the PCB thickness is thicker or equal to the one verified.","NOTE\tThe calculation of the crack should be re assessed taking into account the FM PCB thickness.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3a","Requirement","ECSS-Q-ST-70-61_1510934",1,"Created","Verification by similarity shall not apply to leadless castellated ceramic chip carrier components, ceramic resistor arrays or no-lead Quad Flat Packs."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3b","Requirement","ECSS-Q-ST-70-61_1510935",1,"Created","Verification by similarity for leaded packages, described in 10.4.7, 10.4.10, 10.4.11 and 10.4.13 shall only be applied when all the following conditions are met:\n1.\tPackage is smaller than the verified Lmax, Wmax and Hmax,\n2.\tPackage weight is lower than the maximum verified,\n3.\tLead pitch, nominal thickness, nominal width, and materials composition are identical,\n4.\tCoated lead finishes on the termination are identical,\n5.\tBending dimensions and shape are identical,\n6.\tPackages are constructed from the same materials.\n7.\tWhen existing, the bottom termination or exposed pad has the same aspect ratio to the component body as the one verified. ","NOTE\t1\tto item 2: Radiation shielded packages are heavier than standard flatpack and not covered by similarity.\nNOTE\t2\tto item 6: Glass to metal sealed, glass sealed side-brazed, top-brazed, and bottom-brazed packages are different families.\nNOTE\t3\tto item 6: Dual side pin arrangements are different to quad side pin families.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3c","Permission","ECSS-Q-ST-70-61_1510936",1,"Created","For flat pack components, described in 10.4.10, verification by similarity may apply even if the lead materials are different.","NOTE\tKovar and Alloy 42 leads are considered similar.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3d","Requirement","ECSS-Q-ST-70-61_1510937",1,"Created","Verification by similarity for end-capped and end-metallized components with rectangular body, described in 10.4.2, shall only be applied when all the following conditions are met:\n1.\tComponent length is between Lmin and Lmax of the verified component,\n2.\tComponent width is between Wmin and Wmax of the verified component,\n3.\tComponent height is less than Hmax of the verified component,\n4.\tCeramic material type is identical,\n5.\tMetallization of the termination and the barrier layers on components are identical, and\n6.\tComponent manufacturer is identical.","NOTE\t1\tto item 1 and 2: For example, 0402 - 2220 does not qualify 1825 as the width is outside the max 20 verified. \nNOTE\t2\tto item 4: Ceramic chip capacitors can be very sensitive to mounting conditions and generally, type I chip capacitors are less sensitive than type II. The sensitivity is design and process related and can therefore vary from one manufacturer to another. Within a manufacturer type II range one or more different ceramic materials can also be used. It is therefore impossible to apply similarity rules between type I and type II ceramic chip capacitors and different manufacturers. Lower capacitance values are less sensitive than higher, based on the increased ratio between electrode layers and ceramic material. It is therefore good practice to select the highest capacitance values in a class or type I or type II ceramic capacitors range to be submitted to assembly verification.\nNOTE\t3\tto item 4: Examples of ceramic types are NPO, Z5U and Y7R.\nNOTE\t4\tto item 5: Flexible and non-flexible terminations are not identical.\nNOTE\t5\tto item 5: termination platings Sn60 and Sn63 are equivalent and different from Sn85 which in turn is equivalent with Sn95.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3e","Permission","ECSS-Q-ST-70-61_1510938",1,"Created","For leadless chip resistors, described in 10.4.2, thick film resistors may be verified by similarity to thin film resistors provided that the supplier has successfully performed a full verification programme according to clause 13.2 for at least one thin film resistor technology, covering the dimensions, termination plating and the type of material, in accordance with requirements 13.8.3d.1, 2, 3, 5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3f","Requirement","ECSS-Q-ST-70-61_1510939",1,"Created","Verification by similarity for thermistors and fuses described in 10.4.2, for MELF resistors and MELF diodes in 10.4.3, for leadless chip inductors in 10.4.4, and L-Shape inwards components in 10.4.5, shall only be applied when all the following conditions are met\n1.\tComponent length is less than Lmax of the verified component,\n2.\tComponent width is less than Wmax of the verified component,\n3.\tComponent height is less than Hmax of the verified component,\n4.\tMaterial type is identical,\n5.\tPackage shape is identical and\n6.\tMetallization of the termination and the barrier layers on components are identical."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3g","Permission","ECSS-Q-ST-70-61_1510940",1,"Created","For components with inward formed L-shaped leads, described in 10.4.5, verification by similarity may apply even if the lead materials are different. ","NOTE\tTantalum leaded capacitors can have copper alloy or Alloy 42 leads for which impact is considered negligible. \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3h","Requirement","ECSS-Q-ST-70-61_1510941",1,"Created","Verification by similarity for leadless component with plane termination according to clause 10.4.6 shall only be applied when all the following conditions are met\n1.\tComponents are smaller than the verified Lmax , Wmax and Hmax\n2.\tConstruction of the component package is identical to the verified component package, and\n3.\tMaterials are identical.","NOTE\tto item 2: SMD0.2 exists in 2 versions which are not identical.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3i","Requirement","ECSS-Q-ST-70-61_1510942",1,"Created","Verification by similarity for components with ribbon terminals without stress relief, according to clause 10.4.12, shall only be applied when all the following conditions are met\n1.\tPackage is smaller than the Lmax, Wmax and Hmax of the verified component,\n2.\tPackage weight is lower than the maximum weight of the verified component,\n3.\tLead nominal thickness, nominal width and materials composition are identical to the verified component,\n4.\tLead finishes on the termination are identical to the verified component,\n5.\tBending dimensions and shape are identical to the verified component,\n6.\tPackages are constructed from the same materials."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.3j","Requirement","ECSS-Q-ST-70-61_1510943",1,"Created","Verification by similarity for area array components, described in 10.4.14, shall only be applied when all the following conditions are met\n1.\tPackage is smaller than the Lmax, Wmax and Hmax of the verified component,\n2.\tPackage weight is lower than the maximum weight of the verified component,\n3.\tNumber of columns is lower than the one of the verified components,\n4.\tColumn pitch is the same,\n5.\tColumn dimensions are the same,\n6.\tColumn distribution are the same,\n7.\tColumn materials are the same,\n8.\tColumn construction is the same,\n9.\tColumn manufacturer is the same,\n10.\tColumn attachment process is the same,\n11.\tPackage has the same construction and materials, and \n12.\tPackage has the same body shape (aspect ratio)."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","13.8.4a","Requirement","ECSS-Q-ST-70-61_1510944",1,"Created","Verification by similarity for solderless assembly described in 10.7, shall only be applied when all the following conditions are met\n1.\tComponent and interposer lengths are less than Lmax of the verified component and interposer,\n2.\tComponent and interposer widths are less than Wmax of the verified component and interposer,\n3.\tInterposer has the same height as the verified interposer,\n4.\tComponent weight is lower than the verified component,\n5.\tNumber of terminations is lower than the verified component,\n6.\tPitch is the same as the verified component,\n7.\tMaterials for both component and interposer are the same as the verified component,\n8.\tComponent and interposer finishes are the same as the ones verified,\n9.\tManufacturer and technology for the interposer are the same as the one verified,\n10.\tMechanical construction and mounting principle are the same as the one verified and,\n11.\tComponent and interposer have the same body shape (aspect ratio).","NOTE\tto item 7 and 8: In case the interposer connects two PCBs, the component requirements refer to the PCBs.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.2a","Requirement","ECSS-Q-ST-70-61_1510945",1,"Created","Visual inspection shall be performed on each of the verification boards according to clauses 12.1, 12.2 and 12.3.","NOTE\tFor leadless ceramic components with plane terminations such as SMD0.5, it is good practice to add intermediate visual inspection point to identify when any crack in the ceramic occurs.. The aim is to cover the ground testing thermal cycles.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.3a","Requirement","ECSS-Q-ST-70-61_1510946",1,"Created","X-ray inspection shall be performed when required according to clauses 8, 10 and 13.","NOTE\tX-ray inspection is used for hidden solder joints, for example for bottom terminated components, soldered exposed pads and area array components.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.4a","Requirement","ECSS-Q-ST-70-61_1510947",1,"Created","The supplier shall perform cleanliness verification according to clause 11.1.2."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.5a","Requirement","ECSS-Q-ST-70-61_1510948",1,"Created","Warp and twist of PCB shall be performed as part of the verification programme for wave soldering according to clause 13.2.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.5b","Requirement","ECSS-Q-ST-70-61_1510949",1,"Created","Warp and twist shall be measured on each of the verification boards and recorded in accordance with clause 9.3.3.2 and 9.3.3.3 of ECSS-Q-ST-70-60.","NOTE\tWarp and twist control is part of the verification flow for wave soldered components.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6a","Requirement","ECSS-Q-ST-70-61_1510950",1,"Created","Electrical continuity measurement in accordance with this clause shall be performed as part of the following verification programmes:\n1.\tceramic area array components according to clause 13.3,\n2.\tassembly verification with electrical testing procedure according to clause 13.4, or\n3.\tverification of solderless process according to clause 13.6.","NOTE\tSee clause 14.7 for electrical continuity measurements for wave soldered multilayer PCBs\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6b","Requirement","ECSS-Q-ST-70-61_1510951",1,"Created","Electrical continuity shall be measured with a daisy chained component including 100 % of the component connections.","NOTE\tIt is good practice to add test points whenever possible for failure investigation.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6c","Requirement","ECSS-Q-ST-70-61_1510952",1,"Created","For AAD resistance measurement at ambient temperature shall be done after assembly, before and after any mechanical testing."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6d","Requirement","ECSS-Q-ST-70-61_1510953",1,"Created","Continuous electrical monitoring of daisy chain shall be performed during the thermal cycling. ","NOTE\t1: The number of thermal cycles for each verification is defined in the respective clause for each type of verification programme. \nNOTE\t2: Alternative electrical monitoring methods can be agreed with the Approval Authority.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6e","Requirement","ECSS-Q-ST-70-61_1510954",1,"Created","The sampling time for the continuous electrical monitoring shall be maximum 10 s."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6f","Requirement","ECSS-Q-ST-70-61_1510955",1,"Created","No interrupts in the electrical monitoring shall be detected throughout the thermal cycles. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6g","Requirement","ECSS-Q-ST-70-61_1510956",1,"Created","The maximum increase of each individual daisy chain resistance after the full number of thermal cycles shall not be more than 10 % compared to the initial resistance recorded during the first 5 (five) cycles."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.6h","Permission","ECSS-Q-ST-70-61_1510957",1,"Created","The supplier may provide their own criteria for an electrical failure to Approval Authority for approval."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7a","Requirement","ECSS-Q-ST-70-61_1510958",1,"Created","Electrical continuity measurements shall be performed as part of the verification programme for wave soldering on multilayer PCBs according to clause 13.2.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7b","Requirement","ECSS-Q-ST-70-61_1510959",1,"Created","Electrical continuity shall be measured on at least 25 % of all holes."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7c","Requirement","ECSS-Q-ST-70-61_1510960",1,"Created","The electrical continuity measurement shall include at least one internal connection per hole."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7d","Requirement","ECSS-Q-ST-70-61_1510961",1,"Created","Initial resistance measurement shall be performed at ambient temperature."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7e","Requirement","ECSS-Q-ST-70-61_1510962",1,"Created","Electrical continuity measurements shall be performed by continuous electrical monitoring of the daisy chain resistance during the first 5 (five) thermal cycles and the last 10 (ten) thermal cycles."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7f","Requirement","ECSS-Q-ST-70-61_1510963",1,"Created","The maximum increase of each individual daisy chain resistance after the full number of thermal cycles shall not be more than 5 % compared to the initial resistance measured in requirements 14.7d.and 14.7e. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.7g","Requirement","ECSS-Q-ST-70-61_1510964",1,"Created","Electrical continuity measurements for multilayer boards with positive changes greater than 10 % shall be recorded as failed in the verification report. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8a","Requirement","ECSS-Q-ST-70-61_1510965",1,"Created","The test specimen shall be vibration tested according to test flow chart described in Figure 14-1.","NOTE\tVibration testing methodology - From the input levels required by the projects in progress, the maximum deformation of the printed circuit board at the part level is established for each configuration (component type, location on the printed circuit board).\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8b","Requirement","ECSS-Q-ST-70-61_1510967",1,"Created","The PCB design and mechanical mounting including fittings such as stiffeners, frames or spacers shall be representative of the flight model."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8c","Requirement","ECSS-Q-ST-70-61_1510968",1,"Created","The mechanical mounting configuration of the PCB for the vibration tests shall be identified."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8d","Permission","ECSS-Q-ST-70-61_1510969",1,"Created","In order to take into account test samples imperfections, notching may be used to reduce non-representative mechanical over stresses provided that the following two conditions are met:\n1.\tNotching is justified to the Approval Authority, and\n2.\tInternal notching is identified in the vibration test report."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8e","Requirement","ECSS-Q-ST-70-61_1510970",1,"Created","Minimum vibration levels shall be as specified in Table 14-1, Table 14-2 and Table 14-3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8f","Requirement","ECSS-Q-ST-70-61_1510971",1,"Created","The vibration levels and duration during verification shall fulfil the project requirements"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8g","Requirement","ECSS-Q-ST-70-61_1510972",1,"Created","A modal survey shall be performed to detect any primary resonance frequency.","NOTE\t1\tModal survey can be done with sine or random vibration\nNOTE\t2\tIt is a good practice, for generic applications, that the verification board exhibits a primary resonant frequency in the range of 500 Hz - 800 Hz.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8h","Requirement","ECSS-Q-ST-70-61_1510973",1,"Created","For sine modal survey, the conditions shall be as defined in Table 14-1a."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8i","Requirement","ECSS-Q-ST-70-61_1510974",1,"Created","For random modal survey, the conditions shall be as defined in Table 14-1b."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8j","Permission","ECSS-Q-ST-70-61_1510975",1,"Created","High level sine vibration may be omitted, provided that the resonance frequency is above 300 Hz for both the verification board and flight model"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8k","Requirement","ECSS-Q-ST-70-61_1510976",1,"Created","Transfer function shall be issued from modal survey and presented to customer."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8l","Requirement","ECSS-Q-ST-70-61_1510977",1,"Created","Input vibration levels shall be measured at the interface between the vibration plate and the PCB."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8m","Requirement","ECSS-Q-ST-70-61_1510978",1,"Created","The response acceleration of the assembled PCB shall be monitored and recorded during testing."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8n","Requirement","ECSS-Q-ST-70-61_1510979",1,"Created","The accelerometers shall be placed on the PCB as well as on the base plate to determine the acceleration of the PCB.","NOTE\tIt is a good practice to mount the accelerometers on the PCB area of largest deflection.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8o","Requirement","ECSS-Q-ST-70-61_1510980",1,"Created","Vibration testing shall be performed in the three orthogonal axes: one out-of-plane and two in-plane."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.8p","Requirement","ECSS-Q-ST-70-61_1510981",1,"Created","The severity of the vibration test shall not be less than that shown in Table 14-2 and Table 14-3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.9a","Requirement","ECSS-Q-ST-70-61_1510985",1,"Created","Mechanical shock test shall be performed in assembly verification for area array components in accordance with requirements in clause 13.3, for solderless assemblies in accordance with requirements in clause 13.6 and for the following components:\n1.\tRelay\n2.\tQuartz\n3.\tMagnetic components (RM)\n4.\tTransformer and self\n5.\tHybrid\n6.\tTantalum capacitor\n7.\tHeavy or large component\n8.\tOptical components\n9.\tLow insertion force DIP socket \n10.\tSemiconductors (IC) components, Hybrid components, relays, capacitors with cavities","NOTE\tThe list of components is taken from Table 17-1 of ECSS-E-HB-32-25A (14July2015) that is reproduced in this Standard as Table 14-4.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.9b","Requirement","ECSS-Q-ST-70-61_1510986",1,"Created","For components listed in requirement 14.9a, assembly verification shall be made with functional testing to be capable to identify degradation due to shock tests."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.9c","Requirement","ECSS-Q-ST-70-61_1510987",1,"Created","The levels and duration of the shock shall be provided in the verification report."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.9d","Requirement","ECSS-Q-ST-70-61_1510988",1,"Created","The mechanical shock levels shall be set to meet the intended mission with margin."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.9e","Permission","ECSS-Q-ST-70-61_1510989",1,"Created","Mechanical shock may be omitted if it can be demonstrated that the design has robust margin or proven heritage."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.10a","Requirement","ECSS-Q-ST-70-61_1510990",1,"Created","Damp heat test shall be performed as part of the verification programme for solderless processes according to clause 13.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.10b","Requirement","ECSS-Q-ST-70-61_1510991",1,"Created","Damp heat test conditions shall be (93 ± 3) % at (40 ± 3) °C for 240 hours in compliance with the Annex C of ECSS-Q-ST-70-14."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11a","Requirement","ECSS-Q-ST-70-61_1510992",1,"Created","The test specimen shall be temperature cycled in an air circulating or inert gas purged chamber."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11b","Requirement","ECSS-Q-ST-70-61_1510993",1,"Created","Before the start of the temperature cycling, the test specimen shall be baked out to remove the internal humidity according to clause 7.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11c","Permission","ECSS-Q-ST-70-61_1510994",1,"Created","The bake-out may be part of the first temperature cycle."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11d","Requirement","ECSS-Q-ST-70-61_1510995",1,"Created","The temperature cycling shall be between -55 (-5/+0) °C and +100 (-0/+5) °C."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11e","Requirement","ECSS-Q-ST-70-61_1510996",1,"Created","The first temperature cycle shall be hot."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11f","Requirement","ECSS-Q-ST-70-61_1510997",1,"Created","The rate of temperature change during the temperature cycle shall not exceed 10 °C per minute.","NOTE\tHigher ramp rates reduce the stresses in the solder joint but increase the stresses within the ceramic materials.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11g","Requirement","ECSS-Q-ST-70-61_1510998",1,"Created","The soak time at each temperature extreme shall be a minimum of 15 minutes."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11h","Requirement","ECSS-Q-ST-70-61_1510999",1,"Created","The monitoring thermocouple shall be attached to the surface of the printed circuit board."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.11i","Requirement","ECSS-Q-ST-70-61_1511000",1,"Created","The number of thermal cycles shall be in accordance with: \n1.\tclause 13.2 for general verification programme, \n2.\tclause 13.3 for assembly verification of ceramic area array components, \n3.\tclause 13.4 for assembly verification with electrical testing procedure, \n4.\tclause 13.5 for verification programme with reduced temperature range, and \n5.\tclause 13.6 for verification for solderless components.","NOTE\tThe number of thermal cycles can be higher for SMD, PTH or AAD, based on specific mission requirements.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12a","Requirement","ECSS-Q-ST-70-61_1511001",1,"Created","Temperature cycling with reduced temperature range shall be performed as part of the special verification programme in accordance with requirements in clause 13.5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12b","Permission","ECSS-Q-ST-70-61_1511002",1,"Created","The stresses during temperature cycling may be reduced by modification of the temperature cycling conditions as follows: \n1.\tDecreasing the thermal range during temperature cycling by increasing the minimum temperature from the nominal one, or\n2.\tdecreasing the thermal range during temperature cycling by decreasing the maximum temperature from the nominal one, or\n3.\tdecreasing the temperature cycling gradient from the nominal one, or\n4.\tany combination of 1 to 3 above.","NOTE\tThe modifications refer to changes from the nominal temperature cycling conditions as described in requirements 14.11d and 14.11f.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12c","Permission","ECSS-Q-ST-70-61_1511003",1,"Created","The temperature cycling may be performed in several steps, with different conditions in the different steps.","NOTE\tA typical stepwise temperature cycling test is to perform the cycling in 2 steps as follows:\n·\tStep 1: Temperature range tailored so that the minimum and maximum temperature on board level during the on-ground qualification conditions are covered including the minimum and maximum temperatures during cold start, non-operating and operating, as required for the intended mission. Number of cycles in this step tailored such that the on-ground qualification conditions are covered at least with a safety margin of 2.\t \nThe lower temperatures often result in largest stresses, and it is therefore good practice to cover cold start conditions in this first step so that the number of cycles at the larger temperature range are minimized.\t \nExample: 20 cycles between -40°C/+85°C with a gradient of 2°C/min and a dwell time of 15 minutes corresponds to 15,5 cycles of -55°C/+100°C with a gradient of 10°C/min as calculated with the equation in requirement 14.12g.\n·\tStep 2: Temperature range tailored so that the minimum and maximum temperature on board level during the in-orbit conditions are covered. Number of cycles in this step tailored such that steps 1 and 2 in total correspond to the nominal temperature cycling range that is required for the type of components being verified, typically 500 cycles, when re-calculated with the modified Coffin-Manson (Norris-Landzberg) equation.\n\tExample: 981 cycles between -10/+100°C with a gradient of 10°C/min or slightly lower and 15 minutes of dwell time. 981 such cycles correspond to 484,8 cycles -55/+100°C with gradient ~10°C/min, as calculated with the equation in requirement 14.12g.\n\tThus the cycling during step 1 and step 2 in total covers the full 500 cycles (15,5 + 484,8 = 500,3) required for surface mounted components as required by requirement 13.2.1cc.\nNOTE\t2\tThe reason behind dividing the temperature cycling in different steps is to decrease the risk of thermally overstressing the assembly while not prolonging the schedule more than necessary.\nNOTE\t3\tIt is recommended to perform the tailoring of the temperature cycling such that the envelope of all intended mission requirements can be covered. A case-by-case trade-off between cost, schedule and risk is though often needed. \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12d","Requirement","ECSS-Q-ST-70-61_1511004",1,"Created","The total number of cycles shall be tailored such that all the steps in total correspond to the nominal number of thermal cycles with nominal temperature cycling range that is required for the type of components being verified. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12e","Requirement","ECSS-Q-ST-70-61_1511005",1,"Created","The temperature conditions during temperature cycling shall cover the minimum and maximum board temperatures seen by the component in the intended mission profile including on ground qualification testing."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12f","Requirement","ECSS-Q-ST-70-61_1511006",1,"Created","The corresponding number of thermal cycles for the on-ground qualification and in-orbit environment shall be covered at least with a safety margin of 2. ","NOTE\tTemperature on board level are taken into account during all the on-ground qualification conditions including the minimum and maximum temperatures during cold start, non-operating and operating, as required for the intended missions.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.12g","Requirement","ECSS-Q-ST-70-61_1511007",1,"Created","The modified Coffin-Manson (Norris-Landzberg) equation used for the calculation of the equivalent thermal cycles shall be the following: \n \nwhere:\nAF = Acceleration factor between lab and field conditions\nTmax and Tmin = Maximum and minimum temperatures [Kelvin]\n∆T = Temperature difference between Tmax and Tmin\nf = Frequency of the cycling when considering each plateau and the gradients [cycles/24h]","NOTE\tThe coefficients specified are valid for soldering with SnPb solder only.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.13a","Requirement","ECSS-Q-ST-70-61_1511008",1,"Created","Life test shall be performed as part of the assembly verification for solderless components in accordance with requirements in clause 13.6."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.13b","Requirement","ECSS-Q-ST-70-61_1511009",1,"Created","Life test conditions shall be 2000 hours at 125 °C or at maximal operational temperature during flight mission."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14a","Requirement","ECSS-Q-ST-70-61_1511010",1,"Created","Visual inspection of each verification sample shall be made using the list of nonconformance criteria of clause 12.3."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14b","Requirement","ECSS-Q-ST-70-61_1511011",1,"Created","Prior to microsectioning, the components shall be in conformance with the dimensional and solder fillet requirements of clause 8,clause 9 and clause 10."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14c","Requirement","ECSS-Q-ST-70-61_1511012",1,"Created","Any identified nonconformance during the visual inspection specified in 14.14a, before any aging test, shall lead to rejection of the verification sample."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14d","Requirement","ECSS-Q-ST-70-61_1511013",1,"Created","Any identified nonconformance during the visual inspection specified in 14.14a, after any aging test, shall be recorded in the traveller sheet of the verification sample."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14e","Requirement","ECSS-Q-ST-70-61_1511014",1,"Created","In the case of visual failures, an analysis shall be performed to identify if the failure results from the component or the assembly process."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14f","Recommendation","ECSS-Q-ST-70-61_1511015",1,"Created","The identified nonconformances of 14.14d should be classified in acceptable or unacceptable depending on performed test flow.","NOTE\t\tAfter the environmental test campaign, some defects are acceptable. For example disturbed solder joints are typical after verification programme and are acceptable provided that the microsectioning acceptance criteria are fulfilled. In case of visible cracks in the solder joints, it is difficult to know the crack length from external visual inspection only. Cracks in solder joints can therefore be acceptable provided that the microsectioning acceptance criteria are fulfilled. \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.14g","Requirement","ECSS-Q-ST-70-61_1511016",1,"Created","The nonconformances identified in 14.14b and 14.14d shall be notified to the Approval Authority within one week."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.1a","Requirement","ECSS-Q-ST-70-61_1511017",1,"Created","The Approval Authority shall make available a list of laboratories available to perform microsection.","NOTE\tThe list of available laboratories is on ESCIES website, see www.escies.org, Technologies - ESA SMT Verification: ESA-TECMSP-MO-013165 “ESA recommended microsectioning facilities”.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.1b","Requirement","ECSS-Q-ST-70-61_1511018",1,"Created","Microsections shall be performed by a laboratory specified in 14.15.1a except the case specified in the requirement 14.15.1c."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.1c","Requirement","ECSS-Q-ST-70-61_1511019",1,"Created","When in-house or other non-listed microsection facilities are used, the supplier shall demonstrate the following:\n1.\tthe capability of the laboratory on representative samples including chip components, LCCs and FPs as well as conformal coating.\n2.\ta report with associated microsections sent to the Approval Authority for review and assessment of quality of microsectioning.","NOTE\tIn accordance with ESA memo ESA-TECMSP-MO-013161. See www.escies.org, Technologies - ESA SMT Verification.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2a","Requirement","ECSS-Q-ST-70-61_1511020",1,"Created","At least one microsection shall be made per assembly configuration after environmental testing on each type of component, size and assembly processes and soldering processes.","NOTE\t1\tDifferent soldering processes and different staking, bonding or conformal coating are examples of different configurations.\nNOTE\t2\tSuccessive polishing planes can be performed.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2b","Requirement","ECSS-Q-ST-70-61_1511021",1,"Created","Microsectioning of repaired sample shall cover the manually soldered assembly, provided the same configuration."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2c","Requirement","ECSS-Q-ST-70-61_1511022",1,"Created","The microsection shall be done on the component having the worst solder joint appearance as identified at MIP2."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2d","Requirement","ECSS-Q-ST-70-61_1511023",1,"Created","For assembly sensitive components, 5 (five) components shall be microsectioned per assembly configuration."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2e","Permission","ECSS-Q-ST-70-61_1511024",1,"Created","Additional microsections may be requested by the Approval Authority in case of cracks or other features detected during the first microsection sampling.."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2f","Requirement","ECSS-Q-ST-70-61_1511025",1,"Created","Adhesive bonding for thermal or mechanical purpose underneath a component shall be microsectioned."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.2g","Requirement","ECSS-Q-ST-70-61_1511026",1,"Created","The microsections of the component shall be done as specified in Table 14-5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1a","Requirement","ECSS-Q-ST-70-61_1511027",1,"Created","The integrity of the assembly shall be assessed by microsectioning. ","NOTE\tIntegrity covers PCB, solder joints, adhesives and packages. \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1b","Requirement","ECSS-Q-ST-70-61_1511028",1,"Created","After microsectioning, the microsections shall be in compliance with requirements of Table 14-5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1c","Requirement","ECSS-Q-ST-70-61_1511029",1,"Created","The microsection shall be inspected with a magnification of 50x to 200x except the case specified in the requirement 14.15.3.1d"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1d","Recommendation","ECSS-Q-ST-70-61_1511030",1,"Created","The microsection for components with small stand-off should be inspected with magnification up to 500x. ","NOTE\tExamples of small stand-off components are LCCs, chip resistors and capacitors, QFN.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1e","Requirement","ECSS-Q-ST-70-61_1511031",1,"Created","In case the microsection shows a crack more than 75 % of acceptable crack, the component type shall be classified as assembly sensitive. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1f","Requirement","ECSS-Q-ST-70-61_1511032",1,"Created","If the component type is classified as assembly sensitive, according to requirement 14.15.3.1e, all remaining components from verification boards shall be microsectioned in order to confirm that acceptance criteria are still fulfilled. ","NOTE\tFor a first verification of a new component not identified as assembly sensitive, 3 components are sufficient.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1g","Requirement","ECSS-Q-ST-70-61_1511033",1,"Created","The Approval Authority shall have access to the moulded microsection and pictures. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.1h","Requirement","ECSS-Q-ST-70-61_1511034",1,"Created","The verification board and associated microsections shall be stored for a period of at least ten years.","NOTE\t1\tIt is good practice to store the boards until end of mission. \nNOTE\t2\tBoards can assist the analysis of in-orbit failures.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2a","Requirement","ECSS-Q-ST-70-61_1511035",1,"Created","Cracks in the solder joint outside of the critical zone shall be accepted."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2b","Requirement","ECSS-Q-ST-70-61_1511036",1,"Created","Cracks in the mechanical bonding shall not be accepted."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2c","Permission","ECSS-Q-ST-70-61_1511037",1,"Created","Cracks in the mechanical bonding may be accepted provided that the criteria defined in Table 14-5 are met and accepted by Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2d","Requirement","ECSS-Q-ST-70-61_1511038",1,"Created","Cracks in the mechanical staking shall not be accepted."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2e","Permission","ECSS-Q-ST-70-61_1511039",1,"Created","Cracks in the mechanical staking may be accepted provided that one of the following items are met:\n1.\tat completion of verification the criteria defined in Table 14-5 are met and accepted by Approval Authority.\n2.\tafter vibration and a minimum of 50 thermal cycles, visual inspection show absence of cracks in the staking and photos of staking are provided."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2f","Requirement","ECSS-Q-ST-70-61_1511040",1,"Created","Cracks in the thermal bonding shall not be accepted."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2g","Permission","ECSS-Q-ST-70-61_1511041",1,"Created","Cracks in the thermal bonding may be accepted at the completion of the verification testing when they are perpendicular to PCB surface plane."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2h","Requirement","ECSS-Q-ST-70-61_1511042",1,"Created","Any damage to the component beyond the ones acceptable by the component datasheet shall be identified as a verification failure."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.3.2i","Permission","ECSS-Q-ST-70-61_1511043",1,"Created","Damages outside of what is allowed in the component data sheet may be acceptable providing acceptance of Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.4a","Requirement","ECSS-Q-ST-70-61_1511045",1,"Created","Solder joint of ceramic chip capacitors after microsectioning shall be in compliance with Table 14-5."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.15.4b","Requirement","ECSS-Q-ST-70-61_1511046",1,"Created","For ceramic chip capacitors damages inside the component after microsectioning shall be in compliance with Table 14-6.","NOTE\t1\tThe cracks in the ceramic observed at completion of assembly verification may be located either on the top terminations or on the bottom terminations. The cause of the cracks depends on their location on the component.\nNOTE\t2\tCracks in the ceramic material at the bottom terminations can have several different root cause: \n·\tMechanical stress from bending the PCB during handling, depanelization, integration of the PCB in the unit or from mechanical testing. \n·\tThermal shock during soldering due to excessive solder tip temperature or the solder tip touching the component termination. \nDue to the different root causes the repeatability of bottom side ceramic cracks are low. \nThe risk of bottom side terminations can be reduced by for example pre-heating the board before soldering, and using lower soldering tip temperatures, as also noted in requirement 10.2.5q.\nNOTE\t3\tCracks in the ceramic material at the top terminations can be caused by the pull stress occurring at cold temperatures during temperature cycling. Verification with reduced temperature range in accordance with clause 13.5 reduce the amount and size of such top side cracks.\nEIA-469 issue E criteria for minimum insulation of the cover plate has been used to define the acceptance criteria of these cracks at the completion of assembly verification. EIA 469 issue E requires a minimum insulation of 80 µm for 50 V and above. \nThe as received thickness of the cover plate vary between different chip capacitor values and ratings, as well as between different batches. The ceramic cracks could furthermore occur on all corners of the part. Therefore the acceptability of ceramic cracks is assessed by projecting the worst crack seen on all 4 corners of the component and also by comparing it to the flight batch of the component. \nNOTE\t4\tFor chip capacitors it is good practice to perform the verification on the capacitance value used which has the thinnest cover plate and most densely packed dielectric planes.\nNOTE\t5\tEIA-469 issue E has been used to define the acceptance criteria for delaminations. \n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.16a","Requirement","ECSS-Q-ST-70-61_1511048",1,"Created","After verification testing the acceptance criteria of ECSS-Q-ST-70-60 clause 10.3 and 10.5 shall apply, except for the case specified in requirements 14.16b and 14.16c.","NOTE\t1\tECSS-Q-ST-70-60 includes acceptance criteria for cracks in dielectrics for PTH.\nNOTE\t2\tECSS-Q-ST-70-60 Table 10-25 includes acceptance criteria for pad lift types and Table 10-26 for dielectric cracks.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.16b","Permission","ECSS-Q-ST-70-61_1511049",1,"Created","Anomalies outside the conditions specified in requirement 14.16a may be accepted provided that at least one of the following conditions is met:\n1.\tPresence of anomaly also during PCB procurement, either on the PCB coupons or in certificate.\n2.\tPresence of anomaly also on a spare non-assembled nor tested PCB.\n3.\tPresence of anomaly also on a spare footprint, included on the verification board, showing that the defect was not caused by the assembly processes. ","NOTE\tIt is good practice to include additional footprints on the verification board, which are not populated, to assist failure investigations.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.16c","Permission","ECSS-Q-ST-70-61_1511050",1,"Created","Cracks in the dielectrics under SMT footprints, outside the conditions specified in requirement 14.16a, may be accepted provided that the remaining insulation distance of the flight PCB is in conformance with the PCB definition dossier."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.16d","Requirement","ECSS-Q-ST-70-61_1511051",1,"Created","Cracks in the Printed Circuit Board that have not been identified in the clause 10 of ECSS-Q-ST-70-60 shall be unacceptable."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","14.16e","Requirement","ECSS-Q-ST-70-61_1511052",1,"Created","Defects, such as footprint lifting, cracks in laminate, cracks in via, cracks of tracks, PCB delamination shall be recorded as a nonconformance and analysed."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1a","Permission","ECSS-Q-ST-70-61_1511053",1,"Created","A supplier may be designated for outsourcing from a customer provided that the following conditions are met: \n1.\tOutsourcing activities are limited to degolding and pretinning, lead forming, hand soldering, bonding, staking and conformal coating.\n2.\tThe manufacturing processes to be performed are included in the customer's PID approved by the Approval Authority.\n3.\tThe manufacturing at the supplier site is performed with the same materials as the one used by the customer.\n4.\tThe manufacturing at the supplier site is performed in compliance with the manufacturing procedures of the customer PID.\n5.\tIn case the outsourcing includes lead forming activities, the demonstration that lead geometry is identical are provided to the customer.\n6.\tThe customer is responsible for the assembly carried out by the supplier,\n7.\tThe supplier fills in the manufacturing traveller of the customer.\n8.\tIn case the supplier is not equipped to fill in the manufacturing traveller of the customer, he can use his own manufacturing traveller provided that it has been reviewed and accepted by the customer.\n9.\tAll operators and inspectors working at the supplier site are trained and certified according to clause 17.8 and being active in their certification status.\n10.\tAll operators and inspectors working at the supplier site for the customer as outsourcing are trained on customer applicable PID procedures and certified by the instructor of the customer.","NOTE\tFor the requirement 15.1a.3, ideally those materials are provided in the kitting.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1b","Requirement","ECSS-Q-ST-70-61_1511054",1,"Created","The operators and inspectors shall work only on one set of specified process procedures at a time at the supplier site."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1c","Requirement","ECSS-Q-ST-70-61_1511055",1,"Created","The customer shall issue and maintain a certification matrix of the certification status of the supplier’s operators and inspectors including the name of the instructor and the supplier assembly contact point name."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1d","Requirement","ECSS-Q-ST-70-61_1511056",1,"Created","The customer PID shall identify the certification matrix with the associated names of the supplier involved personnel."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1e","Requirement","ECSS-Q-ST-70-61_1511057",1,"Created","The manufacturing dossier of the boards and unit shall identify the operations performed by the supplier."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1f","Requirement","ECSS-Q-ST-70-61_1511058",1,"Created","The customer shall appoint a person in charge of NCRs issued by customer and supplier."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1g","Requirement","ECSS-Q-ST-70-61_1511059",1,"Created","The supplier shall be informed about assembly NCRs in the customer assembly line."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1h","Requirement","ECSS-Q-ST-70-61_1511060",1,"Created","The customer shall conduct an audit at supplier according to clause 13.1.3 to verify the compliance of the assembly line."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1i","Requirement","ECSS-Q-ST-70-61_1511061",1,"Created","The customer shall provide to the Approval Authority the audit report."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1j","Requirement","ECSS-Q-ST-70-61_1511062",1,"Created","In case of modification in the procedures, the supplier operators and inspectors shall be informed, trained, and certified according to requirement 15.1a.10."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1k","Requirement","ECSS-Q-ST-70-61_1511063",1,"Created","KIPs shall be performed by the customer inspector,"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1l","Requirement","ECSS-Q-ST-70-61_1511064",1,"Created","The customer shall have a storage, packing and transportation procedure for the hardware manufactured at supplier assembly line,"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1m","Requirement","ECSS-Q-ST-70-61_1511065",1,"Created","Incoming inspections of the assembly shall be performed by the customer to verify absence of damage due to the storage, packing and transportation,"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1n","Requirement","ECSS-Q-ST-70-61_1511066",1,"Created","Every 4 years the customer shall invite the Approval Authority to participate the audit of the supplier assembly line, in compliance with requirement 13.1.3f."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","15.1o","Requirement","ECSS-Q-ST-70-61_1511067",1,"Created","The customer shall list in its PID the supplier as “outsourcing” to manufacture hardware."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.2a","Requirement","ECSS-Q-ST-70-61_1511068",1,"Created","Prior to any start of verification, the supplier shall provide a draft PID to the Approval Authority, in conformance with the DRD in Annex C."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.2b","Permission","ECSS-Q-ST-70-61_1511069",1,"Created","The PID may supersede the requirements from this standard in case supplier can demonstrate that any deviation recorded in the PID is approved by Approval Authority based on tests results."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.3a","Requirement","ECSS-Q-ST-70-61_1511070",1,"Created","The PID shall be submitted to the Approval Authority"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.3b","Requirement","ECSS-Q-ST-70-61_1511071",1,"Created","The Approval Authority shall approve the PID.","NOTE\tThe approval can be achieved by PID signature or minutes of meeting being signed by the Approval Authority.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.4a","Requirement","ECSS-Q-ST-70-61_1511072",1,"Created","The supplier shall appoint a contact person for assembly topics. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.5a","Requirement","ECSS-Q-ST-70-61_1511073",1,"Created","A PID shall represent the verified manufacturing processes and production controls. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.5b","Requirement","ECSS-Q-ST-70-61_1511074",1,"Created","Any proposed change to the PID shall be agreed by the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.5c","Requirement","ECSS-Q-ST-70-61_1511075",1,"Created","At least every two years the supplier shall perform a review of the PID, the summary table and the relevant applicable documents for agreement by the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","16.5d","Requirement","ECSS-Q-ST-70-61_1511076",1,"Created","The PID shall be managed in accordance with configuration control requirements of ECSS-M-ST-40."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.1a","Requirement","ECSS-Q-ST-70-61_1511077",1,"Created","Requirements from clause 5 from ECSS-Q-ST-20 shall apply for \"Quality assurance\"."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.2a","Requirement","ECSS-Q-ST-70-61_1511078",1,"Created","Quality records shall be retained for at least ten years, or in accordance with the project contract.","NOTE\tExample of quality records are travellers log, work orders.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.2b","Requirement","ECSS-Q-ST-70-61_1511079",1,"Created","Quality records shall be gathered in the Verification report in conformance with the DRD in Annex B."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.2c","Requirement","ECSS-Q-ST-70-61_1511080",1,"Created","The following documents, as a minimum, shall be made available to supplier\n1.\tPID.\n2.\tAudit report established by the Approval Authority.\n3.\tVerification report."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.3a","Requirement","ECSS-Q-ST-70-61_1511081",1,"Created","The requirements from clauses 5 and 6 from ECSS-Q-ST-10-09 shall apply for \"Nonconformance\"."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.4a","Requirement","ECSS-Q-ST-70-61_1511082",1,"Created","Equipment and tools, degolding and pretinning bathes, soldering equipment, and measuring equipment shall be calibrated within a period of one year."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.4b","Requirement","ECSS-Q-ST-70-61_1511083",1,"Created","The supplier shall maintain records of the calibration according to clause 5.2.6 of ECSS-Q-ST-20."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.4c","Requirement","ECSS-Q-ST-70-61_1511084",1,"Created","A suspected or confirmed tool or equipment failure shall be recorded as a project nonconformance.","NOTE\tThe records can aid early detection of a trend towards nonconformance.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.4d","Requirement","ECSS-Q-ST-70-61_1511085",1,"Created","Defective or out of calibration date equipment or tools shall be labelled or removed from work areas."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.4e","Requirement","ECSS-Q-ST-70-61_1511086",1,"Created","The Approval Authority shall be notified of the nonconformance."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.5a","Requirement","ECSS-Q-ST-70-61_1511087",1,"Created","The requirements from clause 5.2.5 of ECSS-Q-ST-20 shall apply for traceability."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.6a","Requirement","ECSS-Q-ST-70-61_1511088",1,"Created","The supplier shall prepare in-house visual workmanship standards to be made available to each operator and inspector.","NOTE\t1\tExamples are: Satisfactory work samples or visual aids which illustrate the quality characteristics of all types of soldered connection involved in the task.\nNOTE\t2\tThe illustrations presented in Annex F and Annex E this standard can be included as part of the examples.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.7a","Requirement","ECSS-Q-ST-70-61_1511089",1,"Created","During all stages of the process, the inspection points defined in the manufacturing flow chart shall be carried out. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.7b","Requirement","ECSS-Q-ST-70-61_1511090",1,"Created","The inspection shall be performed in conformance with clause 12."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8a","Requirement","ECSS-Q-ST-70-61_1511091",1,"Created","Trained and certified personnel shall be employed for soldering operations and inspections."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8b","Requirement","ECSS-Q-ST-70-61_1511092",1,"Created","A training programme shall be developed, maintained and implemented by the supplier to provide excellence of workmanship and personnel skills in soldering."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8c","Requirement","ECSS-Q-ST-70-61_1511093",1,"Created","Records of training, testing and certification status of the operators and inspectors shall be maintained for at least 10 years."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8d","Requirement","ECSS-Q-ST-70-61_1511094",1,"Created","The training programme shall include procedures for the training, internal certification, maintenance of certified status, recertification, and revocation of certified status for soldering and inspection personnel."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8e","Requirement","ECSS-Q-ST-70-61_1511095",1,"Created","Training success shall be based on objective evidence of soldering quality, resulting from practical training and inspection of soldered joints."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8f","Requirement","ECSS-Q-ST-70-61_1511096",1,"Created","Personnel shall be retrained or re-assessed in the following circumstances:\n1.\tRepeated quality nonconformance.\n2.\tChange in soldering techniques.\n3.\tChange in soldering parameters.\n4.\tAdditional process skills."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8g","Requirement","ECSS-Q-ST-70-61_1511097",1,"Created","The operators performing X-ray inspection shall be trained and in-house certified to perform and assess X-ray results."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8h","Requirement","ECSS-Q-ST-70-61_1511098",1,"Created","Operators, inspectors and instructors shall be certified at an ESA school in compliance with ESA STR-258 or in-house training authorised by the Approval Authority."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","17.8i","Permission","ECSS-Q-ST-70-61_1511099",1,"Created","Operators and inspectors may be re-certified at an ESA school or by an in-house instructor authorised by the Approval Authority.","NOTE\tThe supplier company is responsible for checking the constant visual acuity of its workers i.a.w. ESA STR-258 to maintain certification status of personnel.\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","A.2.1a","Requirement","ECSS-Q-ST-70-61_1511100",1,"Created","The verification programme documentation shall contain as a minimum the following:\n1.\tIndication of process of the assembly:\n(a)\tsoldering process\n(b)\trepair process.\n2.\tSubstrate information: \n(a)\tPCB material and manufacturer \n(b)\tPCB footprint surface finish \n(c)\tNumber of layers \n(d)\tThickness\n(e)\tBuild up with identification of signal and full copper plane \n(f)\tConnection of the footprints to the internal layer representative of the FM\n(g)\tLocation of the components on the PCB \n(h)\tFor through hole component, ratio of hole to lead diameter\n(i)\tLocation of the mechanical fixation or stiffeners if any\n(j)\tNumber of PCB used for the verification programme.\n3.\tMaterials used\n(a)\tSolder paste and wire designation, commercial trademark, and composition with associated flux class\n(b)\tFlux class used for pretinning and soldering\n(c)\tConformal coating\n(d)\tAdhesive, potting, underfill and encapsulants used for mechanical and for thermal purpose\n(e)\tSolvent\n(f)\tOthers. \n4.\tList of components with their materials leads and finish\n5.\tEnvironmental test conditions and facility\n6.\tElectrical continuity test specification, procedure\n7.\tVerification method Microsection or Electrical monitoring \n(a)\tMicrosection laboratory.\n8.\tPID and Manufacturing document process references\n9.\tVerification workflow\n10.\tVerification by similarity\n11.\tCertification status of the operators and inspectors\n12.\tCompliance status of the operators and inspectors\n13.\tCompliance of the manufacturing room\n14.\tAdditional information. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","A.2.1b","Permission","ECSS-Q-ST-70-61_1511101",1,"Created","b.\tThe content of Verification programme specified in requirement A.2.1a may be tailored for companies already having an approved PID in accordance with this standard."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","B.2.1a","Requirement","ECSS-Q-ST-70-61_1511102",1,"Created","The verification documentation shall contain as a minimum the following:\n1.\tIndication of process of the assembly:\n(a)\tsoldering process\n(b)\trepair process.\n2.\tPCB information: \n(a)\tPCB material and manufacturer \n(b)\tPCB footprint surface finish \n(c)\tNumber of layers \n(d)\tThickness\n(e)\tBuild up with identification of signal and full copper plane \n(f)\tConnection of the footprints to the internal layer representative of the FM\n(g)\tLocation of the components on the PCB \n(h)\tFor through hole component, ratio of hole to lead diameter\n(i)\tLocation of the mechanical fixation or stiffeners if any\n(j)\tNumber of PCB used for the verification programme.\n3.\tMaterials used\n(a)\tSolder paste and wire designation, commercial trademark, and composition with associated flux class\n(b)\tFlux class used for pretinning and soldering\n(c)\tConformal coating\n(d)\tAdhesive for mechanical, and for thermal\n(e)\tSolvent\n(f)\tOthers.\n4.\tList of components with their materials leads and finish (including traceability).\n5.\tMechanical specification of the component with associated manufacturer specification.\n6.\tEnvironmental test conditions and facility\n7.\tVisual inspection report established in conformance with the requirements of clause 12\n8.\tSummary of cleanliness test results in conformance with clause 11.1.2 of ECSS-Q-ST-70-61 or equivalent process when applicable\n9.\tTests results concerning the warp (bow) and twist of circuit board in conformance when applicable\n10.\tElectrical continuity test report for multilayer boards when applicable\n11.\tVerification method Microsection or Electrical monitoring \n(a)\tMicrosection laboratory\n12.\tPID and Manufacturing document process references\n13.\tVerification workflow\n14.\tVerification by similarity\n15.\tNCRs\n16.\tCertification status of the operators and inspectors\n17.\tCompliance status of the operators and inspectors\n18.\tCompliance of the manufacturing room\n19.\tQuality records\n20.\tAdditional information. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","B.2.1b","Requirement","ECSS-Q-ST-70-61_1511103",1,"Created","The verification report shall contain the results of all tests performed according to clauses 12 and 14."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","B.2.1c","Requirement","ECSS-Q-ST-70-61_1511104",1,"Created","The verification report shall contain photographic evidence of the tested assembled boards where possible."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","B.2.1d","Requirement","ECSS-Q-ST-70-61_1511105",1,"Created","The verification report shall contain the manufacturing soldering log according to clause 13.2.4."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","B.2.1e","Requirement","ECSS-Q-ST-70-61_1511106",1,"Created","The verification report shall contain the list of all NCRs referring to assembly and test of verification boards and associated reports."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<1>a","Requirement","ECSS-Q-ST-70-61_1511107",1,"Created","The PID shall contain the following information about the Document Format:\n1.\tCover page: document title, document reference, revision number and date, page numbering, signing of Production and Quality representatives,\n2.\tFollow-up of PID updates: registration of PID updates indicating the nature of the update and the sections and pages updated,\n3.\tPurpose and scope of the document,\n4.\tTable of contents."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<2>a","Requirement","ECSS-Q-ST-70-61_1511108",1,"Created","The PID shall contain the Manufacturing control flow chart of the verified assembly.","NOTE 1\tThis illustrates the various stages of procurement, manufacturing and inspection operations specific to this technology in a flow chart format.\nNOTE 2\tIt can be used to identify, among others:\n·\tthe operation,\n·\tthe body responsible for its implementation,\n·\trelated documents: (only their reference),\n·\tprocurement specifications (for materials),\n·\tacceptance inspection procedures (for materials and components),\n·\tmanufacturing procedures,\n·\tmanufacturing and quality control procedures during and at the end of production.\n·\tstorage documentation\n"]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<3>a","Requirement","ECSS-Q-ST-70-61_1511109",1,"Created","The PID shall contain the following information about Specifications:\n1.\tList of procurement specifications, assembly procedures and inspection procedures concerning the technology dealt within the PID, including the precise title, the reference or number, the revision number and date of each document\n2.\tPrinted circuit design rules in compliance with requirements from ECSS-Q-ST-70-12. \n3.\tGeneral Quality Assurance documents relating to the technology."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<4>a","Requirement","ECSS-Q-ST-70-61_1511110",1,"Created","The PID shall contain the following information about Organisation:\n1.\tRepresented as a flow chart: organization of the company, organization of production department and organization of the quality Department.\n2.\tFocal point and PID responsible,\n3.\tOperators and inspectors’ certification methodology. "]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<5>a","Requirement","ECSS-Q-ST-70-61_1511111",1,"Created","The PID shall contain as a minimum the following information about the Manufacturing traveller or log file: \n1.\tThe sequencing of the various operations in their logical order of execution,\n2.\tThe references of the documents referred to and used during these operations, \n3.\tThe references of the Quality documents to trace the various batches of material used (record reference), together with the workstations and tools employed,\n4.\tThe signatures of the various actors with the date on which the task was completed."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<6>a","Requirement","ECSS-Q-ST-70-61_1511112",1,"Created","The PID shall contain as a minimum the following information about the list of verified technology:\n1.\tList of materials,\n2.\tTemperature and time profiles for the soldering machines used in the verification,\n3.\tList of verified components per assembly configuration, \n4.\tList of assembly sensitive components,\n5.\tList of components with limited project verification,\n6.\tFor limited project verification, non-compliance with clause 13 shall be clearly identified."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<7>a","Requirement","ECSS-Q-ST-70-61_1511113",1,"Created","The PID shall contain as a minimum the following about the Description of production line:\n1.\tLayout of premises with associated surface area, with indication of location of production machines and quality inspection,\n2.\tWorking environment; cleanliness class, ambient temperature limits, humidity, and positive pressure limits for each type of activities."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<8>a","Requirement","ECSS-Q-ST-70-61_1511114",1,"Created","The PID shall contain a list of all machines and tools utilised during the manufacturing activity."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<9>a","Requirement","ECSS-Q-ST-70-61_1511115",1,"Created","The PID shall contain range and capability of supporting laboratory services."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","C.2.1<10>a","Requirement","ECSS-Q-ST-70-61_1511116",1,"Created","The PID shall contain a list of assembled board with associated assembly process by year manufactured in accordance with the PID."]
["ECSS-Q-ST-70-61C","ECSS - Current v0.9","D.2.1a","Requirement","ECSS-Q-ST-70-61_1511117",1,"Created","The assembly summary table shall include the following data:\n1.\tAssembly processes\n2.\tPID reference with issue \n3.\tSolder type for machine reflow and for hand assembly\n4.\tConformal coating\n5.\tSubstrate type\n6.\tComponent data. ","NOTE\tAn example of a component type preparation and mounting configuration table is given in Figure D-1.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.1a","Requirement","ECSS-Q-ST-70-40_1500001",1,"Created","The engineering authority together with the brazing responsible shall select the brazing design."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.1b","Requirement","ECSS-Q-ST-70-40_1500002",1,"Created","The engineering authority together with the brazing responsible shall specify the requirements relevant for brazing to ensure compliance with all system and mission requirements."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.1c","Requirement","ECSS-Q-ST-70-40_1500003",1,"Created","Brazing Procedure Specification (BPS) specified in clause 8 shall be in compliance with all design requirements. "]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.1d","Requirement","ECSS-Q-ST-70-40_1500004",1,"Created","The engineering authority together with the brazing responsible shall specify controls to demonstrate that brazing joints are satisfying the design requirements.","NOTE\tDirections for design of brazed components can be found in DIN 65169:2017. Brazed and high-temperature brazed components- directions for design."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.2a","Requirement","ECSS-Q-ST-70-40_1500005",1,"Created","Brazing joints classified as Class 1 and Class 2 shall be designed to be inspectable."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.2b","Requirement","ECSS-Q-ST-70-40_1500006",1,"Created","Brazing joints shall be designed that excess of filler material is not affecting inspectability of sensitive areas."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","5.2c","Requirement","ECSS-Q-ST-70-40_1500007",1,"Created","In case that Class 1 and Class 2 joints are not inspectable an alternative test shall be agreed with the customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2a","Requirement","ECSS-Q-ST-70-40_1500008",1,"Created","Brazers performing brazing processes requiring manual interaction shall be trained and certified."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2b","Requirement","ECSS-Q-ST-70-40_1500009",1,"Created","The training for manual brazers shall be performed with test pieces according to national and international standards or by an equivalent dedicated training plan established by brazing responsible.","NOTE\tExample of international standards: ISO 11745:2016.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2c","Requirement","ECSS-Q-ST-70-40_1500010",1,"Created","Brazing operators shall be trained to demonstrate compliance to the BPS specified in the clause 8 with specific brazing test piece representative for production part."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2d","Requirement","ECSS-Q-ST-70-40_1500011",1,"Created","The training of the brazers and brazing operator shall be traceable in a written document."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2e","Permission","ECSS-Q-ST-70-40_1500012",1,"Created","After training, the brazer and brazing operator may operate for a maximum period of two years."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.2f","Permission","ECSS-Q-ST-70-40_1500013",1,"Created","Validity of training may be extended indefinitely provided the two following conditions are met:\n1.\tA record is maintained from the date of the initial training,\n2.\tBrazer and brazing operator use the process at least once every six months from initial training."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.3a","Requirement","ECSS-Q-ST-70-40_1500014",1,"Created","Brazing inspectors shall be nominated by the company with involvement of quality assurance responsible."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","6.3b","Requirement","ECSS-Q-ST-70-40_1500015",1,"Created","Brazing inspectors shall be trained for this standard and the specific BPS with the involvement of the brazing responsible "]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.1a","Requirement","ECSS-Q-ST-70-40_1500016",1,"Created","All equipment used for brazing shall be subject to testing, inspection and maintenance in accordance with the requirements of the equipment manufacturer and the process necessities."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.1b","Requirement","ECSS-Q-ST-70-40_1500017",1,"Created","When there is no period for the inspection and maintenance defined, inspection and maintenance shall be performed at least every 12 months. "]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.2.1a","Requirement","ECSS-Q-ST-70-40_1500018",1,"Created","Filler metals shall be procured according to clause 5.6 of ECSS-Q-ST-70.","NOTE\tFiller materials are specified for example in EN ISO 17672:2016.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.2.2a","Requirement","ECSS-Q-ST-70-40_1500019",1,"Created","Flux shall be procured according to clause 5.6 of ECSS-Q-ST-70.","NOTE\tFlux materials are specified for example in 1045:1997.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.2.3a","Requirement","ECSS-Q-ST-70-40_1500020",1,"Created","Only the tooling and fixtures specified in the BPS in Annex A shall be used for the brazing operation.","NOTE\tChange of tooling can have impact on brazing joints. This can be e.g. because of different coefficients of thermal expansion impacting directly the solder gap and capillary effects and thus brazing joint quality.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","7.2.3b","Requirement","ECSS-Q-ST-70-40_1500021",1,"Created","Tooling and fixtures shall be checked for cleanliness to comply with requirements from the clause 8.4."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.1a","Requirement","ECSS-Q-ST-70-40_1500022",1,"Created","A Brazing Procedure specification shall be written in accordance with DRD in Annex A."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.1b","Requirement","ECSS-Q-ST-70-40_1500023",1,"Created","A BPS specified in requirement 8.1a shall be established for each type of brazed joint in a space application."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.1c","Requirement","ECSS-Q-ST-70-40_1500024",1,"Created","All brazing joints shall be in conformance with the BPS specified in the DRD in the Annex A."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.2a","Requirement","ECSS-Q-ST-70-40_1500025",1,"Created","Features for all brazing joints shall be specified either on the engineering drawing or in supporting documentation."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.2b","Requirement","ECSS-Q-ST-70-40_1500026",1,"Created","The information related to the brazing on the drawing shall be in conformance with BPS from DRD in Annex A.","NOTE\tA template for a table of brazing details can be similar as shown for welding in DIN 65118:2010.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.2c","Requirement","ECSS-Q-ST-70-40_1500027",1,"Created","The drawing shall contain the BPS-reference."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.3a","Requirement","ECSS-Q-ST-70-40_1500028",1,"Created","The minimum of documentation for process description shall be in conformance with information required from DRD in Annex A."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.4.2a","Requirement","ECSS-Q-ST-70-40_1500029",1,"Created","To minimise the contribution to the contamination budget during brazing, the following requirements shall apply for operators and other personnel involved in the brazing process:\n1.\tWhen brazing is in a clean room: use only nitrile gloves,\n2.\tWhen brazing is outside a clean room: wear lint free clothing and lint free gloves for assembly and brazing of flight hardware,\n3.\tEnsure that tooling and fixtures are not a source of contamination to the brazed hardware,\n4.\tRemove corrosive residues from brazing process.","NOTE\tTo avoid cross-contamination it is good practice that the molecular and particular cleanliness of tooling and fixtures is at least same level as the brazed H/W. In addition, contaminants transfer mechanisms depending on the used process are considered, for example from outgassing and condensation during vacuum brazing.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","8.4.2b","Requirement","ECSS-Q-ST-70-40_1500030",1,"Created","After brazing, the brazed parts shall be cleaned as specified in the BPS."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","9.1a","Requirement","ECSS-Q-ST-70-40_1500031",1,"Created","The selected NDT method shall be able to detect the compliance with the defined acceptance criteria."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","9.1b","Requirement","ECSS-Q-ST-70-40_1500032",1,"Created","NDT method shall be selected from the following list:\n1.\tVisual examination;\n2.\tUltrasonic examination;\n3.\tRadiographic examination;\n4.\tLeak testing;\n5.\tProof testing;\n6.\tThermography.","NOTE\t1\tFor example use methods in accordance with ECSS-Q-ST-70-15 and EN12799:2000. \nNOTE\t2\tVisual inspection of brazing joints is described in the DIN ISO 19828:2021.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","9.1c","Requirement","ECSS-Q-ST-70-40_1500033",1,"Created","Any acceptance criteria for the NDT, not covered in clause 10.3, shall be agreed with the customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","9.2a","Requirement","ECSS-Q-ST-70-40_1500034",1,"Created","The selected destructive test-method shall be able to demonstrate the compliance with the acceptance criteria from clause 10."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","9.2b","Requirement","ECSS-Q-ST-70-40_1500035",1,"Created","For destructive testing the test method shall be selected from the following list:\n1.\tShear test,\n2.\tTensile test,\n3.\tMetallographic examination,\n4.\tHardness testing,\n5.\tPeel testing,\n6.\tBend testing,\n7.\tBurst test.","NOTE\tFor example use methods in accordance with EN12797:2000.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.1a","Requirement","ECSS-Q-ST-70-40_1500036",1,"Created","The baseline acceptance criteria for brazing joints shall be in conformance with the requirements of clause 10.3, except cases specified in the requirements 10.1b and 10.1c."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.1b","Requirement","ECSS-Q-ST-70-40_1500037",1,"Created","In case the brazing acceptance criteria are different to that specified in the requirements of clause 10.3, an RfA shall be raised."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.1c","Requirement","ECSS-Q-ST-70-40_1500038",1,"Created","For imperfections that are not covered by requirements specified in 10.2, the brazing acceptance criteria shall be agreed with the customer.","NOTE\tActive brazing can produce features looking like local melting. This is not an imperfection in the context of this brazing method.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.2a","Requirement","ECSS-Q-ST-70-40_1500039",1,"Created","The imperfections in brazing joints shall be classified into groups as follows:\n1.\tGroup I: Cracks,\n2.\tGroup II: Cavities,\n3.\tGroup III: Solid inclusions,\n4.\tGroup IV: Bonding imperfections,\n5.\tGroup V: Shape and size imperfections,\n6.\tGroup VI: Miscellaneous imperfections.","NOTE\tThe classification is derived from EN ISO 18279:2004.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.3a","Requirement","ECSS-Q-ST-70-40_1500040",1,"Created","The acceptance criteria for brazed joints, specified in Table 10-1, shall be applied."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.3b","Requirement","ECSS-Q-ST-70-40_1500041",1,"Created","Limits specified in Table 10-1 shall be used in absence of other application specific definition agreed with the customer.","NOTE\tThe evaluation of brazed joints in Table 10-1 is derived from the EN ISO 18279:2004 Table B.1 \"Quality levels for brazed joints imperfections”.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","10.4a","Requirement","ECSS-Q-ST-70-40_1500042",1,"Created","For the selection of the quality levels from Table 10-1 the following rule shall apply:\n1.\tFor Safety Class 1: Quality Level A,\n2.\tFor Safety Class 2: Quality Level B as a minimum,\n3.\tFor Safety Class 3: Quality Level C as a minimum."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2a","Requirement","ECSS-Q-ST-70-40_1500044",1,"Created","A Brazing Verification Test Plan (BVTP) shall be issued for brazing procedure verifications according to the DRD in Annex B."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2b","Requirement","ECSS-Q-ST-70-40_1500045",1,"Created","The test sequence shall be selected with consideration of the reliability under application loads and mission environmental condition."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2c","Requirement","ECSS-Q-ST-70-40_1500046",1,"Created","In case that there are no specific brazing joint tests defined, standard tests with standard test specimen shall be planned.","NOTE\tA test matrix of standard test can be found in Table 11-1.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2d","Requirement","ECSS-Q-ST-70-40_1500047",1,"Created","In case of specific requirements from the application, specific test shall be planned to verify compliance.","NOTE\tExamples of specific tests are Leak Test, Pressure Test, Noise and Vibration Test, Creep, Fatigue, Corrosion.\n"]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2e","Requirement","ECSS-Q-ST-70-40_1500048",1,"Created","In case that the brazed assembly is under thermo-elastic stress, specimen representative for the brazed assembly shall be defined."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2f","Requirement","ECSS-Q-ST-70-40_1500049",1,"Created","Test specimen from the requirement 11.2e shall be submitted to thermal cycling in the test sequence."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.2g","Requirement","ECSS-Q-ST-70-40_1500050",1,"Created","Pass-Fail criteria of the verification test sequence shall be specified in the Test Plan."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.3a","Requirement","ECSS-Q-ST-70-40_1500051",1,"Created","The samples shall be marked and serialised."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.3b","Requirement","ECSS-Q-ST-70-40_1500052",1,"Created","In the case when at least one measurement on one sample is non-compliant with the requirements of clause 11, the verification shall be rejected."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.4a","Requirement","ECSS-Q-ST-70-40_1500053",1,"Created","In case one or more parameters in an approved BPS are changed outside the allowed range, a delta verification shall be performed."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.4b","Requirement","ECSS-Q-ST-70-40_1500054",1,"Created","The decision to perform a delta verification or a complete verification shall be under the responsibility of the brazing responsible."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.4c","Requirement","ECSS-Q-ST-70-40_1500055",1,"Created","Every change in the existing brazing configuration shall be agreed with the customer to specify if a re-verification or delta verification is necessary."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5a","Requirement","ECSS-Q-ST-70-40_1500056",1,"Created","After the brazing operation has been completed, visual examination shall be performed by the brazing operator and the brazing inspector."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5b","Requirement","ECSS-Q-ST-70-40_1500057",1,"Created","Re-brazing shall be verified using the same method as for verification."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5c","Requirement","ECSS-Q-ST-70-40_1500058",1,"Created","Two additional brazing shall be produced in the brazing verification phase for re-brazing."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5d","Permission","ECSS-Q-ST-70-40_1500059",1,"Created","In case defects are observed, then a maximum of two attempts may be made for in-process correction."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5e","Requirement","ECSS-Q-ST-70-40_1500060",1,"Created","The use of in-process correction shall be documented in the inspection report and shop traveller."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.5f","Requirement","ECSS-Q-ST-70-40_1500061",1,"Created","In case the two re-brazing attempts cannot result in the required level of in process correction, the following shall be performed:\n1.\tA NCR is raised in conformance with requirements from clause 5 of ECSS-Q-ST-10-09.\n2.\tRepair brazing is performed in accordance with the requirements from clause 11.6."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.6a","Requirement","ECSS-Q-ST-70-40_1500062",1,"Created","Repair-brazing shall only performed following the raising of an NCR in conformance with requirements from clause 5 of ECSS-Q-ST-10-09.","NOTE\tReason for repair can be for example that 2 re-brazing attempts have not been successful, the use of wrong filler metal or flux, or when a re-braze extends outside the original brazing zone."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.6b","Requirement","ECSS-Q-ST-70-40_1500063",1,"Created","Repair-brazing shall be performed using a BPS which is approved for brazing repair."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.6c","Requirement","ECSS-Q-ST-70-40_1500064",1,"Created","Re-inspection of all repaired brazing areas shall be performed using the same methods and requirements as the original brazing."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.6d","Requirement","ECSS-Q-ST-70-40_1500065",1,"Created","For multiple repair-brazing, it shall be demonstrated that design strength requirements are met in any given area."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.7a","Requirement","ECSS-Q-ST-70-40_1500066",1,"Created","For the verification of the brazing process, the following documents shall be issued:\n1.\tBrazing Verification Test Plan (BVTP) in conformance with the DRD from Annex B.\n2.\tBrazing Verification Test Report (BVTR) in conformance with Test Report DRD from Annex C of ECSS-E-ST-10-02.\n3.\tBrazing Procedure Specification (BPS) in conformance with the DRD from Annex A for every dimension and material combination."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.7b","Requirement","ECSS-Q-ST-70-40_1500067",1,"Created","Tailoring of the BVTP for other tests shall be agreed with the supplier and customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","11.7c","Requirement","ECSS-Q-ST-70-40_1500068",1,"Created","Documents specified in the requirements from 11.7a.1 to 11.7a.3 and 11.7b shall be controlled in conformance with ECSS-M-ST-40."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.1a","Requirement","ECSS-Q-ST-70-40_1500069",1,"Created","Prior to the start of manufacturing the following documents shall be made available:\n1.\tBVTR,\n2.\tComplete set of drawings,\n3.\tBPS from DRD of Annex A."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.1b","Requirement","ECSS-Q-ST-70-40_1500070",1,"Created","Any brazing performed on flight hardware shall be in conformance with the approved BPS."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.1c","Requirement","ECSS-Q-ST-70-40_1500071",1,"Created","Any brazing performed on flight hardware shall be performed under configuration control."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.2.1a","Requirement","ECSS-Q-ST-70-40_1500072",1,"Created","The preparation of a shop traveller shall be completed."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.2.1b","Requirement","ECSS-Q-ST-70-40_1500073",1,"Created","Only approved BPS shall be used for the brazing of flight hardware."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.2.1c","Requirement","ECSS-Q-ST-70-40_1500074",1,"Created","During brazing of flight hardware, the cleanliness requirements of clause 8.4 shall apply."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.2.2a","Requirement","ECSS-Q-ST-70-40_1500075",1,"Created","Prior to flight hardware production, application of Alpha and Beta samples or alternative brazing control technique in compliance with the Table 12-1 shall be agreed with the customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","12.2.2b","Requirement","ECSS-Q-ST-70-40_1500076",1,"Created","Techniques specified in the requirement 12.2.2a shall be: \n1.\tDemonstrated during verification, and \n2.\tResults approved by the customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.1a","Requirement","ECSS-Q-ST-70-40_1500078",1,"Created","All changes to the BPS from DRD from Annex A shall be controlled in conformance with the ECSS-M-ST-40."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.1b","Requirement","ECSS-Q-ST-70-40_1500079",1,"Created","As a result of modifications to the brazing process specified in the requirement 13.1a, the BPS from DRD from Annex A shall be updated.","NOTE\tFor example, changes to the jigs, parameter changes."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.1c","Requirement","ECSS-Q-ST-70-40_1500080",1,"Created","Modifications to brazing parameters which fall outside the BPS shall lead to the issue of a new brazing configuration."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.1d","Requirement","ECSS-Q-ST-70-40_1500081",1,"Created","In case of an issue of a new brazing configuration specified in the requirement 13.1c the existing brazing configuration shall become obsolete."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.1a","Requirement","ECSS-Q-ST-70-40_1500082",1,"Created","The data generated during mechanised brazing shall be recorded."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.1b","Requirement","ECSS-Q-ST-70-40_1500083",1,"Created","All mechanised brazing data shall be available for review."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2a","Requirement","ECSS-Q-ST-70-40_1500084",1,"Created","In case of anomalies occurring during the brazing process, leading to the brazing activities to be stopped in a controlled manner, the brazing operators shall inform the brazing responsible.","NOTE\tAn unexpected change in one or more process parameters can be considered as anomalies."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2b","Requirement","ECSS-Q-ST-70-40_1500085",1,"Created","For Safety Classes 1 and 2, all anomalies identified in compliance with the requirement 13.2.2a shall be classified as major, and a major NCR in conformance with clause 5 of ECSS-Q-ST-10-09 be raised."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2c","Requirement","ECSS-Q-ST-70-40_1500086",1,"Created","For Safety Class 3, depending on the anomaly identified from the requirement 13.2.2a being minor or major, an NCR shall be raised as minor or major in conformance with clause 5 of ECSS-Q-ST-10-09 accordingly."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2d","Requirement","ECSS-Q-ST-70-40_1500087",1,"Created","Malfunctions of the brazing equipment shall be documented in the maintenance book."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2e","Requirement","ECSS-Q-ST-70-40_1500088",1,"Created","Malfunctions of the brazing equipment shall be reported to the brazing responsible."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2f","Requirement","ECSS-Q-ST-70-40_1500089",1,"Created","A NCR shall be raised in case a flight part is affected by the equipment malfunction."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.2g","Requirement","ECSS-Q-ST-70-40_1500090",1,"Created","All the major and minor anomalies shall be recorded and made available for the customer to review upon request."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.3a","Requirement","ECSS-Q-ST-70-40_1500091",1,"Created","Inspection shall be performed on brazing joints to demonstrate compliance with the requirements from the clauses 9.1 and 9.2."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","13.2.3b","Requirement","ECSS-Q-ST-70-40_1500092",1,"Created","Any nonconformance shall be recorded in compliance with clause 5 of ECSS-Q-ST-10-09 and made available to the customer."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<1>a","Requirement","ECSS-Q-ST-70-40_1500093",1,"Created","The BPS shall include the date, issue and revision number."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<1>b","Requirement","ECSS-Q-ST-70-40_1500094",1,"Created","The BPS shall contain the following information:\n1.\tBrazing process steps,\n2.\tBrazing process parameters,\n3.\tParent material,\n4.\tFiller and Flux,\n5.\tJoint type,\n6.\tCleaning procedure,\n7.\tMechanical or thermal treatment before and after brazing,\n8.\tQuality level for imperfections acceptance criteria,\n9.\tInspection steps."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<2>a","Requirement","ECSS-Q-ST-70-40_1500095",1,"Created","The BPS shall define the manufacturer as follows:\n1.\tIdentification of the lower tier supplier who performs the brazing,\n2.\tReference to the BVTR or other applicable documents."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<3>a","Requirement","ECSS-Q-ST-70-40_1500096",1,"Created","The BPS shall include the identification of the equipment, model and serial number, used to perform the brazing."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<4>a","Requirement","ECSS-Q-ST-70-40_1500097",1,"Created","The BPS shall specify the tooling and fixtures used to perform the brazing."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","A.2.1<5>a","Requirement","ECSS-Q-ST-70-40_1500098",1,"Created","The BPS shall specify all non-destructive inspection techniques."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","B.2.1<1>a","Requirement","ECSS-Q-ST-70-40_1500099",1,"Created","The BVTP shall include the date, issue and revision number."]
["ECSS-Q-ST-70-40C","ECSS - Current v0.9","B.2.1<1>b","Requirement","ECSS-Q-ST-70-40_1500100",1,"Created","The BVTP shall include the following information:\n1.\tBrazing process,\n2.\tParent material combination,\n3.\tFiller material and Flux,\n4.\tJoint type,\n5.\tCleaning procedure,\n6.\tTypes of test for the brazing verification,\n7.\tNumber and type of samples to be tested,\n8.\tCriteria of acceptance of a brazing joints."]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.2a","Requirement","ECSS-S-ST-00_1000001",1,"Unchanged","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"]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.2b","Requirement","ECSS-S-ST-00_1000002",1,"Unchanged","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"]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.2c","Requirement","ECSS-S-ST-00_1000003",1,"Unchanged","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"]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.2d","Requirement","ECSS-S-ST-00_1000004",1,"Unchanged","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"]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.3a","Requirement","ECSS-S-ST-00_1000005",1,"Unchanged","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"]
["ECSS-S-ST-00C Rev.1","ECSS - Current v0.9","9.3b","Requirement","ECSS-S-ST-00_1000006",1,"Unchanged","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1a","Requirement","ECSS-U-ST-20_1430001",1,"Created","The PPAA shall provide to the supplier planetary protection related obligations of relevant external authorities.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1b","Requirement","ECSS-U-ST-20_1430002",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1c","Requirement","ECSS-U-ST-20_1430003",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1d","Requirement","ECSS-U-ST-20_1430004",1,"Created","The Planetary Protection Requirements document shall be subject to approval by the PPAA and released at the latest at SRR.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1e","Requirement","ECSS-U-ST-20_1430005",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1f","Requirement","ECSS-U-ST-20_1430006",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.1g","Requirement","ECSS-U-ST-20_1430007",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.2.1a","Requirement","ECSS-U-ST-20_1430008",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.2.2a","Requirement","ECSS-U-ST-20_1430009",1,"Created","A probability of impact analysis on protected Solar system bodies shall be performed and a report delivered for customer and PPAA review.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.2.2b","Requirement","ECSS-U-ST-20_1430010",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.2.3a","Requirement","ECSS-U-ST-20_1430011",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.1a","Requirement","ECSS-U-ST-20_1430012",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.1a","Requirement","ECSS-U-ST-20_1430013",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.1b","Requirement","ECSS-U-ST-20_1430014",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.1c","Requirement","ECSS-U-ST-20_1430015",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.1d","Requirement","ECSS-U-ST-20_1430016",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.1e","Requirement","ECSS-U-ST-20_1430017",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2a","Requirement","ECSS-U-ST-20_1430018",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2b","Requirement","ECSS-U-ST-20_1430019",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2c","Requirement","ECSS-U-ST-20_1430020",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2d","Requirement","ECSS-U-ST-20_1430021",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2e","Requirement","ECSS-U-ST-20_1430022",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.2f","Requirement","ECSS-U-ST-20_1430023",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.3a","Requirement","ECSS-U-ST-20_1430024",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.3b","Requirement","ECSS-U-ST-20_1430025",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.3c","Requirement","ECSS-U-ST-20_1430026",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.4a","Requirement","ECSS-U-ST-20_1430027",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.4b","Requirement","ECSS-U-ST-20_1430028",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.2.4c","Requirement","ECSS-U-ST-20_1430029",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3a","Requirement","ECSS-U-ST-20_1430030",1,"Created","Requirements in clause 5.3.2.2.3 shall be applied to the outbound leg of a Mars sample return mission.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3b","Requirement","ECSS-U-ST-20_1430031",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3c","Requirement","ECSS-U-ST-20_1430032",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3d","Requirement","ECSS-U-ST-20_1430033",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3e","Requirement","ECSS-U-ST-20_1430034",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.2.3f","Requirement","ECSS-U-ST-20_1430035",1,"Created","No unsterilised portion of the materials returned from Mars shall be released from containment unless approved by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.1a","Requirement","ECSS-U-ST-20_1430036",1,"Created","The probability of inadvertent contamination of a subsurface ocean by viable terrestrial organisms shall be ≤ 1 x 10-4 per mission.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.1b","Requirement","ECSS-U-ST-20_1430037",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.1c","Requirement","ECSS-U-ST-20_1430038",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.2.2a","Requirement","ECSS-U-ST-20_1430039",1,"Created","Requirements in clause 5.3.2.2.3, shall be applied to the outbound leg of a sample return mission.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.2.2b","Requirement","ECSS-U-ST-20_1430040",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.2.2c","Requirement","ECSS-U-ST-20_1430041",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.3.2.2d","Requirement","ECSS-U-ST-20_1430042",1,"Created","No unsterilised portion of the materials returned from Europa or Enceladus shall be released from containment unless approved by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.1a","Requirement","ECSS-U-ST-20_1430043",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.1b","Requirement","ECSS-U-ST-20_1430044",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.1c","Requirement","ECSS-U-ST-20_1430045",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.2.2a","Requirement","ECSS-U-ST-20_1430046",1,"Created","Category IVb requirements in clause 5.3.2.2.3, shall be applied to the outbound leg of a sample return mission.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.2.2b","Requirement","ECSS-U-ST-20_1430047",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.2.2c","Requirement","ECSS-U-ST-20_1430048",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.3.4.2.2d","Requirement","ECSS-U-ST-20_1430049",1,"Created","No unsterilised portion of the materials returned from Mars shall be released from containment unless approved by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.1a","Requirement","ECSS-U-ST-20_1430050",1,"Created","Requirements from clause 5 of ECSS-Q-ST-70-58 shall be applied for bioburden controlled environments.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2a","Requirement","ECSS-U-ST-20_1430051",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2b","Requirement","ECSS-U-ST-20_1430052",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2c","Requirement","ECSS-U-ST-20_1430054",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2d","Requirement","ECSS-U-ST-20_1430055",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2e","Requirement","ECSS-U-ST-20_1430056",1,"Created","The methods for calculation surface bioburden and bioburden densities shall be agreed with PPAA. \n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.2f","Requirement","ECSS-U-ST-20_1430057",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.3a","Requirement","ECSS-U-ST-20_1430058",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.4a","Requirement","ECSS-U-ST-20_1430059",1,"Created","Dry heat microbial reduction shall be performed in compliance with requirements from clause 5 of ECSS-Q-ST-70-57.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.4b","Requirement","ECSS-U-ST-20_1430060",1,"Created","Hydrogen peroxide microbial reduction shall be performed in compliance with requirements from clause 5 of ECSS-Q-ST-70-56.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.4c","Requirement","ECSS-U-ST-20_1430061",1,"Created","Use of other bioburden reduction procedures shall be approved by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.4.4d","Requirement","ECSS-U-ST-20_1430062",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.5a","Requirement","ECSS-U-ST-20_1430063",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.5b","Requirement","ECSS-U-ST-20_1430064",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.6a","Requirement","ECSS-U-ST-20_1430066",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.6b","Requirement","ECSS-U-ST-20_1430067",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.7a","Requirement","ECSS-U-ST-20_1430068",1,"Created","ECSS-Q-ST-10-09 shall be applied for nonconformances and waivers.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.7b","Requirement","ECSS-U-ST-20_1430069",1,"Created","All nonconformance related to planetary protection shall be specified as major nonconformance.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.7c","Requirement","ECSS-U-ST-20_1430070",1,"Created","The disposition of nonconformances related to planetary protection requirements shall be subject to approval by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","5.7d","Requirement","ECSS-U-ST-20_1430071",1,"Created","The approval of waivers related to planetary protection requirements shall be subject to approval by the PPAA.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","A.2.1a","Requirement","ECSS-U-ST-20_1430072",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","A.2.2a","Permission","ECSS-U-ST-20_1430073",1,"Created","The Mission description, specified in A.2.1a.1, may be covered by a reference to another project document.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","B.2.1a","Requirement","ECSS-U-ST-20_1430074",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","B.2.2a","Permission","ECSS-U-ST-20_1430075",1,"Created","The Mission description, as per B.2.1a.1. may be covered by a reference to another project document.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","B.2.2b","Permission","ECSS-U-ST-20_1430076",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","B.2.2c","Permission","ECSS-U-ST-20_1430077",1,"Created","The compliance matrix, as per B.2.1a.6. may be included in a project level compliance and verification matrix.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","B.2.2d","Permission","ECSS-U-ST-20_1430078",1,"Created","The Verification matrix as per B.2.1a.8. may be included in a project level compliance and verification matrix.\n"]
["ECSS-U-ST-20C","ECSS - Current v0.9","C.2.1a","Requirement","ECSS-U-ST-20_1430079",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","D.2.1a","Requirement","ECSS-U-ST-20_1430080",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","E.2.1a","Requirement","ECSS-U-ST-20_1430081",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","F.2.1a","Requirement","ECSS-U-ST-20_1430082",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","G.2.1a","Requirement","ECSS-U-ST-20_1430083",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","H.2.1a","Requirement","ECSS-U-ST-20_1430084",1,"Created","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"]
["ECSS-U-ST-20C","ECSS - Current v0.9","H.2.1b","Requirement","ECSS-U-ST-20_1430085",1,"Created","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"]
["ECSS-U-AS-10C Rev.1","ECSS - Current v0.9","3a","Requirement","ECSS-U-AS-10_1300003",2,"Normative Change","ISO 24113:2019, Space systems - Space debris mitigation requirements, Third edition 2019-07 shall apply with the modifications and clarifications listed in Table 3‑1."]