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Untitled - EMITS Invitation To Tender System

1. MS PA REQ 0710 Verification Traces EXM MS RS ESA 00002 PA SY 230 All major non conformances shall be notified to the Customer within 2 working days MS PA REQ 0720 Verification Traces EXM MS RS ESA 00002 PA SY 240 Accidents incidents shall be processed according to the non conformance control system and treated as major non conformance The reporting shall be done in accordance to ECSS Q 40B NR A16 paragraph 4 9 and Annex E Any non conformance affecting the NR 07 requirements shall be classified and reported major non conformance MS PA REQ 0730 Verification Traces EXM MS RS ESA 00002 PA SY 260 The NCRs numbering shall follow a project system as defined in the management requirement document EXM MS RS ESA 00012 Para 2 1 2 For planned departure from requirement the subcontractors and suppliers shall submit a request for deviation as required in ECSS M 40B para 5 3 2 6 For unplanned departure from requirement the subcontractors and suppliers shall issue an NCR major When the NCR disposition is use as is or repair the NRB will assess the necessity of RFW issuing in accordance to ECSS Q 20 09B para 5 5 4 Subcontractors shall include subcontractor and suppliers NCR RFW RFD tracking lists in regular PA status reports Suppliers shall include supplier and products NCR RFW RFD tracking lists in regular PA status reports THALES ve All rights reserved 2007 Thales Alenia Space
2. MS PA REQ 2720 Verification Traces High reliability and safety shall be provided for pyrotechnic devices by the use of approved practices including the shielding of all leads and electronics MS PA REQ 2730 Verification Traces All pyrotechnics shall be initiated via spacecraft dedicated interfaces All pyrotechnics commanding path shall incorporate the required safety inhibits THALES REH All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 2740 Verification Traces Any pyrotechnic actuation separation system shall be self contained before and after operation i e no released components or debris are allowed 6 6 Failure tolerance MS PA REQ 2750 Verification Traces Failure tolerance is a basic safety requirement that shall be used to control hazards The failure tolerance requirements are defined in Para 5 3 2 Failure Tolerance of these Product Assurance Requirements MS PA REQ 2760 Verification Traces Multiple failures which result from common cause or common failure mechanisms shall be considered as single failures for determining failure tolerance MS PA REQ 2770 Verification Traces Alternate or redundant safety critical functions shall be physically and functionally separated o
3. No MIL spec applicable ESCC 3004 Level C MIL PRF 23269 FRL R MIL PRF 23269 FRLR _ ESCC 3007 Level C MIL PRF 87164 FRL R ESCC 3006 Level C MIL PRF 83421 FRL R ESCC 3006 Level C REFERENCE DATE ISSUE Applicable Screening Note Requirements Note 1 1 1 7 5 ESCC 3006 Level C MIL PRF 19978 FRL R CSI and DPA requirements 21 01 2011 05 EXM MS RQM AI 0004 PAGE Precap Final DPA Note 2 Notes 2 3 Note 4 Note 23 x lt x lt x lt x lt x lt x lt Number of unit Note 3x3 17 3X3 17 3X3 17 3X3 17 3X3 17 THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION M032 EN 100181547K EN CONTROLLED DISTRIBUTION gt REFERENCE EXM MS RQM AI 0004 la ThalesAler DATE 21 01 2011 Space ISSUE 05 PAGE CSI and DPA requirements Ref Part Family Applicable Screening Note Precap Final Number of unit Requirements Note 1 Note 2 Notes 2 3 Note 4 Note Note 23 21 Resistors Fixed wire wound accurate RBR E type 22 Resistors Fixed RWR type Wire wound power type MIL PRF 39009 FRL R chassismounted RER type 24 Resistors Fixed ESCC 4001 Level C ENEE ER Film insulated RLR type 25 Resistors Fixed high precision film RNC type except RNC 90 26 Resistors Fixed 3X3 high precision film RNC 90 X 17 type 27 Resistors TC precision SS
4. Nuclear Safety Authority The RHU units are an ESA NASA furnished equipment for the ExoMars mission The Nuclear Safety Authority is responsible for checking that all the nuclear activities of a space project related to a space vehicle with nuclear sources on board are in conformance with the relevant THALES DEE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE regulations and providing the associated authorizations MS PA REQ 2420 Verification Traces The main contractors in charge of the design of main elements containing the RHU e g Rover Module shall appoint a Nuclear Safety Representative This function shall be in charge of assessing engineering design compatibility with the safety requirements this task is different from the RHU integration activities MS PA REQ 2430 Verification Traces The contractors shall provide adequate expertise available to support the engineering function with respect to the peculiar nuclear safety needs The composition of the industrial teams shall give evidence accordingly and provide CV s of dedicated team members C This requirement should be able to be met by a team member with functional competence but not necessarily dedicated entirely to this task MS PA REQ 2440 Verification Trac
5. CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE 4 5 1 Failure analysis MS PA REQ 0740 Verification Traces Failure analysis which may be destructive and other investigations shall be performed on the nonconforming items only when and as required by the NRB 4 6 Waivers MS PA REQ 0750 Verification Traces In adition to ECSS Q 20B para 5 6 9 Waiver submittal shall be done by electronic mean as reference and also in paper MS PA REQ 0760 Verification Traces EXM MS RS ESA 00002 PA SY 280 The RFWs numbering shall follow a project system as defined in the management requirement document EXM MS RS ESA 00012 Para 2 1 2 4 7 Alert System MS PA REQ 0770 Verification Traces EXM MS RS ESA 00002 PA SY 320 This chapter supersedes clause 5 7 of ECSS Q 20B CPPA as well as users shall participate to the ESA alert system and screen alerts and problem notification as a day by day activity of the component control plan For self procured components the user is responsible to perform the tasks described in these paragraphs The applicable ESA alert procedure is available on line http alerts esa int THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Ale
6. The subcontractors shall prepare an Audit Plan in line with DRD PA 2 of ExoMars PA 2 DRL DRD covering external and in house audits and provide it to TAS ESA for review and approval MS PA REQ 0470 Verification Traces More specifically audits shall be performed to assess the overall capability to perform the necessary tasks required for the ExoMars project if sufficient or satisfying audit data is not available MS PA REQ 0480 Verification Traces The first priority for audits shall be new suppliers and suppliers using new technologies Audit shall be performed by the subcontractors using a check list MS PA REQ 0490 Verification Traces EXM MS RS ESA 00002 PA SY 170 It is responsibility of the authority that will perform the audit to prepare the check list and present it to TAS ESA with the audit notification at the latest for approval At the end of the audit the subcontractors shall prepare the audit report to be submitted to TAS ESA within two weeks MS PA REQ 0500 Verification Traces EXM MS RS ESA 00002 PA SY 180 The report shall include identification of areas of non compliance or weakness corrective actions with due dates conclusions with statement on the acceptability to proceed with the activities and the completed audit checklist THALES ema All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE
7. All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 4 175 Para 5 4 8 Part derating analysis Req PA SY 680 text from req PA SY 1320 added Para 5 4 11Hazardous commands identification PA SY 720 update categories and add link to DRD PA 19 Para5 5 Inputs to Critical items list CIL PA SY 730 SPF definition for CI list clarified Para 5 6 Dependability Testing PA SY 740 modified to address applicability of Q 30 chapter 9 Para 5 7 Failure Propagation PA SY 750 760 Failure propagation requirement reworded and NOTE added Para 6 SAFETY 6 1 General PA SY 770 780 PA SY 870 moved added CSG safety reqs references removed added pointer to Launch site reqs Removed Proton references Para 6 1 PA SY 870 editorials Para 6 2 Safety Management and Planning PA SY 890 Nuclear safety authority editorials Nuclear safety authority Section updated removed references to GEP Lander Para 6 3 Hazard Severity Categories PA SY 960 970 Updated safety severity categories table to be in line with Q 40 table added Para 6 3 PA SY 980 revised Para 6 4 Hazard Analysis Residual Hazards PA SY 1000 editorials Para 6 5 Safety engineering editorials Para 7 EEE COMPONENTS Paragraphs completely updated Main Modification due to 1 IPDR RIDs implementation for B2X closure RID AP 84 RID
8. INR A28 ECSS Q ST 70 20C Determination of the susceptibility of silver plated copper wire and cable to red plague corrosion NR A29 ECSS Q ST 70 22C The control of limited shelf life materials INR A30 Deleted THALES cade All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE INR 015 Moved as IR NR A31 ECSS Q ST 70 22C The control of limited shelf life materials NR A32 ECSS Q ST 70 28C The repair and modification of printed circuit board assemblies for space use INR A33 ECSS Q ST 70 30C Wire wrapping of high reliability electrical connections INR A34 Deleted INR A35 Deleted INR A35 Deleted NR A36 ECSS Q ST 70 36C Material selection for controlling stress corrosion cracking NR A37 ECSS Q ST 70 37C Determination of the susceptibility of metals to stress corrosion cracking NR A38 ECSS Q ST 70 45C Standard methods for mechanical testing of metallic materials INR A39 ECSS Q ST 70 46C Requirements for manufacturing and procurement of threaded fasteners NR A40 ECSS Q 70 71A rev1 Data for selection of space materials and processes INR A99 ECSS Q ST 70 06C The particle and ultraviolet UV radiation testing of space materials INR A100 ECSS
9. identified e Equipment developed built and qualified for other space projects under PA requirements equivalent to the ones of this document equipment S S equipment may be used for flight applications e Equipment developed and built for commercial aviation or military applications equipment CAM CAM equipment may be used for non flight applications MS PA REQ 4760 Verification Traces EXM MS RS ESA 00002 PA SY 2260 The use of OTS equipment shall not lead to the violation of any applicable safety requirement MS PA REQ 4770 Verification Traces EXM MS RS ESA 00002 PA SY 2270 System level reliability and safety analyses e g the FMEA shall consider also OTS equipment failures Candidate OTS equipment shall be reviewed by an Equipment Suitability Board chaired by a customer representative and including the PA function It shall ensure that the proposed OTS meet the environmental and PA requirements MS PA REQ 4780 Verification Traces EXM MS RS ESA 00002 PA SY 2280 Following the review the board shall issue an assessment and justification report The Report shall contain as a minimum e ExoMars Technical specification identifying the ExoMars requirements e Justification file clearly identifying any non compliance between the ExoMars requirements and the actual characteristics performances of the item e Delta activities program describing all necessary tasks to be perfor
10. mechanical bond strength and environmental seal The open end of the wire shall not be exposed to the etchant 8 6 Bioburden control MS PA REQ 4400 Verification Traces EXM MS RS ESA 00002 PA SY 1760 Hardware compatibility with bioburden control procedures as defined in the Planetary protection requirements EXM MS RS ESA 00005 NR 26 shall be demonstrated Output The requirement shall be fulfilled through the deliverables PA 27 and PA 28 8 7 Bioburden Reduction Deleted Deleted Deleted MS PA REQ 4410 Verification Traces EXM MS RS ESA 00002 PA SY 1800 The bioburdan reduction process on assemblies and the impact of bioburden reduction on long duration effects e g during storage and flight shall be demonstrated on critical hardware e g parachute airbags THALES KEE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 We Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Output PA 32 Data for compatibility with processes for bioburden reduction 8 8 Vacuum MS PA REQ 4420 Verification Traces EXM MS RS ESA 00002 PA SY 1810 The acceptance criteria for materials used for space applications vacuum compatibility is also applicable to GSE to be installed in the chamber shall be compliant with ECSS Q ST 70 02 with the addition of the following MS PA REQ 4430 Verificat
11. As well as the RVT reports shall be delivered to users In case of drift failures anomalies occurring during RVT SEE test TD characterization test major NCR shall be issued Users approval of any NRB dispositions is in this case mandatory MS PA REQ 3280 Verification Traces In case of consistent self procurement user shall organize a radiation review at Preliminary Design Review time frame PDR in order to address the following points e To review total dose test reports in order to validate the subcontractor radiation database These data will be used for equipment circuit WCA e To determine part types that shall be submitted to a characterization and or a RVT selected parameters to be measured and to review radiation test plan for such parts e To review proposed packaging design approach to achieve maximum inherent shielding To review preliminary shielding analysis e To review preliminary circuit design analysis e To review SEU parts data in order to validate the subcontractor radiation database These data will be used for equipment SEU effects analysis e To determine part types that shall be submitted to a Single Event Upset testing and to review radiation test plan for such parts MS PA REQ 3290 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 0
12. EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 0510 Verification Traces EXM MS RS ESA 00002 PA SY 160 Audits shall be notified to TAS ESA 10 working days in advance TAS ESA reserve the right to participate to the audits and to request additional audits performing Assembly and test facilities which may be used for the ExoMars project shall be certified to ECSS Q 20 07 or verified to be able to meet the project need 4 3 1 Audits Addition to ECSS Q 20B para 4 6 MS PA REQ 0520 Verification Traces EXM MS RS ESA 00002 PA SY 150 The Subcontractor shall establish an Audit plan covering external and in house audits linked to the Risk Management programme Thus new processes shall be audited Critical items will be audited on a case by case basis pending the risk management Auditing may be required by the customer Thus the audit planning shall also evolve with the risk monitoring 4 4 Critical Items Control MS PA REQ 0530 Verification Traces The ECSS Q 20B is applicable with modifications as per the following paragraphs ECSS Q 00 para 3 3 56 ECSS Q 20B para 4 8 and ECSS Q 30B para 8 4 shall apply with the following supplement MS PA REQ 0540 Verification Traces EXM MS RS ESA 00002 PA SY 190 Subcontractors and suppliers shall establish and maintain an integrated Critical Items Control Program in line with ECSS Q 20 04A The Cri
13. The subcontractor shall perform for each product under its responsibility a safety assessment report in line with the safety analysis MS PA REQ 2870 Verification Traces After compliance assessment the subcontractor shall deliver a formal liability Declaration of Conformity mentioning the legal data asserted by the EU directives THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 7 EEE COMPONENTS 7 1 General MS PA REQ 2880 Verification Traces EXM MS RS ESA 00002 PA SY 1040 The ECSS Q ST 60 NR 089 applies with the amendments specified here below The requirements of ECSS Q ST 60 NR 089 for Class 2 components para 5 and Table 7 2 Quality levels for Class 2 components quality level ESCC and MIL shall apply in the Exomars project unless explicitly tailored or modified in the next paragraphs The quality level others shall not be applied for ExoMars In the event of conflict in requirements this document shall prevail MS PA REQ 2890 Verification Traces EXM MS RS ESA 00002 PA SY 1050 The requirements reported in this section apply to any EEE parts used in flight hardware or to parts which come in direct contact with flight hardware For Engineering and or engineering qualification standard hardware the paragraph
14. severity categories Para 5 3 2 1 Reintroduced failure tolerance requirements description for System Level failure effects Para 5 3 2 2 Added sentence which points to other system design requirements documents for possible additional specific requirements Para 5 3 3 PA SY 550 added reference to Rover Requirements in addition to the already specified Mission amp System Requirements 6 SAFETY 6 1 General PA SY 840 Deleted 7 EEE SECTION 10 05 10 Para 7 1 reference to normative document updated Reference to other paragraphs updated Para 7 2 1 reference to PA SY 1130 deleted Para 7 2 2 reference to PA SY 1100 changed to PA SY 1130 Para 7 4 1 reference changed to new issue ECSS Q ST 70 08C Para7 3 reference DCL format Para7 4 1 1 reference to PA SY 1200 deleted Reference to normative document updated Para 7 4 2 2 reference to PA SY 1280 and PA SY 1310 splitted Multiple reference to PA SY 1250 corrected Reference to PA SY 1300 moved in the paragraph to remove multiple reference Para 7 4 4 multiple reference to PA SY 1370 corrected Reference to normative document updated Para 7 4 6 reference to normative document updated Para 7 4 6 1 reference to normative document updated Para 7 4 6 2 reference to normative document updated Para 7 4 6 3 reference to normative document updated Para 7 4 6 4 reference to PA SY 1580 deleted Para 7 4 7 reference to PA SY 1430 and PA SY 1440 corrected Reference to normative docum
15. subsystem equipment and unit level MS PA REQ 2050 Verification Traces The analysis details e g failure rates mathematical models assumptions shall be provided THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 ser Space ISSUE 05 PAGE MS PA REQ 2060 Verification Traces Reliability calculations shall take into account the possible exposure of all components to the environment chemical thermal radiation etc as defined by the applicable environmental cleanliness and planetary protection requirements MS PA REQ 2070 Verification Traces MIL HDBK 217F notice 2 taking into account the appropriate quality levels shall be used preferably as the failure rate database The part stress prediction method shall be used Where components are not covered by MIL HDBK 217F notice 2 individual failure rates shall be agreed with the Prime ESA MS PA REQ 2080 Verification Traces Mechanical parts shall be addressed in the reliability prediction and the reliability data sources shall be provided 5 4 7 Worst Case Analysis MS PA REQ 2090 Verification Traces EXM MS RS ESA 00002 PA SY 660 ECSS Q 30 Clause 8 2 2 h applies MS PA REQ 2100 Verification Traces EXM MS RS ESA 00002 PA SY 670 Miss
16. taken on a case by case basis evaluating the criticality and the peculiarity of each application in the frame of SRR of the relevant unit The development of any new ASIC or FPGA shall be considered a critical item and thus its development shall be followed by tracking H in the user CIL The FPGA ASIC reviews both public and internal as required in the ECSS Q ST 60 02 shall be thoroughly planned and reported in the general schedule of the relevant unit For any ASIC FPGA design developed in the frame of the project the user and developer is required to make public the following reviews e Preliminary Design Review PDR shall be organised as described in ECSS Q ST 60 02 Explicit TAS ESA approval needs to be obtained to proceed further from the PDR of the ASIC or FPGA e Qualification Review Acceptance review QR AR shall be organised as required in ECSS Q ST 60 02 this review shall result in the final acceptance of the design and release for FM production concluding the design validation At the end of this review the FPGA specification or Altered Item Drawing shall be frozen Explicit TAS ESA approval needs to be obtained MS PA REQ 3540 Verification Traces EXM MS RS ESA 00002 PA SY 1560 In any case TAS and ESA reserve the right of access to all ASIC FPGA documentation file as required by ECSS Q ST 60 02 MS PA REQ 3550 Verification Traces EXM MS RS ESA 00002 PA SY 1600 For testing verification trouble shouting a
17. transportation and launch MS PA REQ 2300 Verification Traces The Launch Site and Launcher safety requirements and regulations are fully applicable and must be considered as design drivers for the complete spacecraft system spares GSE and all activities at Launch site MS PA REQ 2310 Verification Traces The Subcontractor is responsible to ensure the safety of his products The safety programme relates to flight hardware and associated Ground Support Equipment is under the responsibility of the subcontractor MS PA REQ 2320 Verification Traces EXM MS RS ESA 00002 PA SY 810 The Subcontractor and Supplier shall identify and plan all activities required to obtain approval from the launch authority THALES BEER All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 2330 Verification Traces EXM MS RS ESA 00002 PA SY 820 The Subcontractor and Supplier shall deliver the documentation requested by the launch authority MS PA REQ 2340 Verification Traces EXM MS RS ESA 00002 PA SY 830 The Subcontractor and Supplier shall submit all required safety data package to TAS ESA and he is responsible for the correct implementation of the safety requirements towards TAS ESA In addition he shall support ESA in all acti
18. 2011 SE Space ISSUE 05 PAGE 3 PRODUCT ASSURANCE REQUIREMENTS MS PA REQ 0010 Verification Traces A Product Assurance Program shall be implemented for the EXOMARS project which is properly planned and executed with sufficient authority and expertise with emphasis being placed on the optimization of design safety aspects timely prevention of deficiencies and verification of the adequate quality of the products and services to be supplied The spacecraft design and operation regime shall be developed in compliance with these requirements which are applicable to the Sub contractors and suppliers It is the responsibility of the contractor to allocate these requirements to sub contractors and suppliers and to ensure their implementation It is emphasized that a policy of Prevention rather than Cure shall apply MS PA REQ 0020 Verification Traces EXM MS RS ESA 00002 PA SY 10 The prime objective of the Contractors PA programme shall be to ensure that their own product and activity inside the ExoMars Programme will accomplish its intended objectives successfully This shall be achieved in the most cost effective way 3 1 Organisation and Management MS PA REQ 0030 Verification MOD A T RoD S S S A T RoD S EQP A T RoD S Traces EXM MS RS ESA 00002 PA SY 20 The Subcontractor shall implement a PA programme The Product Assurance program to be carried out by the subcontractors and
19. 2011 een Space ISSUE 05 PAGE 7 5 8 Electrical and Qualification Model EM EQM MS PA REQ 4190 Verification Traces EXM MS RS ESA 00002 PA SY 1060 The EEE parts procurement for EM and EQM is responsibility of the User For EM standard hardware the EEE parts shall be selected to be form fit and function representative of the FM components Additionally if thermal vacuum test are envisaged for the EM for use in so called EQM for example the EEE parts used in it shall be made of the same materials finish and processes as the flight equivalent part different screening levels can be considered In addition to the above requirement parts to be used in models intended for qualification purpose EQM will preferably have the same manufacturer as the parts to be used in PFM and FM The components selected for EQM shall be hermetic sealed and compatible to dry heat sterilization process if EQM will be used to qualify the planetary protection compatibility plastic packages shall be avoided and shall meet the extended temperature range as a minimum from 55 C to 125 C or compatible to dry heat sterilization temperature if requested The FPGA used in EM EQM shall be necessarily from the same manufacturer with the guarantee to be fit form and function representative possibly with the same chip as the parts intended for flight The P N of the FPGA to be used in EM EQM shall be listed in the user DCL relevant to FM properly rema
20. 5 working days after receiving the Alert assessement feedback notification THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION M032 EN 100181547K EN W s Th alesAlenia ev SPACE 12 4 Class acronyms CONTROLLED DISTRIBUTION REFERENCE DATE ISSUE EXM MS RQM AI 0004 21 01 2011 05 PAGE Class A approval R review information THALES MOSSEN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN ThalesAlenia Space CONTROLLED DISTRIBUTION REFERENCE DATE ISSUE END OF DOCUMENT THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION EXM MS RQM AI 0004 21 01 2011 05 PAGE M032 EN 100181547K EN
21. Cleanrooms and associated controlled environments Part 1 Classification of air cleanliness INR 116 Moved as IR NR TBD ECSS Q ST 70 31C Application of Paints and Coating on Space Hardware THALES Dee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE INR 015 Moved as IR NR 128 JPL D 64939 Launch Service Requirement Document NR 129 AFSCPSMAN 91 710 V3 Air Force Space Command Manual Vol 3 01 07 2004 NR 130 NASA STD 8719 9 Standard for Lifting devices and Equipment w Change 1 NR 131 10 CFR Part 71 amp 49 CFR Parts 171 178 Transportation of radioactive material 2 2 Informative Documents 2 2 1 Definition of Informative Documents Informative References are applicable to this document only when specifically called up in the text with specific indications of the parts of the document that are to be applicable Otherwise the documents are listed below for information only as an aid for the purpose of understanding For dated references subsequent amendments to or revisions of any of these document apply to this list only when incorporated in it by amendment or revision For undated references the latest signed version is applicable and must be incorporated by the contractor in the project baseline 2 2 2 Thales Alenia Space Italia I
22. DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE 11 PA REQUIREMENT FOR GSE MS PA REQ 4850 Verification Traces This chapter gives clarification about the requirements dedicated to GSE 11 1 PA Management MS PA REQ 4860 Verification Traces The Subcontractor shall implement a PA programme The Product Assurance program to be carried out by the subcontractors and suppliers shall be in accordance with ECSS Q 00A and shall include the disciplines of Quality Assurance Software Product Assurance Safety Assurance Dependability Component Quality Selection and Procurement Materials Parts and Process Selection and Control Configuration management Control and Acceptance Activities ref para 3 and 4 of this document 11 1 1 Reviews MS PA REQ 4870 Verification Traces As per para 3 and 4 of this document 11 1 2 Design and Manufacture MS PA REQ 4880 Verification Traces Appropriate quality requirements and procedures shall be established and achieved through the design procurement fabrication assembly inspection testing packing and storing phases of the contract THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05
23. DPA shall be performed and described in the relevant PAD MS PA REQ 3480 Verification Traces EXM MS RS ESA 00002 PA SY 1530 e DPA requirements shall be implemented as found in ECSS Q ST 60 NR 089 paragraph 4 3 9 with the modifications of paragraph 4 3 9 b detailed in table 1 The DPA shall be performed on three pieces per lot any deviation on the above rule shall be agreed via PAD approval process MS PA REQ 3490 Verification Traces Post programming conditioning sequence in user programmable devices like anti fuse technology PROM shall be specified and approved on a case by case basis in the relevant PAD in case of coordinated procurement user shall produce post programming conditioning flow to EXO PCB for review and approval THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE 7 4 6 2 HYBRIDS MS PA REQ 3500 Verification Traces Hybrids shall be manufactured in a validated hybrid line qualified and screened in accordance with ESA PSS 01 608 level B or MIL PRF 38534 Class K or ECSS Q ST 60 05 or alternative document approved by TAS ESA The qualification of the die mounting shall be performed by the hybrid manufacturer in order to validate and demonstrate the compatibility between the micro component and the hybrid manufa
24. ECSS Q 00A para 3 5 3 MS PA REQ 0120 Verification Traces EXM MS RS ESA 00002 PA SY 100 PA progress reporting shall be part of the overall project progress reporting and shall include as a minimum e Status of the PA activities since the last progress report separated for the different disciplines eg QA Dependability Safety EEE components Materials amp Processes Software PA e outline of lower tier subcontractors status e alert status e non conformances status e request for Deviation waiver status e critical items status e explanation of performed activities e planned accomplishments in next reporting period e identified problems amp risk factors e activities planned to control identified problems amp risk factors THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Risk management technical highlighting problems which may affect the customer requirements Accomplishments during the reporting period Planned accomplishments in the next reporting period Identified problems which may affect customer requirements schedule and cost Alerts assessment and status report Accidents incidents 3 3 Product Assurance Plan MS PA REQ 0130 Verification Traces The subcontractors shall provide a ExoMars Product Assurance Pl
25. In case a time critical hazard that may affect mission objectives is detected from which autonomous recovery and continuation of nominal operation is not possible the affected unit shall be configured into a safe mode when feasible to await Ground Control intervention MS PA REQ 1780 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE The management of anomalies within a unit subsystem or instrument shall be handled in a hierarchical manner such that resolution is sought on the lowest level possible MS PA REQ 1790 Verification Traces The fault management functions at all levels shall be able to carry out consistency verification checks on redundant sensor readings whenever redundancy is available before starting the recovery actions MS PA REQ 1800 Verification Traces Any automatic reconfiguration shall only be made from Prime to Redundant and not reverse MS PA REQ 1810 Verification Traces The implementation of any autonomous action shall avoid switching back and forth between unhealthy units MS PA REQ 1820 Verification Traces Switch over to redundant units shall be possible without affecting unrelated units MS PA REQ 1830 Verification Traces It
26. MIP KIP programme TAS ESA shall have the right to select its MIP KIPs from the Contractors MIP KIP list TAS ESA may THALES Ge All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE elect to add to the Contractor proposed MIP KIPs if so necessary TAS ESA shall be notified by formal communication of the actual date for planned MIP KIP events e A MIP shall require invitation at least 10 working days before the event and participation of TAS ESA or its written agreement to proceed without TAS ESA participation e A KIP shall require the same invitation but the notified activity may be performed as scheduled if there is no reaction from TAS ESA MS PA REQ 1170 Verification Traces The notification shall contain as a minimum e Item identification e Reference to the MIP KIP List e Supplier and location of inspection activity contact personal e Planned date and duration e Any proposal change to the event as identified in the MIP KIP list 4 16 Electrostatic Discharge Control MS PA REQ 1180 Verification Traces Electrostatic Discharge ESD Control has to be implemented for manufacturing storage inspection assembly and test activities under Subcontractor and Supplier responsibility MS PA REQ 1190 Verification Traces The ESD Control will
27. PA SY 420 The subcontractors and suppliers shall ensure that test facilities are suitably qualified to perform the tests to be conducted and do not cause any degradation to the test article or its interface This compliance shall be confirmed during the test readiness reviews TRR 4 9 1 Test Performance Monitoring This chapter is a supplement of clause 9 4 of ECSS Q 20 which is also applicable If a test has a hazard potential with consequence severity of category critical or catastrophic the test procedure shall highlight the nature of the hazard and the hazard controls and safety devices shall be specified at the relevant operational steps Test procedures shall be signed by subcontractors or suppliers PA function 4 10 Test Reports This chapter is a supplement to clause 9 3 2 of ECSS Q 20B which is also applicable Each test report shall contain a conclusion stating the actual achievement of test objectives and shall identify any specific deficiencies Test Reports shall include reference to NCRs relevant for the test subject of the test report 4 11 End item Data package EIDP MS PA REQ 0920 Verification Traces This chapter complements clause 10 2 of ECSS Q 20B MS PA REQ 0930 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011
28. Q ST 70 38C High reliability soldering for surface mount and mixed technology printed circuit boards NR 56 ISO 14644 1 Cleanrooms and associated controlled environments Part 1 Classification of air cleanliness NR 57 ISO 14644 2 Cleanrooms and associated controlled environments Part 2 Specification for testing and monitoring to prove continued compliance with ISO 14644 1 NR 58 MSFC SPEC 250 Protective Finishes For Space Vehicle Structures and Associated Flight Equipment General Specification NR A42 ECSS Q 80B Software Product Assurance INR 084 ECSS Standard Space Project Management Configuration and Information Management ECSS M ST 40C NR 050 EXM MS RS ESA 00027 ExoMars Tailoring of ECSS E40 Software Part 1B NR A47 EXM MS RS ESA 00029 ExoMars Tailoring of ECSS E40 Software Part 2B NR 03 Moved as IR NR 01 Moved as IR NR 65 NASA STD 6001 Flammability Odor Offgassing and Compatibility Requirements and Test Procedures for Materials in Environments that support Combustions NR 66 MIL QML 19500 Semiconductor Devices NR 67 MIL QML 38534 Hybrid Microcircuits NR 68 MIL QML 38535 Integrated Circuits Microcircuits Manufacturing INR A101 ECSS 9000 Integrated Circuits Monolithic hermetically sealed NR 70 MIL HDBK 5 Metallic materials and elements for aerospace vehicle structures NR 71 TBD KSC ELV Payload Safety TBD NR 097 ECSS Q ST 60 14C Relifing Procedure EEE Components NR 103 ISO 14644 1
29. RS ESA 00013 ExoMars Mission Environmental Specification NR A09 ECSS P 001A Glossary of Terms INR A10 ECSS Q 00A Policy and principles NR A12 ECSS Q 20B Quality Assurance NR A11 ECSS Q 20 04A Critical Item control NR A95 ECSS Q 20 07A Quality Assurance for test centres THALES eee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE INR 015 Moved as IR NR 085 ECSS Q 20 09B Non Conformance control system NR A14 ECSS Q 30B Dependability NR A13 ECSS Q 30 02A Failure Modes Effects and Criticality Analysis NR 092 ECSS Q ST 30 11C Derating EEE Parts NR A16 ECSS Q 40B Safety INR A43 Deleted INR A44 Deleted INR A45 Deleted INR A46 Deleted NR A96 RNC CNES R 15 CSG Nuclear Safety requirements NR A08 ECSS M 00 03B Risk Management NR 089 ECSS Q ST 60C EEE Components NR 093 ECSS Q ST 60 02C ASIC and FPGA development NR 095 ECSS Q ST 60 05C Generic Requirements for Microcircuit NR A97 ECSS Q ST 60 12C Design Selection procurement and use of die form monolithic microwave integrated circuits MMICs INR 098 PSS 01 605 The capability approval programme for thin film microcircuits INR 099 PSS 01 606 The capabil
30. Rev C 47Bis Transformers Non ESCC 3201 Level C molded 1 Minimum screening requirements may be used as guidelines variations implemented by high reliability manufacturers and documented are allowed pending a PAD approval 2 For qualified Military class level B parts class Q parts class K parts JANTXV parts QPL listed ER MIL passive parts QPL listed Military specifications passive parts and ESCC qualified parts as defined in table 1 including the required quality level the customer source inspections precap and final source inspections are not required The exceptions are identified by XX in table 1 3 Final source inspection of delivery lots will be conducted before shipment to ensure conformance with requirements of the POs procurement specification s and data requirements This source inspection shall include final acceptance test witnessing as required It may be replaced by incoming inspection under EXO PCB approval 50 Cables Wires Low Frequency THALES ema All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 ait Tha les Aleria DATE 21 01 2011 Space ISSUE 05 PAGE 4 DPA shall not be required for qualified Military class level B parts class Q parts class K parts JANTXV parts QPL listed ER MIL passive parts QPL listed Military specifications passive parts and ESCC qualified parts as defined in table 1
31. Traces Redundant function housed in a common box shall be separated by continuous metallic wall acting as heat sink and EMC shield Failure detection isolation recovery MS PA REQ 1650 Verification Traces Each equipment assembly subsystem shall provide on board failure detection capabilities MS PA REQ 1660 Verification Traces The anomaly detection system must ensure that only valid information is used MS PA REQ 1670 Verification Traces Autonomous failure detection and recovery shall not be based on a single sensor readout THALES er All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1680 Verification Traces All mission and safety critical functions shall be monitored by independent parameters MS PA REQ 1690 Verification Traces Anomaly detection shall be confirmed by using more than one sample of the same measurement MS PA REQ 1700 Verification Traces Spurious anomaly detection false alarm shall be avoided MS PA REQ 1710 Verification Traces Trigger limits shall have adequate and quantified margins MS PA REQ 1720 Verification Traces Trigger limits shall be adjustable on ground and in flight Limits which are not adjustable o
32. Unit CDR Final approval of as BUILT at DRB To be updated also in support of System Reviews At equipment DRB the DCL shall reflect the as built configuration including D C of components For proposal special attention shall be paid to LLIs PA 23 PA Radiation Hardness Assurance A as part of PA 01 23 Plan PA 24 PA Radiation Analysis x x x AR Final approval at 24 Subsystem Unit CDR and QR PA 25 PA Parts Application Analysis DELETED 25 Parts Stress Analysis covered by PA 14 PA 26 PA Part Approval Document PAD As A Final approval at 26 generated equipment CDR PA 27 PA Element Subsystem Unit Level x x D A Form excel 27 Declared Materials List DML provided by TAS PA 28 PA Element Subsystem Unit Level x x x A It can bea 28 Declared Mechanical Part List separate section DMPL of DML PA 29 PA Element Subsystem Unit x x D A Form excel 29 Declared Processes List DPL provided by TAS I PA 30 PA Material and Processes Control DELETED 30 Board PA 31 PA Process witness materials DELETED THALES eer All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION e REFERENCE EXM MS RQM AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE Item Numb DRD Title Submital Proposal PDR MRR CDR QR DRB Class Remark Re
33. an Analysis might be considered necessary for the project during the design and development phase MS PA REQ 2180 Verification Traces The availability activities shall consider also the Ground Segment of ExoMars and related GSE tools models needed for the successful completion of the mission 5 4 11 Hazardous commands identification MS PA REQ 2190 Verification Traces EXM MS RS ESA 00002 PA SY 720 The Subcontractor and Supplier shall identify any command or command sequence that can cause consequences THALES KORE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE of the safety severity category 1 catastrophic or dependability severity category 1 or cause damage to flight hardware if issued inadvertently or not issued when required out of sequence commanding The identified hazardous commands shall be reflected in the Hazard Analysis DRD PA 19 5 5 Inputs to Critical items list CIL MS PA REQ 2200 Verification Traces EXM MS RS ESA 00002 PA SY 730 ECSS Q 30 Para 8 4 Critical items list applies with the following modifications Clause 8 4 2 shall be read As minimum Single Point Failure items of the hazard severity category 1 and 2 catastrophic critical and dependability severity level 1 and 2 shall
34. and users will be invited as necessity The EXO PCB members have the following tasks e To manage and control the part procurement program at all levels THALES Veer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE e To implement the Parts Approval cycle through PAD approval including review of part manufacturer evaluation qualification plan and test reports if applicable status of qualification approval of procurement specifications quality and lot acceptance levels and procurement inspections DPA radiation sensitivity assessment e To review the procurement status and to identify risks like U S parts under Export license restrictions ITAR e To assess parts technical issues such as Non conformances Waivers Deviations and alerts PCBs will be held as a minimum until the approval of all parts has been finalized and the procurement of most critical items successful concluded 7 2 2 User tasks in EXO PCB MS PA REQ 2940 Verification Traces EXM MS RS ESA 00002 PA SY 1 130 Subcontractors called users in this context shall propose through DCL the procurement approach for each item clearly defining the relevant need dates for EXO PCB approval As general approach co ordinated procurement shall be the preferred approach Users shall procure as much as possible throug
35. be supported by e the requirements and associated rules description the verification methods and periodicity periodic audits failed parts record and destructive physical analyses as necessary e e e e Personnel training THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 5 DEPENDABILITY 5 1 Dependability Assurance MS PA REQ 1200 Verification Traces The contractor shall analyse the product to verify compliance with the dependability and Safety requirements The contractor shall reduce and control all dependability and safety risks that lead to the non conformance to dependability and safety requirements The contractor shall provide identification of undesirable events leading to the loss or degradation of product performances together with their classification into categories related to the severity of their consequences The contractor shall investigate the possible scenarios leading to the occurrence of undesirable events and shall identify related failure modes failure origins and causes detailed failure effects The contractor shall identify hazards related to the production assembly handling operation of the hardware and software system under his responsibility and shall implement means of reducing and controlling the hazar
36. by means of appropriate prediction tools PROFIT SIMPA The applicable LET spectra curve is reported in the ESA ExoMars mission environmental specification EXM MS ESA RS 00013 The relevant SEE criticality ana ysis shall be included in the Radiation Analysis or in the FMECA for the system impact assessment MS PA REQ 3200 Verification Traces EXM MS RS ESA 00002 PA SY 1310 In principle parts showing a LET threshold lower than 3 7MeV cm mg shall not be used If it is used the radiation hardness section of the relevant PAD shall in this case report exaustively the reference to applicable test report and test method and condition and summary of test results THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 er SDOCE ISSUE 05 PAGE MS PA REQ 3210 Verification Traces For SET sensitivity the following requirement apply the subcontractor will perform a SET effect analysis in order to determine the effect of SET on equipment performance The table provided here below can be used as reference of worst case pulse amplitudes and duration in case non reliable test data and or equivalent table based on subcontractors specific experience are available OP amps AV max Voc amp Atmax 15US Comparators AV max Voc amp Atmax 10uUs Voltage Reg AV m
37. flight hardware software The requirements defined here are applicable to all phases of the project up to the launch of the fully integrated and tested flight element The P A program shall be implemented for all produced hardware and software flight and ground The subcontractors and the suppliers shall implement the requirements of this document and prepare the required documentation at the level of assigned responsibility within the program e g modules subsystems units etc These requirements shall be made directly applicable to their suppliers These requirements are applicable as well to the EEE Components Procurement Agency CPPA The subcontractors and the suppliers shall notify to TAS any requirements discrepancies This document contain a set of requirements to be verified by RoD A T according to ECSS The verification method for each requirement shall be identified in the next issues of this document THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN ThalesAlenia Space 2 DOCUMENTS CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 DATE 21 01 2011 PAGE ISSUE 05 TAS Normative and Informative References for ExoMars project are listed in document EXM MS LIS AI 0001 2 1 Normative Documents 2 1 1 Definition of Normative Documents Normative References are directly applicable in their entirety to this document and are listed below as dated
38. including the required quality level The exceptions are identified by XX in Table 1 5 Applicable for styles CYR51 52 and 53 only 6 a For parts family 12 Capacitors Fixed Electrolyte Solid Electrolyte Tantalum 100 Surge Current screening shall be performed in accordance with MIL PRF 39003 10B as defined in Group A inspection b For parts family 14 Capacitors Chips Fixed Tantalum 100 Surge Current screening shall be performed for all surface mounted tantalum capacitors types in accordance with MIL PRF 55365 issue F 1 2 1 Stock parts procured with surge current test option A no additional test is required Stock parts procured with no surge current test 100 surge current test option B is required For new procurement 100 surge current test option B or option C is required Or 100 Surge Current screening shall be performed for all surface mounted tantalum capacitors types in accordance with ESCC 3002 9 22 e Burn in for variable capacitors is not required Temperature cycling vibration only on air dielectric types and driving torque will be performed on a 100 basis with critical parameters verified Air variable capacitors shall be internally inspected cleaned and lubricated in lieu of radiographic inspection and destructive physical analysis DPA Parameter drift screening applies only to air dielectric type variable capacitors from pre to post vibration 8 168 hours burn in on PTC thermistors is performed at maximum
39. inspection e electrical measurements before test e thermal cycling e high temperature storage minimum 96 H optional e final electrical measurements MS PA REQ 3590 Verification Traces Table 1 Minimum Screening and Inspection Requirements X X Not Applicable Required for non standard parts see applicable note X Systematically Required for Non Qualified and Qualified Parts THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE CSI and DPA requirements Requirements Note 1 Note 2 Notes 2 3 Note 4 Note Note 23 1 Diodes El 5000 Low Frequency PIND where applicable High Frequency where applicable Sei MIL PRF 19500 wa PIND wa applicable 3 Transistors oo 5000 ne Low Frequency 1 MIL PRF 19500 JANTXV PIND where applicable 4 Transistors HF Ae 5010 level i PIND 3 Deeg Sec LC H MIC PRF 19500 Lauren PIND ea applicable 5 Monolithic Microwave 3 integrated Circuits EEN 18 Lac tems packaged Tut eat e zs QMLQ PIND where applicable X 6 Integrated Circuits ESCC 9000 ASICs and Memories MIL PRF 38535 QML Q PIND 1 Except One time where applicable programmable types 7 FPGA and Memories ESCC 9000 One time Programmable MIL PRF 38535 QML Q PIND where ap
40. listed in QML e g failure in recent procured lot unknown manufacturer MS PA REQ 3650 Verification Traces EXM MS RS ESA 00002 PA SY 1460 EXM MS RS ESA 00002 PA SY 1480 For hybrids both new design and recurrent the procurement will include LAT as per PSS 01 608 or ECSS Q ST 60 05 if applicable to the hybrid manufacturer For OTS hybrids listed in QML 38534 QCI group C2 steady state life test will be performed on the procured batch Reduction of sample size will be agreed via PAD on case by case basis MS PA REQ 3660 Verification Traces EXM MS RS ESA 00002 PA SY 1470 New design ASIC from non qualified sources will be subjected to chart F4 of ESCC 9000 7 4 8 Long Lead Items MS PA REQ 3670 Verification Traces Long lead parts shall be identified early in the program in order that procurement can proceed to meet the program schedule A part shall be considered long lead if e The time between the date of purchase order to the manufacturer or to the procurement agent and the delivery is greater than 52 weeks Parts that have an anticipated delivery date exceeding the earliest User need date Parts submitted to export regulation restriction from the US Department of Defense Parts available from a unique manufacturer e g rad hard MOSFETs New design ASICs MMIC and hybrids New technologies that shall be submitted to qualification In case of serious schedule concern for long lead items e g LAT
41. not applicable to Exomars programme The list shall be generated in tabular format organized by family and group The DCL shall be compatible with electronic transmission and shall be provided also in an unlocked pdf format with meta data filled in Any change after equipment CDR or during equipment manufacturing shall be managed through updating of DCL and PAD approval process The list shall report for each line item the proposed procurement approach co ordinated or self and the need quantity splitted between engineering need quantity and manufacturing attrition In case of self procurement the relevant line item shall report the approval status of the PAD Users shall clearly indicate the need date for FM components The DCL format applicable to Exomars project will be provided by TAS I These Declared Component Lists shall be submitted to TAS ESA via EXO PCB for acceptance of the proposed procurement approach and for starting the co ordinated procurement Users shall then update the DCL for the established program reviews as requested in the SOW In case the subcontractor is responsible of subsystem the DCL shall be presented as aggregated of lower level lists with identification of open critical issues and status of consolidation RID open close expected updating status of EE parts approval etc It shall be a CPPA task to provide for each EXO PCB an updated master parts list organized by group and family of the parts approved for cent
42. of the Module System nominal activity It shall be possible to perform reading writing under Ground direct control or by time tagged commands Means to avoid inadvertent modifications shall be implemented THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 nev Space ISSUE 05 PAGE 5 3 3 Design approach MS PA REQ 1890 Verification Traces EXM MS RS ESA 00002 PA SY 540 The Supplier shall follow Clause 7 3 3 of ECSS Q 30 MS PA REQ 1900 Verification Traces EXM MS RS ESA 00002 PA SY 550 In addition for Fault Detection Isolation and Recovery FDIR On Board reconfiguration handling and accessibility the Contractor shall refer to the corresponding sections of the Mission System Requirements document Note this could be part of the engineering activity 5 4 Dependability Analyses MS PA REQ 1910 Verification Traces All Q 30 Paragraph 8 Dependability analysis is applicable with modifications Clause 8 2 2 Reliability analyses clause 8 2 3 Maintainability analyses and clause 8 2 4 Availability analyses are superseded by the following paragraphs MS PA REQ 1920 Verification Traces During the preliminary design phase the contractor shall classify functions operations and products into criticality categories The criticalit
43. power rating of part and on NTC thermistors the test is non operating storage 9 Wire link fuses are forbidden Only ceramic fuses are allowed 10 Fusistors shall be burned in at 50 of the current rating of part for 168 hours minimum 11 Diodes procured to Source Control Specifications that are rated at greater than 1 Amp of current or 1 Watt of power shall be considered as power diodes In this case the 100 screening sequence shall include a thermal impedance test based thermal transient method of MIL STD 750 test method 3101 and a sample surge current test shall also be imposed 12 MIL PRF 19500 JANTXV PIND and ESCC 5010 level C PIND screening are used as a guideline variations may be used by high reliability manufacturers provided they are approved and documented Proposed screening shall be agreed during the PAD NSPAR approval process e ASIC Additional qualification Conformance Testing or lot Acceptance Testing LAT may be required for parts of these type categories as defined in the relevant PAD 13A For EEPROMs The procurement specification shall specify the data retention time guaranteed over the full operating temperature range This specification shall detail all the tests performed at die revision level part level and lot level in order to guarantee this data retention time e For MMIC procured items packaged devices ESCC 9010 level C PIND or MIL PRF 38535 Q PIND may be used as a guideline Proposed deviations shall be agree
44. pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE ExoMars specific safety requirements in accordance with ECSS Q 40 paragraph 4 2 In case the verification process is not completed the certification shall include a statement that open verification shall be closed in accordance with the established verification tracking log and do not affect further safe processing at third party premises MS PA REQ 2380 Verification Traces EXM MS RS ESA 00002 PA SY 880 The Subcontractor and Supplier shall ensure that for testing and general handling of the spacecraft at third party premises the required Ground Support Equipment has a valid calibration acceptance certification for the planned activities 6 2 Safety Management and Planning MS PA REQ 2390 Verification Traces EXM MS RS ESA 00002 PA SY 890 In addition to ECSS Q 40 paragraph 4 2 2 the following requirement shall apply MS PA REQ 2400 Verification Traces EXM MS RS ESA 00002 PA SY 900 The Subcontractor and Supplier project safety management shall be familiar with national and international safety standards health requirements and the requirements of the launch facilities He shall make sure that hardware manufactured and used within the project is safe and that any required safety certification is obtained well prior to any intended use in order to avoid any delay in the progress of the project MS PA REQ 2410 Verification Traces
45. problem and of the range of components affected indicating Alert number generic part type manufacturer plant Lot Date code summary of the problem recommendations The user shall perform an alert assessment taking into account their application boundary For self procured components the user is responsible to perform the tasks above described MS PA REQ 3690 Verification Traces EXM MS RS ESA 00002 PA SY 320 CCPA and users is responsible to maintain an Alert status list treacing applicability and corrective actions if any as requested in para 4 7 7 4 10 Attrition MS PA REQ 3700 Verification Traces Additional parts for manufacturing attrition shall be calculated and ordered by users to CPPA for co ordinated procured items or procured directly by users for self procurement Attrition shall be calculated at unit level or to total number in case of identical units MS PA REQ 3710 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE The attrition rules shall be declared in the users PA plan MS PA REQ 3720 Verification Traces At the time being the following table can be taken as reference 1to5 3 samples 6 to 10 4 samples 11 to 30 6 samples 31 to 50 8 samples 51 to 100 12 samples g
46. programme with respect the program whose stock belongs to MS PA REQ 3980 Verification Traces When EEE parts from existing stocks are proposed to be used the following conditions shall be met e The parts have been stored according to 22 C 5 C humidity RH 55 max e The lot homogeneity and traceability can be demonstrated e The EEE parts documentation including LAT RVT QCI TCI documentation of the concerned lot is available and the content is acceptable in accordance with the programme requirements including materials planetary protection provisions and radiation data THALES oer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE e The minimum overall requirements e g screening are in accordance with the present document e No open NCR or no applicable alert exist for the relevant lot date code 7 5 5 EEE parts Documentation MS PA REQ 3990 Verification Traces All documentation as required by the paragraph 5 7 of ECSS Q ST 60 shall be retained and made available for TAS ESA MS PA REQ 4000 Verification Traces The delivery of documentation to TAS shall be conducted as specified in the DRD Other documents related to EEE parts like component manufacturer s data relevant to procurement or lot specific results shall remain av
47. rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE Part Number Lot Date Code Quantity Flight details Courier details Special storage requirements Bioburden status sterile clean uncontrolled manufactured 7 5 7 1 Dispatch Documentation MS PA REQ 4150 Verification Traces The CPPA shall ensure for each delivery of a flight lot that the following documentation is attached CoC Receiving inspection report Any applicable NCR with the complete history Dispatch note Bioburden status sterile clean uncontrolled manufactured Any additional user requested documentation upon EXO PCB approval MS PA REQ 4160 Verification Traces It is users responsibility for components received from the CPPA to perform a visual inspection to verify absence of defects and to control the associated documentation MS PA REQ 4170 Verification Traces Any anomaly shall be managed by NCR emission MS PA REQ 4180 Verification Traces For self procured items the user is responsible to perform in fully the incoming inspection buy off flow of activities THALES eer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01
48. suppliers shall be in accordance with ECSS Q 00A and shall include the disciplines of Quality Assurance Software Product Assurance Safety Assurance Dependability Component Quality Selection and Procurement Materials Parts and Process Selection and Control Configuration management Control and Acceptance Activities THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 0040 Verification Traces EXM MS RS ESA 00002 PA SY 10 A Product Assurance Manager shall be assigned by the subcontractors and suppliers who shall be responsible to direct and to control the relevant Product Assurance program MS PA REQ 0050 Verification Traces EXM MS RS ESA 00002 PA SY 10 The subcontractors and suppliers Product Assurance Manager shall have the authority to prevent implementation of project decisions which can adversely affect the quality of the spacecraft and shall have unimpeded access to higher company management for this purpose MS PA REQ 0060 Verification Traces EXM MS RS ESA 00002 PA SY 10 The subcontractors Product Assurance Manager shall make sure that lower tier subcontractors have similarly approved Product Assurance organizations to perform tasks required for a proper control of the quality of the spacecraft during all phases of
49. the project MS PA REQ 0070 Verification Traces EXM MS RS ESA 00002 PA SY 10 Competent and sufficient staff shall be assigned and adequate facilities shall be made available to ensure proper and timely completion of all PA tasks MS PA REQ 0080 Verification Traces EXM MS RS ESA 00002 PA SY 10 The planning of the PA activities and status control shall be integrated into the overall project planning to be implemented by the subcontractors and suppliers THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 0090 Verification Traces EXM MS RS ESA 00002 PA SY 10 The subcontractors and suppliers shall provide regular progress reports on the status of the Product Assurance program Where convenient the PA progress report shall be included as a separate section in the overall general project progress report MS PA REQ 0100 Verification Traces EXM MS RS ESA 00002 PA SY 10 Product Assurance Manager shall support the progress meetings as planned in the contract and technical meetings as needed MS PA REQ 0110 Verification Traces EXM MS RS ESA 00002 PA SY 30 In particular the outputs from the PA and Safety programme shall be linked to a Risk Management programme 3 2 PA progress reporting Addition to
50. they will already be managed through Hazard Analysis the CIL will only reference them TST e Adequate ground testing at subsystem or system level is difficult or not practicable e Redundant items without possibility of independent check out after integration QUA e Items not qualified no previous space qualification achieved on components materials processes technologies e High sensitivity to manufacturing processes is expected e Materials with principal characteristics unknown e Items with exceptional qualification circumstances and or process sensitivity e Items which are highly radiation sensitive e Equipment with a known history of flight failures e EEE items developed for the mission hybrid MCM ASIC FPGA detector custom THALES err All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MMIC e Special software e Special GSE B Fracture Critical Items FCI e Structural items whose failure can result in catastrophic or critical hazards C Limited time availability Critical Items LIF e Limited life limited cycle items critical in terms of useful life duration or operating cycles limitation All the items subjected to wear out drift or degradation below the minimum required performance in less than the storage and mission time e Ob
51. 01 2011 een Space ISSUE 05 PAGE 11 1 10 Cleanliness and PP MS PA REQ 5170 Verification Traces The GSE shall be cleanable in order to reach the cleanliness level of the flight hardware with which it interfaces For optical non cleanable devices cleanliness monitoring shall be applied For PP subject apply dedicated program specification EXM MS SSR AI 0007 NR 0120 11 1 11 GSE Certifications UE certification USA certification 11 1 11 1 UE GSE Suppliers MS PA REQ 5180 Verification Traces All GSE to be provided with CE Marking and certified on the bases of the following standard e Directive UE machine 2006 42 EC e Directive LOW Voltage 2006 95 EC 12 12 2006 e Directive EMC 2004 108 EC 15 12 2004 11 1 11 2 USA GSE Suppliers MS PA REQ 5190 Verification Traces e USA GSE will provided by a certification comparable to UE standard CE marking e USA GSE have to satisfy Safety requirements placed in Para 4 3 2 of document KHB 1700 7 THALES ve All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION e REFERENCE ThalesAlenia DATE Space ISSUE 12 DRL FOR PRODUCT ASSURANCE 12 1 HW SW DRL PA DOCUMENTS 25 MS PA REQ 5200 EXM MS RQM AI 0004 21 01 2011 05 PAGE Verification Traces The following table identified complete set of all PA documentation applicable at Program level Spec
52. 010 of deleted requirement 1710 Para 8 4 Req PA SY 1720 reworded to cover DRD PA 31 Output PA 31 deleted Para 8 5 Req Req PA SY 1740 1750 Output added to 1740 text of deleted requirement 1750 Para 8 6 Title changed PA SY 1760 assessment replaced by control Output PA 33 deletion of DRD PA 33 Para 8 7 Req PA SY 1770 1780 1790 deleted Para 8 7 Req PA SY 1800 reference to DRD PA 27 28 29 30 deleted and Output P 32 moved below req PA SY 1800 Para 8 8 Req PA SY 1850 deleted text used as Output for req PA SY 1840 Para 8 12 8 13 8 15 Req PA SY 1930 1950 1970 1990 2010 2090 2110 deleted releated text used as Output for the requirement before Para 8 15 Req PA SY 2000 reworded to cover material combinations and to deleted permanent Para 8 18 PA 36 Deleted Para 8 17 Req PA SY 2050 reworded to provide link to CIL Output PA 35 deleted covered by PA 3 Para Add NR 097 Relifing Procedure EEE Components Para 11 Modified Para 12 UPDATED PA DRL 22 Revised for ESA PA Requirement iss 04 alignment Marco Milazzo Modification due to ESA PA Requirement updating rev3 4 dated 12 03 2010 First Delivery for internal review D Delivery Update to reflect updated Exomars mission concept and specify applicability of updated ECSS documents Para 1 1 Text modified to reflect multiple elements of the Exomars project Para 2 1 3 Replacement of old issues with newer versions NR A43 DELETE NR A44 DE
53. 1 2011 Space ISSUE 05 PAGE 4 QUALITY ASSURANCE REQUIREMENTS MS PA REQ 0370 Verification Traces The requirements stated in ECSS Q 20B are applicable with the following modifications specified in this section 4 1 Quality Assurance Plan MS PA REQ 0380 Verification Traces The subcontractors and suppliers shall assign responsibility to suitably qualified and experienced staff for ExoMars Quality Assurance Management MS PA REQ 0390 Verification Traces The selected staff shall be responsible for the establishment and maintenance of all quality activities which are required by the ExoMars project MS PA REQ 0400 Verification Traces He shall make sure that all quality related requirements are understood and that qualified and certified personnel have been assigned to implement the quality assurance tasks MS PA REQ 0410 Verification Traces EXM MS RS ESA 00002 PA SY 130 The QA plan shall be a part of the PA plan required by clause 3 4 of these requirements THALES KERREN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE 4 1 1 Normative documents MS PA REQ 0420 Verification Traces EXM MS RS ESA 00002 PA SY 140 This chapter is a supplement to clause 2 of ECSS Q 20B Where suitable further existin
54. 1 2011 eer Space ISSUE 05 PAGE In any case the SEE criticality analysis SEECA shall be completed for review and approval before equipment CDR and included in the Radiation analysis Subcontractor shall be available to organise and support adequately a dedicated SEECA review meeting on prime request in order to e To review circuit SEU effects analysis e To review the assessment on displacement damage on electronics if significant e To verify that no impact due to SEE on performance undetected error rate reliability and availability requirement e To verify the SEECA assessment on critical FPGA and ASIC 7 4 3 Component Derating Deleted PA SY 1320 Deleted PA SY 1330 Note These requirements are covered by para 5 4 8 7 4 4 EEE Components Approval MS PA REQ 3300 Verification Traces EXM MS RS ESA 00002 PA SY 1340 The EXO PCB has the task to review any equipment DCL and to approve any candidate for co ordinated procurement taking into account the suitability of the selected component to the EXOMARS requirements quality level operative temperature range lifetime radiation tolerance etc and standardisation related issues procurement channel not recurring effort high MOQ MS PA REQ 3310 Verification Traces EXM MS RS ESA 00002 PA SY 1380 Any component shall be approved for FM use through Part Approval Document PAD prepared by the procurement authority according to the following scheme e Componen
55. 5 2 of ECSS Q 20B which is also applicable The detailed requirements for Marking Packaging and Labelling and Transportation referred to in Paragraphs 10 4 1 10 4 2 and 10 5 2 of ECSS Q 20B are defined in PSS 01 202 Para 2 1 3 and are the detailed applicable requirements MS PA REQ 1040 Verification Traces Each separately identifiable part or sub assembly shall carry an identification consisting of at least the following information a Identification number b Item title c Model identification d Serial number MS PA REQ 1050 Verification Traces All parts or subassembly having the same identification number shall be functionally and dimensionally interchangeable 4 14 Handling Storage Preservation THALES ER All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1060 Verification Traces This chapter is a supplement to clause 3 8 of ECSS Q 20B which is also applicable MS PA REQ 1070 Verification Traces The detailed requirements for handling storage and preservation referred to in paragraphs 5 8 1 5 8 2 and 5 8 3 of ECSS Q 20B are defined in ESA PSS 01 202 Para 2 1 3 and are the applicable detailed requirements 4 15 Inspections PA SY 465 MS PA REQ 1080 Verification Traces In addition t
56. 7 4 07 applies whilst the requirements for GSE parts are reported in paragraph 7 4 8 MS PA REQ 2900 Verification Traces EXM MS RS ESA 00002 PA SY 1070 The following items shall not be considered EEE components and will be controlled at unit or higher level by the relevant disciplines e intermediate products containing discrete components on substrates PCBs motors solar cells cells in batteries HF sub assemblies like coaxial cable assemblies or waveguide elements TWTs and RF switches coaxial or waveguide THALES eer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 7 2 EEE Program management MS PA REQ 2910 Verification Traces EXM MS RS ESA 00002 PA SY 1090 The subcontractor shall implement an EEE Components Control Programme in accordance with all the requirements of ECSS Q ST 60C para 5 taking into account the additions and exceptions as defined below in this section In the event of conflict with ECSS Q ST 60C para 5 this document shall have precedence in ExoMars Mission project 7 2 1 Procurement policy MS PA REQ 2920 Verification Traces EXM MS RS ESA 00002 PA SY 1 100 ExoMars Mission EEE parts procurement is based on a co ordinated approach The EEE components will be procured through a Co ordinated Procurement A
57. 7 5 1 1 3 Evaluation testing MS PA REQ 3850 Verification Traces After successful completion of the constructional analysis and manufacturer evaluation evaluation testing shall be performed This assessment shall determine which inspections or tests are required to provide the confidence that the part type under evaluation will when assembled and tested in accordance with the procurement specification successfully meet the mission requirements MS PA REQ 3860 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Sufficient data must be available upon completion of the evaluation program to demonstrate part stability In addition evaluation testing shall be required where any of the previous stages have identified any anomaly reflecting a design material or process weakness that could shorten the active life of the concerned part and that may not be identified during the final production testing or screening tests included in the procurement specifications MS PA REQ 3870 Verification Traces Because of the wide range of possible anomalies or weaknesses that would require evaluation testing it is not possible to define the precise test program to be followed however the types of testing to be considered would incl
58. A REQ 2800 Verification Traces No single failure or single human error shall cause loss of the emergency and warning functions together with the monitored functions MS PA REQ 2810 Verification Traces Protection systems shall to the greatest extent possible be intrinsically fail safe and shall be capable of being enabled and disabled by commands 6 7 Software Deleted 6 8 Product Liability Requirements MS PA REQ 2820 Verification Traces In addition to safety analyses the subcontractor will address specifically the requirements issued by the European Union in terms of product liability and related directives THALES E All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 2830 Verification Traces The subcontractor shall identify for each product under his responsibility the applicability of the EU directives MS PA REQ 2840 Verification Traces The liability requirements shall apply to every product flight product and ground support equipment under the responsibility of the subcontractor MS PA REQ 2850 Verification Traces Where applicable the subcontractor shall perform the related certification towards the EU directives MS PA REQ 2860 Verification Traces
59. A REQ 5100 Verification Traces As per para 11 1 4 11 1 6 1 Criticality Categories MS PA REQ 5110 Verification Traces As per para 11 1 4 11 1 7 Critical Item THALES BER All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 5120 Verification Traces FMECA A Critical Item List shall be provided the requirements defined in Para 4 4 Critical Items Control and Para 5 5 Inputs to Critical items list are applicable 11 1 8 Safety MS PA REQ 5130 Verification Traces As per para 11 1 4 11 1 9 Materials MS PA REQ 5140 Verification Traces Materials which interfaces with flight hardware shall be selected in order to not degrade or contaminate it MS PA REQ 5150 Verification Traces The selection criteria shall be met for out gassing thermal cycling corrosion stress corrosion fluid compatibility MS PA REQ 5160 Verification Traces In addition the materials shall not be flaking or dusting so that a high degree of cleanliness of the flight hardware can be achieved and maintained THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21
60. AP 61 RID AP 85 RID AP 76 RID AP 79 RID AP 80 RID AP 82 2 ESA environmental spec doc EXM MS RS ESA 00013 ISS 4 DRAFT 0 Para 7 4 2 Radiation Hardness Assurance 3 ESA PA Requirement updating rev3 3 Para 7 1Req PA SY 1040 reference to ECSS Q ST 60C added and quality level changed to Class 2 Para 7 2 Req PA SY 1090 Ref changed to ECSS Q ST 60 para 5 THALES Geh All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 5 175 Para 7 2 1 Req PA SY 1120 ESA participation in PCBs modified Para 7 3 7 4 Req PA SY 1140 reworded and link to ECSS Q ST 60C provided Para Req PA SY 1150 reworded to introduce the ExoMars PPL for parts selection and to address low temperature application and add IR 6 Para 7 4 1 1 Req PA SY 1160 reworded to introduce reference to ECSS Q ST 60C Para 7 4 1 Req PA SY 1200 Para 7 4 1 1 Req PA SY 1210 Para 7 4 2 2 Req PA SY 1260 1270 1280 1300 1310 unit corrected to MeV cm mg Para 7 4 2 2 Req PA SY 1260 1270 1300 radiation level change to 60 MeV cm mg Para 7 4 2 2 Req PA SY 1270 1280 add link to DRD PA 11 24 Para 7 4 2 2 Req PA SY 1310 requirement for PAD added Para 7 4 3 Req PA SY 1320 1330 and output PA 25 deleted and NOTE added that these requirements are covered by para 5 6 8 Para 7 4 4 Req PA SY 1370 add
61. AR approval process 20 Thermostats procured in accordance with MIL PRF 24236 shall be considered as non qualified parts In this case PAD NSPAR and CSI shall be mandatory For each purchase order the primary elements shall be from the same manufacturing lot and only one sealing lot shall be required Endurance test 100 000 cycles with voltage current conditions covering the application shall be performed on non qualified thermostats The endurance test 100 000 cycles shall be performed with voltage current conditions covering the application on 6 sample units In this case DPA shall be only performed after endurance test on 3 sample units out of the 6 sample units e Multi layer Ceramic Capacitors procured with MIL PRF Spec shall be submitted to QCI testing including Steady State Low Voltage Test according to MIL PRF 123 Group B Subgroup 2 85Rh 85 C 22 Procurement of relays in particular TO5 Types according to MIL PRF 39016 only is not allowed For Latching and Non Latching Types a spec Amendment shall include Millipore Cleaning Random Vibration 2500 Miss Test Cycles In addition for Latching types 100 neutral screening test is required 23 For items judged critical no previous heritage unknown manufacturer recent documented DPA failure an increase of DPA samples could be requested by EXO PCB and traced in the relevant PAD 24 Applicable flow for Antifuse based FPGA THALES SE All rights reserved 2007 Thales Alenia
62. AS ESA 3 8 PA involvement in overall project documentation MS PA REQ 0240 Verification Traces The subcontractors PA shall be closely involved in the elaboration and review of the following documents which do not fall directly under the full PA responsibility test plan test report technical notes Audit report Minutes of meetings Manufacturing Flow chart Certificate of qualification 3 9 Integration of lower data at higher level MS PA REQ 0250 Verification Traces The subcontractors shall be responsible for integrating lower level data from subsystems equipment OTS into his level required documentation 3 10 Qualification Status Reporting THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 0260 Verification Traces This chapter is a supplement to clause 6 6 4 4 of ECSS Q 20B which is also applicable MS PA REQ 0270 Verification Traces Subcontractors and suppliers shall give evidence of reached qualification according to ExoMars requirements providing a Qualification Status List QSL MS PA REQ 0280 Verification Traces The document shall contain as a minimum Categorization of Equipment identification of hardware by name Configuration Item model serial number supplier
63. Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 e Thales Alen la DATE 21 01 2011 Se Space ISSUE 05 PAGE MOS BiCMOS BIPOLAR FAMILY Test Test Dose Rate Test Test Dose Rate Sample Criteria Method Criteria Method Size Zener Diodes Existing RD 1bis High or data show Low that for EXO mission they are insensitive Transistors All RD 1bis or High or 2 RD 1bis or Low 5 RD 3 Low RD 3 Analog Ics All RD 1 or Low 1 All RD 3 Low 5 RD 3 Logic Ics 1 RD2 or Low 1 4 RD3 Low 5 RD3 ASICs FPGA AIl RD2or Low 1 All RD3 Low 2 3 RD3 RAM PROM 2 RD2 or Low 1 RD3 Low 2 Processors RD3 RD3 MS PA REQ 3050 Verification Traces 1 For fully MOS technology devices High Dose Rate can be used Table13 2 2 1 Total Dose Screening Matrix MS PA REQ 3060 Verification Traces With M032 EN THALES All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE e RD1 MIL STD 883G METHOD 1019 7 condition C dose rate lt 0 1 Rad S e RD1bis MIL STD 750E METHOD 1019 5 condition C with dose rate lt 0 1Rad S e RD2 MIL STD 883G METHOD 1019 7 condition A with 50Rad s condition B for fully MOS device dose rate to be agreed among the parties e RD3 Total Dose Steady State Irrad
64. C the FMECA shall be performed at parts level MS PA REQ 4990 Verification Traces In the case that a failure may propagate through an interface the contractor shall define agree and trace dedicated actions to remove the non compliance If removal is considered not feasible justification for retention of each identified critical failure shall be submitted to TAS I for approval MS PA REQ 5000 Verification Traces The following failure consequence Severity Categories shall be used in the FMECA for GSE Category 1 Failure propagation Possible damage to or overstress of flight hardware or other hardware Category 2 Failure is contained Degradation of operational capability of the GSE under consideration MS PA REQ 5010 Verification Traces Improper commands or command sequences or software errors shall not cause undesired effects as specified in Para 5 3 2 Failure Tolerance MS PA REQ 5020 Verification Traces The GSE shall by design avoid that its operation alone or connected to the S C could lead to hazardous conditions which may have catastrophic or critical consequences THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 5030 Verification Traces Protection systems such as over v
65. CONTROLLED DISTRIBUTION REFERENCE EXM MS RQM AI 0004 DATE 21 01 2011 ISSUE 05 PAGE 1 175 EXOMARS m PRODUCT ASSURANCE REQUIREMENTS FOR SUBCONTRACTORS DRL DRD N A W P No EB0 1ACA Written by Responsibility M MILAZZO AUTHOR Verified by G BRIA BERTER CHECKER Fau Ee M MILAZZO M SPASARO C CASSI SYSTEM BEE en P SANTORO Documentation Manager P FISSORE The validations evidence are kept through the documentation management system THALES ici All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 2 175 CHANGE RECORDS Sa DATE CHANGE RECORDS AUTHOR 16 07 2007 First issue for ITT preparation Marco Milazzo 18 01 2008 Revised for B2 Including BCR RIDs Marco Milazzo BCR RIDs implementation AP Cl 01 03 Modified para 4 4 AP Cl 01 04 Modified para 4 4 AP PA 11 02 Add Para 4 16 AP PA 14 01 Modified 5 4 9 e 5 4 10 Updated Table 5 3 1 Failure consequence severity categories Updated 5 4 2 FMECA AP SA 03 01 Modified Para 6 2 BCR SC DHS 01 01 Modified affected para AP PA 09 Modified 8 5 1 Modifified 8 8 Para 8 5 2 deleted 23 02 2010 Revised for I PDR implantation and B2X closure Marco Milazzo Printing error Para 7 1 2 BC PCB instead of EXO PCB Page 57 BC PCB instea
66. CSS Q ST 70 26C for crimping ECSS Q ST 70 28C for repair and modification of PCB s ECSS Q ST 70 38C for high reliability soldering for surface mount and mixed technology The requirements shall be fulfilled through the deliverable PA 36 Output PA 36 Deleted MS PA REQ 4630 Verification Traces EXM MS RS ESA 00002 PA SY 2080 Equivalent standards from MIL system or NASA may also be accepted pending compliance review Deleted 8 18 1 Process procedures MS PA REQ 4640 Verification Traces Process procedures shall include sufficient inspections and tests during and at the end of the processing steps to assure that the characteristics of the product are within the required limits MS PA REQ 4650 Verification Traces When not included in specific process procedures appropriates MIPs and KIPs shall be introduced as per ECSS Q 20B section 8 9 for process control THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 nev Space ISSUE 05 PAGE MS PA REQ 4660 Verification Traces Process procedures shall be made available or accessible to TAS ESA upon request e g during audits during the Final Design Review before start of QM FM manufacturing or for failure investigations for review that all processing steps are adequately specified and that adequa
67. E 05 PAGE Item Number DRD Title Submital Proposal PDR MRR CDR QR DRB Class Remark Ref PA 01 Product Assurance D D D A Including the amp Safety Plan incl Compliance Matrix SW QA versus PA Requirements for Subcontractors PA 04 Status lists RFA As A Major for approval NCR M amp m SPR generated minor for review RFD RFW PA TASO7 Product Assurance as Project R Part of Project Progress Report PR Progress Report content see PARS PA 010 End Item Data x AR Acceptance at FAR Package EIDP S W GSE PA 011 FMECA functional D x x A level amp S C interfaces at part level PA 043 Hazard Analysis D D D R PA 044 Inputs to Safety x D x R To be updated also in Submission support of System Reviews on request PA 08 Cleanliness amp D D A as part of PA 01 Contamination Control Plan in PA 01 PA TASO14 Configuration R including software Management Plan Covered by MT 3 incl SW PA TAS013 Software Coding D D x R Standard SCOS PA 38 SW Criticality D x x AR analysis 12 3 Notification Delivery Time Summary MS PA REQ 5220 Verification Traces Notification Delivery Time Summary NCR major Notification within 48 hours after occurrence MIP KIP Notification 10 working days in advance TRR TRB Notification 10 working days in advance tbc Audits Notification 10 days in advance EIDP Delivery 14 days in advance to DRB Alert Notification
68. E 21 01 2011 Space ISSUE 05 PAGE e request for waivers e verification control document e CE Certifications and ITAR Certification for extra Europe import item MS PA REQ 0970 Verification Traces The EIDP shall be delivered in hard copy plus CD ROM support 15 days before the relevant DRB for review MS PA REQ 0980 Verification Traces Final hard copy plus final CD ROM support shall be delivered together to the item 4 12 Delivery review boards MS PA REQ 0990 Verification Traces This chapter is a supplement to clause of ECSS Q 20B para 10 3 MS PA REQ 1000 Verification Traces The Delivery Review Board DRB shall be chaired by the P A Manager or his delegated of contractual authority MS PA REQ 1010 Verification Traces EXM MS RS ESA 00002 PA SY 450 TAS ESA reserves the right to attend DRBs at any lower level of suppliers as board member THALES ale All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1020 Verification Traces EXM MS RS ESA 00002 PA SY 460 Any DRB shall be notified to TAS ESA at least 10 working days in advance 4 13 Packaging Marking and Labelling Transportation MS PA REQ 1030 Verification Traces This chapter is a supplement to clause 10 4 1 10 4 2 and 10
69. EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 4100 Verification Traces Traceability of component application and relevant documentation shall be established and maintained updated under Q A responsibility MS PA REQ 4110 Verification Traces The procurement authority is also responsible to retain and store appropriately identified all LAT type approval QCI and destructive test samples MS PA REQ 4120 Verification Traces Whenever is needed the CPPA or users shall organize a Quarantine Store that must be separated to the EXOMARS flight store to store any non flight parts As well for the quarantine stored items the traceability against NCR LAT type approval history shall be maintained 7 5 7 Shipment MS PA REQ 4130 Verification Traces Any shipment shall not be authorized if LAT RVT DPA type approval testing OCT full data review and CoC are not completed A user may request a premature shipment by taking over the fully responsibility A shipment is constituted by the flight parts plus documentation MS PA REQ 4140 Verification Traces Whenever a shipment of components batch is ready the CPPA shall communicate to the user copy to the Prime Contractor via Fax or within the Internet communication system scheme as a minimum the following information e programme THALES adi All
70. EQSR Para 7 4 4 Req PA SY 1380 CPPA PAD submission responsibility Para 7 4 5 Req PA SY 1390 reworded to address CDR and EQSR Reference to PAD deleted covered by PA SY 1340 Para 7 4 5 Req 1390 reference changed to ECSS Q ST 60C Para 7 4 5 Req PA SY 1400 1410 deleted covered by ECSS Q ST 60C Para 7 4 6 Req PA SY 1420 reworded to provide reference to ECSS Q ST 60 Para 7 4 7 Req PA SY 1430 1440 1460 reworded and PA SY 1450 deleted LAT requirements reworded to p rovide reference to ECSS Q ST 60C and to detail LAT for additional components Para 7 3 1 Req PA SY 1490 change to grade 2 Para 7 4 6 1 Req PA SY 1520 1530 reworded PA SY 1540 deleted Requirements re worded deleted to provide reference to ECSS Q ST 60C and detail PRECAP for additional components Para 7 4 6 4 7 4 5 Req PA SY 1550 1560 1570 reference changed to ECSS Q ST 60 Para 7 5 1 Req PA SY 1620 modified to provide reference to ECSS Q ST 60V Para 8 2 Req PA SY 1650 and Output PA 45 RFA added in the requirement and as DRD Para 8 2 1Req PA SY 1690 reworded with the text and DRD PA 30 DRD deleted and output PA 30 replaced by Progress Report Para 8 3 8 3 1Req PA SY 1700 1710 Output added to 1700 text THALES SS All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 6 175 04 15 05 2
71. LETED NR A18 NEW ECSS ISSUE NR A19 NEW ECSS ISSUE NR A20 NEW ECSS ISSUE NR A21 NEW ECSS ISSUE NR A23 NEW ECSS ISSUE NR A24 NEW ECSS ISSUE NR A25 NEW ECSS ISSUE NR A98 NEW ECSS ISSUE NR A26 NEW ECSS ISSUE NR A27 NEW ECSS ISSUE NR A28 NEW ECSS ISSUE NR A29 NEW ECSS ISSUE THALES SEN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 7 175 NR A30 DELETED NR A31 NEW ECSS ISSUE NR A32 NEW ECSS ISSUE NR A33 NEW ECSS ISSUE NR A34 DELETED NR A35 DELETED NR A35 DELETED NR A36 NEW ECSS ISSUE NR A37 NEW ECSS ISSUE NR A38 NEW ECSS ISSUE NR A39 NEW ECSS ISSUE NR A99 NEW ECSS ISSUE NR A100 NEW ECSS ISSUE NR A97 NEW ECSS ISSUE Addition of new doc Para 2 2 3 NR TBD ECSS Q ST 70 31C Application of Paints and Coating on Space Hardware Para 2 2 3 IRA 94 Document reference corrected now 0016 Para 8 7 Vacuum Rewording of PA SY 1840 due to updated NR A18 ECSS Q ST 70 02C Thermal vacuum outgassing test for the screening of space materials Modification due to ESA PA Requirement updating rev3 5 dated 15 03 2010 P version update for Project CCB review Change log References to page numbers in changelog deleted Issue revision number of D Delivery modified from 4 draft to 3 4 Para 5 6 Replacement of Segment with Elements Para 1 1Clarifications of GSE compliance Modifica
72. NCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 4490 Verification Traces EXM MS RS ESA 00002 PA SY 1890 When considering the materials environment it should be noted that atomic oxygen might be present during the earth escape orbit and the Mars insertion operation orbit The amount of atomic oxygen shall be predicted and its effect on materials shall be estimated Particularly sensitive materials shall be avoided The survivability of materials in the Martian environment atmosphere sand etc for orbit landing and operation shall be demonstrated if applicable MS PA REQ 4500 Verification Traces EXM MS RS ESA 00002 PA SY 1900 Materials exposed to the sun shall comply with PSS 01 706 for UV radiation and if applicable for particle radiation Materials exposed to space but not to the sun shall comply with PSS 01 706 and the ExoMars radiation environment 8 11 Micrometeoroid Debris Environment MS PA REQ 4510 Verification Traces EXM MS RS ESA 00002 PA SY 1910 The influence of a Micrometeoroid Debris Environment on the materials shall be examined on a case by case basis 8 12 Electrochemical Compatibility MS PA REQ 4520 Verification Traces EXM MS RS ESA 00002 PA SY 1920 When bimetallic contacts are used the choice of the pair of metallic materials used shall take into account ECSS Q 70 71A rev1 paragraph 5 2 14 or MSFC SPEC 250 Protect
73. ONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 6 SAFETY 6 1 General MS PA REQ 2250 Verification Traces EXM MS RS ESA 00002 PA SY 770 ECSS Q 40 NR 10 shall apply with the following deletion modification and supplements The contractor shall assure that all hardware software and activities to be performed during ground operations are compliant with existing national safety regulations at all locations where the equipment is manufactured or used and where ExoMars related activities are carried out Existing national regulation shall prevail in case of conflict with ECSS Q 040 NR 10 requirements MS PA REQ 2260 Verification Traces EXM MS RS ESA 00002 PA SY 780 Accidents and incidents shall be reported as defined in ECSS Q 40 NR 10 paragraph 4 9 MS PA REQ 2270 Verification Traces EXM MS RS ESA 00002 PA SY 790 A Safety program shall be established by the Subcontractor and Supplier to achieve the following objectives e to preserve EXOMARS system during ground operations to preserve operations personnel GSE and ground facilities to minimise hazards to the general public and private property to protect the launcher vehicle including other launcher payloads to protect the environment and to comply with the planetary protection requirements MS PA REQ 2280 V
74. PAGE MS PA REQ 4890 Verification Traces Quality assurance activities shall be applied to the following subjects e Safety provision including assurance that the flight hardware will not be exposed to potentially hazardous conditions during handling or testing e Safety verification with appropriate certification e g proof loading test for lifting devices Reliability of the interface to the flight hardware shall be verified by FMECA Configuration Control Non Conformance control during acceptance testing Handling and Storage control Identification marking Calibration Quality Assurance of materials and parts where contact is made to flight standard hardware Witness of acceptance testing Quality assurance of software 11 1 3 Documentation MS PA REQ 4900 Verification Traces The GSE shall be delivered with the following documentation Certificate of Compliance Compliance Matrix VCD List of deliverable items List of spare items Configuration Status List As design as built Drawing files with all necessary drawings ICD Pin Allocation Lists Installation Documents etc List of NCR Major and Minor NCR NRB Reports Major only RFD RFW List and copies Historical records Calibration Data Status List Calibration Dates Inspection Results Acceptance Test Reports User Manuals Maintenance manuals DRB MOM s TRR s PTR s MOM s Action Item Lists Open Work Deferred Work Open Test Temporary Installation Transpor
75. Q 020B para 9 5 PA TAS12 Test Review Board Report As l As called by generated ECSS Q 020B para 9 3 PA TAS13 S W PA deliverable Deleted documentation PA TAS14 Configuration Management A including Plan software Covered by MT 3 PA TAS15 Part Procurements As R documentation generated PA TAS16 Components Control Plan A as part of PA 1 PA TAS17 Failure analysis report As R generated PA TAS18 Hardware Software Interaction x x D R as part of PA 11 Analysis PA TAS19 Common Mode Common x x D R as part of PA 11 Cause analyses PA TAS20 Functional Analysis Report x x x R as part of PA 11 PA TAS21 Contingency Analysis Report D D H Deleted for PDR PA TAS22 As Built Configuration List D R as part of EIDP ABCL PA TAS23 As Built EQM Components list D H as part of EIDP 12 2 GSE DRL PA DOCUMENTS 25 MS PA REQ 5210 Verification Traces The following table identified complete set of all PA documentation applicable at Program level Specifically required PA documents related to each item are listed in the relevant SOW DRL CONTROLLED DISTRIBUTION Ref For GSE contractors the following listed items are applicable THALES a All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION e REFERENCE EXM MS RQM AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSU
76. S I ESA approval via the RFA process MS PA REQ 4250 Verification Traces EXM MS RS ESA 00002 PA SY 1660 A breakdown of such lists is given in ECSS Q 70B In addition the lists shall include proper definition of bioburden reduction environment and indication for compatibility THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 8 2 1 PMP Item number MS PA REQ 4260 Verification Traces Sequential item number once assigned to a material part process inside the List shall not be changed deleted or re assigned MS PA REQ 4270 Verification Traces EXM MS RS ESA 00002 PA SY 1670 The Prime contractor shall determine and decide upon the acceptability of each line item on the DML DMPL and DPL prior to delivering each list to ESA for final approval MS PA REQ 4280 Verification Traces EXM MS RS ESA 00002 PA SY 1680 The DML DMPL DPL shall be provided in an electronic form that is exchangeable searchable and sortable and suitable for storage and retrieval Outputs e PA 27 Declared Material List DML PA 28 Declared Mechanical Part List DMPL PA 29 Declared Process List DPL PA 45 Request For Approval MS PA REQ 4290 Verification Traces EXM MS RS ESA 00002 PA SY 1690 A Materials amp Process C
77. SS Se E 28 Resistors network thick 3X3 o enke Ral Meal a RE level 29 Resistors Fixed thick film ESCC 4001 Level C MM chips Fixed thin film chips MIL PRF 55342 FRL R XX 3X3 17 30 Thermistors thermally sensitive resistors 31 Coils fixed molded MIL PRF 39010 X MIL STD 981 Eq Class S 32 Coils fixed Non molded ESCC 3201 Level C MIL STD 981 Eq Class S THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 e Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE CSI and DPA requirements Ref Part Family Applicable Screening Note Precap Final DPA Number of unit Requirements Note 1 Note 2 Notes 2 3 Note 4 Note Pe ae ES 33 EMI filters ESCC 3008 Level C MIL PRF ee Class B 34 Crystal units quartz ESCC 3501 LevelB 3501 Level B EZ MIL PRF 3098 Class S 35 RELAYS Electromagnetic Ee ae 3601 Level B latching and non latching Ee ae 3602 Level B relays MIL PRF 39016 SCD a 3 18 corresponding to FRL S 22 36 Connectors RF coaxial ESCC 3402 LevelB sd ee PRF 39012 Out gassing Spec Amendment 37 Connectors electrical circular and rectangular Se DTL 24308 Class M rectangular MIL DTL 38999 Classes G and H circular MIL PRF 835 13 Class M 38 Connectors electrical RF filters ESCC 3405 Level B MIL DTL 24308 MIL DTL 24308 ClassM M ee 4008 Level C MIL PRF 234 19 40 FUSI
78. STORS ESCC 4008 Level C oome o 42 Thermostat Switches ESCC 3702 Level B XX XX Thermostatic MIL PRF 24236 FRLS 43 Switches Mechanical non ESCC 3701 Level sd RF sensitive and push MIL PRF 8805 FRL WIEBE 3o0e FRLS a snap action THALES SEN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION gt REFERENCE EXM MS RQM AI 0004 la ThalesAler DATE 21 01 2011 nev Space ISSUE 05 PAGE CSI and DPA requirements Ref Part Family Applicable Screening Note Precap Final DPA Number of unit Requirements Note 1 Note 2 Notes 2 3 Note 4 Note Note 23 44 Microwave passive parts p isolators and power ESCC 3404 Level B BOR divider coupler coaxial MIL PRF 23971 X X X 1 18 X 3 18 45 Microwave passive parts ESCC 3403 Level C MIL STD 981 Eq Class S SSQ 22676 Rev C 48 Procured hybrids ESA PSS 01 608 Level B ECSS Q60 05A MIL PRF 38534 Class K 49 Oscillator Controlled MIL PRF 55310 Class S ESCC 3901 Level B MIL W 22759 19 MIL DTL 27500 9 attenuators and loads MIL DTL 3933 Attenuators S Part number level i XX XX XX 18 MIL PRF 39030 loads S Part number level XX XX XX 1 18 51 Coaxial ESCC 3902 Level B A Cables MIL DTL 17 NOTES 46 Surface Acoustic ESCC 3502 Level B waves filters SAW 47 Transformers molded ESCC 3201 Level C MIL STD 981 Eq Class S SSQ 22676
79. STRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 3180 Verification Traces EXM MS RS ESA 00002 PA SY 1290 For digital technologies the subcontractor will be required to use parts with a well known SEU sensitivity in terms of LET threshold and cross section The subcontractor shall include in the equipment radiation analysis the SEE rate prediction and analysis of effects of the possible identified events showing that for all the memories the probability of uncorrectable errors shall be 1E 11 error bit day SEU effect shall not induce unwanted lose of critical circuit e For critical function a flight automatic recovery procedure shall be foreseen in order to avoid loosing mission for SEU effect e EDAC scrubbing of the memories parity bit implementation Checksum verification and algorithm to reduce corruption of memories contents shall be implemented At least one error shall be corrected and 2 shall be identified e Procedure to reset on demand volatile RAMS or FPGA for critical part shall be foreseen MS PA REQ 3190 Verification Traces EXM MS RS ESA 00002 PA SY 1280 If the orbit is exposed to proton environment and if the Heavy lons LET threshold is lower than 15 MeV cm2 mg components need to be submitted to high energy proton test In case data are not available and upon customer approval contractor can extrapolate the expected induced error rate
80. Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 0 PAGE i TEST CONDITIONS SAMPLING PLAN Sub grp 1 Serialization 100 Sera a On Visual Inspection CSO SSCA BOOS STD 883 method 2009 100 Note C Temperature Cycling MIL STD 883 method 1010 100 Note A and Note C test condition C PIND Test MIL STD 883 method 2020 100 Note A and Note C cond A Radiographic MIL STD 883 method 2012 100 Note A and Note C Seal Fine and Gross MIL STD 883 method 1014 Note A and Note C Sub grp 2 Virginity Test if applicable Programming Note B Checksum Control Electrical Measurements Ta 25 C 100 Read and Record static and functional Ta 55 C 125 C 100 Go no Go Burn In Ta 125 C 168h min 100 Dynamic condition by means of proper test vectors dynamic bias for FPGA with activated clocks and activated logic and sequential chains Electrical Measurements Ta 25 C Read and Record static and functional Drift calculation 25 Electrical Measurements Ta 55 C and 125 C static and functional Percentage Defective Rejects on tests 13 and 14 Whole lot Rounded upwards to the calculation PDA 5 nearest whole number External Visual Inspection MIL STD 883 method 2009 Note C Note A Not to be performed if already performed by the manufacturer during initial screen
81. UTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 10 QUALIFICATION STATUS REPORTING 10 1 Off the shelf OTS Equipment DRD PA 42 MS PA REQ 4710 Verification Traces Subcontractor and Supplier will prepare an OTS list This document to be submitted to TAS ASI for review and Approval as per DRD PA 42 MS PA REQ 4720 Verification Traces EXM MS RS ESA 00002 PA SY 2220 An Off the shelf item is an item originally developed for a different project though possibly with a common or generic application which has been selected for reuse in the current project MS PA REQ 4730 Verification Traces EXM MS RS ESA 00002 PA SY 2230 The Contractor who decides to use an OTS item shall demonstrate its full suitability with the ExoMars requirements both on technical and PA aspects MS PA REQ 4740 Verification Traces EXM MS RS ESA 00002 PA SY 2240 OTS equipment shall be able to withstand the environmental conditions applicable to the ExoMars Mission during all mission phases MS PA REQ 4750 Verification Traces EXM MS RS ESA 00002 PA SY 2250 THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE Depending on the intended use the following classes of OTS equipment can be
82. Y 1270 removed S PDR RID PA PP 150 Para 7 4 2 2 MS PA REQ 3170 and MS PA REQ 3180 text of MS PA REQ 3170 partially moved to MS PA REQ 3180 editorial correction Para 7 4 2 2 MS PA REQ 3180 typo corrected error rate 1E 11 error bit day Para 7 4 2 2 MS PA REQ 3240 rewording according to S PDR RID PA PP 150 Approval of destructive single events sensitive components via RFD RFW Para 7 4 2 2 MS PA REQ 3230 rewording Para 2 1 2 update of reference documents THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION PAGE 9 175 M032 EN 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE TABLE OF CONTENTS 1 INTRODUCTION BE 15 1 1 EDD 15 1 2 Applicability sia veces anna ies ea enn ence eset enc ete eee AAAA eee Dace ese tein eee nce eset eee enter once AAAA EAA nce ARNAR 15 gn EECHER gege 16 2 1 Normative Documents cccetcssteeeeseeeeeeeee scene en eeeeeeaeeesaeeeeaeeeeeeeegaaesaseee se seeeseaaesaseeeeeseeeseaesasaesaeeenseeeeeas 16 2 1 1 Definition of Normative Documents sssssesssssensssrtnetttnetttttnnttttnntttt tnnt tA Annt tE Annt EE Annt EE Annn EAEan EEEn Enen 16 2 1 2 Thales Alenia Space Italia Normative Documents 16 2 1 3 ESA NASA Normative Documents 16 2 2 Informative Ne En LC 19 2 2 1 Definition of Informative Documents 19 2 2 2 Thales Alenia Space Italia Informative Docum
83. ailable for review by TAS ESA for the duration specified in the contract MS PA REQ 4010 Verification Traces TAS ESA reserves the right to request at any time a Data Package Review to verify that all activities and specifications as agreed in the relevant PADs have been effectively put in place in the procurement of components intended for Flight application prior to the actual integration of the components into Flight hardware MS PA REQ 4020 Verification Traces All initiated PADs shall be provided to TAS ESA prior to actually commencing the evaluation and or procurement of the relevant EEE component for ExoMars TAS may decline responsibility if the procurement authority CPPA or users fails to complain with this requirement THALES eer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 4030 Verification Traces Additionally upon request the procurement authority is responsible for the delivery to TAS ESA of the following documentation relevant to EEE components used in the project in electronic unlocked pdf format with meta data filled in Part Approval Documents signed Component procurement specifications Component Evaluations Radiation Test data Construction Analysis and DPAs MS PA REQ 4040 Verific
84. al Rectifier design requirements are as follow THALES aa All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE N Channel VG 0 Volt amp P Channel VG 0 Volt in OFF condition Single Event Gate Rupture sensitive parts could be used upon a case by case basis MS PA REQ 3240 Verification Traces EXM MS RS ESA 00002 PA SY 1300 As a preferred baseline approach only Single Event Latchup Free parts shall be used If it may be inevitable by performance requirements to use latch up sensitive components user shall demonstrate taking into account the Latch up figure of the device to have implemented suitable device countermeasures e g adequate fast current sensing and limiting and the rate of such events is so low than it will not affect the availability of the unit The following statistical approach could be proposed for not critical application only and whenever countermeasures implementation is not feasible Parts sensitive to Destructive Single Event Effects Latchup Gate Rupture Burnout may be used after the following analysis process Step 1 e To perform a heavy ion testing in order to get the accurate device cross section vs LETequ characterization curve e Tests will be performed at the application bias conditions no interpolation H The LET
85. all cause effects at System level of the severity categories 1 2 as defined in Table 5 3 1 No single hardware failure or operator error shall cause effects at Subsystem or Equipment level of the severity categories 1 2 3 as defined in Table 5 3 1 THALES heer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 er SDOCE ISSUE 05 PAGE MS PA REQ 1450 Verification Traces Improper command or command sequences or software errors e g originating from Single event Upsets shall not cause damage of hardware and shall not result in operational conditions which cannot be restored by ground command This is also applicable for ground testing of flight hardware Exceptions shall be approved by TAS ESA and shall be reflected in the ExoMars User manual MS PA REQ 1460 Verification Traces The failure tolerance requirement does not apply to hazards failures which are controlled by compliance with specific requirements other than failure tolerance so called Design for Minimum Risk areas of design Note examples are mechanisms structures glass pressure vessels pressurized lines and fittings functional pyrotechnic devices material compatibility flammability etc Controls related to these areas are extremely critical and warrant careful attention to the details of verificati
86. an for TAS approval in line with DRD PA 1 as per Document Requirements Description EXM MS RS ESA 0001 0 NR 015 MS PA REQ 0140 Verification Traces It shall become a formal and binding document which describes in detail the policy which will be implemented and the activities which will be carried out in order to fulfill the PA policy and requirements MS PA REQ 0150 Verification Traces The PA plan shall provide e A description of the Product Assurance responsibility and organization e A description of how the Product Assurance program will be implemented including critical areas for the ExoMars project and addressing each section of these PA requirements in the Product Assurance Plan e A Compliance Matrix wrt PA requirement document and for ECSS of level 1 and 2 ECSS Q XX where Q 00A 20B 30B 40B 60 B 70B 80B e A description of how the Product Assurance activities of the lower tier subcontractors will be defined and controlled THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 0160 Verification Traces The basic planning of the Product Assurance activities with correlation to the various project milestones shall be included in the Product Assurance Plan 3 4 Product Assurance data file and databases Addi
87. applicable qualification requirements with reference documents and relevant RFDs applicable documents which show the qualification achievement and relevant RFWs issued during the test campaign e the qualification status OPEN CLOSED MS PA REQ 0290 Verification Traces In addition the QSL shall contain a paragraph with a complete and exhaustive description of modification implemented on flight hardware e g design materials processes EEE components changes With respects to the hardware where the qualification achievement has been declared e g FM versus EQM including rationale for their acceptance MS PA REQ 0300 Verification Traces Final issue of QSL shall be submitted at the flight hardware Delivery Review Board THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 0310 Verification Traces In addition the subcontractors and suppliers shall provide at each project review a status list of proposed OTS to be used in the ExoMars project MS PA REQ 0320 Verification Traces The subcontractors shall demonstrate how the OTS complies with ExoMars requirements 3 11 PA and Safety Plan Addition to ECSS Q 00A para 3 2 MS PA REQ 0330 Verification Traces EXM MS RS ESA 00002 PA SY 60 The contractor s
88. ation Traces In case of confidential proprietary documentation users shall be available to organise meeting at their facilities in order to allow TAS ESA review 7 5 5 1 Parts manufacturer s documentation requirements MS PA REQ 4050 Verification Traces As a minimum the following documentation is required from the manufacturer for each delivery lot e Certificate of Conformance verifying that all requirements of the applicable purchase orders are met e Recorded values of measured parameters and calculated deltas related to serial numbers if applicable e LAT test report QClI report on the procured lot whenever requested e QCI generic lot data whenever requested e Any other data defined in the applicable procurement standards The originals of the documentation shall be stored at the facilities of the procurement authority and TAS ESA shall have access to these originals on request 7 5 6 Components Packaging Handling and Storage THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 ev SPACE ISSUE 05 PAGE MS PA REQ 4060 Verification Traces Parts delivered to the users shall be packaged in accordance with the requirements of the procurement specification For co ordinated procured items CPPA is responsible for an adequate packaging of the parts Users is re
89. ational illness or Loss of launch site facilities or Severe detrimental environmental effects on earth Critical Temporarily disabling but not life threatening injury to persons or temporary occupational illness or major damage to ground facilities or private public property or major detrimental environmental effects on earth 3 Marginal Minor injuries to persons or minor occupational illness or minor damage to or deterioration of property including the earth environment Table 6 3 1 Hazard severity categories MS PA REQ 2510 Verification Traces EXM MS RS ESA 00002 PA SY 980 Failure modes or activities which e g in case of human error can lead to consequences classified as category 1 2 or 3 shall be identified Potential hazards of category 1 and 2 shall be reported in Hazard Reports according to relevant DRD MS PA REQ 2520 Verification Traces Safety critical items shall be monitored and tracked in the CIL as part of the project risk management approach 6 4 Hazard Analysis Residual Hazards THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 2530 Verification Traces EXM MS RS ESA 00002 PA SY 990 The Subcontractor and Supplier shall carry out hazard analyses as earl
90. ax Vcc A Atmax 10us Voltage Ref AV max Vcc A Atmax 10uUs PWMs Double pulses two missing pulses multiple missing pulses in a row device shut off Asses impact in specific application MS PA REQ 3220 Verification Traces For each application subcontractor will demonstrate that a SET will not produce an out of specification and that the SET induced errors will not propagate outside the equipment The subcontractor will provide an evaluation of tha maximum pulse duration that his design will tollerate without detrimental effects This analysis will be included in the radiation analysis FMECA MS PA REQ 3230 Verification Traces EXM MS RS ESA 00002 PA SY 1250 As a preferred baseline approach only MOSFET operating in Single Event Burnout free condition shall be authorized In order to prevent permanent damage bias requirement is as follow For N Channel Power MOSFETs from International Rectifier design requirements are as follow VDS 50 BVDSS BVDSS 200 Volts For VDS above 50 or BVDSS gt 200 Volts for IR parts or other manufacturers Heavy lons data will be provided in order to demonstrate that the application is inside the SEB safe operating area of the part On top of tha above the ECSS Q ST 30 11 requirement para 6 29 applies POWER MOSFET P CHANNEL and BIPOLAR POWER transistors are SEB free As a preferred baseline only MOSFET SEGR free shall be used For Power MOSFETs from Internation
91. be listed and processed as critical items 5 6 Dependability Testing MS PA REQ 2210 Verification Traces The chapter 9 of ECSS Q 30 NR 7 applies with the following additional requirement MS PA REQ 2220 Verification Traces EXM MS RS ESA 00002 PA SY 740 Dependability testing shall also verify the correct functioning and performance of the on board FDIR capabilities Where ground intervention is required to perform FDIR for the flight segment to assure mission success the function and performance of these capabilities shall be verified end to end 5 7 Failure Propagation THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 2230 Verification Traces EXM MS RS ESA 00002 PA SY 750 No hardware or software failure shall propagate across the interface to a redundant item or functional path Note Requirement does not apply for functions which depend on other functions e g power Design shall be such that failure in one function shall not cause a fault in any other function MS PA REQ 2240 Verification Traces EXM MS RS ESA 00002 PA SY 760 No hardware or software failure of Ground Support Equipments shall cause damage to interfacing Flight Hardware THALES SE All rights reserved 2007 Thales Alenia Space C
92. csusuetesencastavanansseseaenssnenaiserntesenseesersanaqenseasasenteneastmnceawis 155 10 QUALIFICATION STATUS REPORTING isiiscscssessentsssxssnexicecanessaviaecesnennenesntexexstneanessonenceveanivnens 156 10 1 Off the shelf OTS Equipment DRD PA 42 s cccsssseeeeeseseceenseceeeeenseseeeenseneeesnseseeesnseseenenseeeenes 156 10 2 Qualification Status List QSL csscsssseesseeesseeseneeeenseeeeesaeseseeeenseeeeseseseaeseseeeeneeeeesaesessanensceeesensens 158 11 PA REQUIREMENT FOR GSE is eekkeueesseeeekieeekiteeg eseeteken eene EE de CEA EhEE ege 160 11 1 PA Manageme nt ccccesteeceeeesneeeeenseeeeennneeeeenaneeeeenaneeeeenaneeseeenaneeeeenaneeseeeaneeseesanaeseesaneeseesanaeseenaneeeeensne 160 11 1 1 FROVIGWS E E O E S E E 160 11 1 2 Design and Manufacture 160 11 1 3 DOCUMENTATION EE 161 11 1 4 GSE Dependability and Gate 162 11 1 5 General Requirements ccccccceccceeeeeeeeeeeee cess eeeaaaeegeeeecaaeeteaaesdeaeeseaeeecaaesseaaeseeeeeseaeseeaaeseeeeeeeeeess 166 11 1 6 MUER Crear er Spee ett re Eege ec 166 11 1 6 1 Criticality Categories A 166 11 1 7 Uer 166 11 1 8 OOTY sxe eeh Aeddi Eege ed eeh canada fiusathgkacdbeauepesatbabaetadaceessit Ae 167 11 1 9 EE 167 111 10 CleanlineSS and PP cscs ssccctvescescvaceqeveset sasdeastancedsseatdesiacsves aed vacasasassseviideawed vidadecssttaceatviaaseasiaiaeasdads 168 11 1 11 GSE Certifications UE certification USA Certification ec ceeeeeee eet e
93. cturer processes Complementary qualification shall be performed whenever micro component definition design processes mask has changed Each micro component Active or Passive lot shall undergo a User Lot Acceptance Test or element evaluation in accordance with ESA PSS 01 608 level B or MIL PRF 38534 Class K or ECSS Q ST 60 05 or alternative document approved by TAS ESA 7 4 6 3 MMICs MS PA REQ 3510 Verification Traces The design development manufacturing and testing of custom MMICs will follow the ECSS Q ST 60 12C MMIC in chip form to be used in hybrids In case of new development the procurement of working samples shall be considered in order to allow users experimenters to verify at least the suitability of the performances before starting the evaluation qualification flow 7 4 6 4 ASIC FPGA MS PA REQ 3520 Verification Traces EXM MS RS ESA 00002 PA SY 1550 The development prototyping manufacturing testing and validation of custom ASIC or FPGA for ExoMars shall follow the rules of ECSS Q ST 60 02 THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 3530 Verification Traces EXM MS RS ESA 00002 PA SY 1590 Users shall present to TAS ESA approval the trade off between ASIC and FPGA the decision shall be
94. d during the PAD NSPAR approval process 15 For crystals units the raw materials must be cultured premium Q swept for high stability application For crystals units the temperature and duration of the aging test shall be adequate to demonstrate and document that the frequency stability of the crystal meets the program life requirements The demonstration of the frequency stability of the crystal may be documented by the use of an equation of the form f t A In Bt 1 fo Where f t is the frequency of the crystal unit t days after the start of the aging cycle and A B and fo are constants to be determined from the least square fit The calculated frequency fo is the beginning of the aging cycle e Lot acceptance testing life test shall be performed on non qualified relays to show that the devices pass a minimum of 100 000 cycles 125 C operational test at the maximum rated voltage and current THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE 17 3 values lowest middle highest values by lot date code or periodically in order to verify processes stability e By lot date code 19 If the silver thickness is less than 2 um a corrosion test shall be performed to determine the suitability of silver plated wire cable materials Proposed test shall be agreed during the PAD NSP
95. d in ESCC QPL may be waived if 1 and 2 below are verified 1 In cases where design construction or process changes have not taken place compared to previous procurements 2 And only if LAT2 successful results have been obtained during the 24 months prior to the expected date code However LAT2 shall be implemented for certain families as follows regardless the history of the manufacturing line or previous LATs 1 LAT2 per assembly date code is required on non qualified chip solid Tantalum capacitors crystals fuses relays thermostats 2 LAT2 per wafer lot is required on non qualified microwave diodes integrated circuits F4 subgroups 2 and 3 per ESCC9000 NR 69 MMICs and microwave transistors MS PA REQ 3640 Verification Traces EXM MS RS ESA 00002 PA SY 1460 For MIL systems the following paragraph applies Regarding non space qualified components of US origin Quality Conformance Inspection QI and Periodic Inspection PI shall be implemented as required by the relevant MIL generic specification The sample sizes can be reduced for expensive components Such relaxation shall be agreed in the relevant PAD THALES er All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE QCI generic data shall be requested in case of critical procurement of components
96. d of EXO PCB Page 83 BC PCB instead of EXO PCB Para 4 11 Add DCL AS BUILT add note Para 4 8 1 Wrong reference to applicable DRL PA 9 instead PA 8 PARA 12 3 DELIVERY DAY OF EIDP 14 Instead of 15 EEE Para 4 7Alert System ADD PA SY 320 reference add sentence CPPA and users is responsible to maintain an Alert status list treacing applicability and corrective actions if any as requested in para 4 7 Para 7 4 8 Electrical and Qualification Model EM EQM ADD PA SY 1060 PA SY 1270 Modified printing error From I PDR RID PA 27 AND 29 Para 5 3 1 2 single point failure RID PA 84 Para 7 4 8 Electrical and Qualification Model EM EQM UPDATED RID PA 76 Para 7 3 2 Radiation radar hard Para7 3 2 Radiation hardness assurance add sentence ref table set maximum tolleration of transient hight THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 3 175 level Due to ESA PA Requirement updating rev3 3 Para all Typo corrected phase D included Para all ECSS Q 60C now applicable Para 2 1 3 modified to identify additional standard Para 2 1 3 ECSS Q 70 38A replacing former PSS document Para 2 1 3 ECSS M 40B now applicable Para 12 Exchanged numbering of outputs PA 32 and 33 Para 2 1 3 Suppressed reference to standard ASTM and added contamination depositio
97. d with the Spacecraft MS PA REQ 2140 Verification Traces EXM MS RS ESA 00002 PA SY 690 The Subcontractor and Supplier shall identify the preventive and corrective maintenance actions for ground operations including storage for both Flight Hardware and GSE Emergency restoration or repair activities necessary to sustain system capabilities crucial to mission success and launch availability shall be also identified THALES ee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 2150 Verification Traces EXM MS RS ESA 00002 PA SY 700 The contractor shall identify in a maintainability report those items that cannot be checked after integration that require late servicing access or replacement and limited life items or consumables MS PA REQ 2160 Verification Traces The maintainability activities shall consider also the Ground Segment of ExoMars and related GSE tools models needed for the successful completion of the mission 5 4 10 Availability analysis MS PA REQ 2170 Verification Traces EXM MS RS ESA 00002 PA SY 710 No numerical availability requirements have been defined for ExoMars However the Subcontractor and Supplier shall support any activity or analyses to derive outage frequency and duration if such
98. dentification of hardware by name Configuration Item number and model Next higher assembly level Manufacturer s name Supplier Proposed category A B C or D as defined hereabove Current qualification status screening and applicability of qualification test versus requirements with applicable qualification requirements with reference documents and relevant RFDs e basis for qualification qualification test results heritage and qualification on other projects programme on which the qualification test was conducted issued from specific Equipment Qualification Status Review as far as a heritage is identified Applicable documents which show the qualification T H A L E S M032 EN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE achievement and relevant RFWs issued during the test campaign e Project on which the test was conducted e test Report number e Identification of developments models EM EQM QM PFM to be manufactured and tested for the project if necessary e the qualification status MS PA REQ 4840 Verification Traces The qualification model will be fully representative of the flight model and any differences have been analysed to evaluate their effects on the qualification status THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED
99. diation susceptibility of the parts is at least the radiation design dose that is 2 times greater than the expected total dose for the whole mission This will be part of the radiation analysis In agreement to the applicable mission dose depth curve Total Design Dose TDD has been established considering the end of life deposited dose in the following configurations Orbiter Electronic Units mission duration 6 94 years 2mm Al eq from Spacecraft 2mm Al eq from box wall EOL Dose 7 96KRad that gives a TDD 16Krad Entry Descent Landing Demostrator Module EDM mission duration 296d up to separation 2 04mm Al eq from Shell 2 57mm Al eq from box walls that is 2mm perpendicular from box walls that gives 4 61 mm Al eq EOL Dose 1 63KRad that gives a TDD 4kKrad Rover Module Electronic Units mission duration 296d up to separation 218 sols around 520d dose depth curve applicable to EDM that is to 2016 mission because Nasa mission data are not available at the time of writing 2 04mm Al eq from Shell 2 57mm Al eq from box walls that is 2mm perpendicular from box THALES SES All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE walls that gives 4 61 mm Al eq RHU contribution around 1 7Krad for a silicon target at a minimum dista
100. ds so as to minimize the consequences to personnel flight hardware launch vehicle and facilities the Earth and Mars environment MS PA REQ 1210 Verification Traces EXM MS RS ESA 00002 PA SY 470 The Subcontractor and Supplier shall assign responsibility to suitably qualified and experienced staff for ExoMars Dependability Management MS PA REQ 1220 Verification Traces EXM MS RS ESA 00002 PA SY 480 The Subcontractor and Supplier shall be responsible for the establishment and maintenance of all dependability activities which are required by the ExoMars project THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1230 Verification Traces EXM MS RS ESA 00002 PA SY 490 The Subcontractor and Supplier shall participate in the approval of design documents to make sure that dependability requirements are suitably defined and implemented e g derating redundancy policy etc MS PA REQ 1240 Verification Traces EXM MS RS ESA 00002 PA SY 500 The Subcontractor and Supplier shall review non conformance reports change requests and MRB decisions to ensure that any impact on the system reliability has been accounted for MS PA REQ 1250 Verification Traces EXM MS RS ESA 00002 PA SY 510 The Subcontractor and Supplier sha
101. e CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 2640 Verification Traces Whenever feasible a fail safe design approach shall be used such that a failure brings the product in a safe state MS PA REQ 2650 Verification Traces The product design shall provide the capability for detecting failures that result in degradation of failure tolerance with respect to the hazard detection signaling and safing function The performance of these functions shall be verifiable during flight and ground operational phases MS PA REQ 2660 Verification Traces Emergency warning and caution data out of limit annunciation and safing commands shall be given priority over other data processing and command functions MS PA REQ 2670 Verification Traces Material selection shall assure that potential hazards associated with material characteristics are either eliminated or controlled If this is not feasible the design of the system and its parts shall include the necessary provisions to control potential hazards associated with material characteristics MS PA REQ 2680 Verification Traces Execution of functions which are identified as Safety critical severity category 1 and 2 if not performed shall be implemented by two or three independently routed n
102. e Mission and System Requirements Document and Rover Requirements Document if this is the case they will supersede the general requirements spelled out in this document Implementation of redundancy MS PA REQ 1490 Verification Traces Redundancy concepts shall be considered to minimize consequences of single point failures Whenever practical design based on redundant elements shall be implemented This shall include the use of redundant wiring connectors and functions where commensurate with mass etc Specific redundancy requirements shall be defined in the applicable specifications document sections MS PA REQ 1500 Verification Traces Where redundancy is employed the design shall allow operating and verifying the redundant item function independently from the nominal one MS PA REQ 1510 Verification Traces Each redundant path or function shall meet the full performance requirements THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1520 Verification Traces The specified function and performance of each redundant element shall be capable of being measured during specified test phases MS PA REQ 1530 Verification Traces Cross strapping shall be incorporated in betwee
103. e applicable Planetary protection EXM MS SSR AI 0007 NR 0120 MS PA REQ 0830 Verification Traces EXM MS RS ESA 00002 PA SY 350 The Contractor shall identify the hardware and facilities that require specific controls for molecular or particulate contamination This includes e g ultra cleaning for hardware coming in contact or surfaces in direct view to such hardware with Mars samples Definition of requirements their means of verification and control shall be stated Deleted MS PA REQ 0840 Verification Traces EXM MS RS ESA 00002 PA SY 370 The introduction of the additional requirement of bioburden for planetary protection requires the consideration of all three entities molecular contamination particulate contamination bioburden in conjunction MS PA REQ 0850 Verification Traces EXM MS RS ESA 00002 PA SY 380 THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE In addition to par 6 5 in the ECSS Q ST 70 01A Packing containerization transportation and storage the condensation of moisture or contaminants on cold surfaces during test or transportation shall be prevented MS PA REQ 0860 Verification Traces EXM MS RS ESA 00002 PA SY 390 Whenever possible optical equipment shall be closed and purged with ultra clean
104. e warranted Alert Status and resolution of alerts shall be included in regular PA status reports This alert status reporting shall cover SW production environment e g compilers production SW and COTS 4 8 Cleanliness and Contamination Control MS PA REQ 0810 Verification Traces THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Cleanliness and Contamination Control requirements are contained in the TAS specification EXM MS SSR AI 0005 EXOMARS Cleanliness and Contamination control Requirements NR106 with the following supplement e All requirements relevant the cleanliness levels identified by ECSS process documents have to be considered e The subcontractors and suppliers shall evaluate the specific needs of contamination prevention monitoring and control at all stages of handling testing integration transportation and operation for spacecraft components and they shall provide facilities and implement procedures which prevent contamination in accordance with requirements and guidelines outlined in NR106 Deleted MS PA REQ 0820 Verification Traces EXM MS RS ESA 00002 PA SY 340 All MAIT manufacture assembly integration and testing activities shall be performed in an ISO class 8 clean room or cleaner in conjunction with th
105. eas 70 5 4 4 COMLINGENCY En EE 71 5 4 5 Common Mode and Common Cause Failure analyses seeseesieeieeieeeineernssirestnesrnnsrnnsrnnsnnssrnsnrnn 71 THALES e All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 5 4 6 Reliability Prediction cc ccceecsceceeececeeeeeeeaeeeeeeeeaeeeeeaaeeeeeeecaeeeeaaeeseaaeseeeeeseaeessaaesseaeeeseaeescaeeesieeseeneeseas 71 5 4 7 Worst Case Analysis ccccccecseeceeeeececeeeeeaeeeeeeeeseaeeeeaaeegeeeeceaeeseaaeeseaaeseeeeeseaaeeseaaeseeeeseaeessaeeesaeseeeeesaas 72 5 4 8 Part derating analysis 73 5 4 9 Maintainability Aesesement cece aeeeeaaeeeeeeeceaeeecaaeeeeaaeseeeecaeeseaaeeseeeeeseaeeesaesnaaeseeeeeeeas 73 5 4 10 Availability analysis 74 5 4 11 Hazardous Commands Wenttftcaiion eee tte tertsen nssr rsttn ttn netnnstnnstnnsttnsnustnnsrnnsen nanta 74 5 5 Inputs to Critical items list CIL EE 75 5 6 Dependability Testing EE 75 5 7 Failure PropaQ ations acesancccntecesieetsctvesccceessceesaneccestenseweteocecsacueeucdeetecivendeseuaceeronsvdetteescesesenucectedevadeseenuerects 75 Gis SREY spss eiseiict ccna acini E A A E A A A 77 6 1 EE g l e E A E E E E E 77 6 2 Safety Management and Planning cs ecceceeeeeeeeeeeeeeeseeeeeeeeeesaesesneeeneeeeeeaesasaaesaseeeeeeeeeseaeseeseeeeeneeneanes 80 6 3 Hazard Severity Categories sirini
106. ed from MIL HDBK 5 Metallic materials and elements for aerospace vehicle structures Other sources shall be subject to ESA approval Composite structure allowable stresses shall allow for degradation due to moisture temperature and process variables The material justification shall prove hardware structural integrity during storage and on orbit life time MS PA REQ 4580 Verification Traces EXM MS RS ESA 00002 PA SY 2030 Fracture sensitive materials shall be subjected to fracture control as in ECSS E 30 01 Fracture control ECSS Q ST 70 36 Material selection for controlling stress corrosion cracking and ECSS Q ST 70 37 Determination of susceptibility of metals to stress corrosion cracking Materials for which no fracture mechanics data is available from MIL HDBK 5 NR 70 shall be tested in acc with ECSS Q ST 70 45 8 17 Limited Life Time THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 ser Space ISSUE 05 PAGE MS PA REQ 4590 Verification Traces EXM MS RS ESA 00002 PA SY 2040 Materials with limited life characteristics shall be subject to lot batch acceptance tests according to ECSS Q ST 70 22 Control of Limited Shelf life Materials MS PA REQ 4600 Verification Traces EXM MS RS ESA 00002 PA SY 2050 Items and materials that have a limited l
107. ed test program the test methods and sample size shall be approved as defined in the Parts Approval section of this document before test commencement and shall be available for review After completion of the evaluation testing a final review of the proposed procurement specification shall be carried out to determine if the obtained results will have an impact on the content of the procurement specification 7 5 1 1 4 Evaluation report MS PA REQ 3910 Verification Traces The full details of the evaluation testing the results achieved and an overall assessment of the complete evaluation program shall be included within the evaluation report which once complete shall be available for TAS ESA approval 7 5 1 2 Radiation characterization MS PA REQ 3920 Verification Traces Radiation tests shall be performed to assess the parts sensitivity for EXOMARS environment in accordance with the radiation requirements as described in para 7 4 2 7 5 2 EEE NCR MS PA REQ 3930 Verification Traces EXM MS RS ESA 00002 PA SY 1630 ECSS Q 20 09B applies In particular paragraph 6 1 shall be read in conjunction to the following The NCR shall be issued by the procurement authority The NCR may occur either at the parts manufacturer during shipment after receipt at CPPA after receipt at the user on ExoMars equipment failure due to a parts problem The non conformance control shall be applied throughout the progra
108. eeeeeaaeeeceesaeeeceeeaaeesssesaeeesssaaeeesseqaeeeeseateeeseaas 97 7 4 2 1 Displacement damages and NIE 102 L CNR EE 103 T 4239 RADIATION REVIEW s2epissecccses tedesds conc veces eeneg aE aE RE A EAEE NES 106 LAS COMPONENT DeratiNg EE 108 74 4 EEE Components Approval isiiisccccvesscecsncessacecessecvet dee cece visa sac cadeedoscyasised coven caste niaset cava aai aaa ais 108 7 4 5 EEE component procurement specification ccccccceeceeeeeceeeeeeeeeeeeeeeeeeeesaeeseaeeseeeeeseaeeseaeeneeeeess 109 TAG Quality LOVE carns eaea E E E ege dE ebe gege 110 GAGA Additional ests ET 111 7c oye AER 113 THALES acs All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION ThalesAlenia 7 5 7 5 1 7 5 1 1 7 5 1 2 7 5 2 7 5 3 7 5 5 7 5 5 1 7 5 6 8 1 8 2 8 2 1 8 3 8 3 1 8 4 8 5 8 5 1 8 6 8 7 8 8 8 9 8 10 8 11 8 12 8 13 7 4 6 3 7 4 6 4 7 4 6 5 7 4 7 7 4 8 7 4 9 7 4 10 7 4 11 MATERIALS PROCESSES AND MECHANICAL PARTS MPM CONTROLLED DISTRIBUTION REFERENCE DATE Space ISSUE Quality Assurance amp EEE Parts NCR q cccccssccsseesseeeeeeeeeesneeeeseeeeneeeneeae Manufacturer and part evaluation 0 cccccceeeeeceeeeeeneeeeeeeeseeeeeeeeteeeees Evaluation program oe cececececceeecceeeenseeeeeeeteaeeeeeaeseeaeeeseaeeeseaeeteeeteaes Radiation charachertzaton eerren Components in Off the shelf eouipments rerne 7 5 4 Use of St
109. eeeeeeeaeeseeeeeteaeeeeaeeeeaes 168 11 1 11 1 WE GSE lee EC 168 11 112 RE MEIER EE 168 12 DRL FOR PRODUCT ASSURANCE sissceisscraseiserstszsannasencieiacansncansnasdcenanasaseessetacaensenreieneaninseniens 169 12 1 HW SW DRL PA DOCUMENTS 25 nesnnennnnununnnnunnnunnnnnnnnnnnnnnnnnnnnannnannnnnnnnunnnnnnnnnnnunnnunnnnnnnannnnannn annen 169 12 2 GSE DRL PA DOCUMENTS bt geeENEE NEESS EENS 172 12 3 Notification Delivery Time SUIMMALPY ccccceeeeseeeeeeeeee sees eeneeeeneeeeeeaeeesaesesneeeeeaeseseaesaseeeeneeeeneneas 173 12 4 ClASS ACHOMYINS E 174 THALES RE All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE 1 INTRODUCTION 1 1 Scope This document defines the EXOMARS Product Assurance requirements for Subcontractors The Flight elements operation regime and associated GSE and associated HW SW shall be designed manufactured tested and operated in compliance with these requirements which are applicable to subcontractors and their suppliers 1 2 Applicability The requirements are applicable to the all Flight elements flight hardware flight software and flight spares Other hardware and software shall be safe for ground operations and shall be representative of flight hardware with respect to form fit and function and shall not lead to the failure or degradation of
110. eer Space ISSUE 05 PAGE The subcontractors and suppliers shall prepare the EIDP for any deliverables as per applicable SOW MS PA REQ 0940 Verification Traces Lower level EIDPs shall be maintained and relevant data shall be integrated into higher level EIDP MS PA REQ 0950 Verification Traces The EIDP shall be in accordance to ECSS Q 20B Annex C and B MS PA REQ 0960 Verification Traces It shall contain as a minimum e certificate of conformance as built configuration list including DCL as built temporary installation records e g remove before flight items open deferred work open tests missing items proof load certificate cleanliness and PP certificate integration operation and maintenance manual including engineering drawings and electrical functional schematics special packaging handling and shipping procedures packing list including loose items and spares MIP KIP tracking list MIP reports design and verification compliance matrix acceptance test reports interface control document logbook DRB minutes of meeting critical items list limited life items list CIDL qualification status list status lists NCRs RFDs RFWs non conformances reports major and minor request for deviations THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DAT
111. emperature of a material during the lifetime is exceeding for longer periods 50 C the use of such material shall be evaluated further through an appropriate test program mutually agreed between customer and supplier Such program shall ensure that the characteristics of the material at the EOL are still within the specified requirements Output The requirment shall be fulfilled through the deliverable PA 27 Deleted MS PA REQ 4460 Verification Traces EXM MS RS ESA 00002 PA SY 1860 In view of contamination criticality for instance in the vicinity of sensitive optical surfaces or surfaces that come in contact with Mars samples more stringent requirements or more detailed material information such as outgassing data according to ESA VBQC test are required The results shall be reflected in DRD PA 09 8 9 Thermal Cycling MS PA REQ 4470 Verification Traces EXM MS RS ESA 00002 PA SY 1870 Materials incl non flight hardware subject to thermal cycling shall be assessed to ensure their capability to withstand the induced thermal stresses following ECSS Q ST 70 04 MS PA REQ 4480 Verification Traces EXM MS RS ESA 00002 PA SY 1880 Materials used at cryogenic temperatures 80 K or lower shall be qualified for the worst case conditions 8 10 Environmental Interaction THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERE
112. en the test will be continued up to 20 krad with standard low dose rate of 0 1 rad s A step of room temperature annealing need to be added e g 24hrs This would mean around 12 days of test MS PA REQ 3130 Verification Traces For Rover the effect of residual gamma and neutron emission of RHU shall be considered in the radiation analysis 7 4 2 1 Displacement damages and NIEL MS PA REQ 3140 Verification Traces EXM MS RS ESA 00002 PA SY 1 240 The utilization of optoelectronic CCD APS etc silicon Ga As and other compounds shall be analysed as far as sensitivity to proton induced displacement damage and generally to NIEL End of mission expected proton fluence normalized 10MeV is Orbiter Electronic Units mission duration 6 94 years 2mm Al eq from Spacecraft 2mm Al eq from box wall for silicon target EOL Total Fluence 1 99 10 that gives with a safety factor of 2 a DDEF 4 10 10 MeV eq protons cm Entry Descent Landing Demostrator Module EDM mission duration 296d up to separation 2 04mm Al eq from Shell 2 57mm Al eq from box walls that is 2mm perpendicular from box walls that gives 4 61 mm Al eq for silicon target EOL Total Fluence 4 13 10 that gives with a safety factor of 2 a DDEF 8 3 10 10 MeV ea protons cm Rover Module Electronic Units mission duration 296d up to separation 218 sols around 520d dose depth curve applicable to EDM that is t
113. enseeesecaesesenseeeeeeenaes 27 3 11 PA and Safety Plan Addition to ECSS Q 00A para 3 2 ccessceseeseeeeeseeesenessessnensenesseessnenseeesseesnes 29 4 QUALITY ASSURANCE REQUIREMENTS cccccccccssssssssteeeeeeeeeeeeneeneeneeeeeeeeeesaseeneeeeeeseseseeeeeesnones 31 4 1 Quality Assurance Plan s ssssnssunssunnnunneunneunnnunnunnnnnnnnnnnnnnnn unnn nnnnnnnnn nunn nnnn nnne nnnn ennn nnnn ennnen nnna nn nanne anneanne ennen 31 G D S Neu Ve elen EE 32 41 2 QA Stirveillance EE 32 4 2 FRO CUU IONIC INES EE 32 THALES ee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 4 3 PA Programme Audits ccceeeetceceeeeee ee eeeeee ee eeenee sees neon see eeee sens eeee see eeeeeeseseeneeseseeeeeseseeneeseseeneeseseneeeeseenanes 32 4 3 1 Audits Addition to ECSS Q 20B pDara4g cece eee aeeeeaee senses case eeeaaeseeeeeeeaeeeeaeeseeeseeeees 34 4 4 Critical tems Control ege EEN senda caves suas dE SEN 34 JAT Critical Item defiNitionS ccc ecececssscecscsseeeecsecaceecscueeecsesaeeecseaaeeecsesaesececesaeeecseaaeeesseaaeseceseeesseneeesees 35 4 5 Non conformance Control System RFW and Deviations ccsssccseeeseeesseeseseeeeeeeeeseeeseneeneneeeeees 38 4 5 1 Failure analysis 20 2 cece eeeeee cece ee eeceeeeaaeeeeeee eee eeeeaaeedeaee cease ca aeeeeaaeseeeeeseeeesa
114. ent updated Para 7 4 8 BC PCB corrected in EXO PCB Para 7 5 1 reference to PA SY 1620 corrected 8 Material and Processes Para 8 X ref PA SY 1810 1830 1870 1980 2030 2070 2120 modified for new ECCSS alignment Para 11 1 11 add paragraph GSE Certifications UE certification USA certification PARA 12 1 DRL Updated 25 ADD TAS I PA Requirements numbering e g MS PA REQ XXXX THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN 21 01 2011 CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 SPDR RIDs Implementation REF RID ACTION BDREPAPP2AR003 Para 2 1 2 EXM MS SSR AI 0005 NR 106 Cleanless contamination and conrol requirements iss 07 NR0438 ExoMars RM Cleanliness and Contamination Control Requirements EXM RM SSR AI 0015 NR0439 ExoMars RM Cleanliness and Contamination Control plan EXM RM PLN AI 0078 Para 11 1 11 1 TAS I to update the PA requirements for sub co s to include the information concerning CE marking as stated in TAS I reply from RID PA PP 97 Change with correct references a Low Voltage Directive 2006 95 EC 12 12 2006 b EMC Directive 2004 108 EC 15 12 2004 Para 7 4 2 MS PA REQ 3120 ELDR test method updated S PDR RID PA PP 150 Para 7 4 2 2 MS PA REQ 31xx new requirement to address PA SY 1270 S PDR RID PA PP 150 Para 7 4 2 2 MS PA REQ 3170 reference to PA S
115. ents cccccceeeeeeeeeeceeeeeeaeeeeaeeseeeeeeeaeeetaaeeseaeeseeeee 19 2 2 3 ESA NASA Informative Documents 19 3 PRODUCT ASSURANCE REQUIREMENTS cccccccccesssseeeeceeeeenseseeneeeeeeseseseeeesesneeeeseseseeeeeseneeees 21 3 1 Organisation and Manageme nt ccccssccssseeeseeeeeeeeeseeeeeseeeeeeaesesaaeseseeeeeeeeesaesaaeeeeneeeeeseaesaseeeeneeeenenenas 21 3 2 PA progress reporting Addition to ECSS Q 00A para 3 5 3 ccccsseseeeseeeseeenseenseenseeneeenseeeseeneneees 23 3 3 Product Assurance Plan cesseecceceeeeeeeeeeeeeseneeeee ee eeenee sees eeee seen eneeseseeneeseseeeenseseseeeseseeneeseseeeeeseseneeeeseeeanes 24 3 4 Product Assurance data file and databases Addition to ECSS Q O0 cssssensseseenessseeneeeesenes 25 3 5 Subcontractors Suppliers PA Program s cccescesseeeeseeeeeeneeeenesesaeeneeeeeesaesesaaesaseeeeeeeeeseaesaseeeenseeeeeeees 26 3 6 Right of Access Participation ccccsseccceseeeseeeeeeeeeeeeeeeeeeeeeeeeeeseeeeeseeeeeeeeseseeeeeseseeeeeseseenensesaeeeeeeseenenes 26 3 7 eege EUR Ee 27 3 8 PA involvement in overall project COCUMENtATION scccseeeeeeeeeeeeeeeseeeeeeeneeeeaeseseeeenseeeeeeeeeneaeseeeeeeees 27 3 9 Integration of lower data at higher level ccceeececeeeeeeeeeeeeeeeeeeeeeeseseeeeeseeeeneeseseeneeseesesneeseseeeneseenaees 27 3 10 Qualification Status REPOrting cecccesceessseeeeeeee eens eeseeeeeeeeeeeeesesnaeesneeeeeeeeeesaaesaseee
116. erification Traces The Safety effort will be directed e to identify potential hazards during ground operations e to eliminate the hazards from the design where possible e to minimise and or control the non eliminated hazards residual hazards THALES Ke All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE e to recommend management decision to resolve hazards or to assume the residual risk e to document those areas for which a decision has been taken to assume the risk including the rationale for the decision e to implement appropriate control measures for residual hazards e to support the Safety Review Process for the pertinent responsibility level e to certify that the ExoMars Spacecraft Composite including the Descent Module the Rover Module and all the scientific experiments is safe and complies with the applicable Safety requirements for the pertinent responsibility level MS PA REQ 2290 Verification Traces EXM MS RS ESA 00002 PA SY 800 The safety programme shall ensure compliance to the Launch Authority safety requirements and the applicable international and national safety regulations including the legal European Union requirements related to the product liability where appropriate during design manufacturing integration testing handling
117. es The contractors shall provide the safety data packages in compliance with the Launch site and the Nuclear Safety Authority requirements MS PA REQ 2450 Verification Traces EXM MS RS ESA 00002 PA SY 910 The Subcontractor and Supplier Project Safety Management shall review system and subsystem specifications to ensure that these specifications address the project specific safety requirements and that compliance is adequately verified by analyses reviews of design test and or inspection and that this verification is fully documented Project Safety representatives shall participate in all system design reviews and provide evidence that the specific objectives and tasks of each project phase are met THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 2460 Verification Traces EXM MS RS ESA 00002 PA SY 920 The Subcontractor and Supplier Project Safety Management shall make sure that the safety requirements are known and implemented by all contractors participating in the project MS PA REQ 2470 Verification Traces EXM MS RS ESA 00002 PA SY 930 The Subcontractor and Supplier shall describe in his Product Assurance Plan or in a separate Safety Assurance Plan the detailed tasks and the procedures which will satisfy the req
118. eseeaaeeseeeeeeeessaeeseeeseeeeens 40 4 6 WAIVGIS sons ccictccceccetsteececctcescce edanan oaa a aaia daada aea aaraa aa aaeain iaaa dai eecuaseud vexezeecenesteers 40 4 7 Alert Syste seess Eege 40 4 7 1 Details about Alert Problem notification see para 7 3 9 of this document 41 4 8 Cleanliness and Contamination Control ccsecccescesseeeesneeeeeeeesceeseseeeeeeeesescaeseseeenseeesseesesnaesenseeeeeeanas 41 4 8 1 Cleanless and contamination control Plan 43 4 9 Test Fea Cultus cis sc at es cee ecg ce sated aaa aa Seca Peek nse aap aaaea aaa a aa aaa aa aA a a a 43 4 9 1 Test Performance Monttoring nnna 44 AAO TOSt RE POMS a E E E A 44 4 11 End item Data package EIDP ccccssccssseeeeeeeeeeeeeee seen ee eeeeseaeseaaae sa seeeeeeesaaesaaneeeneeeeesaesaseeesneeeenseaess 44 4 12 Delivery review bards cccsecccceeeee eee eeeeeeeeeeeeee seen seen sees eeeeseseeeeeseeeeeeeeseseeneeseseneeeseseeeeeseseeneeseeeeneeeeenenes 46 4 13 Packaging Marking and Labelling TranSportation cccseecccceeseeeeeeeeeneeeeeeeeeeeeeeeeseeeseeeseeeseeneeeeseees 47 4 14 Handling Storage Preservation ccccsscccsecsseeseseeeseeeeeseeeeseaeseseeeenseaeessesesaesaseeeeeeeeeessaesaseaeeneeeeneeaeas 47 4 15 Inspections PA SY 465 sicciiiciceccisisceriiesccesccusserediencetiawmnecerdesscey teusteouedanseersuansuceysvesteevedanbecrvesuesteveuwcsey 48 4 16 Electrostatic Discharge COntroll ccccssccssseeceseeeeeeeseseeeeneneeeeeae
119. f 31 inventory list PA 32 PA Data for compatibility with x x x x AR Acceptance at 32 processes for bioburden QR only To be reduction updated also in support of System Reviews PA 33 PA Hardware compatibility with DELETED 33 bioburden assessment covered by PA procedures 27 28 29 PA 34 PA Materials justification for COVERED BY 34 contamination critical hardware PA 09 PA 35 PA Limited life items status list DELETED 35 Covered by PA 3 PA 36 PA High reliability soldering for DELETED 36 surface mount and mixed technology PA 37 PA Software PA Plan x x D AR for acceptance at 37 KO and s s PDR others for review PA 38 PA Software Criticality Analysis x x x AR for acceptance at 38 Report System PDR and S S PDR others for review PA 39 PA SW PA Requirements for Subco has to use 39 Subco s TAS I doc EXM MS RQM AI 0010 PA 40 PA Software Product Assurance x x D D R 40 Report PA 41 PA Software Maintenance File D D for acceptance at 41 QR and for review at FAR PA 42 PA OTS list and related justification x 42 reports Included in PA TAS1 PA 43 PA Hazard Analysis and Safety DELETED 43 critical functions at System Applicable PA Level 19 PA 44 PA Inputs to Safety Data Package safety DELETED part 44 for Launch Vehicle reviews of PA 17 and PA 19 PA 45 PA Request For Approval RFA for As A 45 materials amp processes generated PA TAS1 Qualification Status List D D D D D R Including pr
120. f functionality Any other effect Table 5 3 1 Failure consequence severity categories Note Subsystem level e g Data Handling Power Guidance and Navigation etc for each Module Unit or Equipment Level any unit or equipment belonging to a specific subsystem 5 3 1 2 Single Point Failure Definition THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1370 Verification Traces Single Point Failure SPF an item or function for which no redundancy or back up is implemented in the design a failure will result in the unrecoverable failure of the analysed product MS PA REQ 1380 Verification Traces Critical Single Point Failure e SPF with a consequence severity category 1 or 2 e SPF with a consequence having hazard severity category 1 or 2 i e Catastrophic or Critical due to safety reason MS PA REQ 1390 Verification Traces Single point failures with a consequence severity category 1 2 3 shall be summarised in a Single Point Failure List MS PA REQ 1400 Verification Traces EXM MS RS ESA 00002 PA SY 730 Critical Single point failures which cannot be eliminated from the design with reasonable effort or fault tolerance requirements which cannot be met shall be tracked in the Cr
121. failure schedule slips qualification problems a backup procurement must be initiated The obsolescence risk shall be kept under control when components are selected and approved for project application their availability throughout the project lifetime shall be assessed by the procurement authority and when an availability risk is expected a backup solution shall be identified Subcontractors shall provide to TAS a Long Lead Item List status with the information relevant to the reason for long delivery estimated delivery in weeks need dates date of purchase order placement as part of the progress report THALES eo All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE CPPA shall provide to TAS ESA with a planning for parts procurement that shall be updated for each EXO PCB 7 4 9 Alert Problem notification MS PA REQ 3680 Verification Traces EXM MS RS ESA 00002 PA SY 300 CPPA as well as users shall participate to the ESA alert system and screen alerts and problem notification as a day by day activity of the component control plan Any alert problem applicable to a component listed in EXO Master Part List shall be notified immediately by the CPPA to the users and to EXO PCB The CPPA is responsible to provide with the user EXO PCB any details available of the
122. failures This shall be performed at the level of the Software Requirements Baseline and Interface Requirements MS PA REQ 2010 Verification Traces EXM MS RS ESA 00002 PA SY 620 The HSIA shall be performed in accordance with section 4 10 of ECSS Q 30 02 and reflected in the FMECA THALES are All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 5 4 4 Contingency Analysis MS PA REQ 2020 Verification Traces EXM MS RS ESA 00002 PA SY 630 ECSS Q 30 section 8 2 2 c shall not apply 5 4 5 Common Mode and Common Cause Failure analyses MS PA REQ 2030 Verification Traces EXM MS RS ESA 00002 PA SY 640 CMF and CCF analyses shall be performed to identify single potential causes capable to take out redundancy Comment The analysis shall be performed as part of the FMECA 5 4 6 Reliability prediction MS PA REQ 2040 Verification Traces EXM MS RS ESA 00002 PA SY 650 ECSS Q 30 Clause 8 2 2 g shall apply with the following addition A quantitative reliability requirement numeric figure for probability of success is not required for the ExoMars spacecraft composite However upon request by Prime ESA quantitative reliability assessment shall be prepared to show the reliability of the design and used for comparison of alternate design concepts on system
123. g documentation can be applied Besides ECSS this can be MIL NASA or ISO standards In case of conflict ECSS standards shall prevail 4 1 2 QA Surveillance MS PA REQ 0430 Verification Traces QA surveillance for development and engineering models shall be proposed as part of PA Plan by the subcontractors and suppliers considering the complexity of activities consequences of potential mistakes and relevant impact to the overall program It will be implemented upon received approval from TAS ESA 4 2 Requirements MS PA REQ 0440 Verification Traces The quality assurance plan which defines how the subcontractors and suppliers will ensure compliance with the quality assurance requirements defined in this document shall be part of the Product Assurance Plan 4 3 PA Programme Audits MS PA REQ 0450 Verification Traces Besides regular monitoring of the Product Assurance activities the subcontractors shall plan and implement a program of audits on his own and on his lower tier subcontractors facilities and activities in THALES REH All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE order to ensure that they are adequate for the intended applications and comply with applicable requirements MS PA REQ 0460 Verification Traces
124. gency under TAS ESA control The CPPA under TAS ESA direction will enforce since the design phase a program for control and selection of components which will ensure maximum use of qualified parts minimise the number of part types guarantee the radiation tolerance required by the mission assess the compatibility with sterilization techniques harmonise as far as possible the experimenters and the satellite users needs schedule minimize the ITAR covered items and keep them under a tight control with the goal of achieving an effective component standardisation In order to cope with the stringent program schedule a Preferred Parts List will be prepared as one of the first agency B2 task The EXO PPL will be reviewed and approved by the Exo PCB during early phase B2 The PPL will not be limited to EPPL and NSPL listed qualified components but will be a living document listing those critical functions that are needed by the users applications and need a particular effort in standardization due to delta qualification effort different package layout etc Any subsystem unit contractor called user in this context shall use the EXO PPL as baseline for the components selection MS PA REQ 2930 Verification Traces EXM MS RS ESA 00002 PA SY 1110 EXM MS RS ESA 00002 PA SY 1120 Periodical dedicated meeting EXOMARS Parts Control Board EXO PCB are convened in accordance to EXM MS PLN AI 0024 among CPPA TAS and ESA Components manufacturers
125. h the coordinated channel and shall pro actively cooperate with CPPA in the standardization task providing if necessary technical justification for the selection of part types not included in EXO preferred part list master part list Users shall support CPPA and TAS with his specific expertise for selecting suitable part manufacturers providing background information for the preparation of specifications type approval screening programs and approval documents Users are requested to nominate within their ExoMars team a key person responsible to interface the CPPA for any technical programmatic or financial issue This point of contact shall have also the task to participate to the communication system that will be implemented in the program he shall be requested to participate to the standardization process to the EXO PCB on request to NCR process whenever applicable He shall also act as point of contact between CPPA EXO PCB and engineering quality and purchasing department of the relevant company Even in case of full coordinated procurement users are considered fully responsible concerning selection and application of EEE parts with respect to the project requirements They also are considered responsible for self procurement of special parts not supplied through CPPA The Self procurement will be authorized on a case by case basis Typical examples of self procured items are e Customized items Unique parts exotic parts ASIC MMIC In
126. hall establish and maintain a PA plan to describe the resources tasks responsibilities methods and procedures selected for the implementation of the PA and Safety requirements MS PA REQ 0340 Verification Traces EXM MS RS ESA 00002 PA SY 70 The PA and Safety plan shall describe how the contractor intends to verify that the programme will be accomplished and how he intends to perform supervisory and monitoring actions on sub contractors and suppliers MS PA REQ 0350 Verification Traces EXM MS RS ESA 00002 PA SY 80 The PA and Safety Plan shall be supported by a compliance matrix against the normative requirements and the ExoMars Mission specific modifications cited in this document including an organisation chart showing responsibilities and reporting The contractor shall provide a justification and an equivalent THALES EE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE alternative approach for any non compliance MS PA REQ 0360 Verification Traces EXM MS RS ESA 00002 PA SY 90 The PA and Safety plan shall be delivered with the proposal to be approved by TAS I ESA THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 0
127. he procurement responsible and any later EEE parts user during storage handling MS PA REQ 3790 Verification Traces Traceability of EEE parts during installation in unit shall be ensured by the Subcontractor to provide the traceability of the actually mounted components manufacturer lot Date Code number This shall be reflected in an as built DCL parts list 7 5 Quality Assurance amp EEE Parts NCR 7 5 1 Manufacturer and part evaluation MS PA REQ 3800 Verification Traces EXM MS RS ESA 00002 PA SY 1610 THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Users for authorized self procurement shall ensure that the parts are procured from the selected manufacturer and in compliance with the requirements defined in this document In case that a valid and acceptable qualification cannot be demonstrated a Part Evaluation program in conformance with requirements of Class 2 parts in ECSS Q ST 60 shall be implemented The content and extent of such a program requires approval of EXO PCB The results of the test audit analysis performed in the frame of the evaluation programme shall be collected in an evaluation report submitted to EXO PCB review and approval in case the evaluation has been conducted by CPPA in the frame of co ordinated
128. hods and design analysis to be in line with ECSS Q 20 04A Annex C MS PA REQ 0620 Verification Traces Subcontractors and suppliers shall detail in the Critical Item List all issues that cannot be resolved and single point failures that cannot be eliminated with detailed retention rationale MS PA REQ 0630 Verification Traces The CIL produced by the supplier will be processed and approved by each customer of the ExoMars customer supplier chain MS PA REQ 0640 Verification Traces The CIL will take inputs from lower level CIL in a build up process to generate the subsystems and spacecraft higher level CIL MS PA REQ 0650 Verification Traces Criticality classification will be assessed to rank lower level effects and establish their resulting influence on higher level functions THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 0660 Verification Traces Progress Report shall contain the status of Critical Items including the updated Critical Items control forms MS PA REQ 0670 Verification Traces EXM MS RS ESA 00002 PA SY 200 These risk items shall be tracked and controlled via the project risk management programme which shall be reported on a monthly basis except where fai
129. house manufactured hybrids add on dice parts for hybrid Parts that were selected late in the project e g due to late functionality definition NCR corrective action for which the user could not place the purchase order within the CPPA established cut off dates Users shall interface directly the CPPA to define orders quantity lead time and recurrent cost The direct cost for parts ordered for the ExoMars flight units shall be paid directly by the relevant users to CPPA The indirect or non recurring cost shall be included in the total charge for the general services provided by the CPPA in the frame of the contract All services for parts ordered by the CPPA for the THALES ES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE EXO units after the cut off date as it will be defined in the frame of early phase B shall be fully charged to the concerned user In case of unique part the EXO PCB reserves the right of accept it for coordinated procurement but charging all the not recurrent costs to the relevant user 7 3 Declared Component List Users shall issue a Declared Components List as per ECSS Q ST 60C para 5 1 4 identifying all component types needed and this list will be kept under configuration control Bullet d and bullet f of the above mentioned ECSS paragraph are
130. iation Test Method ESCC Basic Specification N 22900 issue 3 March 2007 CATEGORY TEST CRITERIA All All diffusion lot tested 1 Lot tested if flight diffusion lot number different of data diffusion lot number and data date code older than 1 year 2 Lot tested if flight diffusion lot number different of data diffusion lot number and data date code older than 2 year 4 Lot tested if flight diffusion lot number different of data diffusion lot number and data date code older than 4 year 6 Lot tested if flight diffusion lot number different of data diffusion lot number and data date code older than 6 year 10 Lot tested if flight diffusion lot number different of data diffusion lot number and data date code older than 10 year Table 13 2 2 2 RADLAT Test Criteria MS PA REQ 3070 Verification Traces Low Dose Rate is lower or equal to 360 rad hour 0 1 rad sec MS PA REQ 3080 Verification Traces The RADLAT set up shall be tailored to cover the project requirements as per users input that is worst application conditions among the different users configurations In case of no or late input from the users the CPPA for co ordinated procured items will establish the test bias conditions taking the worst case configuration as reported in the procurement specification MS PA REQ 3090 Verification Traces Silicon Nitride layer will be avoided unless RADLAT data demonstrates an acce
131. ife after assembly integration shall be identified and processed in the Critical Item List CIL PA 3 Output PA 35 Deleted 8 18 Processes MS PA REQ 4610 Verification Traces EXM MS RS ESA 00002 PA SY 2060 This chapter is a supplement to clause 7 7 of ECSS Q 70B MS PA REQ 4620 Verification Traces EXM MS RS ESA 00002 PA SY 2070 The Contractor shall maximize the use of existing ESA specifications The following specifications listed in the normative documents list shall be applicable ECSS Q ST 70 08C for soldering ECSS QST 70 18C for RF coaxial cable assembly ECSS Q 70 26A for crimping ECSS Q ST 70 28C for repair and modification of PCB s e ECSS Q ST 70 38C for high reliability soldering for surface mount and mixed technology The requirements shall be fulfilled through the deliverable PA 36 Output PA 36 High Reliability soldering for surface mount and mixed technology THALES eer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 4620 Verification Traces EXM MS RS ESA 00002 PA SY 2070 The Contractor shall maximize the use of existing ESA specifications The following specifications listed in the normative documents list shall be applicable ECSS Q ST 70 08C for soldering ECSS QST 70 18C for RF coaxial cable assembly E
132. ifically required PA documents related to each item are listed in the relevant SOW DRL Item Numb DRD Title Submital Proposal PDR MRR CDR QR DRB Class Remark Ref For HW SW contractors the following listed items are applicable PA 1 PA Product Assurance PA and x x x AR Including the 01 safety plan Compliance Matrix versus PA Requirements for Subcontractors PA 2 PA Audit plan x D A Living document 02 Audit report R For each audit performed PA 3 PA Critical Items Control Plan D D x D A Can be part of 03 PA Plan Critical Items List x x x x A including Limited Life Items list was PA 35 PA 4 PA Non Conformance Reports As A Major for 04 NCR generated approval minor for review PA 5 PA Request for Waiver RFW D D D x x A Approval of 05 R template at KO later updates for review PA 6 PA Alert assessment report D D D D D AR Approval of 06 template at KO later review final approval at FAR At progress meeting updated alert status list PA 7 PA Cleanliness Requirement N A to subco 07 Specification CRS PA 8 PA Cleanliness and Contamination x x A 08 Control Plan C amp CCP PA 9 PA End of Life Cleanliness Analysis x x D AR Approval at CDR 09 PA 10 PA End Item Data Packages D AR Acceptance at 10 EIDP for all h w and s w FAR PA 11 PA Failure Mode Effect and x x x A Use TAS I 11 Criticality Analysi
133. ights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE e GSE design manufacturing operation having impact on safety e g MGSE testing documentation for lifting slings with the clarifications and modifications presented in this section MS PA REQ 4950 Verification Traces For GSE purpose the FMECA shall be limited to the interfaces with flight hardware The analysis shall not be limited to electrical interfaces As appropriate mechanical thermal optical interfaces etc shall be included MS PA REQ 4960 Verification Traces The FMECA shall consider functional failures inside the GSE that may propagate via the interfaces with the flight hardware or other hardware MS PA REQ 4970 Verification Traces The FMECA shall be supported by a functional block diagram showing all units analysed and a short description of each block The breakdown of each block and its identification shall be such that they can be traced in the FMECA sheets MS PA REQ 4980 Verification Traces THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE For the GSE interfaces with the S
134. igns of past and present life on Mars 2018 w YES S2 To investigate the water geochemical environment as a function of depth in the YES shallow subsurface 2018 S3 To study Martian atmospheric trace gases and their sources 2016 and 2018 YES YES Programmatic P1 To support Mars proximity communications of international surface assets YES 2016 Note System and Subsystem level failure severity categories as defined in Table 5 3 1 shall be applied for each individual 2016 and 2018 mission THALES Se All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE 5 3 1 1 Failure Consequence Severity Definition MS PA REQ 1340 Verification Traces The definition of the consequence severity has been summarised in the following Table 5 3 1 MS PA REQ 1350 Verification Traces A severity level shall be assigned to each assumed failure mode and each identified hazard according to its effect defined without considering possible redundancy to compensate the effects of initial failure The severity category for a particular failure mode shall be determined by the most severe effect of the failure considered worst case A suffix R shall be added to the severity category number if redundancy is provided A suffix SPF shall be added to the severity ca
135. igured procurement THALES ca All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE specification based on ESCC or MIL documents structure for High Reliability parts submitted to customer TAS I ESA approval through the relevant PAD PA SY 1400 Deleted PA SY 1410 Deleted MS PA REQ 3360 Verification Traces EXM MS RS ESA 00002 PA SY 1570 As far as ASIC are concerned Alterate Item Drawings AID based on US MIL system and ASIC sheets based on the EQML system REPO06 are considered acceptable for ExoMars and shall be provided to the contractual customer up to prime and ESA together with the relevant PAD sheets All encapsulated high reliability parts shall be procured preferably directly from EEE parts manufacturers 7 4 6 Quality Level MS PA REQ 3370 Verification Traces EXM MS RS ESA 00002 PA SY 1420 EEE parts screening level shall be in accordance with ECSS Q ST 60 paragraph 5 3 3 and table 7 2 with the exception that commercial paerts are not applicable as not allowed in Exomars For hybrids the ECSS Q ST 60 05 testing level 1 or MIL PRF 38534 class K shall apply For optocoupler procured in accordance to MIL PRF 19500 JANS screening applies MS PA REQ 3380 Verification Traces The following documents can be used as applicable ECSS Q ST 60 05 te
136. ing Note B Only one programming run is allowed for each part Note C Use of an alternate procedure is allowed pending prior approval from TAS ESA 7 4 7 LAT QCI MS PA REQ 3600 Verification Traces EXM MS RS ESA 00002 PA SY 1430 Exomars LAT requirements are found in ECSS Q ST 60 NR 089 paragraph 5 3 5 with the modifications identified in the following paragraphs The ECSS Q ST 60 NR 089 requirements for Lot Acceptance on commercial parts are not applicable as these parts are not allowed in Exomars THALES ema All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 3610 Verification Traces EXM MS RS ESA 00002 PA SY 1440 For the definition of LAT requirements the ECSS Q ST 60 NR 17 wordings space qualified shall be interpreted in Exomars as follows For European components such references are equivalent to the listing in the ESCC QPL For US components such reference is restricted to Class Q M items in MIL QML 38535 NR 68 Class K items in MIL QML 38534 NR 67 JANS optocouplers in MIL QML 19500 JANTXV items in MIL QML 19500 NR 66 and Established Reliability R items in other QPLs as long as type and value are listed in NPSL MS PA REQ 3620 Verification Traces EXM MS RS ESA 00002 PA SY 1480 The LAT2 on European parts not liste
137. ion Traces EXM MS RS ESA 00002 PA SY 1820 The primary data source for assessment of vacuum compatibility shall be the ESA database available online http esmat esa int Services outgassing data outgassing data html MS PA REQ 4440 Verification Traces EXM MS RS ESA 00002 PA SY 1830 When relevant outgassing data are not available e g obsolete if test conducted more than 10 years ago or unacceptable because missing information such as report reference or insufficient materials processes description out gassing tests shall be carried out as per ECSS Q ST 70 02 MS PA REQ 4450 Verification Traces EXM MS RS ESA 00002 PA SY 1840 The outgassing and condensation acceptance criteria for a material depends upon the application and location of the material and may be more severe than the general outgassing requirements for material selection which are defined as RML lt 1 0 and CVCM lt 0 10 The validity of this screening test as a means for determining the suitability of a material for a specific application shall depend on the environmental conditions during the lifetime of the material as well as the vicinity of critical or sensitive THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE surfaces Especially in cases were the expected maximum t
138. ion specific aging and drift effects shall be evaluated on the basis of the mission environment application conditions and manufacturer data THALES fer All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 5 4 8 Part derating analysis MS PA REQ 2110 Verification Traces EXM MS RS ESA 00002 PA SY 680 Each subcontractor shall deliver a Parts Stress Analysis and submit it to TAS I ESA approval as required in the DRD PA 14 and in the DRL in para 12 1 of the present document Clause 8 2 2 1 of ECSS Q 30 applies with the following modification ECSS Q 60 11 is replaced by ECSS Q ST 30 11 Exomars Mission specific stresses will be reviewed to evaluate whether to apply additional different deranting 5 4 9 Maintainability Assessment MS PA REQ 2120 Verification Traces The Module System Subsystem layout shall permit an easy replacement of any equipment The layout shall permit replacement of a unit without dismounting any unit other than the one to be replaced MS PA REQ 2130 Verification Traces Each subsystem unit shall be designed to require a minimum of special tools and test equipment to maintain calibration and identify malfunctions Each unit shall be designed to avoid necessity of routine maintenance and refurbishment once integrate
139. it progress meeting TAS and ESA shall be invited to attend to dedicated major design reviews as appropriate for the relevant technology For non standard parts that is parts not included in the above mentioned lists the procurement responsible shall put in place a configuration control system to ensure that any change of the product i e mask manufacturing or assembling process affecting evaluation performance quality reliability and interchangeability is communicated to him by the manufacturer e g EPN In case of change the procurement responsible shall inform the subcontractor The subcontractor shall ensure the compatibility of the change with its application The change shall be submitted to costumer up to ESA for approval 7 4 1 EEE components requirements on materials and processes THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 2980 Verification Traces EXM MS RS ESA 00002 PA SY 1180 Users shall be requested to ensure all materials which are not hermetically sealed within components meet the requirements of ECSS Q 70B regarding off gassing out gassing flammability toxicity and or other criteria defined by the intended use MS PA REQ 2990 Verification Traces EXM MS RS ESA 00002 PA SY 1 190 The procurement auth
140. itical Item List with a detailed retention rationale They are subject to formal approval by ESA on a case by case basis MS PA REQ 1410 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE Multiple failures resulting from common cause or common mode failures shall be considered as single failures when determining failure tolerance 5 3 2 Failure Tolerance 5 3 2 1 Basic requirements MS PA REQ 1420 Verification Traces EXM MS RS ESA 00002 PA SY 530 Clause 7 3 2 a of ECSS Q 30 shall be read a The contractor shall verify the capability of the design to sustain single or multiple failures as defined by the following failure tolerance requirements MS PA REQ 1430 Verification Traces Safety No two hardware failures two operator errors a combination of a hardware failure and an operator error shall cause effects on any level of the ExoMars system of the Hazard Severity category 1 No single hardware failure or operator error shall cause effects on any level of the ExoMars system of the Hazard Severity category 1 or 2 Hazard Severity category definitions are provided in Table 6 3 1 MS PA REQ 1440 Verification Traces Dependability No single hardware failure or operator error sh
141. ity approval programme for thick film hybrid microcircuits NR 090 ECSS 12300 iss 1 Dec 2006 The EPPL and its management NR 099B ESCC 22900 iss 3 March 2007 Total dose Steady State Irradiation test Method NR 099C ESCC 25100 iss 1 Oct 2002 Single Event effects Test method and guidelines NR 07 EXM MS RS ESA 00005 Planetary Protection requirements NR A41 ECSS Q 70B Materials mechanical parts and processes NR A17 ECSS Q ST 70 01C Contamination and cleanliness control INR A18 ECSS Q ST 70 02C Thermal vacuum outgassing test for the screening of space materials INR A19 ECSS Q ST 70 03C Black anodizing of metals with inorganic dyes NR A20 ECSS Q ST 70 04C Thermal cycling test for the screening of space materials and processes NR A21 ECSS Q ST 70 05C Detection of organic contamination of surfaces by infrared spectroscopy NR A22 ECSS Q 70 07A Verification and approval of automatic machine wave soldering NR A23 ECSS Q ST 70 08C The manual soldering of high reliability electrical connections NR A24 ECSS Q ST 70 09C Measurement of thermo optical properties of thermal control materials NR A25 ECSS Q ST 70 10C Qualification of printed circuit boards NR A98 ECSS Q ST 70 11C Procurement of printed circuit boards NR A26 ECSS Q ST 70 13C Measurement of the peel and pull off strength of coatings and finishes using pressure sensitive tapes NR A27 EECSS QST 70 18C Preparation assembly and mounting of RF coaxial cables
142. ive finishes for space vehicle structure and associated flight equipment general specification for data Galvanic compatibilities shall be selected in accordance with Group 0 couples that can be used without restriction and Group 1 couples that can be used in a non controlled environment of Table 1 of ECSS Q 70 71 Compatible couples for bimetallic contacts Materials not listed in Table 1 of ECSS Q 70 71 shall THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE be evaluated in a mission simulated configuration This requirement applies also to metal to conductive fibre reinforced contacts Deleted MS PA REQ 4530 Verification Traces EXM MS RS ESA 00002 PA SY 1940 Materials for hardware where bioburden assessment procedures will be applied e g wet contact by swabbing wiping shall be considered as being in a non controlled humidity environment Deleted 8 13 Corrosion MS PA REQ 4540 Verification Traces EXM MS RS ESA 00002 PA SY 1960 Aluminium surfaces shall be treated for corrosion protection with a chemical conversion Coating or with the most appropriate method In case that black anodizing protection will be selected for AA series 2xxx and 7xxx ESA ALERT EA 2005 MEP 02 B shall be also followed Mechanical parts made of stainle
143. ll be formally documented through technical notes THALES ee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 2600 Verification Traces The Contractor shall demonstrate that results of the safety analyses confirm that the design is in agreement with the launch authority requirements 6 5 Safety engineering MS PA REQ 2610 Verification Traces Reduction precedence shall be applied to identified hazards hazardous conditions and functions whose failures have hazardous consequences as detailed in ECSS Q 40B 5 2 3 Hazard elimination Hazard minimization Hazard control Safety devices Hazard control Warning devices Hazard control Special procedures MS PA REQ 2620 Verification Traces Inherent safety shall be mandatory for design selection MS PA REQ 2630 Verification Traces Safe without service whenever the safe operation of the system depends on externally provided services e g power cooling fluids etc the system design shall be such that critical or catastrophic consequences are not induced at least for a certain interval of time that shall be defined for each project after the loss or upon the sudden restoration of those services THALES SE All rights reserved 2007 Thales Alenia Spac
144. ll report the progress of the dependability programme as part of the PA progress reporting 5 2 Dependability risk reduction and Control MS PA REQ 1260 Verification Traces All Q 30 Para 6 Dependability risk reduction and control is applicable 5 3 Dependability engineering MS PA REQ 1270 Verification Traces THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 nev Space ISSUE 05 PAGE All Q 30 Para 7 Dependability engineering is applicable with the modifications specified in the following paragraphs 5 3 1 Design criteria MS PA REQ 1280 Verification Traces This chapter supersedes Clause 7 3 1 Consequence Category and Severity of ECSS Q 30 MS PA REQ 1290 Verification Traces EXM MS RS ESA 00002 PA SY 520 ExoMars Failure events on system and subsystem level that will affect mission success shall be classified on the basis of the severity of their consequences according to the severity categories defined in the following Table 5 3 1 this table supersedes in ECSS Q 30 02 paragraph 4 2b and related table 1 ExoMars Programme objectives MS PA REQ 1300 Verification Traces The objectives of the ExoMars Programme will be pursued as part of a broad cooperation with NASA Two missions are foreseen within the ExoMars
145. ls and components THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3010 Verification Traces EXM MS RS ESA 00002 PA SY 1160 EXM MS RS ESA 00002 PA SY 1210 For limited life known instability safety hazard or reliability risk reasons the use of EEE parts as listed in ECSS Q ST 60 NR 89 paragraph 5 2 2 2 d shall be prohibited in ExoMars With respect of healthy and safety if the listed materials are used in the standard design manufacturing processes of a particular part type their use must be approved on a case by case basis with the provision that its application does not constitute an unacceptable safety hazard e Beryllium oxide except if the health and safety hazards are identified in the specification Cadmium Lithium Magnesium Mercury Radioactive material Zinc all materials which may cause a safety hazard 7 4 2 Radiation Hardness Assurance MS PA REQ 3020 Verification Traces EXM MS RS ESA 00002 PA SY 1230 On the basis of ExoMars mission environmental specification EXM MS ESA RS 00013 Iss 4 dr 0 users shall assess the radiation dose that their equipment will receive during all phases of the mission transfer orbit cruise and Mars orbit performing a sectoring analysis of their unit and shall demonstrate that the ra
146. lures occur these shall be reported within 2 working days Significant changes or additions to the Critical Items List shall be included in regular PA status reports 4 5 Non conformance Control System RFW and Deviations MS PA REQ 0680 Verification Traces ECSS Q 20 09B shall apply with the following modifications e Review of lower level NCRs will be performed by TAS ESA on a regular basis for instance at the progress meeting e The subcontractors shall give visibility upon TAS ESA request of all NCRs generated within the contract e TAS ESA reserve the right to reconsider NCR classification for subcontractors and suppliers NCRs including product NCRs MS PA REQ 0690 Verification Traces EXM MS RS ESA 00002 PA SY 210 Subcontractors and suppliers shall make available all NCR reports with attachments on an internet based application visible to TAS ESA This application will be the NCTS tool This application shall be used to process all NCRs generated within ExoMars program THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 0700 Verification Traces EXM MS RS ESA 00002 PA SY 220 The TAS ESA shall concur in the disposition of any NCR affecting system requirements a science instrument and all system level NCRs
147. measurements MS PA REQ 1600 Verification Traces Each Deployable device including activation mechanisms and retention system shall be single failure tolerant MS PA REQ 1610 Verification Traces On board data processing storage and transmission shall be structured in such way that single bit error per word does not disturb normal operation or activate redundancy MS PA REQ 1620 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE The Item SYS SS EQP design shall not include any failure propagation path such that any failure from one function unit causes permanent failure to another function unit of the item or other interfacing items In particular where redundancy is employed a single failure in the nominal unit equipment shall not affect the full operability and performance of the corresponding redundant unit equipment MS PA REQ 1630 Verification Traces Redundant functions shall be implemented and or routed physically separated or protected to prevent propagation of failures mechanical thermal electrical optical biochemical contamination causing degradation or loss of the redundant ones This is valid also to internally redundant units MS PA REQ 1640 Verification
148. med to verify the fulfilment of the ExoMars requirements if any e OTS Item Suitability report presenting the results of the Delta activities and demonstrating the full suitability of the OTS item MS PA REQ 4790 Verification Traces EXM MS RS ESA 00002 PA SY 2290 THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE For each OTS Hem a dedicated OTS Item suitability review shall be held This review shall take place not later than the PDR of the Upper Subassembly level MS PA REQ 4800 Verification Traces EXM MS RS ESA 00002 PA SY 2300 The Delta Activities program shall be completed not later than the CDR of the Upper Subassembly level 10 2 Qualification Status List QSL MS PA REQ 4810 Verification Traces A Qualification Status List QSL will be issued at equipment subsystem and system levels DRD PA TAS 1 MS PA REQ 4820 Verification Traces This document summarises for each configured equipment by reference to design definition or build standard the test requirements and results and the manner by which a qualified status compliant with the Customer s project requirements is achieved MS PA REQ 4830 Verification Traces The list will include the following information Equipment designation i
149. mme Users shall apply a NCR procedure such that all the activities necessary to provide assurance that any non conformance is THALES oe All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION W s Th alesAlenia ev SPACE REFERENCE EXM MS RQN AI 0004 DATE 21 01 2011 PAGE ISSUE 05 detected identified investigated and corrected are completely defined A failure analysis shall be performed as necessary to highlight the failure whenever required by the NRB and the relevant report shall be linked to the NCR Preventive actions shall be defined in such a way that they will minimise risk to the technical success cost or project schedule Criteria for NCR classification as major or minor are included on the table below The NCR numbering shall follow the project numbering system as defined in EXM MS RS ESA 00012 para 9 MAJOR MINOR Functional and or operational performance When the failure does not affect workmanship criteria Functional and or dimensional interfaces and or interchangeability A random failure on EEE parts with no risk of reliability or quality and the form fit and function is not affected Form materials processes weight centre of gravity Minor inconsistencies in the accompanying documentation Personal health and safety Reliability maintainability and durability Acceptance or qualificatio
150. n Para 8 12 Req PA SY 1950 reference to deliverable PA 32 replaced by reference to PA 33 Para 2 1 3Replaced former PSS document by updated ECSS Q 70 38 Para 4 15 MIP KIP MODIFIED Para 1 1 Details ECSS Tailoring and replace mission by Flight Segment Para 1 2 Deleted B2 C D E1 and add all project phases Para 2 1 Used standard text for NR introduction Para 2 2 1 Use standard text for IR introduction Para 4 5 Req PA SY 240 reference to ECSS Q 40B added Para 4 8 Delete PA SY 330 PA SY 360 Para 4 8 Req PA SY 340 change higher to cleaner and delete last word requirements changed ref doc Para 5 3 Dependability engineering Added Dependability in title of paragraph Para 5 3 1 1 Deleted subpara 1 modified subpara 2 Para 5 3 1 2 SPF definition update with addition of ECSS Q 30 02 wording Editorial in critical SPF definitions Para 5 3 2 1 Failure Tolerance Basic requirements change order of bullets and delete SPF removed software error Add note to clarify failure tolerance based on design for minimum risk Para 5 3 2 2 Additional specific requirements section1 degraded to not a requirement deleted ref to triple redundancy Para 5 4 1 Functional Analysis FA Req PA SY 560 570 580 deleted Para 5 4 1 Req PA SY 590 add EXM MS TNO ESA 00005 which is wrong corrected in TNO 00017 Para 5 4 3 Hardware Software Interaction Analysis HSIA PA SY 620 modified requirement THALES SE
151. n assessment of the surrounding parts shall be requested to the user in order to assure that the surroundings components have not been overstressed THALES M032 EN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 7 5 3 Components in Off the shelf equipments MS PA REQ 3950 Verification Traces EXM MS RS ESA 00002 PA SY 1080 All the requirements specified in this document are applicable also for components in OTS equipment intended for flight use Therefore the previous use or approval of a part via PAD or otherwise in any other project shall not be considered in any case as an approval for ExoMars The project explicit approval as required in paragraph 7 4 4 above is applicable Furthermore the Radiation Hardness Assurance requirements of paragraph 7 4 2 is applicable for EEE parts in OTS 7 5 4 Use of Stock Components MS PA REQ 3960 Verification Traces Relife will be performed according to ECSS Q ST 60 MS PA REQ 3970 Verification Traces The use of existing stock parts has to be approved via PAD by EXO PCB CPPA is recommended to verify before starting new procurement the parts stock procured for equivalent ESA programs upon ESA approval making a detailed comparison of quality and environmental requirements of EXOMARS
152. n chains of redundant units so that maximum overall reliability is achieved MS PA REQ 1540 Verification Traces Hot redundancy shall be provided for functions which could result in loss of mission if failing according to mission phases MS PA REQ 1550 Verification Traces Interfaces redundancy shall be provided to avoid that a single failure in the nominal ones affects the full operability and performance of the redundant ones MS PA REQ 1560 Verification Traces Power the primary power conversion and secondary power distribution inside each unit equipment shall provide full redundancy THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1570 Verification Traces Execution of identified mission critical functions severity 1 and 2 shall be implemented by two independently routed nominal and redundant commands telecommands MS PA REQ 1580 Verification Traces Unwanted execution of mission critical functions shall be prevented by implementation of arm execute concept and multiple inhibit levels according to the criticality of the function MS PA REQ 1590 Verification Traces All mission critical functions shall be observable by at least two independently obtained
153. n eaaa aaee aaa aaa a eaaa aeaea aaa aana aae 82 6 4 Hazard Analysis Residual Hazards scccssccsseceeseeeseeesesneeeneeeeescaeseseeeenseaeseaesesaesaseeeeeeeseseaeseseeeenseeeeeas 83 6 5 Safety SNGIMGSKING EE 85 6 6 Failure TE 88 6 7 REIWEN 89 6 8 Product Liability Requirement ccceeccceeeeeeeeeeeeeeeeeeeeee sees seen ee eeeeeeseseeeeeseeeeeeeseeseeeeeseseeneeseseeeeeeseeenes 89 7 TEE COMPONEN Eeer NHN ARNAR RANER RNE AKRA 91 7 1 Ener AE EE E EEA 91 7 2 EEE Program management ssssssnnnesnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnnn nnan n nnana annnm nnana nenanem nanana 92 7 2 1 Procurement policy cccceceesceceeeeeeeeeeesaeeeeeeeeceaeeeeaaeeaeeecaeeeeaaesgeaaesaeeeseaaesgeaaeseeeesaeeseeeseeaaesseneesaas 92 7 2 2 User tasks in ENO PDCH ttnn nt EAAS RE EEANN EEASEE EEANN EEESSEEEAANAE EEES EE EEEN EE Ennen Ennen 93 7 3 Declared Component LiSt ccsseccsseeeeesceeeeeeeseeeenseeeseaeseseeeenseeeeecaesaseeeeaseeeseaesesaaesaaeeeeeeeeeseaesaseeeenseeeeeas 94 Tad As built DOL eege eege eege iiaii i iaiia ii oa iiiad eats 94 7 4 EEE Components Selection Qualification ccccsccsseeeeeeeeeeeeesseeseseeeeeeeeeeseaeseseeeeeeeeeseeseneeeenseeeeeas 95 7 4 1 EEE components requirements on materials and processes ccccceeeeeeeeeeceeeeeeeeeeeeeeeeaeeesaeeeeneeees 95 7 4 1 1 Prohibited materials and components 96 7 4 2 Radiation Hardness Assurance ccccccecesscceecsneeeeeeaeeeceeeae
154. n tests with the requirements High reliability EEE parts failures after delivery from the manufacturer Non compliance of Planetary protection requirements MS PA REQ 3940 Verification Traces For co ordinated procured items in addition to the above provisions the following applies Any major failure occurring during parts procurements and delivery must be notified to EXO PCB within two 2 working days after it is detected The NCR report shall be provided within five 5 working days with a clear description of the failure and a proposed disposition EXO PCB will release the lot for use only after review of the failure analysis report and closure of the corresponding NCR The user shall be in any case informed through the CPPA information system of any NCR independently of the classification Users formal approval of NCR disposition is requested whenever a major NCR could have impact in the form fit function inclusive radiation and planetary protection or potential impact in delivery time In this case NCR shall be distributed to users and they will be invited to the relevant NRB For components failing after during assembly at higher level the user is responsible in performing the initial analysis necessary to identify the failed components and the failure effects failure mode The CPPA shall be involved once it has been shown that there is no misapplication mishandling performed by the user If necessary a
155. nce of 5cm from one reference RHU plus the contributions of all the other RHUs at their places EOL Dose 1 63KRad 1 7Krad 3 33 that gives a TDD 7Krad The TDT of 20 KRad shall be considered for the selection of EEE parts Components which have been proven by valid data to be susceptible to more or at least the TDT are suitable for ExoMars without additional testing and or analysis When no or insufficient data are available for potential sensitive components and in case of components susceptible to less than 20 Krad the procurement authority has to perform the radiation verification test RVT or RADLAT on 5 samples of the procured lot presenting the results to EXO PCB for lot approval MS PA REQ 3030 Verification Traces EXM MS RS ESA 00002 PA SY 1220 Due to the lot to lot variability in Total Dose effect all active parts will be submitted to Radiation Lot Acceptance Tests RADLAT As a general basis the RADLAT testing matrix is given in table here below However on a case by case basis test criteria could be relaxed taking into account total dose data on previous lots For example for a given part Manufacturer if total dose behaviour is steady and if there is no technology modification test frequency can be reduced In any case technical data shall justify this relaxation The generic RADLAT testing matrix is as follow MS PA REQ 3040 Verification Traces THALES are All rights reserved 2007 Thales
156. nceeeeeee cee eeeaaeeeeeeeceaeeesaaeeeeaaesseneeseaeeeseaaessinees Alert Problem notification 0ccccccceceeeeeeeeeeeeeeeeeeeeeeeeeseeeseeeeeeeseneees AU el EE Traceability 00 cee ccc eeeneeeceeeeeceaeeeeaaeeeeeeeeaaeeseaaeseeneeseaeeesesaesseneeenaees Dispatch Documentation Electrical and Qualification Model EMEOM Ground Support Equipment ssseesseesseeeseeseeesnetseernntenntenntrnnnsnnessennnn EXM MS RQM AI 0004 21 01 2011 05 PAGE M032 EN 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 8 14 Siess COMPOSI OM E 150 8 15 Fluid Compatibility gedet 151 8 16 Allowable SUeSS eessen seen 151 8 17 Limited Life Time icceccsca tee cccccece cesta tentcceceseceescesceneceecedie ccna sanneeecuucedtucteneeaeceuensctadvendieececesnderadeecrsteventeceeuces 151 ET GR nnise eaa a a aa ch cases ee dew eaaa Ea eden Das aaae aaa aaa 152 8 18 1 Process Drocecures netr uetnnttnAtEnASEAAEEAASEEEOEEEOEE NSE EnSoEnSoEnnon nnen ntnn sennen 153 8 18 2 Processes for EEE mounting and assembly ccccceeeceeeeeeeeeeeeeaeeeeeeeceeeeeaeeseeeeeseeeesaeeeeaeeeeaes 154 8 19 Printed Circuit BOardS i ccccicccciceccccedieecdens scene ce cues ca da aan da oraaa aiani aaiae adaa aai aiaa aaaea 154 8 20 Fastengete anaia anan aea aaa aaa adaa aa ea wae eee te ca keane decade aa aaa a aa a Kaaa aa aaa 154 9 SWRPRODUCT ASSURANCE sisscssecccscsscvecssn
157. nd failure analysis each FPGA user is requested to realize and keep under configuration control test interface boards and relevant test software and equipment and test procedures which allow all functional and parametric tests to be performed on every programmed part independently from the actual unit where it is intended to be used All programmed FPGAs shall receive a dynamic post programming burn in and testing sequence according to manufacturer s specifications and approved by EXO PCB 7 4 6 5 In House Manufactured Parts THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3560 Verification Traces All EEE parts manufactured by users e g coils and transformers in accordance with internal process procedures will be documented through specifications source control drawings and approved via PAD submission to EXO PCB MS PA REQ 3570 Verification Traces Minimum screening requirements will be those of the nearest applicable ESCC or space level MIL specification for other in house parts the screening sequence and the lot acceptance will be defined in relevant PAD MS PA REQ 3580 Verification Traces For electromagnetic parts minimum screening on a 100 sampling basis in accordance to MIL STD 981 shall be e visual
158. nformative Documents 2 2 3 ESA NASA Informative Documents IRA 111 PSS 01 202 iss 1 Preservation Storage Handling and Transportation of ESA spacecraft hardware IR A04 EXM MS RS ESA 0007 Exomars Mission Objectives Document IR A93 EXM MS TNO ESA 00017 ExoMars EEE Components Failure Modes Table IR A94 EXM MS TNO ESA 00016 ExoMars Low Temperature Qualification Guideline IR116 CLSB 0409 1109 rev 10a Atlas Launcher User Manual IRO1 EXM MS RS ESA 00001 Mission and System Requirements IR10 EXM RM RS ESA 00001 Rover Requirements IRO3 EXM MS RS ESA 00012 Management Requirement Document IRO15 EXM MS RS ESA 00010 ESA Document Requirements Description DRD NR0438 EXM RM SSR AI 0015 ExoMars RM Cleanliness and Contamination Control Requirements THALES ee All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha les Alenia DATE 21 01 2011 Space ISSUE 05 PAGE IRA 111 PSS 01 202 iss 1 Preservation Storage Handling and Transportation of ESA spacecraft hardware INR0439 EXM RM PLN AI 0078 ExoMars RM Cleanliness and Contamination Control plan M032 EN THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01
159. nitrogen or synthetic air to eliminate outgassing products and prevent molecular and particulate contamination MS PA REQ 0870 Verification Traces EXM MS RS ESA 00002 PA SY 400 The allowed particulate bioburden and molecular contamination levels shall be agreed with the subconirctors and instruments providers based on Planetary protection requirements and or acceptable performance losses 4 8 1 Cleanless and contamination control Plan MS PA REQ 0880 Verification Traces All Subcontractors and Suppliers shall prepare a Cleanliness and Contamination Control Plan to be approved by TAS I PA 8 strictly related to their own Planetary Protection Plan The C amp CCP shall also include the definition of necessary tests test s schedule related efforts compliance matrix to CC requirements imposed by TAS I 4 9 Test Facilities MS PA REQ 0890 Verification Traces This chapter supersedes clause 9 1 of ECSS Q 20B THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 0900 Verification Traces EXM MS RS ESA 00002 PA SY 410 The subcontractors and suppliers shall ensure that test facilities either internal or external comply with ECSS Q 20 07 MS PA REQ 0910 Verification Traces EXM MS RS ESA 00002
160. o 2016 mission because Nasa mission data are not available at the time of writing 2 04mm Al eq from Shell 2 57mm Al eq from box walls that is 2mm perpendicular from box walls that gives 4 61 mm Al eq RHU contribution around 2 3 10 10 MeV eq protons cm for a silicon target at a minimum distance of 2cm from one only reference RHU EOL proton fluence 2 3 10 1944 13 10 2 710 that gives a DDEF 5 4 10 10 MeV eq protons cm THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Each component shall have been tested to show immunity to the above reported EXO p fluences 7 4 2 2 SEE assurance MS PA REQ 3150 Verification Traces EXM MS RS ESA 00002 PA SY 1250 All potential SEE sensitive components shall have been subjected to heavy ions proton test Validity of already available results and or extension of test results to components manufactured in the same technology shall be evaluated and approved at EXO PCB level When no SEE sensitivity data are available potential sensitive components will be subjected to heavy ions and or proton test The relevant test plan shall be submitted to EXO PCB for review The final test report shall then be submitted to TAS ESA in the frame of EXO PCB for component approval The responsibili
161. o ECSS Q 20B para 8 9 the following requirements shall apply MS PA REQ 1090 Verification Traces The subcontractors and suppliers shall define beside the Key Inspection Points KIPs the Mandatory Inspection Points MIPs MS PA REQ 1100 Verification Traces The subcontractors and suppliers shall reflect these KIPs MIPs in the Manufacturing Inspection Plan including the manufacturing flow chart as required by ECSSQ 20B para 8 2 2 to be provided to TAS I ESA for approval THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1110 Verification Traces TAS ESA shall be invited to the selected MIPs MS PA REQ 1120 Verification Traces MIPs shall be notified 10 working days in advance MS PA REQ 1130 Verification Traces MIPs shall be performed by Subcontractor Supplier PA QA responsible MS PA REQ 1140 Verification Traces The finding of each MIP KIP shall be documented and recorded as MIP KIP reports to be delivered to TAS ESA MS PA REQ 1150 Verification Traces The MIP KIP tracking list will be part of the PA status reporting and included in the EIDP MS PA REQ 1160 Verification Traces Special emphasis shall be placed to connect the critical items programme with the
162. ock Components EEE parts DOCUMENTATION sessies ARER Parts manufacturer s documentation requirements eseeee Components Packaging Handling and Storage ssssssssensseennnee nenn 7 5 7 Shipment 7 5 7 1 7 5 8 7 5 9 Ge ial eege EE geed Declared Material Parts and Process LiStS sssccssssssssseeseeseeseeenees PMP Item number Technical Requirements for the Selection of Materials Deleted EE Verification Of curing Conditions ccteceeeeeeeeeeeseeeeeeeeeesteeeeneeneeeeeenee Forbidden Materials c0 cccccesessccssssseeesesueeeeensesseeueeeeaeaasseeueeuseaeanseessees Use of radioactive and fluorocarbon materials 00 0 c cece esse eee Bioburdem contre tioii aua da aaaeaii EEN Bioburden REduction ecccceceeeseeeeeeeeeseeeeeeeeeeseaeseseeenseeeeeeeeesnaeeaneeneneees VACUUM E Thermal Cy Chin lt ics lt c0scccctcvccceec ccneccanceseaseectancenntedeasucsseeceendectenssecsnececcuctecs Environmental Interaction ccccscccsseceeseeeeeeeeeeseeseseeeeeeeeeeeseeseseeeenseeeeseees Micrometeoroid Debris Environment cccssseeccseeeeeesseeteeeenseenenenseenenes Electrochemical Compatibility ccseccssecsseeeseeeeeeeeeeseeeseseeneneeeeeesees GGT OSU OM EE THALES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION Oli Uer ASIC FPGA REENEN In House Manufactured Parts EIERE Long Lead eme 0 c ce eeeeee
163. ocurement activities users are requested to organize dedicated PCB at their premises at the early stage of the project in order to have all parts approved by TAS I and ESA prior the equipment CDR EQSR close out and prior to start the manufacturing activities MS PA REQ 3340 Verification Traces EXM MS RS ESA 00002 PA SY 1360 Users are considered fully responsible of parts selection application and procurement in case of self items even after PAD s approval The PAD format applicable to EXOMARS is reported into ECSS Q ST 60C annex A with the following modification Planetary protection compatibility section shall be added below the Radiation assurance section with the following fields e compatibility to Dry Heat sterilization process Y N e temperature and time condition e compatibility to Alcohol cleaning Y N e compatibility to Damp swap assays Y N 7 4 5 EEE component procurement specification MS PA REQ 3350 Verification Traces EXM MS RS ESA 00002 PA SY 1390 All components intended for use in deliverable flight hardware shall be procured according to a controlled specification as described in ECSS Q ST 60 paragraph 5 3 For specific EEE Parts Asics Procured Hybrids transformers etc not covered by an existing Agency specification or for parts having specific requirements the procurement authority that is the CPPA for co ordinated parts or users for authorized self procured parts shall issue conf
164. oltage protection circuits mechanical end stops relief valves etc shall be implemented in the GSE design for those failures which may propagate to any interfacing flight hardware or other hardware or may have safety impacts MS PA REQ 5040 Verification Traces The EGSE shall provide built in self test capability for failure detection and isolation MS PA REQ 5050 Verification Traces EGSE functions shall be continuously self monitored It shall also be possible to monitor them through a local operator interface and remotely by the central checkout system MS PA REQ 5060 Verification Traces The EGSE shall be able to automatically and safely switch off the failed function MS PA REQ 5070 Verification Traces All resources required for detection isolation and switching off the failed function shall be implemented and shall not be affected by the initial failure THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 5080 Verification Traces The Contractor shall identify the equipment parameters and functions that are critical for its performances and safety 11 1 5 General Requirements MS PA REQ 5090 Verification Traces As per para 11 1 4 11 1 6 FMECA MS P
165. ominal and redundant commands telecommands according to the criticality of the function THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 2690 Verification Traces TT Unwanted execution of hazardous functions shall be prevented by at least two or three barriers according to the hazard severity MS PA REQ 2700 Verification Traces Commanded execution of hazardous functions shall be implemented by means of two independent commands arm and execute concept Hazardous functions are those which when executed at the incorrect time could cause effects according the Severity classification provided MS PA REQ 2710 Verification Traces Pyrotechnics and actuators all pyrotechnic releases shall be redundant Redundancy shall be provided by duplication up to and including the initiators and to the mechanism interface as required C The term pyro or pyrotechnic is hereafter used indifferently to mean also other types of one time actuators such as Non Explosive Actuators Non Contaminating Actuators One shot actuators thermal knives and similar Where peculiar characteristics have to be addressed e g induced shock contamination safety hazards etc they shall be specifically mentioned by the Contractor
166. on flight parts i e connector savers interfacing directly with flight hardware during manufacturing assembly and test shall be selected procured and tested at flight standard level THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE 8 MATERIALS PROCESSES AND MECHANICAL PARTS MPM 8 1 General MS PA REQ 4230 Verification Traces EXM MS RS ESA 00002 PA SY 1640 Each supplier shall define in his Product Assurance Plan the Materials Parts and Processes organisation and tasks It shall identify a Materials and Processes Manager for the ExoMars project The requirements of ECSS Q 70B shall be followed with the following modifications 8 2 Declared Material Parts and Process Lists MS PA REQ 4240 Verification Traces EXM MS RS ESA 00002 PA SY 1650 The Subcontractor and Supplier Materials and Processes Manager shall review all lists and produce a fully consolidated e Declared Material List DML e Declared Mechanical Part List DMPL e Declared Process List DPL In addition to the RFA process as defined in ECSS Q 70B RFA shall also be required for parts or materials which are proposed for use after the declared PMP list is approved by TAS I ESA Such parts or materials shall not be incorporated in the Technical Baseline prior to TA
167. on of compliance The failure tolerance requirement shall be applied to these designs as necessary to assure that credible failures that may affect the design do not invalidate the safety margin related properties of the design For example a pressure vessel shall be certified safe based upon its inherent properties to withstand pressure loading that have been verified by analysis and qualification and acceptance testing DMR however failure tolerance must be imposed upon external system that might affect the vessel such as a tank heater to assure that failures of the heater do not cause the pressure to exceed the maximum design pressure of the pressure vessel MS PA REQ 1470 Verification Traces The Subcontractor and Supplier shall describe in its Product Assurance Plan the strategy to be adopted for achievement of the minimum risk 5 3 2 2 Additional specific requirements THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 1480 Verification Traces The following requirements are intended to drive the practical implementation of the previously expressed basic requirements It has to be noted that additional failure tolerance requirements for specific functions could be present in the system requirement documents derived from th
168. ontrol Board shall be established starting after successful PDR Output PA 30 Deleted THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE 8 3 Technical Requirements for the Selection of Materials MS PA REQ 4300 Verification Traces EXM MS RS ESA 00002 PA SY 1 700 Specification ECSS Q 70 71A rev1 contains data on materials that have been evaluated and tested for use in space hardware and it can be used as a source for material selection The data herein shall be used preferentially for the selection of materials with a previous history of space use in similar applications According to ECSS regulations these Informative annexes give additional information e g guidelines suggestions but shall not contain any normative provisions Presence of a material in this informative annex does imply that the material has been used successfully in past space missions This is however in itself not a sufficient justification for its use in another space application Selection shall be based on the availability of relevant and up to date data on the material process as used demonstrating the compatibility of that material process with the given application Equivalent standards from MIL system or NASA may also be accepted pending compliance review Output Thi
169. oposed off the shelf OTS items format template will be provided PA TAS2 Qualification Plan D D D x Included in Eng 25 PA TAS3 MIP KIP Manufacturing amp x D A Inspection Flowcharts LIST PA TAS4 MIP KIP Reports As R Reports to be generated provided at MIP KIP PA TAS5 Non Conformance Report As R Review Board NRB generated PA TAS6 Status lists ALERT RFA PAD x x D x A To be delivered NCR M amp m SPR RFD RFW also as part of MIP PA Progress Report PA TAS7 Product Assurance Progress as Project R Part of Project Report PR Progress Report content see PARS THALES ER All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION e REFERENCE EXM MS RQM AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE Item Numb DRD Title Submital Proposal PDR MRR CDR QR DRB Class Remark Ref PA TAS8 Request For Approval RFA for As A DELETED materials amp processes generated replaced by PA 45 PA TAS9 Procurement Status Report monthly R for selfprocured parts should also be part of PA TAS7 PA TAS10 User Parts List As R The user part list necessary can be in excel format but under configuration control shall be presented to EXM PCB for initiating updating coordinated procurement PA TAS11 Test Readiness Review Report As As called by generated ECSS Q 20 07A anneX B and ECSS
170. or undated references These normative references may be cited at appropriate places in the text For dated references subsequent amendments to or revisions of any of these document apply to this list only when incorporated in it by amendment or revision For undated references the latest signed version is applicable incorporated by the Contractor in the project baseline In case of conflict between this document and normative documents listed herein the Contractor shall inform the TAS Project Office for resolution 2 1 2 Thales Alenia Space Italia Normative Documents NR 0105 EXM MS SSR EXOMARS Space Environment and Requirements Specification Al 0014 NR 0447 EXM MS SSR EXOMARS Rover Module Space Environment Requirements Al 0018 Specification NR 0106 EXM MS SSR EXOMARS Cleanliness and Contamination Control Requirements Al 0005 issue7 NR 0119 EXM MS SW PA Requirements for Subco s RQM AI 0010 NR 0120 EXM MS SSR Planetary protection Implementation Requirements Al 0007 NR 0133 EXM MS PLN Planetary Protection Plan Al 0013 NR 0145 EXM MS PLN ExoMars EEE components control plan Al 00024 NR0438 EXM RM SSR ExoMars RM Cleanliness and Contamination Control Requirements Al 0015 NR0439 EXM RM PLN ExoMars RM Cleanliness and Contamination Control plan Al 0078 2 1 3 ESA NASA Normative Documents NR 015 Moved as IR INR 021 EXM MS
171. ority CPPA for co ordinated items users for self procured items shall select components taking into account the ExoMars Planetary protection requirements in NR 07 The compatibility of any part with such requirements will be assessed and confirmed by EXO PCB as part of the review and approval of its selection MS PA REQ 3000 Verification S S RoD Traces EXM MS RS ESA 00002 PA SY 1200 According to ECSS Q 70 the Subcontractor shall be able to demonstrate the adequacy and the qualification status of his mounting and assembly rules for each package technology and material As aminimum the mounting procedure shall address e compliance to ECSS Q ST 70 08C e Design of Printed Circuit Boards or any support receiving EEE parts thermal requirements rules for implantation of EEE parts e Storage and handling on the assembly line e Preparation of EEE parts before mounting e Mounting process in compliance with maximum rating authorized by the specification component whose internal construction uses metallurgic bonding with a melting temperature not compatible with the end application mounting conditions shall be avoided e Criteria for visual inspection e Storage conditions of Printed Circuit Boards or any support receiving EEE parts These procedures shall be available for review by TAS up to ESA on request TAS ESA reserves the right of access to the qualification file for the mounting processes 7 4 1 1 Prohibited materia
172. ovide an early indication of the probability that the selected part will meet the qualification requirements and the operational goals of EXOMARS mission It is therefore essential that a The standard of fabrication and assembly is fully assessed to identify any area where modifications are required or where specific tests or inspection points should be included within the procurement specification or during procurement b All potential failure modes are identified in order to assess the need for additional tests c Assurance is obtained that no materials or processes have been employed that are likely to deteriorate over time and cause malfunction and that they are compatible with sterilization methods 7 5 1 1 2 Manufacturer assessment MS PA REQ 3840 Verification Traces The purpose of the evaluation of a manufacturer is to assess his capability to ensure the adequacy of his organization plant and facilities and to ascertain his fitness to supply parts to the appropriate specifications for space application This evaluation shall include but not necessarily be limited to a survey of a The overall manufacturing facility and its organization and management b The production line used for the part c The manufacturer s system for inspection and manufacturing control including all relevant specifications procedures and documents The complete manufacturer evaluation shall be included as a section of the evaluation report
173. plicable 8 Opto Couplers ESCC 5000 MIL PRF 19500 JANS MIL PRF 38534 Class K 9 Capacitors Fixed Ceramic Dielectric Molded ESCC 3001 Level C 3x3 MIL PRF 123 FRL R 17 MIL PRF 20 FRL R MIL PRF 39014 FRL R THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN ThalesAlen CONTROLLED DISTRIBUTION W la ex Space Ref Part Family 10 Capacitors Fixed Ceramic Dielectric Chips 11 Capacitors fixed ceramic dielectric stacked 12 Capacitors Fixed ESCC 3002 Level C Electrolyte Solid electrolyte Tantalum MIL PRF 39003 Weibull C ESCC 3003 Level C Use only MIL PRF 39006 22 25 30 31 H designated 13 Capacitors Fixed Electrolyte nonsolid electrolyte Tantalum 14 Capacitors Chips Fixed Tantalum 15 Capacitors Variable piston type and tubular trimmer Avoid for New Design 16 Capacitors Fixed Glass Dielectric 17 Capacitors Fixed MICA Dielectric 18 Capacitors Fixed metallized plastic film Dielectric style CRH ac and dc current 19 Capacitors Fixed Super metallized plastic film Dielectric style CHS dc current for low energy high impedance 20 Capacitors Fixed Plastic or paper dielectric style CQR direct current ESCC 3009 Level C MIL PRF 123 FRLR MIL PRF 55681 FRL R ESCC 3009 Level C MIL PRF 49470 level T devices Weibull C ESCC 3011 Level C ESCC 3012 Level C MIL PRF 55365 Weibull C ESCC 3010 Level C
174. procurement MS PA REQ 3810 Verification Traces EXM MS RS ESA 00002 PA SY 1620 Users are considered anyway fully responsible of the selection and application of the parts to be evaluated and then they shall proactively co operate with CPPA with their specific expertise in defining the evaluation program and collecting the needed information In case of evaluation conducted directly by the user on a self procured item the evaluation report shall be made available during dedicated PCB meeting in case the document are considered proprietary for TAS ESA review Sample parts used for evaluation shall be representative of flight model parts 7 5 1 1 Evaluation program MS PA REQ 3820 Verification Traces The evaluation program shall cover the following elements e Constructional analysis e Manufacturer assessment e Evaluation testing When several part types from a single part family are considered for use the evaluation program may be conducted on a representative sample of part types from the part family 7 5 1 1 1 Constructional analysis MS PA REQ 3830 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Constructional analysis on parts shall be carried out The primary aim of constructional analysis is to pr
175. programme for the 2016 and 2018 launch opportunities to Mars MS PA REQ 1310 Verification Traces The 2016 mission is an ESA led mission that will be launched by a NASA supplied rocket e ESA will supply a Mars Orbiter that will carry an Entry Descent and Landing Demonstrator also supplied by ESA e NASA scientific instruments will be accommodated on the ExoMars Orbiter to support the search and localisation of Methane sources on Mars THALES ema All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 We Th ales Alen la DATE 21 01 2011 nev Space ISSUE 05 PAGE e The Orbiter will allow Mars proximity Data Relay support to the 2018 Rovers mission as well as any other international assets on the surface of Mars for about additional 4 years MS PA REQ 1320 Verification Traces The 2018 mission is a NASA led mission with the contribution of a Rover by ESA e The ESA Rover will be accommodated in a NASA provided aeroshell and will share the journey with a NASA supplied Rover Both Rovers will arrive at the same site on Mars and start independent surface missions after safe landing and egress from the landing platform MS PA REQ 1330 Verification Traces The ExoMars Programme objectives and their allocation to the mission are specified as follows OM EDM RM Technology Scientific S1 To search for s
176. ptable total dose behaviour THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3100 Verification Traces Some device technologies are inherently hard to total dose ionizing dose effects The following classes of parts are considered as total dose insensitive Non Zener Diodes Not sensisitive up to 300 Krad si GaAs Gallium Arsenide devices such as FETs and HEMTs show little parametric variation Std TTL Logic Extensive testing on 54XX 54L 54S devices show these parts to be only marginally degraded ECL Emitter Coupled Logic devices exhibit little parametric shift out to several Mrad si Microwave Step Recovery Varactor Schottky Microwave Mixer and Multiplier Diodes exhibit Devices negligible shifts Quartz No Total Dose testing required unless in Swept technology MS PA REQ 3110 Verification Traces For these parts deposited dose levels will be lower than 300 krad si For Radiation Hardened parts data have to be provided by the part manufacturer Components that have been proven by valid data or dedicated test a sensitivity between 10 and 20Krad for Orbiter application shall be subjected to dedicated EXO PCB and user approval on case by cases basis Orbiter user radiation analysis shall s
177. r protected in such a way that any event that causes the loss of one path shall not result in the loss of alternative or redundant paths MS PA REQ 2780 Verification Traces Hardware or software failures shall not cause additional failures with hazardous effects or propagate to cause the hazardous operation of interfacing hardware THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 SE Space ISSUE 05 PAGE MS PA REQ 2790 Verification Traces Design for minimum risk potential hazards arising from structural failure of mechanical component that cannot have redundant back up such as mechanisms structures pressure vessels pressurised lines and fittings or from toxicity material compatibility and flammability shall be controlled by safety related properties and characteristics of the design to assure that hazards associated with material characteristics are either eliminated or controlled Comment Such provisions may include safety factors fracture control for pressure vessels fail safe design or containment adequate materials selection compatibility with environment with sterilization process avoidance of flammable toxic outgassing materials supported by prototyping amp qualification design for testability during development and integration MS P
178. r are hard coded shall be clearly identified and specifically reported in the documentation MS PA REQ 1730 Verification Traces No single failure or spurious event or false triggering in the on board protection system anomaly detection functions shall cause the Module to enter a safe survival mode THALES EE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE Comment this may be waived if the design of the protection system functional chain can be shown to be inherently robust against spurious events or false triggering Failure Management MS PA REQ 1740 Verification Traces Control laws and parameters for autonomous functions shall be capable of being modified by ground command MS PA REQ 1750 Verification Traces Fault management services capable to monitor and control hazardous functions execution and recover in case of single failures occurrence shall be provided MS PA REQ 1760 Verification Traces The time between the occurrence of the failure and the manifestation of the irreversible consequences propagation time Tp shall be estimated for catastrophic and critical failure consequences to allow proper definition of detection and recovery actions MS PA REQ 1770 Verification Traces
179. races Radioactive materials shall be used only when strictly necessary and using the dedicated control procedures MS PA REQ 4360 Verification Traces Radioactive materials shall be used only when strictly necessary and using the dedicated control procedures MS PA REQ 4370 Verification Traces PTFE polytetrefluoroethylene PTFE and other non treated fluorocarbons materials are sensitive to cold flow The use of wire made of these materials is prohibited Duly justified deviation could be accepted for ex if it is demonstrated that workmanship prevents form cold flow controlled bend radii no contact with sharp objects wire fixation rules etc The use of irradiated ETFE ethylenetetrafluoroethylene TEFZEL wires with improved characteristics against cold flow is accepted THALES EE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 4380 Verification Traces Electrical wires or cables insulated or coated with fluorocarbon shall be etched prior to potting to ensure mechanical bond strength and environmental seal The open end of the wire shall not be exposed to the etchant MS PA REQ 4390 Verification Traces Electrical wires or cables insulated or coated with fluorocarbon shall be etched prior to potting to ensure
180. ralized procurement within ExoMars programme reporting the approval status of the relevant PADs 7 3 1 As built DCL MS PA REQ 2950 Verification Traces The as built DCL taking into account the EEE parts actually installed in the equipment and their Date Code shall be provided for approval as part of EIDP MS PA REQ 2960 Verification Traces The as built DCL shall list passive components one line item for each P N that is not for range The engineering quantity per P N shall be reported as well THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE 7 4 EEE Components Selection Qualification MS PA REQ 2970 Verification Traces EXM MS RS ESA 00002 PA SY 1150 EXM MS RS ESA 00002 PA SY 1170 EXM MS RS ESA 00002 PA SY 1490 As general rule parts included in ExoMars hardware shall be selected in the EXO PPL established by CPPA Major S S contractor TAS ESA in the phase B and regularly updated up to CDR Parts included in EXO PPL will be selected as primary basis in the following lists e ESCC 12300 European Preferred Parts List Part 1 downloadable at lt https escies org gt e Nasa Parts Selection List Grade 2 plus any additional test required in the NPSL for that part available at lt http nepp nasa gov gt In an
181. red which relate to the project even if the information is considered proprietary TAS ESA will undertake not to disclose such information to a third party MS PA REQ 0220 Verification Traces EXM MS RS ESA 00002 PA SY 50 TAS ESA shall have the right to perform or participate in audits surveys source inspection test reviews mandatory inspections KIPs MIPs Delivery Review Boards Non conformance Review Boards etc at THALES GE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE the contractor or supplier facility TAS ESA participation shall not in any way replace or relieve the subcontractors and suppliers of their responsibilities Arrangements shall be made to permit designated TAS ESA personnel free access to all documentation areas and operations within the facilities of the subcontractors and suppliers in which work related to the ExoMars program is being performed Proprietary rights of the subcontractors and suppliers will be respected 3 7 Approval Sequence MS PA REQ 0230 Verification Traces Documents which have to be prepared by the suppliers and which are subject to review by TAS ESA e g Materials Processes and Parts Lists shall first be consolidated reviewed and approved by the subcontractors before they are formally submitted to T
182. ria DATE 21 01 2011 een Space ISSUE 05 PAGE 4 7 1 Details about Alert Problem notification see para 7 3 9 of this document MS PA REQ 0780 Verification Traces EXM MS RS ESA 00002 PA SY 290 The subcontractors shall participate in the Alert System established by ESA for the prompt interchange of information on failures problems which may affect more than one user or may recur in other projects or circumstances if no preventive actions are taken The subcontractors shall ensure that relevant PA experts are involved in e The assessment of any failure to be reported to TAS ESA as a potential for raising an alert by ESA e The investigation until disposition of the item subject of the potential alert e The assessment of incoming alerts for the definitions implementation and follow up of necessary actions e The applicability and a preliminary assessment shall be communicated to TAS ESA within 5 working days MS PA REQ 0790 Verification Traces EXM MS RS ESA 00002 PA SY 300 The subcontractors shall ensure that all subordinate suppliers also participate at least indirectly in the ESA Alert System MS PA REQ 0800 Verification Traces EXM MS RS ESA 00002 PA SY 310 This includes as a minimum that the subcontractors distributes all ESA Alerts to the lower tier suppliers and that there is a method of collecting and assessing inputs from lower tier suppliers to provide inputs to the ESA Alert System wher
183. rked as EM or EQM parts Referring to Paragraph 3 10 of the present documents EEE part changes must be intended as follow e Change of part type or e Change of package or e Change of manufacturer e In case where the application is particular sensitive to an electrical characteristic and the relevant range reported in the specification data sheet is reduced or different e Feature capability used in the EQM parts and not available in the FM part In the EIDP of EQM the EQM component list shall be included This list shall include as a minimum the following information for each line item Part number Description Package Manufacturer Procurement specification 7 5 9 Ground Support Equipment MS PA REQ 4200 Verification Traces THALES een All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE The procurement level of components to be used in EGSE shall be adequate to avoid any impact on mission success MS PA REQ 4210 Verification Traces In particular the following aspects shall be carefully considered when procuring EGSE parts e to avoid EXOMARS troubles caused by EGSE failure e to avoid EXOMARS mission delay caused by EGSE failure e to ensure acceptable life time and availability of EGSE equipment MS PA REQ 4220 Verification Traces N
184. s FMECA Template incl HSIA and CM CC PA 12 PA Reliability Assessment Report D D x R 12 PA 13 PA Worst Case Analysis x x R 13 PA 14 PA Parts Derating Analysis Report D D H Removable for THALES ee All rights reserved 2007 Thales Alenia Space 100181547K EN CONTROLLED DISTRIBUTION CONTROLLED DISTRIBUTION e REFERENCE EXM MS RQM AI 0004 ThalesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE Item Numb DRD Title Submital Proposal PDR MRR CDR QR DRB Class Remark Ref 14 PDR if too early for unit design not consolidated PA 15 PA Maintainability Report D D D AR Acceptance at 15 FAR only PA 16 PA input to FDIR Capabilities DELETED 16 verification report PA 17 PA Safety Data Package safety x D D R To be updated 17 reviews also in support of System Reviews PA 18 PA Safety Certificates incl Accident DELETED 18 Incident Investigation Reports PA 19 PA System Subsystem Equipment D D D R To be updated 19 and Operations Hazard also in support of Analysis System Reviews Acceptance at FAR only PA 20 PA EEE Component Control Plan x x AR as part of PA 1 20 PA 21 PA Parts Control Board DELETED 21 Implementation Plan PA 22 PA Declared Component List D D D x D A Draft at proposal 22 including item to be developed or qualified Final approval of as design DCL at subsystem
185. s shall be fulfilled through the deliverables PA 27 PA 28 and PA 29 8 3 1 Deleted 8 4 Verification of curing conditions MS PA REQ 4310 Verification Traces EXM MS RS ESA 00002 PA SY 1 720 For materials and processes that require witness sampling in process witness samples shall be prepared under representative conditions from the same materials batch as used on hardware The witness samples shall be stored in proper conditions until launch QM and end of mission FM Output PA 31 Deleted 8 5 Forbidden Materials The use of pure mercury tin cadmium zinc and PVC is prohibited For safety reasons the use of Beryllium and Beryllium oxide shall be restricted and in case of use the item shall be suitably labelled THALES Re All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 een Space ISSUE 05 PAGE MS PA REQ 4330 Verification Traces EXM MS RS ESA 00002 PA SY 1 740 Forbidden materials are also applicable to GSE to be installed in the vacuum chambers and clean rooms near flight hardware Output The requirements shall be fulfilled through the deliverables PA 27 PA 28 Deleted 8 5 1 Use of radioactive and fluorocarbon materials MS PA REQ 4340 Verification Traces Carcinogens materials CFC shall not be used MS PA REQ 4350 Verification T
186. sesaeeenseeeeeeesesaesaneeeeeeneeeseaesaaeaesseeeeeseaeas 50 DS DEPENDABILITY geen Seet ee EE EE ee E EE Ee EE 51 5 1 Dependability Assurance cccceeeee eee eeeeee ee eeeeee ee neeeee seen eeee een eeee seen eeee see eeeeeeseseeeeeseseneeeseseeneeeeeeneeeeseeeenes 51 5 2 Dependability risk reduction and COntrOl cccsececeeeeesseeeneeeeeeeeeeeeeeeenseeeeeesesaesaseeeeeeeeesecaesnseeeeeneeneas 52 5 3 Dependability engineering ccceseeececeeeeeeeeeeeee ee eeeeee sees enee seen eeeeseeeeeeeeeseeeeeseseeeeeseseeneeseeseeneeseeeneeseseeanes 52 53A Design criteria WEE 53 5 3 1 1 Failure Consequence Severity Definition ccccceceeeeeeeeeeeeeeeeeeeee eee eeeeaaeeeeeeeseeeesaeeseaeeeeeeeess 55 5 3 1 2 Single Point Failure Definition c cece ceeeececeeeeeneeeeeeeeeaeeeeaaeeeeneeseaeeeseaeeesaaeeseaeeesaeeseaeeseneeeeaees 56 53 2 allure TOlGranCO ies csaicecsreiicsevtedtecaveieidc E EE EE SES dee 58 5 3 2 1 EE Lee TE EC 58 5 3 2 2 Additional specific reouiremente nenn nennnnt 59 593 DeSiGnapprOaC EE 68 5 4 Dependability Amal Ses in 2 accccijccsscccccecnecendectscevensecesndectsasteanccesudececiceeastectune ceded antes ECEEdEE Neue 68 54 41 Functional Analysis EE 69 5 4 2 Failure Modes Effects and Criticality Analysis FMECA ssssessessesssessssssrrssrresrissriesrinsrinsrinssressrn 69 5 4 3 Hardware Software Interaction Analysis HSIA ccccceeeeeeeeeeeeeeaeeeeeeeceeeeseaeeeeaaeseeeeeesaeeesaaeseeeeee
187. shall be possible to enable disable or reverse any on board autonomous function or action by ground command Exceptions e g DC DC converters over voltage protections etc shall be identified and agreed THALES SES All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 1840 Verification Traces A reliable procedure under ground control shall be provided to return to nominal operations after a failure MS PA REQ 1850 Verification Traces No nominal operation shall require the deactivation of the on board protection system MS PA REQ 1860 Verification Traces Deployment mechanisms shall allow contingency operations to correct deployment anomalies e g possibility to power up redundant winding of deployment motors reverse operation of motors by design features which do not introduce severe significant additional complexity MS PA REQ 1870 Verification Traces It shall be possible to reset the data handling subsystem without the need of the command to be processed by software MS PA REQ 1880 Verification Traces Any equipment containing rewritable memory devices shall allow its reading writing for maintenance purpose during the mission This shall not cause interruption or degradation
188. sis FMECA MS PA REQ 1960 Verification Traces EXM MS RS ESA 00002 PA SY 590 The FMECA shall be performed in accordance with the requirements from ECSS Q 30 02 For failure analysis on circuit level EXM MS TNO ESA 00017 shall be used as reference THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1970 Verification Traces EXM MS RS ESA 00002 PA SY 600 FMECA items identified as a safety hazard shall include a cross reference to the corresponding paragraph in the Hazard Analysis where those particular items are treated MS PA REQ 1980 Verification Traces EXM MS RS ESA 00002 PA SY 610 Chapter 5 Process FMECA of ECSS Q 30 02 does not apply MS PA REQ 1990 Verification Traces Lower level FMECAs when available shall be used as input in a build up process to generate the subsystems and higher level FMECAs Severity classification will be assigned to rank lower level effects and establish their resulting influence on higher level functions 5 4 3 Hardware Software Interaction Analysis HSIA MS PA REQ 2000 Verification Traces For equipment containing software a Hardware Software Interaction Analysis shall be performed to ensure that the software is designed to react in an acceptable way to hardware
189. solescent EEE parts components which will be discontinued or that will no longer be available D Items with long supply or manufacturing time LNG e Long Lead Items gt 12 months e Items with ITAR restriction E Planetary Protection critical items PP e Items technologies and operations having impacts on Planetary Protection requirements fulfillment MS PA REQ 0580 Verification Traces Maximum effort will be made to eliminate the possible causes of criticality identified during the early phases of the program MS PA REQ 0590 Verification Traces In case the risk cannot be eliminated adequate solutions or preventive actions will be identified to reduce and or control the risk as identification of additional requirements tests checks and verification of manufacturing processes MS PA REQ 0600 Verification Traces Provisions for Critical Items control shall be initiated as early as possible in the program and shall include actions in one or more of the following areas in order of precedence design manufacturing inspection test operation THALES SEN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 0610 Verification Traces Critical items shall be identified through standard PA control met
190. sponsible for maintaining appropriate packaging of EEE parts up to assembly MS PA REQ 4070 Verification Traces Components dedicated to EXOMARS program shall be stored in suitable containers placed in controlled area in which the access is limited to program involved personnel only MS PA REQ 4080 Verification Traces For co ordinated procured items CPPA has to inform via dispatch note about any special storage handling condition requested e g ESD sensitive devices dry storage under nitrogen etc Warning label indicating the required handling precautions shall be written in English and well visible in the external packages of the items MS PA REQ 4090 Verification Traces Parts will be handled and stored in accordance with the requirements of ECSS Q 20B e Storage conditions shall be adequate to inhibit degradation of the surface finishes of the mounting areas of the components e EEE parts will be stored in cleanliness controlled environment 22 C 5 C and Relative Humidity 55 10 with appropriate measures to segregate and protect components during receiving inspection storage and delivery to manufacturing e Control measures to ensure that electrostatic discharge susceptible components are identified and handled only by properly trained personnel using anti static packaging and tools THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K
191. ss steel shall be passivated Mechanical parts made of Titanium alloys shall be anodised Deleted 8 14 Stress Corrosion MS PA REQ 4550 Verification Traces EXM MS RS ESA 00002 PA SY 1980 Metallic materials used in structural applications shall have a high resistance to Stress Corrosion Cracking SCC and shall be chosen from Table 5 1 of ECSS Q ST 70 36 Metallic materials and welds that are not listed in ECSS Q ST 70 36 or whose SCC resistance is unknown shall be tested and categorised according to the requirements of ECSS Q ST 70 37 Deleted THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE 8 15 Fluid Compatibility MS PA REQ 4560 Verification Traces EXM MS RS ESA 00002 PA SY 2000 Materials that will be in permanent contact during planned operations with an identified fluid shall be compatible with that fluid If compatibility data are not available then testing shall be performed according NASA STD 6001 test number 15 That compatibility shall be identified in the DML and DMPL Output The requirement shall be fulfilled through the deliverables PA 27 and PA 28 Deleted 8 16 Allowable Stress MS PA REQ 4570 Verification Traces EXM MS RS ESA 00002 PA SY 2020 Allowable stresses for materials shall be deriv
192. sting level 1 may be applied for hybrids if ESCC has classified the relevant manufacturer as Category 1 for the technology domain relevant to a particular Hybrid circuit ECSS Q ST60 12C is applicable for all activities up to acceptable dice level MMICs For hybrids according to PSS or manufactured in Europe all add on components shall be listed and traced in the relevant procurement specification THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3390 Verification Traces For US hybrids whose DCLs are not disclosed cause considered proprietary reserved information the procurement authority shall propose alternative mean indicated in the relevant PAD in order to reach the necessary confidence on quality of add on parts traceability radiation assurance MS PA REQ 3400 Verification Traces EXM MS RS ESA 00002 PA SY 1440 Any additional and or alternative screening proposals may be applied for procurement only upon approval of the relevant PAD as required in ECSS Q ST 60 In case of need of components available on the market only in a lower screening level up screening will be planned and the flow of activities provided and approved via life cycle of the relevant PAD The up screening activities will be preferably performed by the manufac
193. t 100 15 MS PA REQ 3730 Verification Traces The attrition rule for one time programmable ICs shall be twice of the standard attrition quantities see above It should be noted that user may be requested to increase the attrition on a case by case basis in order to cover also multiple redesigns e g PROM used for storing boot software MS PA REQ 3740 Verification Traces For highly expensive integrated circuits like FPGA microprocessors memories or for unique devices like customised items connectors bodies heaters etc a reduction of attrition or a CPPA centralised attrition stock may be proposed to EXO PCB acceptance MS PA REQ 3750 Verification Traces The users shall define separately in the DCL the two quantities e Engineering quantity e Attrition quantity THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 7 4 11 Traceability MS PA REQ 3760 Verification Traces Traceability shall be maintained from serialized part to assembly level MS PA REQ 3770 Verification Traces Traceability during EEE parts manufacturing and testing shall be covered by the procurement specifications and the applicable system ESCC or MIL MS PA REQ 3780 Verification Traces Such traceability shall be kept by t
194. tation Handling and Installation Procedures THALES Se All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE Shipping Documents Supporting Documents such as Inspection requirements before use Proof Load certificates Hazard Analysis with the closure of Residual Hazard Sheets S W Configuration Status List FMECA CIL CE Certification SEE section 11 1 11 MS PA REQ 4910 Verification Traces The EIDP shall be initiated prior to and maintained during all stages of assembly inspection and test for each of the equipment specified Complete copies of the EIDP s shall be submitted to higher level contractors Quantity 2 to Thales Alenia Space and Quantity 1 to ESA at least 15 working days prior to the Delivery Review final updates may be given at the review MS PA REQ 4920 Verification Traces The EIDP shall be delivered in hard copies plus CD ROM support MS PA REQ 4930 Verification Traces Updates of EIDP s have to be provided if GSE are returned for any modification corrective actions 11 1 4 GSE Dependability and Safety MS PA REQ 4940 Verification Traces The requirements defined in Para 5 Dependability and Para 6 are applicable to e Portions of the GSE which interface directly with flight hardware THALES RE All r
195. te controls are included proprietary rights will be respected 8 18 2 Processes for EEE mounting and assembly MS PA REQ 4670 Verification Traces The contractor shall demonstrate the adequacy and the qualification status of his mounting and assembly rules for each package technology and material as reported in paragraph 3 4 6 EEE components requirements on materials and processes of this PA requirements 8 19 Printed Circuit Boards MS PA REQ 4680 Verification Traces EXM MS RS ESA 00002 PA SY 2120 Printed circuit boards shall be procured from an ESA qualified source according to ECSS Q ST 70 11C The qualification of printed circuit boards shall comply with ECSS Q ST 70 10C 8 20 Fasteners MS PA REQ 4690 Verification Traces EXM MS RS ESA 00002 PA SY 2130 Fasteners shall be manufactured and procured in acc with the requirements in ECSS Q ST 70 46C THALES Re All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE 9 SW PRODUCT ASSURANCE MS PA REQ 4700 Verification Traces All SW PA Requirements are placed in dedicated and applicable document SW PA Requirements for Subco s EXM MS RQM AI 0010 THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIB
196. tegory number for a single point failure no redundancy or back up implemented A suffix S shall be added to the severity category number in case of hazard risk A suffix CM CC shall be added to the severity category in case of common mode common cause failure MS PA REQ 1360 Verification Traces THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQM AI 0004 WG ThalesAlenia DATE 21 01 2011 anemia SDEP ISSUE 05 Pace SYSTEM LEVEL Dependability Severity Categories Level Severity Failure Effect Consequence Category 1 Critical Loss of mission e Loss of all Technology Demonstration Objectives or e Loss of Surface Mobility with a Rover Objective or e Loss of Programmatic Objective 2 Major Major mission degradation e Loss of two non critical Technology Demonstration Objectives or e Loss of Payload support resulting in loss of all Science Objectives 3 Significant Significant mission degradation e Loss of one non critical Technology Demonstration Objective or e Loss of Payload support resulting in loss of one or more Science Objectives 4 Negligible Negligible e Any other effect SUBSYSTEM ASSEMBLY EQUIPMENT LEVEL Severity Categories Severity category Level Failure Effect Consequence 1 Propagation of failure to other subsystems assemblies equipment Loss of functionality 2 Degradation o
197. th is the last point for which no destructive event is observed Step 2 Calculate Destructive Single Event equivalent Rate Aeq taking into account experimental device cross section vs LET curve A Gd Step 3 The Destructive Single Event device application will be accepted only if 10 where A is the reliability failure rate of the part 25 C hig gt Ea Step 4 if 10 then the Destructive Single Event device application will be accepted only if there is no impact on the equipment and or system reliability analysis The results of this analysis will be included in the radiation analysis and submitted to prime and customer approval via RFD RFW 7 4 2 3 RADIATION REVIEW MS PA REQ 3250 Verification Traces THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE For coordinated procured items the user shall co operate with EXO PCB in the validation of TD and SEE existing data and the agreed data or testing activities on the procured lot if any shall be reported in the PAD of the relevant sensitive part MS PA REQ 3260 Verification Traces For CPPA procured items test report mentioned in the PAD as valid data for TD and SEE sensitivity shall be made available to the users subcontractors MS PA REQ 3270 Verification Traces
198. tical Control Programme shall be subject to TAS approval The contractor shall identify those items which are a risk to the programme e g unqualified processes THALES cea All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE unqualified materials critical items from the dependability and safety analyses special software special GSE When the corresponding actions have been implemented a close out reference shall be added 4 4 1 Critical Item definitions MS PA REQ 0550 Verification Traces The definition of critical item shall be applied to all those elements which have for various reasons a reduced degree of confidence about their own performance in operations if not adequately controlled on ground during the development manufacturing and test phases MS PA REQ 0560 Verification Traces Their criticality may have impact on different areas such as reliability safety fracture control program or operating time MS PA REQ 0570 Verification Traces The following definitions and ranking criteria shall be applied Id A Safety Reliability and Qualification Critical Items SPF e Critical Single Point Failures SPF with a severity category 1 amp 2 at System level SPF classified as safety Catastrophic or Critical Categories 1H and 2H As
199. tion due to ESA PA Requirement updating rev3 6 dated 22 03 2010 A version for Project CCB 42 Discussion Para 2 2 3 Rover requirements Document added EXM RM RS ESA 00001 Para 2 2 3 IR 015 ESA document requirement description DRD EXM MS RS ESA 00010 Standard descriptive text for normative documents added Modification due to ESA PA Requirement updating rev 4 0 dated 24 03 2010 Version for CCB 43 Approved Scope modified to clarify applicability to Groundsegment Para 2 1 Added NR 128 JPL D 64939 Launch Service Requirement Document NR 129 AFSCPSMAN 91 710 V3 Air Force Space Command Manual NR 130 NASA STD 8719 9 Standard for Lifting devices NR 131 Transportation of radioactive material Deleted NR 01 NR 03 and moved to Para 2 2 IR section Para 2 2 Added IR116 Atlas Launcher User Manual IR 01 Mission and System Requirements IR 10 Rover Requirements THALES SEH All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE 8 175 IR 03 Management Requirement Document Para 3 Descriptive text of rewritten add sentences 5 DEPENDABILITY 5 3 Dependability engineering Para 5 3 1 added section on ExoMars Programme objectives from MSRD_6 0 PA Reqs_4 0 and allocation to the 2016 2018 mission Para 5 3 1 1 Table 5 3 1 updated including System Module level
200. tion to ECSS Q 00 MS PA REQ 0170 Verification Traces EXM MS RS ESA 00002 PA SY 110 All PA related data and analyses e g NCRs SPRs RFW PA analyses PA planning alerts EEE components list Materials and processes lists dependability Safety analysis CIL pictures etc shall be stored in an electronic database This shall allow to import and export data from and to sub contractors and the Customer MS PA REQ 0180 Verification Traces EXM MS RS ESA 00002 PA SY 120 The subcontractor shall establish and maintain an up to date Product Assurance Data File It shall contain but not be limited to e PA documents as identified in para XX PA reports and technical notes PA meeting minutes and actions PA review and PA audit results Nonconformances tracking list and reports including NRB minutes RFW reports and tracking lists Critical Item List CIL PA analyses MIP KIP schedule tracking list and reports Manufacturing Flow plans charts Parts Materials Processes Lists with associated approval documents PMP Status Lists EEE parts lists EEE parts lists reference and approval status list PADs status list e Alert status list This data file shall be readily available and accessible to the TAS and ESA project personnel Documents shall be delivered as defined in the Statement of Work It is recommended that the PA data file shall be summarized and made available in computerized THALES wee All rights reser
201. ts approved for co ordinated procurement shall be formally covered by PAD prepared by CPPA and submitted to TAS ESA approval in the frame of EXO PCB CPPA shall gather the customer PAD approval before starting the procurement of the relevant part Users of CPPA service will not need to raise PADs for co ordinated procured items e Each Self Procured and or Self Manufactured component i e component that will be procured manufactured directly by the users shall be approved via PAD prepared by the user and submitted to the upper level contractor chain up to TAS and ESA approval Components that will not be included in the loop of co ordinated procurement need TAS ESA authorisation before starting the self procurement activities even if they meet the quality EXOMARS requirements THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3320 Verification Traces EXM MS RS ESA 00002 PA SY 1350 The previous use or approval of a part via PAD or DCL approval for previous ESA project shall not be considered as an automatic approval for EXOMARS It shall be considered and traced in any case in the section APPROVAL STATUS of the relevant PAD MS PA REQ 3330 Verification Traces EXM MS RS ESA 00002 PA SY 1370 In case of consistent self pr
202. turer its self 7 4 6 1 Additional tests MS PA REQ 3410 Verification Traces In addition to the above specified screening level the following additional tests shall apply MS PA REQ 3430 Verification Traces EXM MS RS ESA 00002 PA SY 1500 e Parts with cavities shall be subjected to PIND test on a 100 basis MS PA REQ 3440 Verification Traces EXM MS RS ESA 00002 PA SY 1510 e All solid tantalum capacitors shall be subjected to surge current testing as per the relevant specification THALES RER All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE MS PA REQ 3450 Verification Traces e EEPROM procurement specification shall specify the data retention time guaranteed over the full operating temperature range This specification shall detail all the tests performed at die revision level part level and lot level in order to guarantee this data retention time MS PA REQ 3460 Verification Traces EXM MS RS ESA 00002 PA SY 1520 e PRECAP inspection shall be performed as defined in the table 1 that describes the pre and post procurement inspections per family specification applicable to Exomars mission MS PA REQ 3470 Verification Traces e f a PRECAP inspection is not possible for the purchased quality level an extended
203. ty of providing reliable SEE susceptibility data is on top of the procurement authority CPPA for co ordinated procured items users for self procured items MS PA REQ 3160 Verification Traces EXM MS RS ESA 00002 PA SY 1260 EXM MS RS ESA 00002 PA SY 1300 A part will be considered Single Event Free if no event is observed at LETequ gt 60 MeV cm mg in addition for destructive events the parts will not experiment any event up to a fluence of 10 ions cm2 7 4 2 2 1 1 Components exhibiting a sensitivity between 15 MeV cm2 mg lt LETth lt 60 MeV cm2 mg shall be subject to the appropriate Heavy lon SEE rate predictions The SEE rate prediction results shall be used in the Radiation Analysis and in the FMECA for the system impact assessment MS PA REQ 3170 Verification Traces EXM MS RS ESA 00002 PA SY 1270 As far as not permanent SEE as SEU Single Event Upset SET Single Event Transient there is no requirement of minimum LET threshold or maximum cross section Each subcontractor will include SEU SET sensitive components in the SEE criticality analysis showing the suitability of the selected part within the unit application The SEE criticality analysis shall be included in the Radiation Analysis or in the unit FMECA for the system impact assessment and upper level contractor Prime ESA approval THALES en All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DI
204. ude a Electrical stress such as accelerated life testing high temperature reverse bias or endurance testing normally used to assess stability b Mechanical stress including shock vibration and centrifuge to evaluate the robustness of the assembly c Environmental stress such as thermal shock or cycling high or low temperature storage and seal tests etc to evaluate package integrity or a particular facet of the design expected to be susceptible to temperature extremes d Radiation testing MS PA REQ 3880 Verification Traces A tailoring or modification of the above reported test campaign can be performed depending on the qualification status of the component and on the specific application condition MS PA REQ 3890 Verification Traces On a case by case basis the evaluation campaign is reduced to specific electrical test long duration power thermal cycles electrical parameters measurement in operating condition outside the qualified operating range E g components that needs to be stored at temperature below minimum storage temperature limit or need to be bias at temperature below the minimum operating temperature limit MS PA REQ 3900 Verification Traces THALES RE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pr Tha lesAlertia DATE 21 01 2011 eer Space ISSUE 05 PAGE The propos
205. uirements defined in the applicable documents The task descriptions and procedures shall include those to be performed and to be applied by his co and subcontractors MS PA REQ 2480 Verification Traces EXM MS RS ESA 00002 PA SY 940 The planning of the safety assurance activities shall correspond to the ExoMars milestone planning and the dates for safety submissions and safety reviews as required by the launcher authority Adequate margins which have to be agreed by ESA shall be included in the planning to allow for review of safety data packages by ESA and for potential corrections before the data packages have to be submitted to the launch authority 6 3 Hazard Severity Categories MS PA REQ 2490 Verification Traces EXM MS RS ESA 00002 PA SY 960 ECSS Q 40 Paragraph 5 3 Table 1 shall be superseded by the following table MS PA REQ 2500 Verification Traces EXM MS RS ESA 00002 PA SY 970 The consequences of a risk related to safety are classified in categories as defined in the following table THALES a All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 ea SCE ISSUE 05 PAGE Severity of identified hazards and consequences Severity of identified hazards and consequences Consequence Catastrophic Loss of human life life threatening permanently disabling injury or occup
206. upport the approval For EDM and Rover applications can be used without any further provisions Components that have been proven by valid data or dedicated test a sensitivity lower than 10 KRad for any applications shall be subjected to dedicated EXO PCB and user approval on case by cases basis Users radiation analysis shall support the approval For parts coming from lot that have been subjected to RVT test the margin factor can be reduced to 1 5 MS PA REQ 3120 Verification Traces EXM MS RS ESA 00002 PA SY 1220 The Total dose assurance shall include the evaluation for bipolar and BICMOS devices of Enhanced Low dose rate 0 01 rad sec sensitivity The ELDR sensitivity shall be addressed in the RVT method and planning The procurement authority of EEE parts either the CPPA or the subcontracotors will be responsible of presenting an appropriate test plan for bipolar and biCMOS linear devices covering the ELDR sensitivity THALES DEEN All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAleni DATE 21 01 2011 Space ISSUE 05 PAGE for customer approval As reference purpose it is included a typical ELDR test methodology For bipolar and biCMOS linear devices the Dose Rate in RVT shall be lt 0 01 rad s up to 10krad During irradiation the part will be biased in the worst configuration at room temperature Th
207. ved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 pe Tha les Aleria DATE 21 01 2011 eer Space ISSUE 05 PAGE databases and as a minimum part materials and processes lists EEE parts lists as well as NCR status lists including actions and configuration status lists shall be made available to TAS ESA in a searchable and index sort able electronic form The structure contents and Database Management system shall be agreed with TAS ESA The PA database shall be capable of importing and exporting data from and to TAS ESA in a mutually agreed format It is recommended to use subcontractors in house tools already in use provided that TAS ESA are satisfied with functionality performance and compatible interfaces are established 3 5 Subcontractors Suppliers PA Program MS PA REQ 0190 Verification Traces Subcontractors Suppliers shall implement a Product Assurance program in accordance to the requirements of this document MS PA REQ 0200 Verification Traces The PA program shall be described in the Suppliers PA Plan 3 6 Right of Access Participation MS PA REQ 0210 Verification Traces EXM MS RS ESA 00002 PA SY 40 TAS ESA shall have the right of access to all technical and programmatic documentation all areas and operations within the contractor s or supplier s facilities in which work is performed or items are sto
208. vities related to safety towards the launch authority including participation in all safety reviews which are required in the applicable documents It is the responsibility of the contractor to determine whether more stringent safety requirements are applicable via requirements specified elsewhere for other locations where equipment is used or activities carried out for the ExoMars project e g for equipment being transported by air The contractor shall assure compliance to such requirements PA SY 840 Deleted MS PA REQ 2350 Verification Traces EXM MS RS ESA 00002 PA SY 850 The acceptance rationale for residual hazards shall identify the reasons the hazard cannot be eliminated all provisions and controls which are applied to reduce the hazard to an acceptable level MS PA REQ 2360 Verification Traces EXM MS RS ESA 00002 PA SY 860 Protection systems shall to the greatest extent possible be intrinsically fail safe and shall be capable of being enabled and disabled by commands MS PA REQ 2370 Verification Traces EXM MS RS ESA 00002 PA SY 870 For safety certification the Subcontractor and Supplier shall certify that the flight and ground system products are in compliance with the requirements of the applicable standards as well as any applicable THALES AREE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004
209. y as feasible and in parallel to the design activities and to the preparation of activities with plans and procedures in order to identify potential hazards to eliminate them as far as practical and as required and or control them to acceptable levels MS PA REQ 2540 Verification Traces EXM MS RS ESA 00002 PA SY 1000 The Subcontractor and Supplier shall perform hazard analyses and demonstrate how the hazards are controlled Residual hazards shall be subject to approval by ESA as well as any non compliance to safety requirements per Request for Waiver MS PA REQ 2570 Verification Traces EXM MS RS ESA 00002 PA SY 1010 The Subcontractor and Supplier shall deliver Hazard Analyses for every design review and before every major integration and test campaign on equipment subsystem and system level MS PA REQ 2580 Verification Traces EXM MS RS ESA 00002 PA SY 1020 Residual Hazards shall be identified and acceptance rationales shall be provided for these reviews on suitable form sheets for formal approval by TAS ESA MS PA REQ 2590 Verification Traces Additional specific safety analyses the Subcontractor and Supplier shall perform additional safety analyses such as venting analysis leak before burst analysis and dedicated thermal analysis of pressurized assemblies as required by the launcher authority or ExoMars TAS ESA to support the safety review process The outcome of these analyses sha
210. y case the selection of each part technology shall be driven by its status of qualification The selection of high reliability EEE parts shall be based therefore on the knowledge regarding technical performance qualification status and history of previous usage in similar applications with maximum use of qualified parts and with established reliability history Preference shall be given to parts from sources that would necessitate the least evaluation qualification effort EEE parts shall be selected in compliance with the requirements of the project Mission life operating stability materials planetary protection safety quality reliability and to withstand all environmental conditions including tolerance to radiation exposure total dose single events and displacement damage effects for active parts As second stage the selection shall take into account e minimization and standardization of the number of different generic part types and families e parts from multiple sources are preferred The EXO PPL will contain as well the list of components that will be covered by the Low temperature evaluation campaign that CPPA is conducting under TAS I and ESA direction to extend the storage temperature range down to 130 C Any new developed item for the mission hybrid MCM ASIC FPGA detector custom MMIC shall be considered as a critical item for the unit and the status of its development shall be tracked in the CIL and updated for each un
211. y category of functions and operations shall be directly related to the severity of the consequences resulting from failure of the function or operation e g a function whose failure induces a catastrophic consequence shall be classified with the highest criticality level The criticality category assigned to a product hardware and software shall be the highest criticality category of the functions associated to the product THALES SE All rights reserved 2007 Thales Alenia Space CONTROLLED DISTRIBUTION 100181547K EN CONTROLLED DISTRIBUTION REFERENCE EXM MS RQN AI 0004 Tha lesAlenia DATE 21 01 2011 Space ISSUE 05 PAGE MS PA REQ 1930 Verification Traces The subcontractor shall establish and maintain a system to track the dependability recommendations originated by the dependability analyses until they are implemented MS PA REQ 1940 Verification Traces The subcontractor shall plan dependability analysis according to the project life cycle development plan and review plan to demonstrate compliance with the dependability requirements MS PA REQ 1950 Verification Traces All the Analyses and documents shall be delivered in an electronic form to be agreed with the Prime suitable for further processing and incorporation into higher level documents if necessary 5 4 1 Functional Analysis FA DELETED DELETED DELETED 5 4 2 Failure Modes Effects and Criticality Analy

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