| 2.3.6-4-1 Ensure the environmental test thoroughness of the Electromagnetic Compatibility (EMC) test program is evaluated against applicable environmental test standard |
Phase A |
Phase B |
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Ensure the environmental test thoroughness of the Electromagnetic Compatibility (EMC) test program is evaluated against applicable environmental test standard. This includes is by system, subsystem, and unit identifying the missing test verification requirements, incomplete requirements, and requirements with negative margin and assigning an individual risk and a roll up risk.
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-2 Ensure the system test plan has correct EMC tests and Electromagnetic Compatibility (EMC) test levels allocated to the system, subsystem, and units |
Phase B |
Phase C |
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Ensure the system test plan has correct EMC tests and Electromagnetic Compatibility (EMC) test levels allocated to the system, subsystem, and units. This includes tracing the requirements from the system, subsystem, and units into the system test plan.
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SFWC 2.4.2.3.4
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-3 Ensure that EMC life issues are identified and included in the system level test plan |
Phase B |
Phase C |
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Ensure that EMC life issues are identified and included in the system level test plan. This includes identifying parts, materials, and processes that have life issues, and ensuring they are included in life testing in the system test plan as requiring life testing.
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-4 Ensure adequate assessment is completed of heritage units and qualification-by-similarity units and their test procedures, test reports, and hardware and software changes made since qualification |
Phase A |
Phase B |
Phase C |
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Ensure adequate assessment is completed of heritage/qualification-by-similarity and their test procedures, test reports, and hardware and software changes made since qualification. This includes any unit that will be qualified by similarity as the qualification is resting on an existing test report. This should be completed as an exit criteria to the preliminary design review as the assumption is the unit meets the requirements.
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2; Test Requirements for Launch, Upper-Stage, and Space Vehicles, Vol II: Applications Guidelines, MIL-HDBK-340; TOR-2009(8546)-8604, Rev A, Reuse of Hardware and Software Products; TOR-2010(8591)-19, Objective Criteria for Heritage Hardware Reuse
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| 2.3.6-4-5 Ensure that Special Test Equipment and Ground Segment Equipment has defined a complete set of Electromagnetic Compatibility (EMC) requirements and has flowed those down with margin to the subsystems and units |
Phase B |
Phase C |
Phase D1 |
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Ensure that Special Test Equipment (STE) and Ground Segment Equipment (GSE) has defined a complete set of Electromagnetic Compatibility (EMC) requirements and has flowed those down with margin to the subsystems and units. This includes and EMC requirements that special test equipment and ground segment equipment may have to meet to ensure that the flight unit, subsystem, system EMC requirements can be verified. This should be completed as an exit criteria to the preliminary design review for the STE and GSE
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-6 Ensure Electromagnetic Compatibility (EMC) test procedures are adequate for facility choice, configuration choice, modes of operation choice, success/fail criteria choice, deviations from Test-Like-You-Fly, test method choice, and telemetry selection/trending choice |
Phase C |
Phase D1 |
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Ensure Electromagnetic Compatibility (EMC) test procedures are adequate for facility choice, configuration choice, modes of operation choice, success/fail criteria choice, deviations from Test-Like-You-Fly, test method choice, and telemetry selection/trending choice. This process starts with a review of the system test plan and continues with the review of the unit, subsystem, and system EMC test plans and test procedures.
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-7 Ensure there are Electromagnetic Compatibility (EMC) test readiness reviews for each test |
Phase C |
Phase D1 |
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Ensure there are Electromagnetic Compatibility (EMC) test readiness reviews for each test. Assure that Reviews are Complete and that there is a Closure Plan for All Open Items
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-8 Ensure Electromagnetic Compatibility (EMC) tests are completed according to the test procedure by witnessing tests |
Phase C |
Phase D1 |
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Ensure Electromagnetic Compatibility (EMC) tests are completed according to the test procedure by witnessing tests. Ensure witnessing of tests takes place to verify compliance with test procedures
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NA
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Integration and Test Plans
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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| 2.3.6-4-9 Ensure Electromagnetic Compatibility (EMC) test failures root causes are accurate and corrective actions are adequate and fully qualified to meet all requirements |
Phase C |
Phase D1 |
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Ensure Electromagnetic Compatibility (EMC) test failures root causes are accurate and corrective actions are adequate and fully qualified to meet all requirements. This includes a review of the adequacy of each root cause and each corrective action. This includes ensuring any design change is qualified to meet all requirements.
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NA
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NA
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TOR-2005(8583)-1, Rev A., Electromagnetic Compatibility Requirements for Space Equipment and Systems; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; MIL-STD-461F, Requirements for the Control of Electromagnetic, Interference Characteristics of Subsystems and Equipment; Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
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