| 4.4.4.7-4-1 Ensure electromagnetic issues are identified and mitigation plans are in place/executed |
Phase B |
Phase C |
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Ensure that MA EMC (Electromagnetic Compatibility) specs are flowed down and that the EMC control plan is generated for the ordnance/pyrotechnics subsystem. Ensure plan addresses any compatibility issues with ordnance/pyrotechnic devices and the system implementation (i.e., installation, to include cables, harness, interconnects, shielding, grounding, etc.). Preliminary plans should be presented at PDR (Preliminary Design Review) and final plans at CDR (Critical Design Review).
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NA
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NA
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Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494; AIAA S-113-2005, Criteria for Explosive Systems and Devices on Space and Launch Vehicles; Mission Assurance Guide, TOR-2007(8546)-6018, Rev B, Requirements chapter; SMC-S-008, ElectroMission Assurance Guide or equivalent; TOR-2007(8546)-6018, Rev Bnetic Compatibility Requirements for Space Equipment and Systems
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| 4.4.4.7-4-3 Ensure compatibility of ignition system to firing electronics |
Phase A |
Phase B |
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Details of ignition system and specific devices for compatibility can be found in referenced specification. Ensure sure fire with appropriate safety no-fire protections.
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NA
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NA
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AIAA S-113-2005, Criteria for Explosive Systems and Devices on Space and Launch Vehicles
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