| 2.3.6-3-1 Ensure that preliminary design is described in enough detail to ensure that it is feasible and has adequate margin or closure plan for each requirement with inadequate or negative margin to proceed with low risk with detailed design |
Phase A |
Phase B |
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Ensure that preliminary design is described in enough detail to ensure that it is feasible and has adequate margin or closure plan for each requirement with negative margin to proceed with low risk with detailed design. This is an exit criteria to the preliminary design review
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NA
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Design Review Data Package
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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; TOR-2006(8506)-4494, Space Vehicle Systems Engineering Handbook
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| 2.3.6-3-2 Ensure that detailed design by review of drawings, analyses, developmental rest results, and design summaries meets each EMC requirement with adequate margin before approving Critical Design Review (CDR) |
Phase A |
Phase B |
Phase C |
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Ensure that critical design is described in enough detail to ensure that it is feasible and has adequate margin or closure plan for each requirement with inadequate margin to proceed with low risk with detailed design.
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NA
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Design Review Data Package; System/Segment Specification (SSS)
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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; TOR-2006(8506)-4494, Space Vehicle Systems Engineering Handbook
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