| 2.3.6-1-1 Ensure analysis or alternatives, request for proposal, and contract incorporate EMI/EMC requirements |
Phase 0 |
Phase A |
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Ensure request for analysis of alternatives, proposal, and contract has an Electromagnetic Compatibility Design/Requirements/Test Program described with adequate supporting evidence to verify analysis of alternatives, proposal, and contract is feasible within programmatic constraints of cost, schedule, performance, and risk
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NA
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Analysis of Alternatives (AoA) and Material Development Decision Products
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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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| 2.3.6-1-2 Ensure procurement specifications contain adequate flow-down of Electromagnetic Compatibility design and test requirements |
Phase 0 |
Phase A |
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Ensure procurement specifications contain adequate flow-down of Electromagnetic Compatibility design and test requirements. This is required in the Statement-of-Work, System Specification, and Prime Item Development Specification or equivalent to ensure traceability from mission to hardware requirements. Each lower level document has increasing detail. Higher level documents have precedence. Final required by System Requirements Review (SRR)
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NA
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System Requirements Document; 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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| 2.3.6-1-3 Ensure requirements traceability from EMC (Electromagnetic Compatibility) system level requirements to unit level procurement specifications |
Phase A |
Phase B |
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Ensure requirements traceability from EMC (Electromagnetic Compatibility) system level requirements to unit level procurement specifications before procurement of units. Unit procurement usually starts short after the preliminary design review. This is required to ensure traceability from system requirements to unit requirements. The system level requirements have precedence over the unit level requirements. This level should have the actual unit level EMC requirements, EMC design requirements, EMC verification requirements including inspection, Final required as exit criteria from (PDR).
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NA
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System Requirements Document; 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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| 2.3.6-1-4 Ensure system constraints on Electromagnetic Compatibility (EMC) design to ensure EMC design meets system requirements |
Phase A |
Phase B |
Phase C |
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Ensure system constraints on EMC design considers mission requirements, heritage hardware capability, weight, structural, thermal, life issues, reliability, radiation, signal integrity, parts/materials/processes, etc.to ensure design meets requirements. Draft constraints should be identified by System Requirements Review. Final system constraints should be identified by PDR. Ensure EMC design meets each systems constraints as exit criteria from CDR.
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NA
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System Requirements Document; 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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| 2.3.6-1-5 Ensure heritage hardware and qualified by similarity hardware evaluated for compliance with EMC (Electromagnetic Compatibility) requirements |
Phase A |
Phase B |
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Ensure heritage hardware and qualified by similarity hardware evaluated for compliance with EMC (Electromagnetic Compatibility) requirements. This includes any hardware that will be procured without requiring EMC qualification or acceptance testing at the unit level. The final evaluation showing margin should be done by the Preliminary Design Review. The task completion may change to system requirements review if there is significant program cost and schedule risk being taken by delaying the task. This is phased for no mission risk.
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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; 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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| 2.3.6-1-6 Ensure Electromagnetic compatibility (EMC) portions of Preliminary Design Review (PDR) packages are evaluated |
Phase B |
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Ensure Electromagnetic compatibility (EMC) portions of Preliminary Design Review (PDR) packages are evaluated as entry criteria to PDR and completed as an exit criteria to PDR. Ensure each requirement has required margin or closure plan.
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NA
|
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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| 2.3.6-1-7 Ensure Electromagnetic compatibility (EMC) portions of Critical Design Review (CDR) packages are evaluated |
Phase C |
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Ensure Electromagnetic compatibility (EMC) portions of Critical Design Review (CDR) packages are evaluated as entry criteria to CDR and completed as an exit criteria to CDR. Ensure each requirement has required margin or closure plan.
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NA
|
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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| 2.3.6-1-8 Ensure the contractor and government EMC Design Assurance Plan for verifying that the detailed design drawings will meet all EMC requirements |
Phase B |
Phase C |
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Ensure plan Includes Responsibility, Processes, Procedures, Inspection Criteria, Review Criteria, Training/Certification, Quality Assurance, and Auditing for each requirement. This includes all drawing notes and manufacturing planning that will be used to implement the design on the drawings
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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; TOR-2006(8506)-4494, Space Vehicle Systems Engineering Handbook
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| 2.3.6-1-9 Ensure verification of all Electromagnetic Compatibility (EMC) requirements is complete and accurate |
Phase C |
Phase D1 |
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Ensure verification of all Electromagnetic Compatibility (EMC) requirements is complete and accurate. Ensure each unit, subsystem, and system EMC verification is complete and accurate. This includes heritage units and qualification by similarity units which require objective data that at least one version of the unit met the requirements. This includes verification by analysis, inspection, demonstration, and test.
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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; TOR-2006(8506)-4494, Space Vehicle Systems Engineering Handbook
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| 2.3.6-1-10 Ensure coordination of space vehicle radiated susceptibility requirements, radio frequency monitoring and retest requirements, and lightning monitoring and retest procedures with range and space vehicle provider |
Phase D1 |
Phase D2 |
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Ensure coordination of space vehicle radiated susceptibility requirements, radio frequency monitoring and retest requirements, and lightning monitoring and retest procedures with range and launch vehicle provider. This is required before the Critical Design Review if there are any mission unique requirements. Otherwise this should be completed before test and integration of the space vehicle is completed.
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NA
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System Requirements Document; Segment Design Specification
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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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