2.3.4 - Electrical Design Integration

2.3.4-3 Level 2 Tasks

Tasks Applicable Mission Phases Description SFWC Artifacts References
2.3.4-3-1 Ensure unit to unit interfaces are clearly defined Phase B | Phase C | Ensure interface specifications includes connector type and pin out. Coordinate with Electrical Design Integration (EDI) to ensure voltage drop analyses are complete and accurate. Ensure harness design satisfies all applicable architecture rules and operations under fault tolerance conditions. NA Intra-Segment ICDs Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2, Interconnect Hardware, Cables, and Connectors chapter; TOR-2008(8583)-8492, Wiring Harness, Space Vehicle, Design and Testing, General Specification for
2.3.4-3-2 Ensure the accuracy of fuse module, fusistor module, and other components that are part of the harness Phase B | Phase C | Phase D1 | Ensure the fuses used are consistent with the fuse sizing analysis. Drawings should include testing call out. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2, Interconnect Hardware, Cables, and Connectors chapter; TOR-2008(8583)-8492, Wiring Harness, Space Vehicle, Design and Testing, General Specification for
2.3.4-3-3 Ensure the accuracy of component termination drawings Phase B | Phase C | Phase D1 | Ensure all parts, materials, and manufacturing processes (PM&P) including rework processes called out in the drawing are flight qualified. Ensure the components call out are consistent with the thermal, command and telemetry data base. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2, Interconnect Hardware, Cables, and Connectors chapter; TOR-2008(8583)-8492, Wiring Harness, Space Vehicle, Design and Testing, General Specification for
2.3.4-3-4 Ensure the cable and harness critical item control plan adequately identifies critical items and are appropriately controlled Phase B | Phase C | Phase D1 | Ensure a system level analysis is performed to identify all single point failures (SPF) and any components that need special attention due to safety or criticality. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2, Interconnect Hardware, Cables, and Connectors chapter; TOR-2008(8583)-8492, Wiring Harness, Space Vehicle, Design and Testing, General Specification for
2.3.4-3-5 Ensure the grounding implementation is evaluated Phase B | Phase C | Ensure all groundings in the grounding diagram are consistent with the EMC specification and EMI/EMC plan. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2, Interconnect Hardware, Cables, and Connectors chapter; TOR-2008(8583)-8492, Wiring Harness, Space Vehicle, Design and Testing, General Specification for