| 4.4.6-8-1 Ensure that all interfaces are identified, requirements are defined, and are consistent with interface control documents |
Phase B |
Phase C |
|
Ensure that all interface requirements are defined by Preliminary Design Review, completed and presented by Critical Design Review. Ensure that both physical and functional interfaces are defined.
|
NA
|
NA
|
Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494, Major Interfaces Chapter
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| 4.4.6-8-2 Ensure end-to-end compatibility of the subsystem with all other subsystems and external systems involved in specific functionality |
Phase B |
Phase C |
Phase D1 |
|
Ensure end-to-end testing verifies functional interface
|
NA
|
NA
|
Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494, Major Interfaces Chapter
|
| 4.4.6-8-3 Ensure all interfaces are tested in an operational-like environment |
Phase D1 |
|
Ensure that the interface testing is described and consistent with the verification planning
|
NA
|
NA
|
Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494, Major Interfaces Chapter; SMC-S-016 "Test Requirements for Launch, Upper-stage, and Space Vehicles 5 Sept 2014 or equivalent
|
| 4.4.6-8-4 Ensure all payload interface thermal requirements (environments, temps, heat transfer) are adequate |
Phase B |
Phase C |
|
NA
|
NA
|
NA
|
Systems Engineer's Major Reviews for National Security Space System Programs, TOR-2004(3909)-3360 Rev 1 pg 36-38, 69-71
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| 4.4.6-8-5 Ensure that TCS interfaces with telemetry, computer heater control, and commands are adequately defined |
Phase B |
Phase C |
|
Ensure sufficient thermal telemetry points to assess critical mission events. Ensure that computer controlled heaters return to safe state after computer swap or reboot.
|
NA
|
NA
|
Systems Engineer's Major Reviews for National Security Space System Programs, TOR-2004(3909)-3360 Rev 1 pg 36-38, 69-71
|