| 2.2.5-4-1 Ensure verification risk assessment is performed |
Phase A |
Phase B |
Phase C |
Phase D1 |
|
MA evaluates key risks to mission success and determines if testing or other methods is the best verification method for segment requirements. Test risk assessment also examines the potential risks to the flight hardware from the proposed test program.
|
NA
|
NA
|
Mission Assurance Guide, TOR-2007(8546)-6018, Rev B
|
| 2.2.5-4-2 Ensure test risk items are evaluated |
Phase A |
Phase B |
Phase C |
Phase D1 |
|
Ensure the selected test methods are appropriate, are conducted at the appropriate level of assembly, and minimize risk to the hardware.
|
AFMAN 63-119 A13.2.6
|
NA
|
Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; AFMAN 63-119 or equivalent
|
| 2.2.5-4-3 Ensure integration risks are evaluated |
Phase B |
Phase C |
|
Ensure interface design is managed as a separate and distinct function and not as an afterthought by specialty engineers. Ensure all integration issues are resolved, risks identified and subsequently mitigated to ensure mission success.
|
NA
|
NA
|
Space Vehicle Systems Engineering Handbook, TOR-2006(8506)-4494
|
| 2.2.5-4-4 Ensure risks associated with deviations from environmental testing standards are evaluated and documented as baseline |
Phase B |
Phase C |
Phase D1 |
|
Ensure environmental testing risks are evaluated and briefed at the program level.
|
AFMAN 63-119 A23.1
|
NA
|
Mission Assurance Guide, TOR-2007(8546)-6018, Rev B; AFMAN 63-119 or equivalent
|
| 2.2.5-4-5 Ensure evaluation of the impacts of repetitive testing on flight hardware at each level of assembly to include retesting |
Phase C |
Phase D1 |
|
Specifically evaluates the impacts of repetitive testing on flight hardware at each level of assembly to include retesting.
|
NA
|
NA
|
Mission Assurance Guide, TOR-2007(8546)-6018, Rev B
|