1. MAB
  2. Program Planning & Systems Engineering
  3. Program Systems Engineering
  4. System Transition
  5. System Validation

2.2.7.1 - System Validation

2.2.7.1-2 Level 2 Tasks

Tasks Applicable Mission Phases Description SFWC Artifacts References
2.2.7.1-2-1 Ensure health and safety of space vehicle is verified Phase D2 | Ensure space vehicle establishes contact with the ground station to verify health and status through telemetry generated by the telemetry, tracking and commanding subsystem and transmitted by the communications subsystem. Ensure command function is working properly NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
2.2.7.1-2-2 Ensure functional checks and deployments are completed Phase D2 | Ensure deployment sequence is executed and each subsystem is turned on and checked out functionally. Ensure each subsystem meets required performance parameters. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
2.2.7.1-2-3 Ensure calibration is complete Phase D2 | Ensure each subsystem is calibrated to make sure that the data coming from the space vehicle accurately reflects how well the space vehicle is doing. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
2.2.7.1-2-4 Ensure inter-segment operability demonstration functions properly as an integrated system and can fulfill mission objectives Phase D2 | Ensure the entire space to ground system, including the space and mission control segments, can function properly and in integrated assembly and can fulfill mission objectives. NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
2.2.7.1-2-5 Ensure executable plan in place to periodically recheck the subsystem calibrations and make adjustments for degradation Phase D2 | Ensure on-orbit maintenance plan includes calibration of redundant system if switched or made primary to verify operability and performance NA NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2
2.2.7.1-2-6 Ensure all anomalies/non-conformances evaluated, closed and/or acceptable to fly as-is Phase D2 | Ensure all anomalous behavior is diagnosed and fix or workaround is validated. SFWC 4.12 NA Space Vehicle Test and Evaluation Handbook, TOR-2011(8591)-2