System Requirements - Safety
Applicable Documents
- Compliance with NSTS1700.7B “Safety Policy and Requirements for Payloads using the Space Transportation System.”
- Utilization of 201.1c(3) “Unpowered Bus Exception” while inside the L/V, incorporating 4 independent inhibit micro-switches, and timers for the case of partial formation loss.
- Compliance with JSC-20793 “Manned Space Vehicle Battery Safety Handbook” for remaining hazard source.
Compliance Efforts
- battery and solar array are hazard sources, controlled by inhibits
- battery needs to be enclosed in leak proof container
- structure testing and documentation will be required
- no deployables on the S/C.