AFI91-202_AFOTECSUP governs safety releases for systems under test, including hazard assessment, risk acceptance, and safety limitations.
View AFI91-202_AFOTECSUP on armypubs.army.mil
It covers system descriptions, environmental, safety, and occupational health hazards, testing safety conclusions, anomalies, and points of contact. It also establishes delivery, review, approval, and content requirements for Launch Vehicle Space Debris Assessment Reports, including orbital debris mitigation compliance.
Any orbital debris mitigation compliance issues not resolved by the PDR require resolution no later than the Critical Design Review (CDR) or equivalent program/project development milestone. (paragraph 1)
Preliminary Design Review (PDR) draft SDAR: 30 days prior to the program or project PDR or equivalent program/project development milestone. (paragraph 1)
The PM will submit the Final Launch Vehicle (LV) SDAR 30 days prior to the launch approval process (Air Force Operational Readiness Review, Flight Readiness Review or equivalent) for approval and signature by the appropriate acquisition authorities (PEO or equivalent, or designated approving official). (paragraph 1)
Prior to final SDAR approval, the Center (or equivalent) technical and safety subject matter expert will independently review the final pre-launch SDAR. (paragraph 1)
Note: SDARs are not required for suborbital missions. (paragraph 1)