AFI91-202_SSCSUP governs safety release documentation for systems under test and launch vehicle space debris assessment reports.
View AFI91-202_SSCSUP on armypubs.army.mil
It addresses system descriptions, ESOH hazards, risk levels, testing safety, anomalies, and required safety release coordination. It also requires scheduled SDAR submissions, reviews, approvals, and specified report content for launch vehicles.
Preliminary Design Review (PDR) draft SDAR: 30 days prior to the program or project PDR or equivalent program/project development milestone. (paragraph 1)
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)
CDR Draft SDAR: 45 days prior to the program or project CDR or equivalent program/project development milestone. (paragraph 1)
The PM will submit the Final Launch Vehicle 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 (Center Commander or equivalent, or designated approving official). (paragraph 1)
Prior to final SDAR approval the Center (or equivalent) technical and/or safety subject matter expert will independently review the final launch vehicle SDAR. (paragraph 1)