AFI91-202_AFSOCSUP governs safety release documentation and launch vehicle space debris assessment requirements for Air Force programs.
View AFI91-202_AFSOCSUP on armypubs.army.mil
It specifies system descriptions, ESOH hazard discussions, risk acceptance information, testing safety conclusions, and notification of safety-related anomalies. It also establishes delivery schedules, reviews, approvals, formats, and content for launch vehicle SDARs, including orbital debris and breakup assessments.
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)
SDARs are not required for suborbital missions. (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)
Each launch vehicle SDAR will follow the format shown in Table 13.4 below and, at a minimum, include the content indicated. (paragraph 1)
The document history page shows each version of the report. This page will include reviews of the previous versions by the Chief Engineer or Safety Office. (paragraph 1)