DAFI91-202_ACCSUP — The Department Of The Air Force (daf) Mishap Prevention Program

DAFI91-202_ACCSUP governs safety release content and launch vehicle space debris assessment report delivery and format requirements.

Search DAFI91-202_ACCSUP

  • Publication number: DAFI91-202_ACCSUP
  • Title: THE DEPARTMENT OF THE AIR FORCE (DAF) MISHAP PREVENTION PROGRAM
  • Date: 2025-12-03

View DAFI91-202_ACCSUP on armypubs.army.mil

It covers system descriptions, ESOH hazards, testing safety conclusions, orbital debris mitigation, and launch vehicle assessments. It requires specified reviews, approvals, notifications, report content, and delivery schedules.

Topics covered

  • Safety release content
  • ESOH hazards
  • Testing safety conclusions
  • Orbital debris mitigation
  • Launch vehicle SDARs
  • Spacecraft descriptions
  • Launch vehicle debris
  • Orbital stage explosions

Questions and answers

When must unresolved orbital debris mitigation issues be resolved?

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)

Who receives the preliminary design review draft SDAR?

The program manager (PM) receives the draft document and distributes it to the Chief Engineer and Safety Office and other offices as required. (paragraph 1)

When is the final Launch Vehicle SDAR due?

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)

Who independently reviews the final pre-launch SDAR?

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)

Are SDARs required for suborbital missions?

Note: SDARs are not required for suborbital missions. (paragraph 1)

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