DAFI91-202_AETCSUP governs safety release documentation and launch vehicle space debris assessment reporting requirements.
View DAFI91-202_AETCSUP on armypubs.army.mil
The publication specifies content for system descriptions, ESOH hazard discussions, risk levels, testing conclusions, limitations, and safety notifications. It also establishes SDAR delivery schedules, review requirements, document formats, and launch vehicle debris 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)
Preliminary Design Review (PDR) draft SDAR: 30 days prior to the program or project PDR 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 (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)
Note: SDARs are not required for suborbital missions. (paragraph 1)