DAFI91-202 governs safety release documentation, system safety assessments, testing safety, and launch vehicle space debris assessment reports.
View DAFI91-202 on armypubs.army.mil
DAFI91-202 specifies information for system descriptions, ESOH hazard discussions, testing conclusions, risk acceptance, and safety-related anomalies. It also establishes delivery schedules and minimum formats for launch vehicle space debris assessment reports, including mission, spacecraft, launch vehicle, and debris data.
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)
Note: SDARs are not required for suborbital missions. (paragraph 1)
Each LV SDAR will follow the format shown in Table 13.4 below, and, at a minimum, include the content indicated. (paragraph 1)