MIL-P-83126A, MILITARY SPECIFICATION: PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR (08 FEB 1980) [SUPERSEDING MIL-A-85041A]

MIL-P-83126A, MILITARY SPECIFICATION: PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR (08 FEB 1980) [SUPERSEDING MIL-A-85041A]., This specification establishes the minimum requirements for the design, development/adaptation, design verification, and service release criteria for Aircrew Escape Propulsion Systems (AEPS) and testing of units manufactured for Aircrew Escape Systems (AES) system and subsystem tests