Document ID:	MIL-P-83126       Scroll down to access document images

Overview

Title:  PROPULSION SYSTEMS, AIRCREW ESCAPE, DESIGN SPECIFICATION FOR Scope:  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. Status:  Active Document Date:  08-FEB-1980         Next Review Due:  06-FEB-1985 FSC/Area:  1377 Doc Category:   Detail Specification

Responsibilities

Lead Standardization Activity:  OS  Naval Surface Warfare Center Indian Head Division (NSWC IHD)     Preparing Activity: OS  Naval Surface Warfare Center Indian Head Division (NSWC IHD) Coordination:  Full   Army Custodian:  AR   US Army Combat Capabilities Development Command, Armaments Center   Navy Custodian:  OS   Naval Surface Warfare Center Indian Head Division (NSWC IHD)   Air Force Custodian:  11   Air Force Life Cycle Management Center - Aircraft Systems

Amendments to military specifications or specification sheets issued after August 1, 2003 are incorporated in the modified document.

Revision History

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