MIL-A-85097/16

AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, PARACHUTE DEPLOYMENT, MARK 122 MOD 0

contributor author	NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD)
date accessioned	2017-09-04T17:17:57Z
date available	2017-09-04T17:17:57Z
date copyright	34673
date issued	1994
identifier other	ZJPMIAAAAAAAAAAA.pdf
identifier uri	http://yse.yabesh.ir/std;query=autho162sear3FCDC52731854DD6EFDEC014A/handle/yse/141291
description abstract	This document covers the requirements for the Mark 122 Mod 0 Parachute Deployment Rocket Motor (PDRM) (see 6.1). Intended Use: The rocket motor described herein is intended for use with SJU-17(V) Navy Aircrew Common Ejection Seat (NACES) as a means of deploying the personal parachute. It is used in the T-45A, F/A-18C/D, and F-14D aircraft. The Mark 122 Mod 0 Parachute Deployment Rocket Motor (PDRM) extracts the personal parachute from the parachute pack and enables the parachute to deploy and develop rapidly without becoming entangled with the seat. The PDRM is a sealed unit consisting of two main parts; (a) a breech at its lower end containing an electrically initiated primary cartridge and a gas-operated secondary cartridge, and (b) a rocket section with an integral gas-operated igniter cartridge.
language	English
title	MIL-A-85097/16	num
title	AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET MOTOR, PARACHUTE DEPLOYMENT, MARK 122 MOD 0	en
type	standard
page	6
status	Active
tree	NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1994
contenttype	fulltext