MIL-DTL-85097/15A
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
Organization:
NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD)
Year: 2005
Abstract: This specification sheet covers requirements unique to the Mark 121 Mod 0 Rocket Motor (see 6.1). Intended Use: The rocket motor is intended to insure proper trajectory divergence of the aircrew during an escape for the TAV-8B Aircraft Escape System. The rocket motor was designed specifically for use with the TAV-8B Aircraft Escape System in a military aircraft, and has no commercial applications.
Subject: N-47
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MIL-DTL-85097/15A
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contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
date accessioned | 2017-09-04T15:04:05Z | |
date available | 2017-09-04T15:04:05Z | |
date copyright | 38684 | |
date issued | 2005 | |
identifier other | AODTIBAAAAAAAAAA.pdf | |
identifier uri | http://yse.yabesh.ir/std/handle/yse/1424 | |
description abstract | This specification sheet covers requirements unique to the Mark 121 Mod 0 Rocket Motor (see 6.1). Intended Use: The rocket motor is intended to insure proper trajectory divergence of the aircrew during an escape for the TAV-8B Aircraft Escape System. The rocket motor was designed specifically for use with the TAV-8B Aircraft Escape System in a military aircraft, and has no commercial applications. | |
language | English | |
title | MIL-DTL-85097/15A | num |
title | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0 | en |
type | standard | |
page | 5 | |
status | Active | |
tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;2005 | |
contenttype | fulltext | |
subject keywords | N-47 | |
subject keywords | TAV-8B |