درباره ما
MIL-DTL-85097/15A
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS); ROCKET MOTOR, MARK 121 MOD 0
| 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 | https://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 |
