MIL-DTL-85097/14D
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET CATAPULT MARK 1 MOD 1 (LOADED ASSEMBLY)
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T15:25:11Z | |
| date available | 2017-09-04T15:25:11Z | |
| date copyright | 06/12/1997 | |
| date issued | 1997 | |
| identifier other | NKQAEAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/25715 | |
| description abstract | This specification sheet covers the requirements unique to the Mk 1 Mod 1 Rocket Catapult, Loaded Assembly (see 6.1). Intended Use: The Mk 1 Mod 1 Rocket Catapult is used to eject the pilot from the A-4E/L aircraft. | |
| language | English | |
| title | MIL-DTL-85097/14D | num |
| title | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET CATAPULT MARK 1 MOD 1 (LOADED ASSEMBLY) | en |
| type | standard | |
| page | 5 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1997 | |
| contenttype | fulltext |

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