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MIL-DTL-85097/1B
AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET CATAPULT MARK 16 MOD 1 (LOADED ASSEMBLY)
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T17:36:53Z | |
| date available | 2017-09-04T17:36:53Z | |
| date copyright | 07/27/1998 | |
| date issued | 1998 | |
| identifier other | DLSBEAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsery=autho162sear79D40527/handle/yse/159776 | |
| description abstract | This specification sheet covers the requirements unique to the Mk 16 Mod 1 Rocket Catapult, Loaded Assembly (see 6.1). Intended Use: The Mk 16 Mod 1 Rocket Catapult is used to eject the pilot from the TA-4J, S-3B, and ES-3A aircraft. As the A-4E/L aircraft is a military aircraft, there is no commercial application for the MK 16 Mod 1 Rocket Catapult. | |
| language | English | |
| title | MIL-DTL-85097/1B | num |
| title | AIRCREW ESCAPE PROPULSION SYSTEMS (AEPS) ROCKET CATAPULT MARK 16 MOD 1 (LOADED ASSEMBLY) | en |
| type | standard | |
| page | 7 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1998 | |
| contenttype | fulltext |
