درباره ما
MIL-DTL-82876A
CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5B/A ASSEMBLY
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T17:44:50Z | |
| date available | 2017-09-04T17:44:50Z | |
| date copyright | 08/04/1995 | |
| date issued | 1995 | |
| identifier other | EHDZDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho47037D83081DAC4261598F1EFDEC014A/handle/yse/167867 | |
| description abstract | This specification covers the requirements for the Rocket Catapult CKU-5B/A loaded assembly. Intended Use: The CKU-5B/A Aircraft Ejection Seat Catapult Assembly is intended to be used to propel an aircraft ejection seat and its occupant safely out and away from a jet aircraft. | |
| language | English | |
| title | MIL-DTL-82876A | num |
| title | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5B/A ASSEMBLY | en |
| type | standard | |
| page | 19 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;1995 | |
| contenttype | fulltext | |
| subject keywords | Rocket catapult | |
| subject keywords | Rocket motor |
