MIL-DTL-32127A
CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5C/A ASSEMBLY
| contributor author | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD) | |
| date accessioned | 2017-09-04T16:51:47Z | |
| date available | 2017-09-04T16:51:47Z | |
| date copyright | 08/03/2005 | |
| date issued | 2005 | |
| identifier other | WRPIIBAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;jsessioutho462sear3FCDCAC4/handle/yse/115410 | |
| description abstract | This specification covers the requirements for the Rocket Catapult CKU-5C/A loaded assembly. Intended Use: The CKU-5C/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. The CKU-5C/A Aircraft Ejection Seat Catapult Assembly was designed for use in a military aircraft and has no commercial application. | |
| language | English | |
| title | MIL-DTL-32127A | num |
| title | CATAPULT, AIRCRAFT EJECTION SEAT, CKU-5C/A ASSEMBLY | en |
| type | standard | |
| page | 19 | |
| status | Active | |
| tree | NAVY - OS - Naval Surface Warfare Center (NSWCIHEODTD):;2005 | |
| contenttype | fulltext | |
| subject keywords | Rocket catapult | |
| subject keywords | Rocket motor |

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