درباره ما
MIL-L-23822C
LIQUID PROPELLANT ROCKET ENGINE LR64 FOR AQM-37A MISSILE TARGET SYSTEM
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T17:09:36Z | |
| date available | 2017-09-04T17:09:36Z | |
| date copyright | 04/30/1971 | |
| date issued | 1971 | |
| identifier other | YNOLDAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/133170 | |
| description abstract | This specification establishes the requirements for the performance, manufacture, testing, acceptance and packaging of the Liquid Propellant Rocket Engine LR64. Intended Use: The Liquid Propellant Rocket Engine LR64 covered by this specification is intended for use in the AQM37A missile target. | |
| language | English | |
| title | MIL-L-23822C | num |
| title | LIQUID PROPELLANT ROCKET ENGINE LR64 FOR AQM-37A MISSILE TARGET SYSTEM | en |
| type | standard | |
| page | 29 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1971 | |
| contenttype | fulltext |
