درباره ما
MIL-R-85363
ROCKET MOTOR, MARK 23 MODS 2 AND 3
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:19:16Z | |
| date available | 2017-09-04T18:19:16Z | |
| date copyright | 02/09/1981 | |
| date issued | 1981 | |
| identifier other | HTQPDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9FCD/handle/yse/201976 | |
| description abstract | This specification establishes the minimum requirements for the manufacture, test, and acceptance of Rocket Motor Mark 23 Mods 2 and 3 (see 6.1). Intended Use: The Rocket Motor is designed for use primarily as a high thrust, short duration power plant to impart initial acceleration to various types of drones and test sleds. | |
| language | English | |
| title | MIL-R-85363 | num |
| title | ROCKET MOTOR, MARK 23 MODS 2 AND 3 | en |
| type | standard | |
| page | 14 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1981 | |
| contenttype | fulltext |
