درباره ما
MIL-R-23452A
ROCKET MOTOR, MARK 25 MODS 0, 1, 2 AND 3
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:19:11Z | |
| date available | 2017-09-04T18:19:11Z | |
| date copyright | 07/19/1982 | |
| date issued | 1982 | |
| identifier other | HTMLDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162sear3FCDCAC426159DD6E273C9FCD/handle/yse/201904 | |
| description abstract | This specification establishes the requirements for the Rocket Motor Mark 25 Mods 0, 1, and 2 (see 6.1). The Rocket Motor Mark 25 will consist of the following Mods: Mod 0 - 30° Canted nozzle Mod 1 - 15° Canted nozzle Mod 2 - 0° Canted nozzle Intended Use: The solid rocket propellant motor covered by this specification is intended for jet assisted takeoff use on piloted aircraft. | |
| language | English | |
| title | MIL-R-23452A | num |
| title | ROCKET MOTOR, MARK 25 MODS 0, 1, 2 AND 3 | en |
| type | standard | |
| page | 12 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1982 | |
| contenttype | fulltext |
