درباره ما
MIL-P-85364A
PROPELLANT, CTBN 23-17
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T18:18:32Z | |
| date available | 2017-09-04T18:18:32Z | |
| date copyright | 09/23/1993 | |
| date issued | 1993 | |
| identifier other | HRWXDAAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho1826AF679D40AC426159DD6E273C9FCD/handle/yse/201323 | |
| description abstract | This specification covers the minimum requirements for one type of solid propellant grain (see 6.1). Intended Use: The propellant described herein is intended for use in the Mk 23 Mods 2 and 3 Rocket Motor. | |
| language | English | |
| title | MIL-P-85364A | num |
| title | PROPELLANT, CTBN 23-17 | en |
| type | standard | |
| page | 7 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1993 | |
| contenttype | fulltext | |
| subject keywords | MK 23 Mod 2 Jato | |
| subject keywords | MK 23 Mod 3 Jato |
