درباره ما
MIL-P-85759
PROPELLANT GRAIN, MARK 93 MOD 0
| contributor author | NAVY - AS - Naval Air Systems Command | |
| date accessioned | 2017-09-04T17:26:35Z | |
| date available | 2017-09-04T17:26:35Z | |
| date copyright | 08/01/1986 | |
| date issued | 1986 | |
| identifier other | CKRPDAAAAAAAAAAA.pdf | |
| identifier uri | http://mapnamagz.yabesh.ir/std;query=authoF23793FDFCDCAC4/handle/yse/149712 | |
| description abstract | This specification covers the requirements for the manufacture and acceptance of the Mark 93 Mod 0 Propellant Grain (see 6.1). Propellant grain, as used herein, refers to an extruded hollow cylinder of propellant with an ethyl cellulose inhibitor disc cemented to one end. Intended Use: The propellant grain described herein is intended for use in the Rocket Motor Mk 117 Mod 0. | |
| language | English | |
| title | MIL-P-85759 | num |
| title | PROPELLANT GRAIN, MARK 93 MOD 0 | en |
| type | standard | |
| page | 6 | |
| status | Active | |
| tree | NAVY - AS - Naval Air Systems Command:;1986 | |
| contenttype | fulltext | |
| subject keywords | Igniter | |
| subject keywords | Ignition delay | |
| subject keywords | Propellant grain | |
| subject keywords | MK 93 | |
| subject keywords | Rocket motor |
