درباره ما
MIL-PRF-25604E
PROPELLANT, UNS-DIMETHYLHYDRAZINE
| contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
| date accessioned | 2017-09-04T15:14:21Z | |
| date available | 2017-09-04T15:14:21Z | |
| date copyright | 35704 | |
| date issued | 1997 | |
| identifier other | MCZAEAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/13148 | |
| description abstract | This specification covers the requirements for unsymmetrical dimethylhydrazine (CH3)2NNH2 propellant (UDMH). Intended Use: The propellant described by this specification is intended for use as an fuel in rocket engines. | |
| language | English | |
| title | MIL-PRF-25604E | num |
| title | PROPELLANT, UNS-DIMETHYLHYDRAZINE | en |
| type | standard | |
| page | 10 | |
| status | Active | |
| tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;1997 | |
| contenttype | fulltext | |
| subject keywords | Fuel | |
| subject keywords | N-Nitrosodimethylamine | |
| subject keywords | Propellant | |
| subject keywords | Rocket engine | |
| subject keywords | uns-Dimethylhydrazine |
