درباره ما
MIL-PRF-26539F
PROPELLANTS, DINITROGEN TETROXIDE
| contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
| date accessioned | 2017-09-04T16:19:06Z | |
| date available | 2017-09-04T16:19:06Z | |
| date copyright | 04/17/2006 | |
| date issued | 2006 | |
| identifier other | THDBJBAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/82505 | |
| description abstract | This specification covers the requirements for all types of dinitrogen tetroxide (N2O4) propellants.Intended Use: The propellant described by this specification is intended for use as an oxidizer in rocket engines. | |
| language | English | |
| title | MIL-PRF-26539F | num |
| title | PROPELLANTS, DINITROGEN TETROXIDE | en |
| type | standard | |
| page | 25 | |
| status | Active | |
| tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2006 | |
| contenttype | fulltext | |
| subject keywords | Dinitrogen tetroxide | |
| subject keywords | Nitric oxide | |
| subject keywords | Oxidizer | |
| subject keywords | Propellant | |
| subject keywords | Rocket engine |
