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MIL-PRF-26536F
PROPELLANT, HYDRAZINE
| contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
| date accessioned | 2017-09-04T18:47:33Z | |
| date available | 2017-09-04T18:47:33Z | |
| date copyright | 04/01/2011 | |
| date issued | 2011 | |
| identifier other | KMFNGEAAAAAAAAAA.pdf | |
| identifier uri | http://yse.yabesh.ir/std;query=autho162/handle/yse/228709 | |
| description abstract | This specification covers the requirements for three grades of hydrazine (N2H4).Intended Use: The propellant described by this specification is intended for use as a fuel in rocket engines. | |
| language | English | |
| title | MIL-PRF-26536F | num |
| title | PROPELLANT, HYDRAZINE | en |
| type | standard | |
| page | 36 | |
| status | Active | |
| tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2011 | |
| contenttype | fulltext | |
| subject keywords | Catalytic Engine | |
| subject keywords | Fuel | |
| subject keywords | Monopropellant | |
| subject keywords | Rocket Engine |
