درباره ما
MIL-PRF-25508H
PROPELLANT, OXYGEN
| contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
| date accessioned | 2017-09-04T18:38:40Z | |
| date available | 2017-09-04T18:38:40Z | |
| date copyright | 40843 | |
| date issued | 2011 | |
| identifier other | JQGFOEAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/220400 | |
| description abstract | This specification covers the requirements for three grades and two types of oxygen.Intended Use: The propellant covered by this specification is intended for use as follows.a. Grade A, type I – Purging and pressurization of propellant systems and rocket engines.b. Grade A, type II – Oxidizer.c. Grade B, type II - Oxidizer.d. Grade F, types I and II – Fuel cell grade that may be used for crew breathing in subsystems utilizing a common storage for both functions. | |
| language | English | |
| title | MIL-PRF-25508H | num |
| title | PROPELLANT, OXYGEN | en |
| type | standard | |
| page | 10 | |
| status | Active | |
| tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;2011 | |
| contenttype | fulltext | |
| subject keywords | Aerospace | |
| subject keywords | Breathing | |
| subject keywords | Cryogenic | |
| subject keywords | Cylinders | |
| subject keywords | Fuel cell | |
| subject keywords | Space vehicle |
