درباره ما
MIL-PRF-7254G
PROPELLANT, NITRIC ACID
| contributor author | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering) | |
| date accessioned | 2017-09-04T18:48:33Z | |
| date available | 2017-09-04T18:48:33Z | |
| date copyright | 35779 | |
| date issued | 1997 | |
| identifier other | KPHBEAAAAAAAAAAA.pdf | |
| identifier uri | https://yse.yabesh.ir/std/handle/yse/229854 | |
| description abstract | This specification covers the requirements for four types of nitric acid propellant. The nitric acid will be of the following types as specified (6.2): The types of nitric acid are as follows: Type IIIA - Nominal 14 percent NO2 content plus corrosion inhibitor Type IIIB - Nominal 14 percent NO2 content, lower solids content, plus corrosion inhibitor Type IIILS - Limited storage propellant with nominal 14 percent NO2 content, lower solids content, plus corrosion inhibitor, and limited iron content Type IV - High density propellant with nominal 44 percent NO2 content, lower solids content, plus corrosion inhibitor, and limited iron content Intended Use: The propellants covered by this specification are intended for use as oxidizers in rocket engines. Type IIILS is intended for special purposes and will not be used for applications where storage life is a criterion because of its tendency to change composition. | |
| language | English | |
| title | MIL-PRF-7254G | num |
| title | PROPELLANT, NITRIC ACID | en |
| type | standard | |
| page | 17 | |
| status | Active | |
| tree | AIR FORCE - 05 - SAF/AQR Deputy Assistant Secretary (Science, Technology and Engineering):;1997 | |
| contenttype | fulltext | |
| subject keywords | Hydrofluoric acid | |
| subject keywords | IRFNA | |
| subject keywords | Missile propellant | |
| subject keywords | Nitric acid | |
| subject keywords | Nitrogen dioxide | |
| subject keywords | Oxidizer | |
| subject keywords | Rocket engines |
