| タイトル | Enriched Storable Oxidizers for Rocket Engines |
| 本文（外部サイト） | http://hdl.handle.net/2060/20100019583 |
| 著者（英） | Sackheim, R. L.; Herdy, J. R., Jr. |
| 著者所属（英） | NASA Marshall Space Flight Center |
| 発行日 | 2010-05-01 |
| 言語 | eng |
| 内容記述 | The name "enriched storable oxidizers" (ESOs) has been coined for a family of optimized mixtures of between two and four oxidizer fluids. For most applications, the constituents of these mixtures would be nitrogen tetroxide (N2O4), nitrous oxide (N2O), and nitrogen dioxide (NO2); in some applications, the mixtures might include inhibited red fuming nitric acid [IRFN (which consists of red fuming nitric acid to which some hydrogen fluoride is added to reduce its corrosive effect]. The optimum proportions of these constituents would be different for different applications. ESOs were originally proposed for use in spacecraft and launch-rocket propulsion systems: ESOs could be especially useful in advanced spacecraft propulsion systems that could operate in multiple modes. ESOs might also be useful in special terrestrial applications that could include ramjet and scramjet aircraft engines. |
| NASA分類 | Man/System Technology and Life Support |
| レポートNO | MFS-32407-1 |
| 権利 | Copyright, Distribution as joint owner in the copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/507138 |
