| タイトル | Advanced helium regulator for a fluorine propellant system |
| 著者（英） | Wichmann, H.; Yankura, G. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech.|Marquardt Corp. |
| 発行日 | 1976-07-01 |
| 言語 | eng |
| 内容記述 | The space storable propulsion module is an advanced high performance (375 seconds Isp minimum) planetary spacecraft propulsion system with a mission life of 5-10 years. The propellants used are liquid fluorine and amine fuel. This application requires high pressure regulator accuracy to optimize propellant depletion characteristics. An advanced regulator concept was prepared which is compatible with both fuel and oxidizer and which features design concepts such as redundant bellows, all-metallic/ceramic construction, friction-free guidance of moving parts and gas damping. Computer simulation of the propulsion module performance over two mission profiles indicated satisfactory minimization of those propellant residual requirements imposed by regulator performance variables. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 76A38155
AIAA PAPER 76-599 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/442558 |
