| タイトル | Orbit Transfer Vehicle (OTV) engine, phase A study. Volume 2: Study |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790025065 |
| 著者（英） | Mellish, J. A. |
| 著者所属（英） | Aerojet Liquid Rocket Co. |
| 発行日 | 1979-06-29 |
| 言語 | eng |
| 内容記述 | The hydrogen oxygen engine used in the orbiter transfer vehicle is described. The engine design is analyzed and minimum engine performance and man rating requirements are discussed. Reliability and safety analysis test results are presented and payload, risk and cost, and engine installation parameters are defined. Engine tests were performed including performance analysis, structural analysis, thermal analysis, turbomachinery analysis, controls analysis, and cycle analysis. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 79N33236
NASA-CR-161298
REPT-32999-F-VOL-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/174476 |
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