| タイトル | Technology requirements for future Earth-to-geosynchronous orbit transportation systems. Volume 3: Appendices |
| 本文（外部サイト） | http://hdl.handle.net/2060/19800011820 |
| 著者（英） | Caluori, V. A.; Jenkins, J. C.; Conrad, R. T. |
| 著者所属（英） | Boeing Aerospace Co. |
| 発行日 | 1980-03-01 |
| 言語 | eng |
| 内容記述 | Technological requirements and forecasts of rocket engine parameters and launch vehicles for future Earth to geosynchronous orbit transportation systems are presented. The parametric performance, weight, and envelope data for the LOX/CH4, fuel cooled, staged combustion cycle and the hydrogen cooled, expander bleed cycle engine concepts are discussed. The costing methodology and ground rules used to develop the engine study are summarized. The weight estimating methodology for winged launched vehicles is described and summary data, used to evaluate and compare weight data for dedicated and integrated O2/H2 subsystems for the SSTO, HLLV and POTV are presented. Detail weights, comparisons, and weight scaling equations are provided. |
| NASA分類 | SPACE TRANSPORTATION |
| レポートNO | 80N20303
NASA-CR-159174 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/173007 |
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