| タイトル | Lunar surface base propulsion system study. Volume 2: Lunar propellant manual |
| 本文（外部サイト） | http://hdl.handle.net/2060/19870012623 |
| 著者（英） | Teeter, Ronald R. |
| 著者所属（英） | Astronautics Corp. of America |
| 発行日 | 1987-02-01 |
| 言語 | eng |
| 内容記述 | The efficiency, capability, and evolution of a lunar base will be largely dependent on the transportation system that supports it. Beyond the space station in low Earth orbit, a lunar-derived propellant supply could provide the most important resource for the transportation infrastructure. The key to an efficient lunar base propulsion system is the degree of lunar self-sufficiency and reasonable propulsion system performance. Lunar surface propellant production requirements must be accounted in the measurement of efficiency of the entire space transportation system. Of all chemical propellant/propulsion systems considered, hydrogen/oxygen (H/O) OTVs appear most desirable, while both H/O and aluminum/oxygen propulsion systems may be considered for the lander. Aluminized-hydrogen/oxygen and silane/oxygen propulsion systems are also promising candidates. Lunar propellant availability and processing techniques, chemical propulsion/vehicle design characteristics, and the associated performance of the total transportation infrastructure are reviewed, conceptual propulsion system designs and vehicle/basing concepts, and technology requirements are assessed. |
| NASA分類 | PROPELLANTS AND FUELS |
| レポートNO | 87N22056
NAS 1.26:171982-Vol-2
NASA-CR-171982-Vol-2 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/150917 |
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