タイトル | In-Space Transportation for GEO Space Solar Power Satellites |
本文(外部サイト) | http://hdl.handle.net/2060/20000034130 |
著者(英) | Donnahue, Benjamin B.; Henley, Mark W.; Martin, James A. |
著者所属(英) | Boeing Co. |
発行日 | 1999-12-22 |
言語 | eng |
内容記述 | This report summarizes results of study tasks to evaluate design options for in-space transportation of geostationary Space Solar Power Satellites. Referring to the end-to-end architecture studies performed in 1988, this current activity focuses on transportation of Sun Tower satellite segments from an initial low Earth orbit altitude to a final position in geostationary orbit (GEO; i.e., 35,786 km altitude, circular, equatorial orbit). This report encompasses study activity for In-Space Transportation of GEO Space Solar Power (SSP) Satellites including: 1) assessment of requirements, 2) design of system concepts, 3) comparison of alternative system options, and 4) assessment of potential derivatives. |
NASA分類 | Space Transportation and Safety |
レポートNO | NASA/CR-2000-210136 NAS 1.26:210136 |
権利 | No Copyright |
URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/227285 |
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