| タイトル | Nuclear electric propulsion system utilization for earth orbit transfer of large spacecraft structures |
| 著者（英） | Byers, D. C.; Silva, T. H. |
| 著者所属（英） | NASA Lewis Research Center|Aerospace Corp. |
| 発行日 | 1980-06-01 |
| 言語 | eng |
| 内容記述 | The paper discusses a potential application of electric propulsion to perform orbit transfer of a large spacecraft structure to geosynchronous orbit (GEO) from LEO, utilizing a nuclear reactor space power source in the spacecraft on a shared basis. The discussions include spacecraft, thrust system, and nuclear reactor space power system concepts. Emphasis is placed on orbiter payload arrangements, spacecraft launch constraints, and spacecraft LEO assembly and deployment sequences. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 80A38975
AIAA PAPER 80-1223 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/421420 |
