| タイトル | Conceptual spacecraft and arcjet propulsion system design for the SP-100 interim reference mission |
| 著者（英） | Bell, M. W. J.; Zafran, S. |
| 著者所属（英） | TRW, Inc. |
| 発行日 | 1990-07-01 |
| 言語 | eng |
| 内容記述 | An arcjet propulsion system, delivering 7.5 N thrust, was defined for the SP-100 Space Reactor Power System Interim Reference Mission. Conceptual design trades and configuration studies of a spacecraft suitable for the mission were performed to the extent necessary to define propulsion system requirements and interfaces. The propulsion system design is based on the use of 30-kW, constricted arc, ammonia arcjet engines operating in parallel during orbit boost from low earth to geosynchronous orbit. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 90A42542
AIAA PAPER 90-2549 |
| 権利 | Copyright |
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