| タイトル | Power, thermal, and attitude control design interactions of the CCE/AMPTE spacecraft |
| 著者（英） | Smola, J. F.; Allen, W. E.; Ray, J. C.; Wingate, C. A., Jr. |
| 著者所属（英） | Johns Hopkins Univ. |
| 発行日 | 1982-09-01 |
| 言語 | eng |
| 内容記述 | The power, thermal and attitude control interactions of the CCE spacecraft and the design compromises resulting from these interactions are described. These compromises result from the conflict between the plane change maneuver requirements and the final on station requirements. The resolution of these conflicts to arrive at an acceptable final design, is given and the resulting power, thermal and attitude control systems are described in some detail. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 82A46986
IAF PAPER 82-200 |
| 権利 | Copyright |
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