| タイトル | Transfer trajectory design for a shuttle launched geosynchronous payload |
| 本文（外部サイト） | http://hdl.handle.net/2060/19790017926 |
| 著者（英） | Defazio, R. L. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1979-04-01 |
| 言語 | eng |
| 内容記述 | The firing of a fixed impulse spin stabilized upper stage following shuttle deployment of a geosynchronous payload was examined in detail. Design of the transfer trajectory was discussed in terms of finding both a nominal and possible dispersion case that can be handled operationally within the allotted trim fuel budget. |
| NASA分類 | ASTRODYNAMICS |
| レポートNO | 79N26097 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/569092 |
