| タイトル | Dynamical in-orbit behavior of the Radio Astronomy Explorer satellite |
| 本文（外部サイト） | http://hdl.handle.net/2060/19720018109 |
| 著者（英） | Walden, H. |
| 著者所属（英） | NASA Goddard Space Flight Center |
| 発行日 | 1972-01-01 |
| 言語 | eng |
| 内容記述 | Onboard sensors and associated ground based processing systems are used to maintain a well stabilized attitude for the RAE 1 in its near circular earth orbit despite the satellite's four extremely long and flexible antenna booms. Boom tip deflection pictures and central hub orientation measurements show that large boom vibrations and major attitude stability problems anticipated prior to launch have not materialized. |
| NASA分類 | SPACE VEHICLES |
| レポートNO | 72N25759 |
| 権利 | No Copyright |
