| タイトル | Electromechanical flight control actuator |
| 本文（外部サイト） | http://hdl.handle.net/2060/19760015172 |
| 著者所属（英） | Delco Electronics |
| 発行日 | 1976-02-01 |
| 言語 | eng |
| 内容記述 | An electromechanical actuator that will follow a proportional control command with minimum wasted energy is developed. The feasibility of meeting space vehicle actuator requirements using advanced electromechanical concepts is demonstrated. Recommendations for further development are given. |
| NASA分類 | SPACECRAFT DESIGN, TESTING AND PERFORMANCE |
| レポートNO | 76N22260
NASA-CR-147557
R76-29 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/186166 |
