| タイトル | Cannon launched electromechanical control actuation system development |
| 本文（外部サイト） | http://hdl.handle.net/2060/19830016622 |
| 著者（英） | Johnston, J. G. |
| 著者所属（英） | Martin Marietta Aerospace |
| 発行日 | 1983-05-01 |
| 言語 | eng |
| 内容記述 | The evolution of an electromechanical control actuation system from trade study results through breadboard test and high-g launch demonstration tests is summarized. Primary emphasis is on design, development, integration and test of the gear reduction system. |
| NASA分類 | STRUCTURAL MECHANICS |
| レポートNO | 83N24893 |
| 権利 | No Copyright |
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