| タイトル | Thrust vectoring systems |
| 本文（外部サイト） | http://hdl.handle.net/2060/19730009089 |
| 著者（英） | Dulgeroff, C.; Vahrenkamp, R.; Schnelker, D.; Ward, J. W.; King, H. J. |
| 著者所属（英） | Hughes Research Labs. |
| 発行日 | 1972-12-01 |
| 言語 | eng |
| 内容記述 | The design, fabrication, and testing of thrust vectorable ion optical systems capable of controlling the thrust direction from both 5- and 30-cm diameter ion thrusters is described. Both systems are capable of greater than 10 deg thrust deflection in any azimuthal direction. The 5-cm system is electrostatic and hence has a short response time and minimal power consumption. It has recently been tested for more than 7500 hours on an operational thruster. The 30-cm system is mechanical, has a response time of the order of 1 min, and consumes less than 0.3% of the total system input power at full deflection angle. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 73N17816
NASA-CR-121142 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/200547 |
|
