| タイトル | Dual deflectable beam strip engine development. |
| 著者（英） | Kami, S.; Ward, J. W.; Zuccaro, D. E.; Dulgeroff, C. R.; Schnelker, D. E. |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | This paper describes a dual beam thruster that has been designed, constructed, and tested. The system is suitable for two-axes attitude control and is comprised of two orthogonal strips, each capable of producing 0.30 mlb thrust and beam deflections of more than plus or minus 20 deg. The nominal specific impulse for the thruster is 5000 sec, and the thrust level from each strip can be varied from 0 to 100%. Neutralizer filaments that were developed and life tested over 2000 hours producing more than 40 mA of electron emission per watt of input power are also discussed. The system power required for clean ionizers is approximately 200 W. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72A28951
AIAA PAPER 72-494 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/462247 |
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