| タイトル | Satellite/spacecraft propulsion |
| 本文（外部サイト） | http://hdl.handle.net/2060/19910018889 |
| 著者（英） | Dowdy, Mack W. |
| 著者所属（英） | Jet Propulsion Lab., California Inst. of Tech. |
| 発行日 | 1991-05-01 |
| 言語 | eng |
| 内容記述 | Propulsion system performance has high leverage for many future missions because of large propellant mass requirements. Relatively small performance improvements can translate into large increases in payload and science return. Contamination control becomes more important as science instruments become more sensitive. This places more emphasis on exhaust plume contamination control. The need for reliable operation and long life places increased importance on health monitoring and control of spacecraft propulsion systems. The need for accurate spacecraft pointing and control increases the need for small impulse-bit thrusters. This presentation is represented by viewgraphs. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 91N28203 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/131466 |
