| タイトル | End-hall thrusters |
| 著者（英） | Kaufman, H. R.; Day, M. L.; Robinson, R. S.; Haag, T. W. |
| 著者所属（英） | Commonwealth Scientific Corp.; Front Range Research; NASA Lewis Research Center; Ford Aerospace Corp.; Colorado State Univ. |
| 発行日 | 1990-07-01 |
| 言語 | eng |
| 内容記述 | The end-Hall thruster can provide electric propulsion with fixed masses, specific impulses, and power-to-thrust ratios intermediate of an arcjet and a gridded (electrostatic) ion thruster. With these characteristics, this thruster is a candidate for missions of intermediate difficulty, such as the north-south stationkeeping of geostationary satellites. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 90A42570
AIAA PAPER 90-2595 |
| 権利 | Copyright |
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