| タイトル | A 30-cm diameter bombardment thruster with a variable magnetic baffle. |
| 著者（英） | Bechtel, R. T. |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | Thruster performance and stability over a range of beam currents is a function of the hollow cathode propellant flow which depends in part on the baffle geometry. Variable magnetic baffles have been used to allow a change in baffle geometry to improve thruster performance and stability. Test results of a 30-cm thruster with magnetic baffle are presented. Thruster performance characteristics are analyzed to show how the magnetic baffle field strength can improve performance at a fixed beam current, as well as increase the range of ion beam current for throttling. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72A26214
AIAA PAPER 72-489 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/462495 |
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