| タイトル | Exhaust flow and propulsion characteristics of a pulsed MPD arc thruster. |
| 著者（英） | York, T. M.; Michels, C. J. |
| 発行日 | 1972-04-01 |
| 言語 | eng |
| 内容記述 | Experimental investigation of the near-field, megawatt, single-shot exhaust for the self-field and auxiliary field cases (0 to 2 tesla) for a pulsed MPD arc thrustor. Plasma impact pressure and number density are correlated to provide velocity profiles (30,000 to 70,000 m/sec), thrust (10 to 120 N), impulse (3 to 16 N-sec) and mass accounting. The data agree with Hugel's self-field theory for the case where thrust is produced entirely by electromagnetic force. The data show that the thrust monotonically increases with auxiliary field. |
| NASA分類 | PROPULSION SYSTEMS |
| レポートNO | 72A26223
AIAA PAPER 72-500 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/462491 |
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