| タイトル | Performance of 10-kW class xenon ion thrusters |
| 本文（外部サイト） | http://hdl.handle.net/2060/19880018704 |
| 著者（英） | Patterson, Michael J.; Rawlin, Vincent K. |
| 著者所属（英） | NASA Lewis Research Center |
| 発行日 | 1988-01-01 |
| 言語 | eng |
| 内容記述 | Presented are performance data for laboratory and engineering model 30 cm-diameter ion thrusters operated with xenon propellant over a range of input power levels from approximately 2 to 20 kW. Also presented are preliminary performance results obtained from laboratory model 50 cm-diameter cusp- and divergent-field ion thrusters operating with both 30 cm- amd 50 cm-diameter ion optics up to a 20 kW input power. These data include values of discharge chamber propellant and power efficiencies, as well as values of specific impulse, thruster efficiency, thrust and power. The operation of the 30 cm- and 50 cm-diameter ion optics are also discussed. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 88N28088
AIAA PAPER 88-2914
NAS 1.15:101292
NASA-TM-101292
E-4272 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/145532 |
