| タイトル | Multi-Thruster Propulsion Apparatus |
| 本文（外部サイト） | http://hdl.handle.net/2060/20160004243 |
| 著者（英） | Patterson, Michael J. |
| 著者所属（英） | NASA Headquarters |
| 発行日 | 2016-03-29 |
| 言語 | eng |
| 内容記述 | An electric propulsion machine includes an ion thruster having a discharge chamber housing a large surface area anode. The ion thruster includes flat annular ion optics with a small span to gap ratio. Optionally, at least a second thruster may be disposed radially offset from the ion thruster. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | No Copyright |
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