| タイトル | 30 cm Engineering Model thruster design and qualification tests |
| 著者（英） | Schnelker, D. E.; Collett, C. R. |
| 発行日 | 1975-03-01 |
| 言語 | eng |
| 内容記述 | Development of a 30-cm mercury electron bombardment Engineering Model ion thruster has successfully brought the thruster from the status of a laboratory experimental device to a point approaching flight readiness. This paper describes the development progress of the Engineering Model (EM) thruster in four areas: (1) design features and fabrication approaches, (2) performance verification and thruster to thruster variations, (3) structural integrity, and (4) interface definition. The design of major subassemblies, including the cathode-isolator-vaporizer (CIV), main isolator-vaporizer (MIV), neutralizer isolator-vaporizer (NIV), ion optical system, and discharge chamber/outer housing is discussed along with experimental results. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 75A26562
AIAA PAPER 75-341 |
| 権利 | Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/448614 |
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