| タイトル | Inert gas ion thruster |
| 本文（外部サイト） | http://hdl.handle.net/2060/19820013378 |
| 著者（英） | Ramsey, W. D. |
| 著者所属（英） | Xerox Electro-Optical Systems |
| 発行日 | 1980-12-01 |
| 言語 | eng |
| 内容記述 | Inert gas performance with three types of 12 cm diameter magnetoelectrostatic containment (MESC) ion thrusters was tested. The types tested included: (1) a hemispherical shaped discharge chamber with platinum cobalt magnets; (2) three different lengths of the hemispherical chambers with samarium cobalt magnets; and (3) three lengths of the conical shaped chambers with aluminum nickel cobalt magnets. The best argon performance was produced by a 8.0 cm long conical chamber with alnico magnets. The best xenon high mass utilization performance was obtained with the same 8.0 cm long conical thruster. The hemispherical thruster obtained 75 to 87% mass utilization at 185 to 205 eV/ion of singly charged ion equivalent beam. |
| NASA分類 | SPACECRAFT PROPULSION AND POWER |
| レポートNO | 82N21252
NASA-CR-165521
REPT-2372-5009
NAS 1.26:165521 |
| 権利 | No Copyright |
| URI | https://repository.exst.jaxa.jp/dspace/handle/a-is/166511 |
