| タイトル | Elimination of Lifetime Limiting Mechanism of Hall Thrusters |
| 本文（外部サイト） | http://hdl.handle.net/2060/20090029929 |
| 著者（英） | Jacobson, David T.; Manzella, David H. |
| 著者所属（英） | NASA Glenn Research Center |
| 発行日 | 2009-03-10 |
| 言語 | eng |
| 内容記述 | A Hall thruster includes inner and outer electromagnets, with the outer electromagnet circumferentially surrounding the inner electromagnet along a centerline axis and separated therefrom, inner and outer poles, in physical connection with their respective inner and outer electromagnets, with the inner pole having a mostly circular shape and the outer pole having a mostly annular shape, a discharge chamber separating the inner and outer poles, a combined anode electrode/gaseous propellant distributor, located at an upstream portion of the discharge chamber and supplying propellant gas and an actuator, in contact with a sleeve portion of the discharge chamber. The actuator is configured to extend the sleeve portion or portions of the discharge chamber along the centerline axis with respect to the inner and outer poles. |
| NASA分類 | Spacecraft Propulsion and Power |
| 権利 | No Copyright |
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