Parametric investigations of a nonconventional Hall thruster

被引：142

作者：

Raitses, Y ^{[1
]}

Fisch, NJ ^{[1
]}

机构：

[1] Princeton Univ, Princeton Plasma Phys Lab, Princeton, NJ 08543 USA

来源：

PHYSICS OF PLASMAS | 2001年 / 8卷 / 05期

关键词：

D O I：

10.1063/1.1355318

中图分类号：

O35 [流体力学]; O53 [等离子体物理学];

学科分类号：

070204 ; 080103 ; 080704 ;

摘要：

Hall thrusters might better scale to low power with nonconventional geometry. A 9 cm cylindrical, ceramic-channel, Hall thruster with a cusp-type magnetic field distribution has been investigated. It exhibits discharge characteristics similar to conventional coaxial Hall thrusters, but does not expose as much channel surface. Significantly, its operation is not accompanied by large amplitude discharge low frequency oscillations. (C) 2001 American Institute of Physics.

引用

页码：2579 / 2586

页数：8

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