Particle-in-cell simulations of Hall thruster acceleration and near plume regions

被引:19
|
作者
Katz, Ira [1 ]
Chaplin, Vernon H. [1 ]
Ortega, Alejandro Lopez [1 ]
机构
[1] CALTECH, Jet Prop Lab, 4800 Oak Grove Dr, Pasadena, CA 91109 USA
基金
美国国家航空航天局;
关键词
MODEL;
D O I
10.1063/1.5054009
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
The results of 1-D azimuthal, and 2-D z-theta, particle-in-cell simulations of Hall thruster acceleration and near plume regions are reported. The 1-D simulations show that fast moving electron waves drive coherent, large amplitude, ion acoustic waves. The ion waves become azimuthally coherent too quickly for ion sound to be the cause; the coherence comes from early electron waves. 2-D simulations with only fast moving, main beam, ions result in ion acoustic wave amplitudes much lower than those in the 1-D calculations. The addition of a small amount of ionization in the domain, at a rate consistent with Hall thruster parameters, causes the potential profile to divide into two distinct regions. In the upstream portion of the domain, the potential profile is very steep; in the downstream portion, the potential profile is almost flat. Electron transport in the two regions is discussed. Published by AIP Publishing.
引用
收藏
页数:12
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