Study on ion energy distribution in low-frequency oscillation time scale of Hall thrusters

被引:4
作者
Wei, Liqiu [1 ,2 ]
Li, Wenbo [1 ]
Ding, Yongjie [1 ,2 ]
Han, Liang [1 ]
Yu, Daren [1 ,2 ]
Cao, Yong [1 ]
机构
[1] Harbin Inst Technol, Inst Adv Power, Plasma Prop Lab, Harbin 150001, Heilongjiang, Peoples R China
[2] Harbin Inst Technol, Elect Drive & Prop Technol Lab, Harbin 150001, Heilongjiang, Peoples R China
基金
中国国家自然科学基金;
关键词
STATIONARY PLASMA THRUSTERS; DISCHARGE; PLUME; MODEL;
D O I
10.1140/epjp/i2017-11714-3
中图分类号
O4 [物理学];
学科分类号
0702 ;
摘要
This paper reports on the dynamic characteristics of the distribution of ion energy during Hall thruster discharge in the low-frequency oscillation time scale through experimental studies, and a statistical analysis of the time-varying peak and width of ion energy and the ratio of high-energy ions during the low-frequency oscillation. The results show that the ion energy distribution exhibits a periodic change during the low-frequency oscillation. Moreover, the variation in the ion energy peak is opposite to that of the discharge current, and the variations in width of the ion energy distribution and the ratio of high-energy ions are consistent with that of the discharge current. The variation characteristics of the ion density and discharge potential were simulated by one-dimensional hybrid-direct kinetic simulations; the simulation results and analysis indicate that the periodic change in the distribution of ion energy during the low-frequency oscillation depends on the relationship between the ionization source term and discharge potential distribution during ionization in the discharge channel.
引用
收藏
页数:10
相关论文
共 28 条
[1]   Low-frequency model of breathing oscillations in Hall discharges [J].
Barral, Serge ;
Ahedo, Eduardo .
PHYSICAL REVIEW E, 2009, 79 (04)
[2]   Low frequency oscillations in a stationary plasma thruster [J].
Boeuf, JP ;
Garrigues, L .
JOURNAL OF APPLIED PHYSICS, 1998, 84 (07) :3541-3554
[3]   Transient phenomena in closed electron drift plasma thrusters:: insights obtained in a French cooperative program [J].
Bouchoule, A ;
Philippe-Kadlec, C ;
Prioul, M ;
Darnon, F ;
Lyszyk, M ;
Magne, L ;
Pagnon, D ;
Roche, S ;
Touzeau, M ;
Béchu, S ;
Lasgorceix, P ;
Sadeghi, N ;
Dorval, N ;
Marque, JP ;
Bonnet, J .
PLASMA SOURCES SCIENCE & TECHNOLOGY, 2001, 10 (02) :364-377
[4]   Effect of magnetic field profile on the anode fall in a Hall-effect thruster discharge [J].
Dorf, L. ;
Raitses, Y. ;
Fisch, N. J. .
PHYSICS OF PLASMAS, 2006, 13 (05)
[5]   Electrode contamination effects of retarding potential analyzer [J].
Fang, H. K. ;
Oyama, K. -I. ;
Cheng, C. Z. .
REVIEW OF SCIENTIFIC INSTRUMENTS, 2014, 85 (01)
[6]  
Fife J. M., 1997, P 33 JOINT PROP C SE
[7]  
Fukushima Y., 2010, 31 INT EL PROP C MIC
[8]   Model study of the influence of the magnetic field configuration on the performance and lifetime of a Hall thruster [J].
Garrigues, L ;
Hagelaar, GJM ;
Bareilles, J ;
Boniface, C ;
Boeuf, JP .
PHYSICS OF PLASMAS, 2003, 10 (12) :4886-4892
[9]   Wall material effects in stationary plasma thrusters. I. Parametric studies of an SPT-100 [J].
Gascon, N ;
Dudeck, M ;
Barral, S .
PHYSICS OF PLASMAS, 2003, 10 (10) :4123-4136
[10]  
Hara K., 2015, IEPC2015283