Critical assessment of a two-dimensional hybrid Hall thruster model: Comparisons with experiments

被引:110
作者
Bareilles, J
Hagelaar, GJM
Garrigues, L
Boniface, C
Boeuf, JP
Gascon, N
机构
[1] Univ Toulouse 3, Ctr Phys Plasmas & Applicat, F-31062 Toulouse 4, France
[2] Aerotherm Lab, F-45071 Orleans 2, France
关键词
D O I
10.1063/1.1719022
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
A discussion is presented on the results and predictive capabilities of a two-dimensional (2D) hybrid Hall effect thruster (HET) model. It is well known that classical (collision-induced) cross-field electron transport and energy losses are not sufficient to explain the observed HET characteristics. The 2D, quasineutral, hybrid discharge model uses empirical parameters to describe additional, anomalous electron transport and energy loss phenomena. It is shown that, for properly adjusted empirical parameters, the model can qualitatively reproduce the observed thruster behavior over a large range of operating conditions. The ionization and transit-time oscillations predicted by the model are described, and their consequences on the time-averaged thruster properties are discussed. Finally, the influence of the empirical parameters on the model results is shown, especially on quantities that can be measured experimentally. (C) 2004 American Institute of Physics.
引用
收藏
页码:3035 / 3046
页数:12
相关论文
共 22 条
[11]  
GASCON N, 2000, THESIS U PROVENCE
[12]   Two-dimensional model of a stationary plasma thruster [J].
Hagelaar, GJM ;
Bareilles, J ;
Garrigues, L ;
Boeuf, JP .
JOURNAL OF APPLIED PHYSICS, 2002, 91 (09) :5592-5598
[13]   Role of anomalous electron transport in a stationary plasma thruster simulation [J].
Hagelaar, GJM ;
Bareilles, J ;
Garrigues, L ;
Boeuf, JP .
JOURNAL OF APPLIED PHYSICS, 2003, 93 (01) :67-75
[14]   Main physical features and processes determining the performance of stationary plasma thrusters [J].
Kim, V .
JOURNAL OF PROPULSION AND POWER, 1998, 14 (05) :736-743
[15]   2-DIMENSIONAL NUMERICAL-MODEL OF PLASMA-FLOW IN A HALL THRUSTER [J].
KOMURASAKI, K ;
ARAKAWA, Y .
JOURNAL OF PROPULSION AND POWER, 1995, 11 (06) :1317-1323
[16]  
Meezan NB, 2001, PHYS REV E, V63, DOI 10.1103/PhysRevE.63.026410
[17]  
Morozov A. I., 1972, Soviet Physics - Technical Physics, V17, P38
[18]  
Morozov AI, 2000, REV PL PHYS, V21, P203
[19]  
PEROT C, 1999, THESIS U ORELEANS
[20]  
PEROT C, 1999, 35 AIAA JOINT PROP C