Determination of the ionization and acceleration zones in a stationary plasma thruster by optical spectroscopy study: Experiments and model

被引:33
作者
Dorval, N
Bonnet, J
Marque, JP
Rosencher, E
Chable, S
Rogier, F
Lasgorceix, P
机构
[1] Off Natl Etud & Rech Aerosp, DMPH, F-91761 Palaiseau, France
[2] Off Natl Etud & Rech Aerosp, CERT, DTIM, Toulouse, France
[3] CNRS, Aerotherm Lab, F-45071 Orleans 2, France
关键词
D O I
10.1063/1.1458053
中图分类号
O59 [应用物理学];
学科分类号
摘要
A stationary plasma thruster is experimentally studied using different optical spectroscopies of xenon ions. Doppler shift in laser induced fluorescence is used for velocity determination while the ion density is determined by emission spectroscopy. These experiments show unambiguously that the ionization and the acceleration zones are spatially distinct inside the thruster channel. Moreover, it is shown that these results can be easily taken into account with a very simple quasineutral stationary one-dimensional model. (C) 2002 American Institute of Physics.
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页码:4811 / 4817
页数:7
相关论文
共 15 条
[1]  
[Anonymous], 1998, THESIS MIT
[2]  
BAREILLES J, 2000, 3 INT C SPAC PROP IC
[3]  
BECHU S, 2000, 36 JOINT PROP C HUNT
[4]   Low frequency oscillations in a stationary plasma thruster [J].
Boeuf, JP ;
Garrigues, L .
JOURNAL OF APPLIED PHYSICS, 1998, 84 (07) :3541-3554
[5]  
BOEUF JP, 1998, ELECT KINETICS APPL
[6]  
CHEN FF, 1984, INTRO PLASMA PHYSICS
[7]  
DAY M, 1997, 25 INT EL PROP C CLE
[8]  
FIFE JM, 1997, 33 AIAA JINT PROP C
[9]  
HARGUS WAJ, 1999, 35 AIAA ASME ASEE JO
[10]  
LYSZYK M, 2000, 3 INT C SPAC PROP IC