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The Limitation Analysis of Two Dimensional Magnetic Field Configuration in Annular Ion Thruster

Authors :
Guangqing Xia
Ziping Wang
Chang Lu
Bin Sun
Source :
International Journal of Aerospace Engineering, Vol 2022 (2022)
Publication Year :
2022
Publisher :
Hindawi Limited, 2022.

Abstract

In this paper, the limitations of two-dimensional magnetic field configuration for an annular ion thruster are analyzed theoretically and numerically. The two-dimensional magnetic field, which is commonly used in traditional ion thrusters, has been proved to be a very effective way for the confinement of primary electrons and ions. Hence, the confinement characteristics of primary electrons and ions in an annular ion thruster with the two-dimensional magnetic field configuration are first analyzed theoretically. Then, according to the analysis, a two-dimensional magnetic field for an annular ion thruster is designed. On this basis, the limitations of the two-dimensional magnetic field configuration are analyzed and discussed by a three-dimensional (3D) Particle-in-cell Monte Carlo collision (PIC-MCC) model. The results show that if the collision process is not considered, a uniform distribution of primary electrons can be achieved theoretically. However, when considering the collision process, the atom forms a significant impedance to the circumferential motion of primary electrons, thus greatly increasing the loss rate of primary electrons. Finally, it is found that, since primary electrons are not guided and constrained in the circumferential direction under the two-dimensional magnetic field, the discharge uniformity cannot be improved only by increasing the magnetic field intensity.

Details

Language :
English
ISSN :
16875974
Volume :
2022
Database :
Directory of Open Access Journals
Journal :
International Journal of Aerospace Engineering
Publication Type :
Academic Journal
Accession number :
edsdoj.bc6a915ed1864b4fa416825a4131b2d1
Document Type :
article
Full Text :
https://doi.org/10.1155/2022/6215047