Two-dimensional numerical model of plasma flow in a Hall thruster-Reference-Cited by-同舟云学术

Two-dimensional numerical model of plasma flow in a Hall thruster

Published:1995-11 Issue:6 Volume:11 Page:1317-1323
ISSN:0748-4658
Container-title:Journal of Propulsion and Power
language:en
Short-container-title:Journal of Propulsion and Power

Author:

Komurasaki Kimiya¹,Arakawa Yoshihiro²

Affiliation:

1. Nagoya University, Chikusa-ku, Nagoya 464-01, Japan

2. University of Tokyo, Bunkyo-ku, Tokyo 113, Japan

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Space and Planetary Science,Mechanical Engineering,Fuel Technology,Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/3.23974

Reference18 articles.

1. Theory of ion acceleration with closed electron drift

2. Performance of double-stage-discharge Hall ion thruster

3. 4Bugrova, A. I., Kirn, V., Maslennikov, N. A., and Morozov, A. I. "Physical Processes and Characteristics of Stationary Plasma Thrusters with Closed Electrons Drift,11Proceedings of the 22nd International Electric Propulsion Conference (Viareggio, Italy), 1991 (IEPC 91-079).

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