Discharge Current Oscillation in Hall Thrusters
Author:
Affiliation:
1. Kyushu University, Fukuoka 816-8580, Japan
2. University of Tokyo, Tokyo 113-8656, 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/10.2514/1.12759
Reference35 articles.
1. Main Physical Features and Processes Determining the Performance of Stationary Plasma Thrusters
2. Technology of closed-drift thrusters
3. Fundamental difference between the two Hall thruster variants
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