Sub-Milli-Newton Class Miniature Microwave Ion Thruster
Author:
Affiliation:
1. National Defense Academy, Kanagawa 239-8686, Japan
2. Japan Aerospace Exploration Agency, Kanagawa 229-8510, 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/10.2514/1.21565
Reference12 articles.
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2. Calculation on 2 cm ECRIT Thrust Regulation Based on 3D PIC Numerical Simulation Method;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2020-08
3. Development and Flight Operation of a Miniature Ion Propulsion System;Journal of Propulsion and Power;2018-07
4. Experimental Research on the Neutralizer of Micro ECR Ion Thruster;Xibei Gongye Daxue Xuebao/Journal of Northwestern Polytechnical University;2018-02
5. Experimental Visualization of Ion Thruster Neutralization Phenomena;IEEE Transactions on Plasma Science;2015-01
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