Microwave power absorption to high energy electrons in the ECR ion thruster

被引:21
作者
Coral, Giulio [1 ]
Tsukizaki, Ryudo [2 ]
Nishiyama, Kazutaka [2 ]
Kuninaka, Hitoshi [2 ]
机构
[1] Univ Tokyo, Grad Sch Engn, Dept Aeronaut & Astronaut, Tokyo, Japan
[2] Japan Aerosp Explorat Agcy, Inst Space & Astronaut Sci, Sagamihara, Kanagawa, Japan
关键词
xenon; ion thruster; electron cyclotron resonance; electric propulsion; microwave absorption; HAYABUSA; MODEL;
D O I
10.1088/1361-6595/aadf04
中图分类号
O35 [流体力学]; O53 [等离子体物理学];
学科分类号
070204 ; 080103 ; 080704 ;
摘要
The microwave power absorption efficiency of the mu 10 ECR ion thruster, utilized in the Japanese asteroid explorers Hayabusa and Hayabusa2, is investigated in order to allow performance measurement and provide information for its improvement. A model detailing the local electron behavior in a real ECR plasma discharge, based the magnetic field characteristics, is presented. Three methods to evaluate the microwave power absorption efficiency are proposed: an estimation based on the chamber geometry and magnetic field characteristics, a measuremen based on performance parameters and a measurement performed with Langmuir probes. The equations used for each method are analytically derived. The local electron behavior model is confirmed with a Langmuir probe experiment. Measurement of the microwave power absorption efficiency is performed with the two independent methods proposed. Results from the two experiments show good agreement with each other and with the theory. Finally, a diffusion model explaining the different electron temperature distributions observed in the chamber is proposed. The model and experiments clarify the physics behind previously observed performance variations and give valuable hints for future chamber improvement.
引用
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页数:13
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