The Relation between Spatial Distribution of Metastable Xe I and Increase in Thrust Force of Microwave Discharge Ion Engine ^|^#956;10

Author:

TSUKIZAKI Ryudo,KOIZUMI Hiroyuki,SHIMAMURA Kohei,NISHIYAMA Kazutaka,KUNINAKA Hitoshi

Publisher

Japan Society for Aeronautical and Space Sciences

Reference14 articles.

1. Development and Demonstration of a Cathodeless Electron Cyclotron Resonance Ion Thruster

2. 2) Nishiyama, K., Hosoda, S., Usui, M., Tsukizaki, R., Hayashi, H., Shimizu, Y. and Kuninaka, H.: Feasibility Study on Performance Enhancement Options for the ECR Ion Thruster μ10, Trans. JSASS Space Tech. Japan, 7 (2009), pp. Pb_113-Pb_118.

3. 3) Tsukizaki, R., Koizumi, H., Hosoda, S., Bodendorfer, M., Nishiyama, K. and Kuninaka, H.: Plasma Luminescence Measurements in the ECR Ion Thruster μ10 Using Optical Fiber Probes, 31st International Electric Propulsion Con-ference, Ann Arbor, Michigan, IEPC-2009-162, 2009.

4. 4) Yokota, S., Matsui, M., Sako, D., Yamamoto, N., Koizumi, H., Komurasaki, K., Nakashima, H. and Arakawa, Y.: Diagnostics of Hall Thruster Plume by Laser Absorption Spectroscopy, 42nd AIAA/ASME/SAE/ASEE Joint Populsion Conference & Exibit, AIAA Paper 2006-5028, 2006.

5. 5) Herman, D. A., McFarlane, D. S. and Gallimore, D.: Discharge Plasma Plume Parameters of a 30-cm Ion Thruster Measured without Beam Extraction Using a High-Speed Probe Positioning System, 28th International Electric Propulsion Conference, Toulouse, IEPC-03-0069, 2003.

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1. Thrust Enhancement of a Microwave Ion Thruster;Journal of Propulsion and Power;2014-09

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