Plume interference effects of the racetrack-shaped anode-layer Hall thruster system
Author:
MIYASAKA Takeshi1, NAGAO Ryo2, FUKAGAWA Kohei2, NAGAMINE Mitsuhiro2, MAEDA Naoto2, KATO Akane2, ASAHARA Makoto1
Affiliation:
1. Department of Mechanical Engineering, Gifu University 2. Department of Intelligence Science and Engineering, Gifu University
Publisher
Japan Society of Mechanical Engineers
Reference14 articles.
1. Beal, B. E. and Gallimore, A. D., The Effects of Cathode Configuration on Hall Thruster Cluster Plume Properties, AIAA Paper 2005-3678 (2005). 2. Feuerborn, S. A., Neary, D. A., and Perkins, J. M., Finding a Way: Boeing’s “All Electric Propulsion Satellite”, AIAA-2013-4126(2013). 3. Funaki, I., Sano, T., Fukatsu, T., Tashiro, Y., Shiiki, T., Cho, S., Matsunaga, Y., and Goto, D., Development Status of 6kW-Class Hall Thrusters at JAXA, International Electric Propulsion Conference, IEPC-2019-441 (2019). 4. Hamada, Y., Kawashima, R., Komurasaki, K., Yamamoto, N., and Tahara, H., Development Status of 5 kW Class Anode-Layer Type Hall Thruster: RAIJIN94, International Electric Propulsion Conference, IEPC-2017-412 (2017). 5. Hamada, Y., Bak, J., Kawashima, R., Koizumi, H., Komurasaki, K., Yamamoto, N., Egawa, Y., Funaki, I., Iihara, S., Cho, S., Kubota, K., Watanabe, H., Fuchigami, K., Tashiro, Y., Takahata, Y., Kakuma, T., Furukubo, Y., and Tahara, H., Hall Thruster Development for Japanese Space Propulsion Programs, Transactions of the Japan Society for Aeronautical and Space Sciences, Vol. 60, No. 5 (2017), pp.320-326.
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