微型霍尔推力器和内部PPU的性能

IF 0.7 4区工程技术 Q4 ENGINEERING, AEROSPACE Transactions of the Japan Society for Aeronautical and Space Sciences Pub Date : 2021-01-01 DOI:10.2322/TJSASS.64.189

Masatoshi Chono, N. Yamamoto, R. Tsukizaki, Takato Morishita, K. Kubota, Shinatra Cho, K. Kinefuchi, Toru Takahashi

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引用次数: 2

摘要

1)日本福冈嘉贺市九州大学先进能源工程科学系2)神奈川县相模原市日本宇宙航空研究开发机构空间宇宙科学研究所3)东京大学航空航天研究所东京113-8656 4)日本宇宙航空研究开发机构东京长阜市182-8522 5)日本宇宙航空研究开发机构神奈川县相模原市252-5210 6)宇宙航空工程系日本名古屋大学，日本爱知县名古屋464-8603;日本福岛县岩城市高桥登木地震研究所，日本福岛972-8326

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Performance of a Miniature Hall Thruster and an In-house PPU

1)Department of Advanced Energy Engineering Science, Kyushu University, Kasuga, Fukuoka 816–8580, Japan 2)Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252–5210, Japan 3)Department of Aeronautics and Astronautics, The University of Tokyo, Tokyo 113–8656, Japan 4)Japan Aerospace Exploration Agency, Chofu, Tokyo 182–8522, Japan 5)Japan Aerospace Exploration Agency, Sagamihara, Kanagawa 252–5210, Japan 6)Department of Aerospace Engineering, Nagoya University, Nagoya, Aichi 464–8603, Japan 7)Takahashi Denki Seisakusyo, Iwaki, Fukushima 972–8326, Japan

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