Art

J-GLOBAL ID：202002275744731154   Reference number：20A1768925

Flight Model Development and Ground Demonstration of Water Resistojet Propulsion System for CubeSats

キューブサットのための水レジストジェット推進システムの飛行モデル開発と地上実証

Author (10)： NISHII Keita (Department of Aeronautics and Astronautics, The University of Tokyo) ,  ASAKAWA Jun (Department of Advanced Energy, The University of Tokyo) ,  KIKUCHI Kosei (Department of Advanced Energy, The University of Tokyo) ,  AKIYAMA Mariko (Department of Advanced Energy, The University of Tokyo) ,  WANG Qihang (Department of Advanced Energy, The University of Tokyo) ,  MUROHARA Masaya (Department of Advanced Energy, The University of Tokyo) ,  ATAKA Yasuho (Department of Aeronautics and Astronautics, The University of Tokyo) ,  KOIZUMI Hiroyuki (Department of Advanced Energy, The University of Tokyo) ,  FUNASE Ryu (Department of Aeronautics and Astronautics, The University of Tokyo) ,  KOMURASAKI Kimiya (Department of Aeronautics and Astronautics, The University of Tokyo)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences (Web)  (Trans Jpn Soc Aeronaut Space Sci (Web))
Volume： 63  Issue： 4  Page： 141-150(J-STAGE)  Publication year： 2020 
JST Material Number： U0630A  ISSN： 2189-4205  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： *artificial satellite ,  small type ,  *propulsion system ,  steam separation ,  energy saving ,  maze ,  thrust ,  transpiration ,  *performance evaluation ,  flight test ,  operation rate ,  intermittent operation ,  consumed electric power
Semi thesaurus term： CubeSat ,  duty cycle ,  気化室 ,  *水レジストジェット推進

Author keywords (4)： CubeSat ,  Micro-propulsion ,  Water ,  Resistojet Thruster

JST classification (1)： Rocket engines  (PB02050J)

Reference (39)：

• 1) SpaceWorks: 2019 Nano/Microsatellite Market Forecast, 9th Edition, 2019.
• 2) Lemmer, K.: Propulsion for CubeSats, Acta Astronautica, 134 (2017), pp. 231-243.
• 3) Poghosyan, A. and Golkar, A.: CubeSat Evolution: Analyzing CubeSat Capabilities for Conducting Science Missions, Progr. Aerospace Sci., 88 (2017), pp. 59-83.
• 4) Funase, R., Inamori, T., Ikari, S., Ozaki, N., Nakajima, S., Ariu, K., Koizumi, H., Kameda, S., Tomiki, A., Kobayashi, Y., Ito, T., and Kawakatsu, Y.: One-year Deep Space Flight Results of the World's First Full-scale 50-kg-class Deep Space Probe PROCYON and Its Future Prospects, Proceedings of the 30th Annual AIAA/USU Conference on Small Satellites, Logan, Utah, SSC16-III-05, 2016.
• 5) Koizumi, H., Kawahara, H., Yaginuma, K., Asakawa, J., Nakagawa, Y., Nakamura, Y., Kojima, S., Matsuguma, T., Funase, R., Nakatsuka, J., and Komurasaki, K.: Initial Flight Operations of the Miniature Propulsion System Installed on Small Space Probe: PROCYON, Trans. JSASS Aerospace Technology Japan, 14 (2016), pp. Pb_13-Pb_22.

Terms in the title (9)： キューブサット ,  水 ,  レジスト ,  ジェット推進 ,  飛行 ,  モデル ,  開発 ,  地上 ,  実証