@techreport{oai:jaxa.repo.nii.ac.jp:00047369,
 author = {和田, 明哲 and 渡邊, 裕樹 and 伊東山, 登 and 月崎, 竜童 and 池田, 知行 and 飯塚, 俊明 and 佐原, 宏典 and 各務, 聡 and 松永, 浩貴 and 伊里, 友一朗 and 塩田, 謙人 and 松本, 幸太郎 and 勝身, 俊之 and 三宅, 淳巳 and 笠原, 次郎 and 志田, 真樹 and 船瀬, 龍 and 船木, 一幸 and 羽生, 宏人 and WADA, Asato and WATANABE, Hiroki and ITOUYAMA, Noboru and TSUKIZAKI, Ryudo and IKEDA, Tomoyuki and IIZUKA, Toshiaki and SAHARA, Hironori and KAKAMI, Akira and MATSUNAGA, Hiroki and IZATO, Yuichiro and SHIOTA, Kento and MATSUMOTO, Kotaro and KATSUMI, Toshiyuki and MIYAKE, Atsumi and KASAHARA, Jiro and SHIDA, Maki and FUNASE, Ryu and FUNAKI, Ikko and HABU, Hiroto},
 month = {Feb},
 note = {For the implementation of future space science missions at the father away from Earth, it is necessary to build the technological platforms for performing various challenging missions with high frequency and to mature the technology, and breakthrough of space propulsion technology is especially indispensable. In order to obtain the exploration flexibility by the propulsion control technology of the micro-spacecraft, our research group is working on the development and research of the high-thrust micro-propulsion systems, which is an important technical issue, and objective of this study is the feasibility of the propulsion technologies. In addition, as the platforms of propulsion technology, we propose the various future micro-spacecraft technology demonstration missions and technology demonstration missions of the propulsion system using micro-spacecraft, with hall-effect thruster propulsion system and high-energetic ionic liquid propulsion system as the representative of propulsion technologies. This paper presents the consideration status and further studies of innovative micro propulsion systems for the future deep space explorations., 形態: カラー図版あり, Physical characteristics: Original contains color illustrations, 資料番号: AA2030017001, レポート番号: JAXA-RR-20-008},
 title = {超小型探査機搭載に向けた革新的超小型推進系技術に関する研究},
 year = {2021}
}