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

• Material Type: 文書・図像類
• 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
• Author/Editor: 和田, 明哲; 渡邊, 裕樹; 伊東山, 登; 月崎, 竜童; 池田, 知行; 飯塚, 俊明; 佐原, 宏典; 各務, 聡; 松永, 浩貴; 伊里, 友一朗; 塩田, 謙人; 松本, 幸太郎; 勝身, 俊之; 三宅, 淳巳; 笠原, 次郎; 志田, 真樹; 船瀬, 龍; 船木, 一幸; 羽生, 宏人; WADA, Asato; WATANABE, Hiroki; ITOUYAMA, Noboru; TSUKIZAKI, Ryudo; IKEDA, Tomoyuki; IIZUKA, Toshiaki; SAHARA, Hironori; KAKAMI, Akira; MATSUNAGA, Hiroki; IZATO, Yuichiro; SHIOTA, Kento; MATSUMOTO, Kotaro; KATSUMI, Toshiyuki; MIYAKE, Atsumi; KASAHARA, Jiro; SHIDA, Maki; FUNASE, Ryu; FUNAKI, Ikko; HABU, Hiroto
• Author Heading: 和田, 明哲; 渡邊, 裕樹; 伊東山, 登; 月崎, 竜童; 池田, 知行; 飯塚, 俊明; 佐原, 宏典; 各務, 聡; 松永, 浩貴; 伊里, 友一朗; 塩田, 謙人; 松本, 幸太郎; 勝身, 俊之; 三宅, 淳巳; 笠原, 次郎; 志田, 真樹; 船瀬, 龍; 船木, 一幸; 羽生, 宏人; WADA, Asato; WATANABE, Hiroki; ITOUYAMA, Noboru; TSUKIZAKI, Ryudo; IKEDA, Tomoyuki; IIZUKA, Toshiaki; SAHARA, Hironori; KAKAMI, Akira; MATSUNAGA, Hiroki; IZATO, Yuichiro; SHIOTA, Kento; MATSUMOTO, Kotaro; KATSUMI, Toshiyuki; MIYAKE, Atsumi; KASAHARA, Jiro; SHIDA, Maki; FUNASE, Ryu; FUNAKI, Ikko; HABU, Hiroto
• Publication, Distribution, etc.: 宇宙航空研究開発機構(JAXA)
• Publication Date: 2021-02-12
• Publication Date (W3CDTF): 2021-02-12
• Alternative Title: Study on Innovative Micro-Propulsion System Technologies for Micro-Space Probes
• Periodical title: 宇宙航空研究開発機構研究開発報告: 将来深宇宙探査に向けた革新的超小型推進系研究グループ 2020年度研究成果報告書 = JAXA Research and Development Report: Technical Report of the Research Activity for Innovative Micro Propulsion Systems for Future Deep Space Explorations (2020)
• No. or year of volume/issue: JAXA-RR-20-008
• Volume: JAXA-RR-20-008
• Pages: 1-5
• ISSN (Periodical Title): ISSN : 2433-2216
• Text Language Code: jpn
• Subject Heading: Micro-Propulsion System; Energetic Ionic Liquid Propulsion; Hall Effect Propulsion; Deep Space Exploration
• Target Audience: 一般
• Note (General): 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
• DOI: 10.20637/00047356
• Access Restrictions: 限定公開
• Data Provider (Database): 国立情報学研究所 : 学術機関リポジトリデータベース（IRDB）（機関リポジトリ）; https://irdb.nii.ac.jp
• Original Data Provider (Database): 宇宙航空研究開発機構 : 宇宙航空研究開発機構リポジトリ