WEKO3
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高温超伝導マグネットによる強磁場印加プラズマ推進
https://jaxa.repo.nii.ac.jp/records/49530
https://jaxa.repo.nii.ac.jp/records/49530f11ba320-cdcc-44a8-a99f-8fafd36788f1
名前 / ファイル | ライセンス | アクション |
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SA6000184074.pdf (489.2 kB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2023-05-23 | |||||
タイトル | ||||||
タイトル | 高温超伝導マグネットによる強磁場印加プラズマ推進 | |||||
言語 | ||||||
言語 | jpn | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_5794 | |||||
資源タイプ | conference paper | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Strong Applied Field Plasma Thruster Using High-temperature Superconducting Magnet | |||||
著者 |
杵淵, 紀世志
× 杵淵, 紀世志× 市原, 大輔× 中野, 僚太× 前島, 大輝× 高木, 涼平× ACHESON, Chris× OLATUNJI, Jamal× GODDARD-WINCHESTER, Max× POLLOCK, Randy× KINEFUCHI, Kiyoshi× ICHIHARA, Daisuke× NAKANO, Ryota× MAESHIMA, Daiki× TAKAGI, Ryohei× ACHESON, Chris× OLATUNJI, Jamal× GODDARD-WINCHESTER, Max× POLLOCK, Randy |
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著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
名古屋大学 | ||||||
著者所属 | ||||||
Victoria University of Wellington | ||||||
著者所属 | ||||||
Victoria University of Wellington | ||||||
著者所属 | ||||||
Victoria University of Wellington | ||||||
著者所属 | ||||||
Victoria University of Wellington | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Victoria University of Wellington | ||||||
著者所属(英) | ||||||
en | ||||||
Victoria University of Wellington | ||||||
著者所属(英) | ||||||
en | ||||||
Victoria University of Wellington | ||||||
著者所属(英) | ||||||
en | ||||||
Victoria University of Wellington | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)(ISAS) | |||||
書誌情報 |
令和4年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium FY2022 発行日 2023-01 |
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会議概要(会議名, 開催地, 会期, 主催者等) | ||||||
内容記述タイプ | Other | |||||
内容記述 | 令和4年度宇宙輸送シンポジウム(2023年1月12日-13日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)) , 相模原市, 神奈川県 | |||||
会議概要(会議名, 開催地, 会期, 主催者等)(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Space Transportation Symposium FY2022 (January 12-13, 2023. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | High performance plasma thruster is required for the further space development and exploration. One of the possible candidates is applying strong magnetic field to improve the thrust efficiency and thrust density. In this study, a new plasma thruster with high-temperature superconducting magnet capable of generating high magnetic field was developed. The superconducting magnet was cooled by a cryocooler, and the thruster operation with an applied field of 0.8 T have been successfully carried out. | |||||
著者版フラグ | ||||||
出版タイプ | AM | |||||
出版タイプResource | http://purl.org/coar/version/c_ab4af688f83e57aa | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: SA6000184074 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | STEP-2022-022 |