WEKO3
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Preparation for an On-Orbit Demonstration of an Electrodynamic Tether on the H-II Transfer Vehicle
https://jaxa.repo.nii.ac.jp/records/22669
https://jaxa.repo.nii.ac.jp/records/226697c7a5b3f-9d3a-4e33-b63a-dd4ae20df824
Item type | 学術雑誌論文 / Journal Article(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2016-06-20 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Preparation for an On-Orbit Demonstration of an Electrodynamic Tether on the H-II Transfer Vehicle | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Space Debris | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Active Debris Removal | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Deorbit | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Electrodynamic Tether | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
アクセス権 | ||||||
アクセス権 | metadata only access | |||||
アクセス権URI | http://purl.org/coar/access_right/c_14cb | |||||
著者 |
大川, 恭志
× 大川, 恭志× 河本, 聡美× 奥村, 哲平× 壹岐, 賢太郎× 堀川, 雄太× 川島, 一能× 三浦, 尚幸× 高井, 元× 鷲谷, 正史× 川崎, 治× 辻田, 大輔× 葛西, 徹× 植松, 洋彦× 井上, 浩一× Ohkawa, Yasushi× Kawamoto, Satomi× Okumura, Teppei× Iki, Kentaro× Horikawa, Yuuta× Kawashima, Kazutaka× Miura, Yoshiyuki× Takai, Moto× Washiya, Masahito× Kawasaki, Osamu× Tsujita, Daisuke× Kasai, Toru× Uematsu, Hirohiko× Inoue, Koichi |
|||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属 | ||||||
三菱重工業株式会社 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構有人宇宙技術部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構有人宇宙技術部門(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構研究開発部門(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Mitsubishi Heavy Industry | ||||||
著者所属(英) | ||||||
en | ||||||
Human Spaceflight Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Human Spaceflight Technology Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Research and Development Directorate, Japan Aerospace Exploration Agency (JAXA) | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | The Japan Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
en : Transactions of the Japan Society for Aeronautical and Space Sciences, Aerospace Technology Japan 巻 14, 号 ists30, p. 1-6, 発行日 2016-02-13 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A flight demonstration of an electrodynamic tether (EDT) on the H-II Transfer Vehicle (HTV) is planned by JAXA. This demonstration plan is called the Konotori Integrated Tether Experiment (KITE). KITE is the first step toward the development of active debris removal (ADR) systems using EDTs. EDTs have many advantages that make them promising candidates for deorbit propulsion systems for ADR, including the absence of consumables, low electric power requirements, the absence of thrust vectoring, and easy attachment to debris. The primary objective of KITE is to demonstrate the key EDT technologies for ADR. KITE mission will be conducted prior to re-entry of the HTV-6. A 700-m-length bare tether, which is deployed from the HTV body toward the zenith, collects electrons from the ambient space plasma, and a field emission cathode on the HTV emits 10-mA-level electrons into the plasma. This collector-emitter combination can provide complete propellant-free deorbit propulsion for ADR. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: カラー図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0485 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/tastj.14.Pb_1 | |||||
関連名称 | info:doi/10.2322/tastj.14.Pb_1 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1610048000 |