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Electrodynamic tether systems for debris removal
https://jaxa.repo.nii.ac.jp/records/6403
https://jaxa.repo.nii.ac.jp/records/64039f7d747d-08c0-4173-b05e-1fecd553d366
名前 / ファイル | ライセンス | アクション |
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49206088.pdf (3.1 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-03-26 | |||||
タイトル | ||||||
言語 | en | |||||
タイトル | Electrodynamic tether systems for debris removal | |||||
言語 | ||||||
言語 | eng | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 導電性テザーシステム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙機推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 宇宙デブリ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 軌道変換 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | カーボンナノチューブ | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 電界放出陰極 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 展開 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 地磁気場 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | electrodynamic tether system | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | spacecraft propulsion | |||||
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 | orbit transfer | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | carbon nanotube | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | field emission cathode | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | deployment | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | geomagnetic field | |||||
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 | |||||
著者 |
河本, 聡美
× 河本, 聡美× 大川, 恭志× 牧田, 健× 吉村, 庄市× 西田, 信一郎× 中島, 厚× 北村, 正治× 曲, 徳路× Cho, Mengu× Kawamoto, Satomi× Okawa, Yasushi× Makida, Takeshi× Yoshimura, Shoichi× Nishida, Shinichiro× Nakajima, Atsushi× Kitamura, Shoji× Kyoku, Norimichi× Cho, Mengu |
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著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
東京都立科学技術大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構 総合技術研究本部 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属 | ||||||
九州工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency Institute of Space Technology and Aeronautics | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Kyushu Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構 | |||||
出版者(英) | ||||||
出版者 | Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙航空研究開発機構特別資料 en : JAXA Special Publication: 9th Spacecraft Charging Technology Conference 巻 JAXA-SP-05-001E, p. 764-769, 発行日 2005-08-01 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | As a countermeasure for suppressing space debris growth, the Institute of Space Technology and Aeronautics, Japan Aerospace Exploration Agency (JAXA), is investigating an active space debris removal system that employs highly-efficient Electrodynamic Tether (EDT) technology as its orbital transfer system. Firstly, a small, expendable EDT package is under development that consists of a bare conductive tether and Field Emission Cathodes (FECs) that utilize carbon nanotubes. This package presents a possible technique for lowering the orbit of a debris removal system without the need for propellant. A test flight experiment using a rocket upper stage or a small satellite is planned for establishing and demonstrating the EDT technology. First, precise numerical simulations are performed for some aspects of mission analysis, such as available electric currents, orbital changes, tether stability, and deployment dynamics. The status of the trial fabrications and some evaluation test of the tether such as electric discharge are also described. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1349-113X | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11984031 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0049206088 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JAXA-SP-05-001E |