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軌道上実証実験を想定した電界放出カソード複数台動作時の性能評価
https://jaxa.repo.nii.ac.jp/records/38701
https://jaxa.repo.nii.ac.jp/records/38701f5b39578-c2ab-4843-9236-12f3a9669a5e
名前 / ファイル | ライセンス | アクション |
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AC1500061000.pdf (1.4 MB)
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Item type | 会議発表論文 / Conference Paper(1) | |||||
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公開日 | 2015-10-26 | |||||
タイトル | ||||||
タイトル | 軌道上実証実験を想定した電界放出カソード複数台動作時の性能評価 | |||||
言語 | ||||||
言語 | jpn | |||||
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 | Carbon Nanotube | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Parallel Operation of FECs | |||||
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 | Experiment of Parallel Field Emission Cathode Operation Preparing for On-orbit Demonstration | |||||
著者 |
井本, 伸
× 井本, 伸× 島田, 温子× 大川, 恭志× 河本, 聡美× 山極, 芳樹× Imoto, Shin× Shimada, Atsuko× Ohkawa, Yasushi× Kawamoto, Satomi× Yamagiwa, Yoshiki |
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著者所属 | ||||||
静岡大学 | ||||||
著者所属 | ||||||
静岡大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
静岡大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Shizuoka University | ||||||
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 |
第58回宇宙科学技術連合講演会講演集 en : Proceedings of 58th Space Sciences and Technology Conference 発行日 2014-11 |
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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 | 第58回宇宙科学技術連合講演会(2014年11月12日-14日. 長崎ブリックホール), 長崎市, 長崎県 | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | "Research of debris removal system using electrodynamic tether (EDT) system has been conducted in JAXA. The EDT system needs active electron emission device in order to drive large electric current through the tether for obtaining adequate de-orbit thrust. A field emission Cathode (FEC) can be a good option of the electron emitter because of its simplicity and potential performance. In the EDT systems, it is expected that several FEC units operates in parallel because of redundancy requirement. Since the interaction between the cathode units may cause instability or performance degradation, experiments of FEC parallel operation is required prior to practical on-orbit operation. This paper describes the result of double FEC operation tests." | |||||
権利 | ||||||
権利情報 | (C)2014 一般社団法人 日本航空宇宙学会 | |||||
著者版フラグ | ||||||
出版タイプ | VoR | |||||
出版タイプResource | http://purl.org/coar/version/c_970fb48d4fbd8a85 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AC1500061000 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: JSASS-2014-4235 |