WEKO3
アイテム
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大気吸込式イオンエンジン(ABIE)に関する実験的研究
https://jaxa.repo.nii.ac.jp/records/16767
https://jaxa.repo.nii.ac.jp/records/167679f87711f-f1b2-4df9-b760-e37f3a82e517
Item type | 会議発表論文 / Conference Paper(1) | |||||
---|---|---|---|---|---|---|
公開日 | 2015-03-26 | |||||
タイトル | ||||||
タイトル | 大気吸込式イオンエンジン(ABIE)に関する実験的研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ion engine, atomic oxygen, air breathing ion engine, low earth orbit, electric thruster | |||||
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 | |||||
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 | |||||
その他のタイトル(英) | ||||||
その他のタイトル | Experimental study about air breathing ion engine (ABIE) | |||||
著者 |
横田, 久美子
× 横田, 久美子× 西山, 和孝× 田川, 雅人× 義澤, 康男× 山本, 大作× 國中, 均× Yokota, Kumiko× Nishiyama, Kazutaka× Tagawa, Masahito× Yoshizawa, Yasuo× Yamamoto, Daisaku× Kuninaka, Hitoshi |
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著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
神戸大学 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究本部 | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Kobe University | ||||||
著者所属(英) | ||||||
en | ||||||
Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究本部 | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA) | |||||
書誌情報 |
宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium 巻 平成20年度, 発行日 2009 |
|||||
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 | 平成20年度宇宙輸送シンポジウム(2009年1月19日-20日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Basic properties of air breathing ion engine (ABIE), which uses upper atmospheric gases as a propellant, were experimentally investigated. Atomic oxygen environment in low Earth orbit was simulated by a laser detonation beam source which has been used for spacecraft material degradation studies. 6 km/s atomic oxygen beam was used for producing oxygen plasma with a prototype of ABIE. It was made clear that the pressure needs to form oxygen plasma is in the range of 10(exp -4) Torr which is similar to that in non-energetic Xe propellant. This result suggested that the hyperthermal atomic oxygen influent into the ABIE was thermalized by a collision at an ABIE reflector. Oxygen ion current of 15 mA at acceleration voltage of 200 V provided a thrust of 120 microN. Propellant utilization efficiency was estimated to be 30 - 40 %, but it would be affected by undecomposed oxygen molecules in the beam. | |||||
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 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AN10324301 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0064292074 |