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外部磁場を印加したMPD推進機の数値シミュレーション
https://jaxa.repo.nii.ac.jp/records/16664
https://jaxa.repo.nii.ac.jp/records/16664623523e1-ed5c-4df6-9b68-8dd5856bfa88
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 | ||||||
タイトル | 外部磁場を印加したMPD推進機の数値シミュレーション | |||||
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 | |||||
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 | Numerical Simulation of Applied-Field MPD Thruster | |||||
著者 |
島倉, 和也
× 島倉, 和也× 李, 鎬式× 上野, 和之× 佐宗, 章弘× 澤田, 恵介× Shimakura, Kazuya× Lee, Hosik× Ueno, Kazuyuki× Saso, Akihiro× Sawada, Keisuke |
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著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属 | ||||||
名古屋大学大学院工学研究科 | ||||||
著者所属 | ||||||
東北大学大学院工学研究科航空宇宙工学専攻 | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate Schoole of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate Schoole of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate Schoole of Engineering, Tohoku University | ||||||
著者所属(英) | ||||||
en | ||||||
Graduate School of Engineering, Nagoya University | ||||||
著者所属(英) | ||||||
en | ||||||
Department of Aerospace Engineering, Graduate Schoole of Engineering, Tohoku University | ||||||
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21年度, 発行日 2010-01 |
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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 | 平成21年度宇宙輸送シンポジウム(2010年1月14日-15日, 宇宙航空研究開発機構宇宙科学研究本部) | |||||
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 (January 14-15, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency(JAXA)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Applied-field magnetoplasmadynamic (AFMPD) thruster is one of promising propulsion systems for deep space missions or piloted exploration because of its ability in achieving high thrust density and high specific impulse. The flow and electromagnetic fields of AFMPD thruster are numerically simulated under an identical condition with a laboratory experiment. Results of preliminary calculations show distribution of the current density and the electromagnetic force. | |||||
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 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: CD-ROM1枚 | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Note: One CD-ROM | |||||
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: AA0064741094 |