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永久磁石とマルチホローカソードを用いた輻射冷却式MPDスラスタの開発研究
https://jaxa.repo.nii.ac.jp/records/16222
https://jaxa.repo.nii.ac.jp/records/16222580b7b50-6bf9-4b0b-b622-4713084b79f7
名前 / ファイル | ライセンス | アクション |
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61856086.pdf (972.3 kB)
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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 | ||||||
タイトル | 永久磁石とマルチホローカソードを用いた輻射冷却式MPDスラスタの開発研究 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | MPD Thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Steady-State | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Applied Magnetic Field | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Permanent Magnet | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Multi-Hollow Cathode | |||||
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 | Research and Development of Radiation-Cooled MPD Thrusters with Permanent Magnets and Multi-Hollow Cathodes | |||||
著者 |
湖山, 典英
× 湖山, 典英× 井端, 公紀× 藤田, 雄也× 田原, 弘一× Koyama, Norihide× Ibata, Hiroki× Fujita, Katsuya× Tahara, Hirokazu |
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著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属 | ||||||
大阪工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka Institute of Technology | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | |||||
出版者(英) | ||||||
出版者 | Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS) | |||||
書誌情報 |
平成24年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2012 発行日 2013-01 |
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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24年度宇宙輸送シンポジウム (2013年1月17日-1月18日. 宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS)), 相模原市, 神奈川県 | |||||
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 FY2012 (January 17-18, 2013. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A pulsed-operation MPD Thruster was not fit for utilization in space. In this study, the MPD thruster doesn't have the coil for external magnetic field application but permanent magnet, Samarium cobalt. So, if magnetic Curie temperature is taken into consideration, the radiation-cooled thruster without cooling water can be designed. The manned Mars explorations which are a final objective of this study are missions for which a high specific impulse is needed. Using hydrogen, we could obtain a result of thrust 41.9 mN, specific impulse 2870 s, and thrust efficiency 12.5 %. We will perform performance improvement and heat analysis for development of a radiation-cooled thruster. And, to decrease cathode damage, we designed multi-hollow cathode. Using it, a new water-cooled thruster with changing anode geometry, distance between electrodes and magnet field strength was made. | |||||
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: PDF | |||||
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 | Physical characteristics: PDF | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0061856086 | |||||
レポート番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | レポート番号: STEP-2012-003 |