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TAL及びSPTホールスラスタの高電圧作動・高比推力化実験
https://jaxa.repo.nii.ac.jp/records/16245
https://jaxa.repo.nii.ac.jp/records/16245fb89ee1f-03ad-4067-9fb3-283f2e7961f1
名前 / ファイル | ライセンス | アクション |
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61856109.pdf (1.0 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 | ||||||
タイトル | TAL及びSPTホールスラスタの高電圧作動・高比推力化実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Electric propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Hall thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | High power | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | High specific impulse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Orbital transfer vehicle | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Mars exploration | |||||
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 on High-Power and High-Specific-Impulse TAL and SPT Hall Thrusters | |||||
著者 |
三藤, 陽平
× 三藤, 陽平× 加藤, 優貴× 山本, 怜× 杉本, 成× 戸川, 和也× 池田, 知行× 田原, 弘一× Mito, Yohei× Kato, Yuki× Yamamoto, Ryo× Sugimoto, Naru× Togawa, Kazuya× Ikeda, Tomoyuki× 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 | ||||||
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 | ||||||
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 | The operational range of Hall thrusters will be hoped to be expanded for future orbital transfer vehicle and Mars exploration. In this study, both SPT and TAL Hall thrusters were operated with higher discharge voltages, that is, with higher input powers and large specific impulses. The input powers and specific impulse for the SPT-type Hall thruster reached above 5 kW and 3000 sec, respectively. In the TAL Hall thruster, they were above 3.5 kW and, 2800 sec, respectively. It was found that the both thrusters are promising for the future missions although the operations were thermally severe. | |||||
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: AA0061856109 | |||||
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-2012-026 |