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パルス型プラズマスラスタのスケーリング則および投入電力増加による推進性能評価実験
https://jaxa.repo.nii.ac.jp/records/16521
https://jaxa.repo.nii.ac.jp/records/16521b56133f9-c141-4697-817d-c6e41860a011
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 | パルス型プラズマスラスタのスケーリング則および投入電力増加による推進性能評価実験 | |||||
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 | Scaling laws for pulsed plasma thruster and experiment of propulsive performance evaluation by increasing input power | |||||
著者 |
三村, 大樹
× 三村, 大樹× 梅田, 恭平× 北園, 陽平× 進藤, 崇央× 青柳, 潤一郎× 竹ヶ原, 春喜× Mimura, Daiki× Umeda, Kyohei× Kitazono, Yohei× Shindo, Takahiro× Aoyagi, Junichiro× Takegahara, Haruki |
|||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属 | ||||||
首都大学東京 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Metropolitan University | ||||||
出版者 | ||||||
出版者 | 宇宙航空研究開発機構宇宙科学研究所 | |||||
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22年度宇宙輸送シンポジウム: 講演集録 en : Proceedings of Space Transportation Symposium: FY2010 発行日 2011 |
|||||
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22年度宇宙輸送シンポジウム(2011年1月20-21日. 宇宙航空研究開発機構宇宙科学研究所), 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 FY2010 (January 20-21, 2011. 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 | We are working on research and development of rectangular PPT that is high specific impulse and coaxial PPT that is high impulse bit. Now, the propulsive performance of the thruster installed in the satellite is requested more widely following the extending the mission. A wide thrust performance was acquired and evaluated by changing the thruster size 0.5cm2 to 8.0cm2 at ablation area and changing the electric power of 3-75W as a thruster for the orbit control of 100kg class satellite in both a rectangular PPT and a coaxial PPT in the present study. It experimented at the high electric power to acquire a wide thrust performance and to evaluate the performance in this experiment. To acquire the operation result, carry out the continuous operation of 1,000,000shot at coaxial PPT. And to establish the stability operation condition, reduce the inductance of the entire system. At the result, continuous operation of 468,000shot was achieved on a coaxial PPT. And the stability operation condition on high electric power was established on a rectangular PPT. | |||||
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: AA0065073074 |