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マイクロ・マルチ・プラズマジェット・アレイ推進機の高性能化
https://jaxa.repo.nii.ac.jp/records/16230
https://jaxa.repo.nii.ac.jp/records/162308c9039ce-0ea0-4079-a9b5-b3043ecae0aa
名前 / ファイル | ライセンス | アクション |
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61856094.pdf (676.6 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 | マイクロ・マルチ・プラズマジェット・アレイ推進機の高性能化 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Micro-plasmajet Thruster | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Micro-Multi-Nozzle-Array | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Micro-Fabrication | |||||
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 | The HighPerformance of Micro Multi-Plasmajet-Array Thruster | |||||
著者 |
小林, 直人
× 小林, 直人× 常松, 春霞× 浅沼, 和貴× 人見, 亮輔× 堀澤, 秀之× 船木, 一幸× Kobayashi, Naoto× Tsunematsu, Haruka× Asanuma, Kazuki× Hitomi, Ryosuke× Horisawa, Hideyuki× Funaki, Ikko |
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著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学 | ||||||
著者所属 | ||||||
東海大学工学部 | ||||||
著者所属 | ||||||
宇宙航空研究開発機構宇宙科学研究所(JAXA)(ISAS) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
Tokai University | ||||||
著者所属(英) | ||||||
en | ||||||
School of Engineering, Tokai 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 | Observation of the micro-nozzle discharges was conducted, and a new thruster with extended nozzle structure for which each electrode element was electrically isolated from nearby elements was developed. The typical values of the thrust, specific impulse and averaged per nozzle element of the 6x6 micro-plasmajet array thruster operated at 27 W with 37.5 mg/sec of propellant mass flow per nozzle element were 39 mN, 107 sec, 33 % respectively. | |||||
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: AA0061856094 | |||||
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-2012-011 |