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液滴を推進剤としたレーザー推進機における推進性能のエネルギー依存性取得実験
https://jaxa.repo.nii.ac.jp/records/17409
https://jaxa.repo.nii.ac.jp/records/174095ad95306-9789-4aa4-8b43-84bf89b2db39
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 | 液滴を推進剤としたレーザー推進機における推進性能のエネルギー依存性取得実験 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザー推進 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | グリセリン推進剤 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | レーザービーム | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | YAGレーザー | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 比推力 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | アブレーション | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 運動量結合係数 | |||||
キーワード | ||||||
主題Scheme | Other | |||||
主題 | 研究開発 | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser propulsion | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | glycerin propellant | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | laser beam | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | YAG laser | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | specific impulse | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | ablation | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | momentum coupling coefficient | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | research and development | |||||
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 | Experiment for the energy dependence of thrust performance of a laser thruster with a propellant of liquid droplets | |||||
著者 |
中野, 正勝
× 中野, 正勝× 藤田, 和久× 内田, 成明× 馬頭, 正文× 新野, 正之× Nakano, Masakatsu× Fujita, Kazuhisa× Uchida, Shigeaki× Bato, Masafumi× Niino, Masayuki |
|||||
著者所属 | ||||||
日本学術振興会 | ||||||
著者所属 | ||||||
日本学術振興会 | ||||||
著者所属 | ||||||
レーザー技術総合研究所 | ||||||
著者所属 | ||||||
大阪大学 大学院工学研究科 | ||||||
著者所属 | ||||||
航空宇宙技術研究所 | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Society for the Promotion of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Society for the Promotion of Science | ||||||
著者所属(英) | ||||||
en | ||||||
Institute for Laser Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Osaka University Graduate School of Engineering | ||||||
著者所属(英) | ||||||
en | ||||||
National Aerospace Laboratory | ||||||
書誌情報 |
宇宙輸送シンポジウム 平成14年度 en : Proceedings of Space Transportation Symposium FY2002 p. 293-296, 発行日 2003-04 |
|||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Impulse generation experiments were conducted using glycerin propellants to obtain the dependence of laser beam energy on laser thruster performance. The radius of the glycerin droplet was 1 to 1.5 mm and the laser beam energy was varied from 60 mJ to 60 J. The maximum specific impulse was measured 18 s at the laser beam energy 55 J. Experimental data were scaled in terms of energy and the radius of the glycerin droplet to extrapolate the thruster performance. It was indicated that the radius of the glycerin droplet should be an order of 0.1 mm to obtain Isp greater than 1,000 s that will be needed to complete with other propulsion systems such as chemical and electric propulsions. | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0045426073 |