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気球を利用した微小重力実験のための,一軸制御型機体システムの開発と飛行実験結果
https://jaxa.repo.nii.ac.jp/records/21664
https://jaxa.repo.nii.ac.jp/records/216640a0231af-661a-42b9-b8ac-c7deb1388e50
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2016-02-17 | |||||
タイトル | ||||||
タイトル | 気球を利用した微小重力実験のための,一軸制御型機体システムの開発と飛行実験結果 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Microgravity | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Balloon | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Flight Experiment | |||||
資源タイプ | ||||||
資源タイプ識別子 | http://purl.org/coar/resource_type/c_6501 | |||||
資源タイプ | journal article | |||||
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 | Development and Flight Experiment Results of Microgravity Experiment System with One-Directional Drag-Free Control using High Altitude Balloon | |||||
著者 |
丸, 祐介
× 丸, 祐介× 石川, 毅彦× 坂東, 信尚× 澤井, 秀次郎× 清水, 成人× 坂井, 真一郎× 吉光, 徹雄× 小林, 弘明× 菊池, 政雄× 山本, 信× 福山, 誠二郎× 岡田, 純平× 菅, 勇志× 梯, 友哉× 福家, 英之× 伊藤, 琢博× 水島, 隆成× 江口, 光× Maru, Yusuke× Ishikawa, Takehiko× Bando, Nobutaka× Sawai, Shujiro× Shimizu, Shigehito× Sakai, Shinichiro× Yoshimitsu, Tetsuo× Kobayashi, Hiroaki× Kikuchi, Masao× Yamamoto, Shin× Fukuyama, Seijiro× Okada, Junpei× Kan, Yuji× Kakehashi, Yuya× Fuke, Hideyuki× Ito, Takahiro× Mizushima, Takanari× Eguchi, Hikaru |
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出版者 | ||||||
出版者 | Japan Society for Aeronautical and Space Sciences | |||||
出版者(英) | ||||||
出版者 | 日本航空宇宙学会 | |||||
書誌情報 |
日本航空宇宙学会論文集 en : Journal of the Japan Society for Aeronautical and Space Sciences 巻 63, 号 6, p. 257(25)-264(32), 発行日 2015-12-05 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | In this paper is presented a microgravity experiment system utilizing a high altitude balloon. The feature is a double shell structure of a vehicle that is dropped off from the balloon and a microgravity experiment section that is attached to the inside of the vehicle with a liner slider. Control with cold gas jet thrusters of relative position of the experiment section to the vehicle and attitude of the vehicle maintains fine microgravity environment. The design strategy of the vehicle is explained, mainly referring to differences from the authors' previous design. The result of the flight experiment is also shown to evaluate the characteristics of the presented system. | |||||
内容記述 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 形態: 図版あり | |||||
内容記述(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains illustrations | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1344-6460 | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11307372 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: DS1540389004 |