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折り目剛性を考慮した宇宙膜構造の非対称展開挙動の解析
https://jaxa.repo.nii.ac.jp/records/22505
https://jaxa.repo.nii.ac.jp/records/2250516694eef-b8fa-404d-8e75-f709fd781cf3
Item type | 学術雑誌論文 / Journal Article(1) | |||||
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公開日 | 2015-05-13 | |||||
タイトル | ||||||
タイトル | 折り目剛性を考慮した宇宙膜構造の非対称展開挙動の解析 | |||||
言語 | ||||||
言語 | jpn | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Spacecraft | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Space Structures | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Membrane Structures | |||||
キーワード | ||||||
言語 | en | |||||
主題Scheme | Other | |||||
主題 | Finite Element Analysis | |||||
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 | Research on Non-synchronous Deployment of Spinning Solar Sail Membrane Considering Crease Stiffness | |||||
著者 |
佐藤, 剛志
× 佐藤, 剛志× 坂本, 啓× 新宅, 健吾× 大野, 剛× 松永, 三郎× 森, 治× 白澤, 洋次× 奥泉, 信克× 大熊, 政明× Sato, Tsuyoshi× Sakamoto, Hiraku× Shintaku, Kengo× Ono, Go× Matsunaga, Saburo× Mori, Osamu× Shirasawa, Yoji× Okuizumi, Nobukatsu× Okuma, Masaaki |
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著者所属 | ||||||
東京工業大学 | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属 | ||||||
東京大学 | ||||||
著者所属 | ||||||
東京工業大学 : 宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
宇宙航空研究開発機構(JAXA) | ||||||
著者所属 | ||||||
東京工業大学 | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
The University of Tokyo | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology : Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Japan Aerospace Exploration Agency(JAXA) | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
出版者 | ||||||
出版者 | 日本航空宇宙学会(JSASS) | |||||
出版者(英) | ||||||
出版者 | Society for Aeronautical and Space Sciences (JSASS) | |||||
書誌情報 |
航空宇宙技術 巻 13, p. 71-75, 発行日 2014-09-27 |
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抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | A solar power sail demonstrator “IKAROS” deployed its square large membrane successfully by centrifugal force. The deployment consisted of two stages. The flight data suggest that the membrane deployment in the second stage was remarkably non-synchronous. This paper reproduces the non-synchronous deployment behavior using a small experimental model deployed in a vacuum chamber. Then, two kinds of finite-element analyses are conducted to show that the effect of membrane creases may have caused the non-synchronous deployment. | |||||
ISSN | ||||||
収録物識別子タイプ | ISSN | |||||
収録物識別子 | 1884-0477 | |||||
DOI | ||||||
識別子タイプ | DOI | |||||
関連識別子 | http://dx.doi.org/10.2322/astj.13.71 | |||||
関連名称 | info:doi/10.2322/astj.13.71 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: PA1510004000 |