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Location of Guided-Pin in Retraction Mechanisms for Large Deployable Space Membrane
https://jaxa.repo.nii.ac.jp/records/7249
https://jaxa.repo.nii.ac.jp/records/72499986eb3d-2a87-4846-8a08-80387447d451
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 | ||||||
言語 | en | |||||
タイトル | Location of Guided-Pin in Retraction Mechanisms for Large Deployable Space Membrane | |||||
言語 | ||||||
言語 | eng | |||||
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 | ||||||
その他のタイトル | ガイドピンを用いた宇宙用大型膜収納機構におけるガイドピン配置の検討 | |||||
著者 |
佐藤, 泰貴
× 佐藤, 泰貴× 古谷, 寛× Sato, Yasutaka× Furuya, Hiroshi |
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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(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
著者所属(英) | ||||||
en | ||||||
Tokyo Institute of Technology | ||||||
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 |
アストロダイナミクスシンポジウム講演後刷り集 en : The 20th Workshop on JAXA Astrodynamics and Flight Mechanics 巻 20, p. 7-12, 発行日 2011-03 |
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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 | 第20回アストロダイナミクスシンポジウム (2010年7月26-27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 | the 20th Workshop on JAXA Astrodynamics and Flight Mechanics 2010 (July 26-27, 2010. Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA)(ISAS)), Sagamihara, Kanagawa Japan | |||||
抄録 | ||||||
内容記述タイプ | Abstract | |||||
内容記述 | 摘要: ソーラーセイル等の超大型膜を地上で簡易に折り畳むため,著者らは膜に折り目を形成させるガイドピンを用いた収納機構を提案してきた.提案した収納機構を用いて収納実験を行った結果,ガイドピンに対する膜の滑りが観察され,この滑りはガイドピン配置に依存することが示された.本研究では,収納機構を用いる際の折り畳みの精度を向上させるため,膜が滑る現象を一次元モデルを用いて表現し,滑りが生じにくいガイドピンの配置条件を明らかにする. | |||||
抄録(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Guided-pin location of retraction mechanisms is examined to improve the fold precision of a large deployable space membrane. The guided-pin, which is introduced to the retraction mechanisms, generates the fold lines on the membrane. The retraction experiments with the guided-pins are performed to investigate the fold precision. In the course of the retraction, the fold precision is interfered by the slips between the guided-pin and the membrane. To investigate the non-slip condition, the mechanics of the slip is examined introducing a one-dimensional slip model for the guided-pin location. Finally, the non-slip condition, which is derived with the slip model, is evaluated by the results of the retraction experiments. | |||||
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(英) | ||||||
内容記述タイプ | Other | |||||
内容記述 | Physical characteristics: Original contains color illustrations | |||||
書誌レコードID | ||||||
収録物識別子タイプ | NCID | |||||
収録物識別子 | AA11567475 | |||||
資料番号 | ||||||
内容記述タイプ | Other | |||||
内容記述 | 資料番号: AA0065115002 |