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  1. 学会・会議発表論文
  2. 学会・会議発表用資料

Evaluation of Folding-Pattern Designs for Large-Scale Square Solar Sail

http://hdl.handle.net/10228/0002001098
http://hdl.handle.net/10228/0002001098
47ea722f-2e3b-4447-9aa2-b49be1e470c2
名前 / ファイル ライセンス アクション
10444305.pdf 10444305.pdf (3.9 MB)
アイテムタイプ 会議発表用資料 = Presentation(1)
公開日 2025-01-10
タイトル
タイトル Evaluation of Folding-Pattern Designs for Large-Scale Square Solar Sail
言語 en
著者 Santos Lula Barros, Leticia

× Santos Lula Barros, Leticia

en Santos Lula Barros, Leticia

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平木, 講儒

× 平木, 講儒

en Hiraki, Koju

ja 平木, 講儒


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Miyagawa, Hiroki

× Miyagawa, Hiroki

en Miyagawa, Hiroki

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Esit, Mehmet

× Esit, Mehmet

en Esit, Mehmet

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Chak, Yew-chung

× Chak, Yew-chung

en Chak, Yew-chung

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Varatharajoo, Renuganth

× Varatharajoo, Renuganth

en Varatharajoo, Renuganth

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Fiqri Abdullah, Amirul

× Fiqri Abdullah, Amirul

en Fiqri Abdullah, Amirul

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Dachwald, Bernd

× Dachwald, Bernd

en Dachwald, Bernd

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抄録
内容記述タイプ Abstract
内容記述 Solar sails are an attractive option for a propellant-less propulsion, but only a few missions have been deployed in space so far, such as IKAROS and LightSail 2. To achieve a high characteristic acceleration, a large sail area is required, but it must also be lightweight and robust. Booms can be employed to make the sail stronger, although they are heavier. The solar sail performance can also be impacted by creases. This study looks at the most effective way to fold a long, square solar sail that can be deployed using four booms. Different design ideas were investigated, including the Miura Ori, the Palmer-Shafer flasher, and the IKAROS-inspired parachute folding. The option of partially deploying the sail is taken into account to reduce the sail deformation brought on by SRP while maintaining a high thrust. Other elements, such as the folding height, symmetric deployment and creases, were used to compare the folding processes. Finite Element Analysis (FEA) has been used to compare various folding methods applied to large square sails deployed in space. Finding a sail that is less prone to deformation when partially folded was possible. The Palmer-Shafer flasher fold has been identified as an acceptable folding pattern when comparing features like symmetry, boom deployment, deformation reduction for various support circumstances, and maximum thrust.
言語 en
備考
内容記述タイプ Other
内容記述 34th International Symposium on Space Technology and Science, The 34th ISTS, June 3-9, 2023, Kurume, Fukuoka, Japan
書誌情報
発行日 2023-06
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
出版タイプ
出版タイプ VoR
出版タイプResource http://purl.org/coar/version/c_970fb48d4fbd8a85
会議記述
会議名 International Symposium on Space Technology and Science
回次 34
開始年 2023
開始月 6
開始日 3
終了年 2023
終了月 6
終了日 9
開催国 JPN
査読の有無
値 no
研究者情報
URL https://hyokadb02.jimu.kyutech.ac.jp/html/19_ja.html
item_27_text_28
値 10444305
item_27_text_62
値 12643
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