MISC

2011年1月27日

A3 「IKAROS」のセイル膜展開挙動の予測・検証法について(IKAROS)

スペース・エンジニアリング・コンファレンス講演論文集 : Space Engineering Conference
  • 宮崎 康行
  • ,
  • 白澤 洋次
  • ,
  • 澤田 弘崇
  • ,
  • 森 治
  • ,
  • IKAROS構造専門部会

2010
19
開始ページ
"A3
終了ページ
1"-"A3-6"
記述言語
日本語
掲載種別
出版者・発行元
一般社団法人日本機械学会

Japanese spin-type solar power sail IKAROS was launched in May 21st 2010 by JAXA, and the 20m-sized sail membrane was successfully deployed in June 2010. The deployment was achieved through two stages. In the first stage, a part of the membrane is unwrapped quasi-statically from the cylindrical spacecraft. In the second stage, the whole membrane is deployed dynamically from the spacecraft. During the design and development process of the sail membrane structure in last three years, the numerical simulation of the deployment dynamics had been one of the most important issues. In this paper, the pre-flight prediction of the deployment behavior in the second stage is summarized, and the flight data is compared with the numerical simulation.

リンク情報
CiNii Articles
http://ci.nii.ac.jp/naid/110008743757
CiNii Books
http://ci.nii.ac.jp/ncid/AA1190222X
ID情報
  • ISSN : 0918-9238
  • CiNii Articles ID : 110008743757
  • CiNii Books ID : AA1190222X

エクスポート
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