@inproceedings{oai:jaxa.repo.nii.ac.jp:00007477,
 author = {森, 治 and 澤田, 弘崇 and 津田, 雄一 and 船瀬, 龍 and 川口, 淳一郎 and 花岡, 史紀 and 松本, 道弘 and 岡田, 俊輔 and 芝崎, 裕介 and 白澤, 洋次 and Mori, Osamu and Sawada, Hirotaka and Tsuda, Yuichi and Funase, Ryu and Kawaguchi, Junichiro and Hanaoka, Fuminori and Matsumoto, Michihiro and Okada, Shunsuke and Shibasaki, Yusuke and Shirasawa, Yoji},
 book = {第17回アストロダイナミクスシンポジウム講演後刷り集　2007, Proceedings of 17th Workshop on JAXA Astrodynamics and Flight Mechanics},
 month = {Mar},
 note = {JAXAでは、深宇宙探査のための新しい推進機関として、ソーラー電力セイルを検討している。本論文では、小型ソーラー電力セイル実証機の膜面形状・配置、展開方式・手順・機構を提案する。また、多粒子モデルを用いた数値シミュレーションにより展開挙動を明らかにし、展開の実現性を示す。, JAXA is studying solar power sail as a new propulsion engine for deep space explorations. In this paper, the sail shape and equipment layout for small-sized solar power sail mission are proposed. The deployment method, sequence and mechanism are also introduced. The deployment motions are analyzed by numerical simulations using multi-particle models in order to verify the deployment., 資料番号: AA0063718040},
 pages = {245--250},
 publisher = {宇宙航空研究開発機構宇宙科学研究本部, Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency (JAXA/ISAS)},
 title = {Deployment demonstration of supersized membrane for spinning solar sail},
 year = {2008}
}