@inproceedings{oai:jaxa.repo.nii.ac.jp:00013525,
 author = {渡辺, 和樹 and 竹澤, 進 and 渡邊, 秋人 and 関谷, 忠彦 and 山川, 宏 and 角田, 博明 and 樋口, 健 and 泉田, 啓 and Watanabe, Kazuki and Takezawa, Susumu and Watanabe, Akihito and Sekiya, Tadahiko and Yamakawa, Hiroshi and Tsunoda, Hiroaki and Higuchi, Ken and Senda, Kei},
 book = {宇宙利用シンポジウム　第23回　平成18年度, Space Utilization Research: Proceedings of the Twenty-third Space Utilization Symposium},
 month = {Mar},
 note = {One of important issues to be addressed to realize the practical space inflatable structure is how to control the movement during its deployment or extension and how to harden the structure and maintain the accuracy of shape for a long term after extended. To resolve this issue, two types of inflatable structure have been developed by making use of structural rigidizing method. One is to keep stiffness of the structure consistently during and after the extension by the shape recovery of open section tubular member that is called SPINAR (Space Inflatable Actuated Rod to keep here in after). The other is to store the tube made of aluminum/PET laminate material into pentalpha folding to ensure straight-ahead movement during the extension and to be rigidized by work-hardening of structural material after the extension. With those two individual methods, experimental model were developed and evaluated through extension test under the low-gravity environment using the plane, Gulfstream-2 in this study. Meanwhile, in this experiment, a semi-active controlled damper system using Electro Rheological Fluid (ERF) damper was applied., 資料番号: AA0063349027},
 pages = {101--104},
 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 = {衛星搭載用スピン軸方向伸展マストの伸展安定性と制振に関する実験},
 year = {2007}
}