@inproceedings{oai:jaxa.repo.nii.ac.jp:00007721,
 author = {松永, 三郎 and 森, 治 and 中谷, 幸司 and 居相, 政史 and 尾曲, 邦之 and 矢部, 秀幸 and Matsunaga, Saburo and Mori, Osamu and Nakaya, Koji and Iai, Masafumi and Omagari, Kuniyuki and Yabe, Hideyuki},
 book = {平成15年度アストロダイナミクスシンポジウム:講演後刷り集, ISAS Proceedings of 13th Workshop on Astrodynamics and Flight Mechanics 2003: A Collection of Technical Papers},
 month = {Feb},
 note = {In this paper, proposed is one membrane deployment method: tether-controlled spinning deployment. Very large, thin and flexible membrane (sail) is packed and then is deployed in orbit. In the process of membrane deployment, controlled tethers are used to stably deploy the membrane. Some types of the system are proposed, and the characteristics and technical issues are briefly mentioned. Numerical simulation results using a distributed mass-tether network model show the potential advantage of the proposed method. An experimental set-up of the proposed deployment using the two-dimensional microgravity simulators developed at Tokyo Institute of Technology is introduced, and the result of preliminary deployment experiments with a thin membrane of 1 m-sized is shown., 資料番号: AA0046652020},
 pages = {124--129},
 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 = {Initial investigation on deployment and control of tether-controlled spinning membrane},
 year = {2004}
}