@article{oai:muroran-it.repo.nii.ac.jp:00010583,
 author = {SHINTAKU, Kengo and MATUNAGA, Saburo and ONO, Go and SAKAMOTO, Hiraku and 坂本, 啓 and SATOH, Takeshi and MORI, Osamu and SHIRASAWA, Yoji and OKUIZUMI, Nobukatsu and 奥泉, 信克},
 issue = {ists29},
 journal = {TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN},
 month = {},
 note = {application/pdf, The small solar power sail demonstrator IKAROS was developed and launched in 2010 by JAXA and deployed its large membrane successfully. Through IKAROS's on-orbit operation, one of the most critical problems was a sail's shape imbalance during the sail deployment sequence. This paper focuses on the evaluation and consideration of the sail's imbalance through high vacuum experiments using a scale-down sail model. The experimental results obtained using the specially designed rotating mechanism and a small scale model lead to a hypothesis of the reason for the IKAROS's imbalanced deployment. The experimental results are extrapolated up to IKAROS's scale, using dimensionless analyses.},
 pages = {Pc_55--Pc_62},
 title = {Experiment and Analysis of Spinning Membrane Deployment Focusing on Shape Imbalance for Solar Sail},
 volume = {12},
 year = {2014},
 yomi = {サカモト, ヒラク and オクイズミ, ノブカツ}
}