@article{oai:muroran-it.repo.nii.ac.jp:00008597,
 author = {NATORI, M.   C. and 名取, 通弘 and SAKAMOTO, Hiraku and 坂本, 啓 and 勝又,  暢久 and KATSUMATA, Nobuhisa and YAMAKAWA, Hiroshi and 山川, 宏 and KISHIMOTO,  Naoko and 岸本, 直子},
 issue = {1},
 journal = {Mechanical Engineering Reviews},
 month = {},
 note = {application/pdf, This paper discusses what has been found and what will be found using conceptual “origami” models to develop deployable space structures. The study covers the following: (i) one-dimensional structural elements, which are axially buckled inflatable tubes; (ii) two-dimensional elements, which are deployable membranes, such as solar arrays and solar sails; and (iii) deployable elements in nature. The study clarifies what design considerations are necessary to adapt the basic concepts to actual space structural hardware, and several limitations of origami models are discussed. Regarding the last subject, this study envisions future space structures using conceptual origami models that imitate three-dimensional deployable structures in nature, such as flowers and insect wings.},
 pages = {1--15},
 title = {Conceptual model study using origami for membrane space structures : a perspective of origami-based engineering},
 volume = {2},
 year = {2015},
 yomi = {ナトリ, ミチヒロ and サカモト, ヒラク and カツマタ, ノブヒサ and ヤマカワ, ヒロシ and キシモト, ナオコ}
}