Research on Construction of Space Structure Systems Using Membrane Structure Modules
Project/Area Number |
23560958
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Research Category |
Grant-in-Aid for Scientific Research (C)
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Allocation Type | Multi-year Fund |
Section | 一般 |
Research Field |
Aerospace engineering
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Research Institution | Waseda University |
Principal Investigator |
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Co-Investigator(Renkei-kenkyūsha) |
YAMAKAWA Hiroshi 早稲田大学, 理工学術院, 教授 (00097263)
KATSUMATA Nobuhisa 室蘭工業大学, もの創造系領域, 助教 (60534948)
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Project Period (FY) |
2011 – 2013
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Project Status |
Completed (Fiscal Year 2013)
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Budget Amount *help |
¥5,330,000 (Direct Cost: ¥4,100,000、Indirect Cost: ¥1,230,000)
Fiscal Year 2013: ¥1,170,000 (Direct Cost: ¥900,000、Indirect Cost: ¥270,000)
Fiscal Year 2012: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000)
Fiscal Year 2011: ¥2,210,000 (Direct Cost: ¥1,700,000、Indirect Cost: ¥510,000)
|
Keywords | 宇宙構造物システム / 展開膜面構造 / 自動構築 / 能動結合要素 / 展開型膜面モジュール / 断続展開 / 振動特性 / 自動組み立てシステム |
Research Abstract |
An approch of construction of space structure systems composed of many homogeneous modules, in which their object final configuration is obtained through the movement of modules in an autonomous and distributed manner, is investigated. Assuming the modules are deployable, the use of active connecting elements having simple functions of release, rotation and latch, is newly proposed, and through the design, manufacturing and testing of their basic conceptual models, it is proven that the basic idea of this research is sufficiently realizable. A simple deployable membrane structure module with booms compatible to the construction approach stated above, which deploy from rolled-up configuration by elastic energy of stowed booms without any actuators, is proposed, and its deployment characteristics are clarified through the model experiment and simulation.
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Report
(4 results)
Research Products
(55 results)
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[Journal Article] IKAROSのセイル展開解析2013
Author(s)
白澤洋次, 宮崎康行, 奥泉信克, 坂本 啓, 森 治, 澤田弘崇, 古谷 寛, 松永三郎, 名取通弘, 津田雄一, 川口淳一郎
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Journal Title
日本航空宇宙学会誌
Volume: Vol.61, No.1
Pages: 14-21
Related Report
Peer Reviewed
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[Journal Article] IKAROSのセイル展開ミッション2012
Author(s)
澤田弘崇, 森治, 奥泉信克, 白澤洋次, 宮崎康行, 名取通弘, 坂本啓, 古谷寛, 松永三郎, 稲川慎一, 木村真一, 津田雄一
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Journal Title
日本航空宇宙学会誌
Volume: Vol.60, No.12
Pages: 429-437
Related Report
Peer Reviewed
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[Presentation] Stepwise Deployment of Membrane Structures with Rolled-up Booms : Experiments and Simulations2014
Author(s)
Okuizumi N., Katsumata N., Kobayashi H., Ikuta H., Yamazaki M., Ito Y., Natori M. C., and Yamakawa H.
Organizer
AIAA Spacecraft Structures Conf., (SciTech2014)
Place of Presentation
National Harbor, Maryland, USA(IAA 2014-1039)
Related Report
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[Presentation] Stepwise Deployment of Membrane Structures with Rolled-up Booms: Experiments and Simulations2014
Author(s)
Okuizumi, N., Katsumata, N., Kobayashi, H., Ikuta, H., Yamazaki, M., Ito, Y., Natori, M.C., and Yamakawa, H.
Organizer
AIAA 2014-1039, AIAA Spacecraft Structures Conf., (SciTech2014)
Place of Presentation
National Harbor, Maryland, USA
Related Report
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[Presentation] Origami-Based Membrane Storage and Deployment Technology for De-orbiting Satellites2013
Author(s)
H. Sakamoto, H. Furuya , Y. Satou, M. C. Natori, A. Watanabe, N. Kawabata, R. Sakai, N. Okuizumi, O. Mori, Y. Shirasawa, M. Takai, N. Katsumata, A. Torisaka and R. Funase
Organizer
64th Int'l. Astronautical Congress
Place of Presentation
Beijing, China(IAC-13-B4.6A.4)
Related Report
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[Presentation] Repeatability of Stored Configuration of a Large Solar Sail with Non-negligible Thickness2013
Author(s)
H. Sakamoto, S. Kadonishi, Y. Satou, H. Furuya, Y. Shirasawa, N. Okuizumi, O. Mori, H. Sawada, J. Matsumoto, M. C. Natori, Y. Miyazaki and M. Okuma
Organizer
54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf.
Place of Presentation
Boston(AIAA 2013-1804)
Related Report
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[Presentation] Repeatability of Stored Configuration of a Large Solar Sail with Non-negligible Thickness2013
Author(s)
H. Sakamoto, S. Kadonishi, Y. Satou, H. Furuya, Y. Shirasawa, N. Okuizumi, O. Mori, H. Sawada, J. Matsumoto, M.C. Natori, Y. Miyazaki and M. Okuma
Organizer
AIAA 2013-1804, 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conf.
Place of Presentation
Boston, USA
Related Report
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[Presentation] Numerical Simulation of Stepwise Deployment of Membrane Structure with Booms Using Multi-Particle Approximation Method2013
Author(s)
Okuizumi, N., Ito, Y., Natori, M., Katsumata, N., Yamakawa, H.
Organizer
ISTS 2013-c-56, 29th Int’l. Symp. Space Technology and Science
Place of Presentation
Nagoya, Japan
Related Report
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[Presentation] Model Study of Membrane Space Structures Based on a Stepwise Deployment Concept2013
Author(s)
Natori, M.C., Katsumata, N., Yamakawa, H., Watanabe, A., Kawabata, N., Okuizumi, N., Mori, O., Shirasawa, Y., Sakamoto, H. and Furuya, H.
Organizer
ISTS 2013-c-55, 29th Int’l. Symp. Space Technology and Science
Place of Presentation
Nagoya, Japan
Related Report
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[Presentation] Origami-Based Membrane Storage and Deployment Technology for De-orbiting Satellites2013
Author(s)
H. Sakamoto, H. Furuya , Y. Satou, M.C. Natori, A. Watanabe, N. Kawabata, R. Sakai, N. Okuizumi, O. Mori, Y. Shirasawa, M. Takai, N. Katsumata, A. Torisaka and R. Funase
Organizer
IAC-13-B4.6A.4, 64th Int’l. Astronautical Congress
Place of Presentation
Beijing, China
Related Report
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