2011 Fiscal Year Final Research Report
A measurement of the nonlinear thermomechanical characteristic and a development of a mathematical model for an ultra-lightweight carbon fiber reinforced plastic
| Project/Area Number |
21360423
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| Research Category |
Grant-in-Aid for Scientific Research (B)
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| Allocation Type | Single-year Grants |
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| Section | 一般 |
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| Research Field |
Aerospace engineering
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| Research Institution | Aichi University of Technology |
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Principal Investigator |
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| Co-Investigator(Kenkyū-buntansha) |
KATO Sumio 琉球大学, 工学部, 教授 (50557105)
SAKAI Takeharu 名古屋大学, 大学院・工学研究科, 准教授 (90323047)
SUZUKI Toshiyuki 宇宙航空研究開発機構, 研究開発本部・未踏技術研究センター, 研究員 (20392839)
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| Project Period (FY) |
2009 – 2011
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| Keywords | 炭素繊維強化プラスチック / CFRP / アブレータ / 高エンタルピ / 宇宙往還 |
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| Research Abstract |
Specific gravity of a heat shield material of several atmosphere reentry capsules which were used for the Hayabusa asteroid probe and the USERS space system is as large as 1.5, it accounted for much of the whole system mass. In this study, we made an ultra-lightweight CFRP which was named the LATS, acquired the nonlinear thermomechanical property of the LATS under several high-temperature environments. Even as for the severe atmosphere reentry environment, the LATS functioned as the heat shield material was shown. It be possible to utilize this LATS for the space industry and the railroad industry and so on, a mathematical model for these industries was developed.
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[Presentation]2009
Author(s)
酒井武治, 冨田昌美, 奥山圭一, 北川一敬, 加藤純郎, 鈴木俊之, 藤田和央
Organizer
宇宙科学術連合講演会
Place of Presentation
京都
Year and Date
20090000
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[Presentation]2009
Author(s)
禹ハンウル, 藤田和央, 鈴木俊之, 高柳大樹
Organizer
宇宙科学術連合講演会
Place of Presentation
京都
Year and Date
20090000
