| Project/Area Number |
23760654
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| Research Category |
Grant-in-Aid for Young Scientists (B)
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| Allocation Type | Multi-year Fund |
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| Research Field |
Composite materials/Physical properties
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| Research Institution | Gifu University |
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Principal Investigator |
OHTANI Akio 岐阜大学, 複合材料研究センター, 特任准教授 (80569533)
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| Research Collaborator |
NAKAI Asami 岐阜大学, 工学部機械システム工学科, 教授 (10324724)
GOTO Ken 宇宙航空研究開発機構, 宇宙科学研究所, 准教授 (40300701)
KITAMURA Masayuki 北陸ファイバーグラス株式会社, 代表取締役
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| Project Period (FY) |
2011 – 2012
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| Project Status |
Completed (Fiscal Year 2012)
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| Budget Amount *help |
¥3,770,000 (Direct Cost: ¥2,900,000、Indirect Cost: ¥870,000)
Fiscal Year 2012: ¥1,820,000 (Direct Cost: ¥1,400,000、Indirect Cost: ¥420,000)
Fiscal Year 2011: ¥1,950,000 (Direct Cost: ¥1,500,000、Indirect Cost: ¥450,000)
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| Keywords | 断熱構造部材 / 繊維強化複合材料 / 発泡成形 / 長繊維強化 / 複合材料 / アブレーター / 3次元強化基材 / 発泡含浸 / 製編技術 |
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| Research Abstract |
In this study, in order to reduce weight of CFRP nozzle liner for solid rocket motors, reinforcements with 3D carbon fiber structure and new foamed resin impregnation method were examined. Several kinds of process condition were examined through the bending test, measurement of thermal conductivities, and erosion test. Finally better fabrication method for light weight nozzle liner could be established.
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