Space applicability study on carbon reinforced shape memory polymer

Authors :: Ishizawa, Junichiro
Minami, Shintaro
Shimamura, Hiroyuki
Source :: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency. :53-56
Publication Year :: 2006
Publisher :: 宇宙航空研究開発機構, 2006.
Abstract: Carbon fiber reinforced shape memory polymer (FR-SMP) has been developed for space deployable structures as solar paddles, antennas, etc. This material is lightweight, low-cost, and has high workability. We have experimentally proved enough tolerance against space environment for its mechanical and shapes recover property. Deploying test using flat plate models has been revealed that unidirectional reinforced configuration has good shape memory property due to well-balanced rigidity and flexibility. Hemisphere model has been produced through newly-developed FR-SMP dry prepreg.<br />資料番号: AA0049500010<br />レポート番号: JAXA-SP-06-006

Subjects :: 炭素繊維強化樹脂
 large space structure
carbon fiber reinforced plastic
prepreg
aerospace environment
大型宇宙構造物
 composite material
航空宇宙環境
 shape memory polymer
形状記憶ポリマ
 複合材料
 glass transition temperature
プリプレグ
 deployable structure
展開式構造
 ガラス転移温度

Language :: Japanese
ISSN :: 1349113X
Database :: OpenAIRE
Journal :: 宇宙航空研究開発機構特別資料: 平成18年度宇宙航空研究開発機構総合技術研究本部宇宙科学研究本部研究成果報告書 = JAXA Special Publication: Report on Research Achievements for FY2006 Institute of Space and Astronautical Science, Institute of Aerospace Technology, Japan Aerospace Exploration Agency
Accession number :: edsair.jairo.........7d8fcf80a060878f665d14834335ef05

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