This paper describes the experimental assessment of gas permeability of carbon fiber/toughened epoxy laminates under cyclic loadings as a fundamental research for the development of composite cryogenic propellant tank for reusable space transportation system. A thin-ply technique, which may contribute to the enhancement of damage resistance of CFRP laminates, is introduced herein, and the damage accumulation behaviors and gas permeability are compared between thin-ply laminates and standard laminates subjected to cyclic tension and impact.
CITATION STYLE
YOKOZEKI, T., KURODA, A., YOSHIMURA, A., OGASAWARA, T., & AOKI, T. (2010). Evaluation of Gas Permeability of CFRP Laminates under Cyclic Loadings. TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, AEROSPACE TECHNOLOGY JAPAN, 8(ists27), Pc_5-Pc_9. https://doi.org/10.2322/tastj.8.pc_5
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