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  5. Energy Dissipation of CFRP-Kevlar Hybrid Composites Shield for Space Use

Energy Dissipation of CFRP-Kevlar Hybrid Composites Shield for Space Use

来源 :第七届亚澳复合材料会议 | 被引量 : 0次 | 上传用户：qiuyuwusheng
【摘 要】
：
In the study, high evergy abosorbing shielding system was studied to protect space crafts from the hypervelocity impact of space debris and micrometeoroids.CFRP-Kevlar hybrid composites were suggested
【作 者】
：
Jin-Bum Moon Gun Lim Chun-Gon Kim Shantanu Bhowmik 
【机 构】
：
Department of Aerospace Engineering,KAIST(Korea Advanced Institute of Science and Technology),Daejeo
【出 处】
：
第七届亚澳复合材料会议
【发表日期】
：
2010年4期
【关键词】
：
composite hypervelocity impact space debris micrometeoroid shielding 
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　　In the study, high evergy abosorbing shielding system was studied to protect space crafts from the hypervelocity impact of space debris and micrometeoroids.CFRP-Kevlar hybrid composites were suggested as a shielding system.It is constituted of two bumper plates and neat Kevlar fabrics inserted in between the two bumper plates.The neat Kevlar fabrics are not constrainted in the planar directions in between CFRP bumper plates.The quasi-isotropically laminated CFRP composite was used as the front bumper plate.CFRP or several poymer plates were used as the rear plate.Each bumper plate has 2mm thickness and 8 plies if Kevlar fabric were inserted.And the total thickness of the shielding system was 6mm.
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