碳(石墨)/环氧复合材料及其在航天器上应用研究进展  

Application of Carbon(grphite) Fiber/Epoxy Composites in the Spacecraft and the Research on Their Behaviors

作　　者：姜利祥[1] 何世禹[1] 杨士勤[1] 陈平[2] 盛磊[2] 

机构地区：[1]哈尔滨工业大学空间材料与环境工程实验室,哈尔滨150006 [2]中国空间技术研究院第508研究所,北京100076

出　　处：《材料工程》2001年第9期39-43,46,共6页Journal of Materials Engineering

摘　　要：综述了空间环境因素的特征及其效应 ,包括太阳电磁辐射、带电粒子辐射、空间真空效应、冷黑环境、原子氧侵蚀、微流星和空间碎片的撞击。碳 (石墨 )纤维、环氧树脂、碳 (石墨 ) /环氧复合材料的性能以及碳 (石墨 )Characters and effects of the space environment factors including solar electromagnetic radiation, charged particles radiation, vacuum circumstance, cold dark condition, erosion of atomic oxygen, micro meteor and impact of space fragment were introduced Properties of carbon (graphite) fiber/epoxy matrix composites were summarized Application and research of design and manufacture for spacecraft of these materials were reviewed

关 键 词：空间环境因素 复合材料 航天器 碳 石墨 环氧树脂 碳纤维 

分 类 号：V258[一般工业技术—材料科学与工程] TB332[航空宇航科学与技术—航空宇航制造工程]