摘要
测试了碳纤维/环氧复合材料的力学性能,设计并测试了热膨胀系数,然后测试了空间辐射后的材料性能,并研究了在空间光学结构中应用碳纤维/环氧复合材料制品的工艺方法。研究表明:碳纤维/环氧复合材料具有高的比强度和比刚度,较铝合金结构可以减重30%以上;碳纤维/环氧复合材料的热膨胀系数可以根据需要进行设计,在需要的方向上可以设计成"零"或负的热膨胀系数;在空间辐射条件下,碳纤维/环氧复合材料性能良好,其总质量损失为0.15%、可挥发的冷凝物质为7.66×10-5g/g、24 h水汽回吸率为0.12%。结果表明,碳纤维/环氧复合材料具有优良的性能指标,在空间光学结构中有广泛的应用。
The mechanical properties of carbon/epoxy composites and their Coefficient of Thermal Expansion(CTE) were tested and the material property after radiation in space was tested. Finally, a processing method of carbon/epoxy composites in the application of space optical structure was studied. The research results show that the weight of optical structure made from carbon/epoxy composite with high specific strength and stiffness can be reduced more 30% than that of aluminum alloy. The CTE of carbon/epoxy composites can be designed as "zero" or "negative" in a certain direction according to requirement. Carbon/epoxy composites have excellent performances under the condition of radiation in space,so that they have a wide application in space optical structure. The experiments give several conclutions, which is Total Mass Loss(TML) of 0.15 %, Collected Volatile Condensable Materials(CVCM) of 7.66)〈 10^-5 g/g, and Water Vapor Regained(WVR) of 0.12%.
出处
《光学精密工程》
EI
CAS
CSCD
北大核心
2007年第8期1181-1185,共5页
Optics and Precision Engineering
基金
国家863高技术计划资助项目