摘要
以M40石墨纤维为增强材料与环氧648-三氟化硼单乙胺为树脂基体材料组成的M40/环氧648复合材料,已成为我国应用卫星结构的主要材料之一。文中通过对其单向板工程常数测定,着重对M40/环氧648准各向同性层板的力学性能进行了分析和讨论。
M40/epoxy 648 composite materials with epoxy 648 boron tri-fluoride monoethylamine as resin matrix material reinforced by M40 graphite fiber has become one of the Principal construction materials widely used in China's applications satellites.The paper analyzes and discusses emphatically the mechanical behavior of M40/epoxy 648 quasi-isotiopic laminates based on the measurements of engineering conrt-ants of monodirectional laminates.
出处
《航天返回与遥感》
1995年第4期45-51,共7页
Spacecraft Recovery & Remote Sensing
