摘要
针对具有良好应用前景的热塑性树脂基复合材料,调研并分析了国外飞行试验获得的数据,从原子氧反应率、力学性能退化、微裂纹等多个方面分析研究了原子氧环境对热塑性树脂基复合材料作用效应,为空间站等低轨道航天器结构材料的设计和选择提供依据。
As the thermoplastic composites （TPCM） are promising for future application, the AO effects on TPCM were discussed in this paper based on the data from flight experiments in foreign countries in aspects of AO erosion rate, mechanical performance degradation, microcracks, etc, so as to provide a reference for material selection and design of low-orbit spacecrafts such space stations in the future.
出处
《装备环境工程》
CAS
2015年第3期64-69,共6页
Equipment Environmental Engineering
关键词
原子氧
热塑性树脂
复合材料
飞行试验
性能退化
atomic oxygen
thermoplastic resin
composite materials
flight experiment
property degradation
