摘要
本文提出了固体火箭发动机壳体用树脂基体的选择原则 ,并分别阐明了增韧和耐高温环氧树脂基体的研究成果及动态 。
This paper gives the guiding principle for resin matrices selection for solid rocket motor case.This paper shows the achievements in researches on epoxy resin matrices with high-temperature resistance and good toughness,point out the way forward for further improvement on related subject.
出处
《纤维复合材料》
CAS
2000年第1期54-56,45,共4页
Fiber Composites
