摘要
描述了超声速导弹弹体的热环境 ,高温树脂基复合材料基体候选树脂 ,重点介绍了双马来酰亚胺、聚酰亚胺树脂和氰酸酯的性能及最新进展 。
Some high temperature resistant composites with resin matrixes of bismaleimide(BMI), polyimide(PI) resins and cyanate ester(CE) for supersonic air intercept missile (AIM) airframes are introduced.Applications of the composites to supersonic missile airframes are reviewed, and their properties and latest development are presented with emphases.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
2002年第5期15-19,共5页
Aerospace Materials & Technology
关键词
树脂基复合材料
超声速导弹
双马来酰亚胺
聚酰亚胺树脂
氰酸酯
材料性能
Missile airframe, Resin matrix composite, Supersonic missile, Bismaleimide(BMI), Polyimide(PI) resin, Cyanate ester(CE)
