宇航材料工艺2012，Vol.42Issue(2)：54-57,4.
树脂基防热材料长时间烧蚀后的变形问题
Distortion of Resin Matrix of Thermal Protection Composites After Long Time Ablation
张宗强 1匡松连 1缪长礼 1尚龙1
作者信息
- 1. 航天材料及工艺研究所,先进功能复合材料技术重点实验室,北京100076
- 折叠
摘要
Abstract
This paper analyzed the causation of distortion of resin composites after long time ablation. And studied the property of the quartz fiber reinforced phenolic resin at different temperature. It is shown that the thermal stress is the dominating reason causing the distortion of resin composites after long time ablation.关键词
树脂基防热材料/长时间烧蚀/变形Key words
Resin matric thermal protection composites/ Long time ablation/ Distortion引用本文复制引用
张宗强,匡松连,缪长礼,尚龙..树脂基防热材料长时间烧蚀后的变形问题[J].宇航材料工艺,2012,42(2):54-57,4.
