%0 Journal Article %T 固体火箭发动机喷管用树脂基烧蚀防热材料研究进展 %T Progress of Ablative Polymer Composite for Solid Rocket Motor Nozzle %A 梁瑜 %A 郭亚林 %A 张祎 %A LIANG,Yu %A GUO,Yalin %A ZHANG,Yi %J 宇航材料工艺 %J Aerospace Materials & Technology %@ 1007-2330 %V 47 %N 2 %D 2017 %P 1-4,13 %K 树脂基烧蚀防热材料;固体火箭发动机;喷管 %K Ablative polymer composites;Solid rocket motor;Nozzle %X 从材料和成型两个方面介绍了树脂基烧蚀防热材料的研究进展情况。主要包括基体材料、增强材料,以及模压、缠绕、铺放与RTM成型工艺的研究情况。 %X The progress of materials and processings for ablative polymer composite is introduced in this paper. The materials include ablation-resistant matrix resins and reinforcement, the processings include die moldings, tape wraps, layups and resin transfer moldings (RTM). %R 10.12044/j.issn.1007-2330.2017.02.001 %U http://www.yhclgy.com/yhclgy/home %1 JIS Version 3.0.0