宇航材料工艺2017，Vol.47Issue(2)：1-4,13,5.DOI:10.12044/j.issn.1007-2330.2017.02.001
固体火箭发动机喷管用树脂基烧蚀防热材料研究进展
Progress of Ablative Polymer Composite for Solid Rocket Motor Nozzle
梁瑜 1郭亚林 1张祎1
作者信息
- 1. 西安航天复合材料研究所,西安710025
- 折叠
摘要
Abstract
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).关键词
树脂基烧蚀防热材料/固体火箭发动机/喷管Key words
Ablative polymer composites/Solid rocket motor/Nozzle分类
通用工业技术引用本文复制引用
梁瑜,郭亚林,张祎..固体火箭发动机喷管用树脂基烧蚀防热材料研究进展[J].宇航材料工艺,2017,47(2):1-4,13,5.
