带药缠绕技术在固体火箭发动机中的应用  

Application of the filament-wound with solid propellant technology in solid rocket motor

作　　者：舒慧明[1] 李宝星 王中[1] 古呈辉[1] 朱佳佳[1] SHU Huiming;LI Baoxing;WANG Zhong;GU Chenghui;ZHU Jiajia(Xi'an Modern Chemistry Research Institute,Xi'an 710065,China)

机构地区：[1]西安近代化学研究所,陕西西安710065

出　　处：《中国高新科技》2021年第4期23-24,85,共3页

摘　　要：文章介绍了带药缠绕固体火箭发动机的基本概念、技术特点和国内外研究及应用情况,并分析了带药缠绕固体火箭发动机研发过程中的关键技术。The basic concept,technical characteristics,research and application at home and abroad of filament-wound with solid propellant in solid rocket motor were introduced in this paper,and the key technologies during researching on the filament-wound with solid propellant in solid rocket motor were analyzed.

关 键 词：带药缠绕技术 固体火箭发动机 

分 类 号：TP181[自动化与计算机技术—控制理论与控制工程]