基于外隔热法的固发烤燃安全性综述  

Safety Survey of Solid Rocket Cook-off Based on External Heat Insulation Method

作　　者：夏成 董可海 赖帅光 陈思彤 王成林 Xia Cheng;Dong Kehai;Lai Shuaiguang;Chen Sitong;Wang Chenglin(Navy Aviation University,Yantai 264000,China;No.92154 Unit of PLA,Yantai 264001,China)

机构地区：[1]海军航空大学,山东烟台264000 [2]中国人民解放军92154部队,山东烟台264001

出　　处：《兵工自动化》2020年第12期12-16,共5页Ordnance Industry Automation

基　　金：武器装备预先研究基金项目(51328050101)。

摘　　要：针对海军固体战术战役导弹高能推进剂在突发性火灾等情况带来的安全性问题,对隔热涂料包括合成树脂以及气凝胶涂料进行探讨。分别对环氧树脂材料、聚氨酯材料和气凝胶材料进行介绍,总结慢速和快速烤燃实验的研究进展,对烤燃实验的数值模拟仿真进行分析,并对未来可用于固体发动机防火隔热的涂料进行展望。该研究对未来该领域的科研生产具有一定的指导意义。In view of the safe problem of navy solid campaign missile high energy propellant when there is sudden fire,discuss heat insulation material including synthetic resin coating and aerogel coating.Separately introduce the epoxy resin material,polyurethane material and aerogel material,summarize the research progress of slow speed and fast speed cook-off test,analyze digital simulation of cut-off test,and look forward to the future coatings that can be used for solid engine fire and heat insulation.This research has certain guiding significance for future scientific research and production in this field.

关 键 词：固体发动机 合成树脂涂料 气凝胶涂料 烤燃实验 烤燃数值模拟 

分 类 号：TJ76.4[兵器科学与技术—武器系统与运用工程]