复合固体推进剂静电危险性研究进展  

Review on Electrostatic Hazards of Composite Solid Propellant

作　　者：鲍桐[1] 张炜[1] 

机构地区：[1]国防科技大学航天与材料工程学院,湖南长沙410073

出　　处：《含能材料》2010年第4期460-466,共7页Chinese Journal of Energetic Materials

基　　金：国家安全重大基础研究课题子专题(批准号:61337030301)

摘　　要：从复合固体推进剂静电危险性实验测试方法、理论预估和静电对推进剂的作用机理等三方面,综述了国内外固体推进剂静电危险性研究的进展。国外使用有关设备测量实际作用于推进剂试样上的静电能量作为静电感度评价标准;"渗透系数"模型可实现对推进剂静电危险性的简单预估,基于热点形成发展的计算模型建立了推进剂的静电危险性与推进剂力学、燃烧性能之间的联系;利用红外测温方法,观察到了静电作用过程中热辐射和热传导,形成了广为接受的"热点"形成机理。国内尚需加强复合固体推进剂静电危险性的系统研究,形成可靠的复合固体推进剂静电危险性评价方法。The progress in research on electrostatic hazards of composite solid propellant was summarized in three aspects,which are experimental testing method,theoretical prediction and electrostatic effect mechanism.Researchers used special equipments to measure the electrostatic energy acted on the sample indeed.This energy was the criterion of electrostatic sensitivity.The percolation coefficient was used as a simple prediction of electrostatic hazard,and the model based on hot spots forming growth was used to predict the electrostatic hazard with the characters of propellant itself,such as mechanical,burning characters.Based on temperature measured by infrared method and observation heat radiation and transfer caused by electrostatic energy,the popularly accepted ＂hot spot＂ mechanism were outlined.

关 键 词：物理化学 复合固体推进剂 静电危险性 

分 类 号：V512[航空宇航科学与技术—航空宇航推进理论与工程]