国外战术导弹固体火箭发动机低易损性改进分析  

Improved Analysis of Low Vulnerability of Solid Rocket Motor for the Foreign Tactical Missile

作　　者：李记威 王君祺[1] 曹军伟[1] 张泽远[1] LI Jiwei;WANG Junqi;CAO Junwei;ZHANG Zeyuan(China Airborne Missile Academy,Henan Luoyang 471009,China)

机构地区：[1]中国空空导弹研究院,河南洛阳471009

出　　处：《弹箭与制导学报》2017年第6期72-78,共7页Journal of Projectiles,Rockets,Missiles and Guidance

基　　金：国家自然科学基金(11402283);中国空空导弹研究院科技创新基金(201604S03)资助。

摘　　要：战术导弹固体发动机低易损性改进对人员及财产具有重要的意义,近年来成为一种重要发展方向。欧美等国家经过近50年的发展,已经形成了较为完备的试验标准和评估方法,积累了大量的低易损改进经验。文中通过对国外低易损试验标准及评估的发展过程、固体发动机低易损性改进进展以及低易损试验进行分析,为国内战术导弹固体发动机低易损性改进提供了参考。The low vulnerability improvement of tactical missile solid motor is of great significance to personnel and property.And it has become an important development direction in recent years.After 50 years evolution,Europe and the United States have formed relatively complete test standards and assessment methods,and accumulated a lot of experience in the improvement of low vulnerability.This article provides a reference for the low vulnerability improvement of domestic tactical missile solid engine,by analyzing the development process of the foreign low vulnerability test standard and criterion,progress in low vulnerability improvement of solid rocket motor and low vulnerability test.

关 键 词：战术导弹 固体火箭发动机 钝感弹药 低易损性 

分 类 号：V435[航空宇航科学与技术—航空宇航推进理论与工程]