基于燃速的助推段固体弹道导弹红外特性分析  

Analysis of infrared radiation characteristics of solid ballistic missile in boosting phase based on burning rate

作　　者：王建华[1] 李小将[2] 王志恒[1] 张东来[1] 

机构地区：[1]解放军装备学院研究生管理大队,北京101416 [2]解放军装备学院航天装备系,北京101416

出　　处：《激光与红外》2012年第10期1154-1160,共7页Laser & Infrared

摘　　要：速燃助推作为应对红外预警卫星的有效手段,直接关系导弹防御系统的作战效能。论述了预警卫星工作原理,总结了速燃助推技术,建立了发动机喷管出口温度、导弹蒙皮温度和导弹尾焰温度特性与发动机燃速的数学模型,采用定量与定性相结合的方式仿真分析了助推段固体弹道导弹的红外特性与燃速的关系,探讨了速燃条件下减小导弹红外辐射特性的有效措施。As an effective technique against the infrared warning satellite, fast boosted missile directly affects the effi ciency of the ballistic missile defense system. This paper analyzes the feasibility of the fast burning boosting way, dem onstrates the penetration principle for fast burning against the infrared warning satellite, explores the elements that de termine the infrared radiation properties of boost phase missile, builds the mathematic models of the temperature of the motor spout, temperature of the missile skin and temperature of the missile exhaust plume, analyzes the relations be tween the missile＇s infrared radiation and burning rate using both quantitative and qualitative methods, explores the ef ficient methods that may decrease the missile＇s infrared radiation properties.

关 键 词：速燃助推 燃速 红外特性 固体导弹 

分 类 号：TJ7[兵器科学与技术—武器系统与运用工程]