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.
出处
《激光与红外》
CAS
CSCD
北大核心
2012年第10期1154-1160,共7页
Laser & Infrared
关键词
速燃助推
燃速
红外特性
固体导弹
fast boost
burning rate
infrared properties
solid ballistic missile
