摘要
对于载机机动环境中顺序离轨分离的空空导弹,导弹发射中在轨段弹架分离涉及导弹发动机和载机安全,其分离安全分析是导弹结构强度设计中必须解决的关键技术问题。本文采用MSC.Dytran软件,对导弹的轨上运动过程以及导弹结构动力强度进行了系统建模和仿真分析,为导弹发射中在轨段分离安全提供了一种有效的解决途径。
The air-to-air missile on maneuvering carrier aircraft launched from orbit by order, the separation involves missile engine and vehicle safeties.The separation security analysis is a key technique must be solved during the design of missile structure strength.In this paper, using MSC.DYTRAN soft-ware, the movement process of missiles on the track and dynamic strength are analyzed in system modeling and simulation, and this provides an effective solution for separating security of missile launch in orbit pe-riod.
出处
《航空兵器》
2014年第6期23-27,共5页
Aero Weaponry
关键词
空空导弹
载机
在轨段
分离安全
结构动力强度
air-to-air missile
carrier aircraft
in orbit
separation security
structural dynamic strength
