首页 | 本学科首页   官方微博 | 高级检索  
     

空空导弹发射在轨段分离安全性研究
引用本文:张鹏,王文博,韩景龙.空空导弹发射在轨段分离安全性研究[J].航空兵器,2014(6):23-27.
作者姓名:张鹏  王文博  韩景龙
作者单位:1. 中国空空导弹研究院,河南洛阳,471009
2. 南京航空航天大学,南京,210016
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。

关 键 词:空空导弹  载机  在轨段  分离安全  结构动力强度

Study on Separation Safety of Air-to-Air Missile Launch in Orbit Period
ZHANG Peng,WANG Wen-bo,HAN Jing-long.Study on Separation Safety of Air-to-Air Missile Launch in Orbit Period[J].Aero Weaponry,2014(6):23-27.
Authors:ZHANG Peng  WANG Wen-bo  HAN Jing-long
Affiliation:ZHANG Peng, WANG Wen-bo, HAN Jing-long (1. China Airborne Missile Academy, Luoyang 471009, China; 2. Nanjing University of Aeronautics and Astronautics, Nanjing 210016,China)
Abstract: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.
Keywords:air-to-air missile  carrier aircraft  in orbit  separation security  structural dynamic strength
本文献已被 维普 万方数据 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号