高速动能导弹推力速度方案设计  

Dseign of Propulsion and Velocity Scheme for Hypersonic Velocity Kinetic Energy Missile(HVKEM)

作　　者：于剑桥[1] 文仲辉[1] 刘莉[1] 

机构地区：[1]北京理工大学,北京100081

出　　处：《弹箭与制导学报》2003年第S1期134-136,140,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：以高速动能导弹在有效射程范围内命中目标的最小速度要求为约束条件,确定了其可能采取的推力速度方案。针对每一种可能的推力速度方案进行了总体方案的初步设计,通过对设计结果进行对比分析给出了高速动能导弹推力速度方案设计的初步结论。The possible propulsion and velocity schemes of hypersonic velocity kinetic energy missile(HVKEM)are identified based on the minimum speed demand of hitting the target.In accordance with every propulsion and velocity scheme,the possible HVKEM overall schemes are designed and the conclusion of HVKEM propulsion and velocity scheme design is given by comparing the results of overall scheme design.

关 键 词：导弹 高速动能导弹 

分 类 号：TJ760.3[兵器科学与技术—武器系统与运用工程]