摘要
根据高速动能导弹动力系统的特点,以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,建立了起飞质量优化设计的数学模型,给出了此模型对高速动能导弹起飞质量进行优化设计的初步结果。
A group of mathematical models for Hypersonic Velocity Kinetic Energy Missile (HVKEM)take-off mass design is established based on the characteristics of propulsion system and the minimum speed demand of bitting the target.An initial design result of HVKEM take-off mass is given by using the mathematical models.
出处
《弹箭与制导学报》
CSCD
北大核心
2003年第S5期101-102,108,共3页
Journal of Projectiles,Rockets,Missiles and Guidance
关键词
导弹
高速动能导弹
起飞质量
missile
hypersonic velocity kinetic energy missile
take-off mass
