摘要
给出近程战述地地导弹弹道／团体火箭发动机一体化优化设计的数学模型、设计方法与数值优化算法等。并针对某地地导弹，作了大量的弹道仿真，得到了弹道与发动机的最优匹配，使起飞总重明显下降。
The mathematical model. design method and optimal simulation algorthms are studied for a tactical missile ballistics/solid propellant rosket engine. A large amount of numerical simulations have been done for a tactical missile.The optimal matching of ballistics and solid propellant rocket engine is obtained to descend total takeoff weight of the missile.
出处
《弹道学报》
CSCD
1995年第1期1-6,共6页
Journal of Ballistics
关键词
面对面导弹
飞行弹道
火箭发动机
一体化设计
ground-to-ground tactical missile, ballistics, solid propellant rocket engine, optimal design, numerical simulation
