摘要
论述了火箭质量偏心所引起的初始扰动和等效起始扰动及其对火箭弹道性能的影响,推导了最大限度地减小其引起火箭散布的弹道控制条件,为火箭武器系统总体设计提供了依据.
This paper expounds the initial and equivalent disturbances respectively caused bythe rocket mass malalignment,and their effect on the ballistic performances of rocket.Theballistic control conditions which most magnificently reduce the dispersion of rocket caused bythe mass malalignment are derived.It also provides a kind of basis for the general design ofrocket weapon system.
出处
《弹道学报》
EI
CSCD
1992年第4期33-35,共3页
Journal of Ballistics
关键词
弹道学
弹道设计
火箭
发射装置
起始扰动
ballistics
ballistic design
rocket
launcher
initial disturbance