火箭空中点火机构动态延时计算模型研究  

Studieson the Dynamic Delay-Time of a Rocket-Portfire in the Air for a Hybrid Extended-Range Projectile

作　　者：钱建平[1] 赵国志[1] 申屠德忠[1] 郭献安 

机构地区：[1]南京理工大学机械工程学院,江苏南京210094

出　　处：《弹箭与制导学报》2002年第3期52-55,共4页Journal of Projectiles,Rockets,Missiles and Guidance

摘　　要：底排一火箭复合增程弹火箭空中点火延时机构延期时间的控制对于最大限度发挥火箭增程效率有着极其重要的作用。根据“固体粒子”效应理论 ,建立了点火延期管动态燃速数学模型 ,导出了点火延期管动态延时时间计算模型 ,并分析了底排一火箭复合增程弹火箭空中点火延期管的安装位置及其形态对其延期时间的影响。It is very important that the extended range effect is improved farthest by being master of the dynamic delay time of a rocket-portfire in the air. According to the 'solid particle' theory model, a theory model of the dynamic burining velocity of a rocket portfire in its igniting delay time cannulation is established, a theory model of the dynamic delay time is educed. The factors are analyzed, setting position and shape of a igniting delay time cannulation that affect its igniting delay time.

关 键 词：空中点火机构 动态延时 计算模型 底排-火箭复合增程弹 点火延时机构 "固体粒子"效应 

分 类 号：TJ413.4[兵器科学与技术—火炮、自动武器与弹药工程]