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1. 概述本文是《全向立体交会导弹-破片-目标运动数学模型及引爆方程》一文的续篇。在文中所建立的 SKS 引爆数学模型(严格说来它是真空条件下的引爆数学模型),对破片速度取了平均值。对于最大脱靶量不大于10米的高精度小型战术导弹来说,由于破片飞越时间很短,破片速度衰减不很明显,且破片平均速度也易于在地面试验中求得,这种职平均值的处理方法,在理论上是允许的,工程设计中也是必要的。但对于那些脱靶量比较大的战
1. Overview This article is a sequel to the article “Omnidirectional Intersection Missile-Fragment-Target Mathematical Model and Detonation Equation.” The SKS detonation mathematical model established in this article (strictly speaking, it is a detonation mathematical model under vacuum conditions) was used to average the fragment velocity. For the high-precision small tactical missiles with a maximum miss distance of not more than 10 meters, the fragment velocity is not attenuated obviously due to the very short flying time and the average fragment velocity can also be easily obtained in the ground test. Processing method, in theory, is allowed, engineering design is also necessary. But for those relatively large off-target war