本文总结了 Missile DATCOM计算机程序用于寻常导弹的适用范围和估算精度。文中提到的部件装配法是一种理论的、半经验的与纯经验技术的混合法、它是从一千多种方法的计算数据作了比较,平衡了它们所适用的外形、估算精度和使用成本等项因素后挑选出来的。在用以考核的导弹形状和飞行状态中有百分之八十六证明了用这种方法在初步设计阶段可以得到所要的精度,同时也弄清了预估值与试验值不一致的地方。 This article summarizes the Missile DATCOM computer program for the scope and accuracy of conventional missiles. The component assembly method mentioned in this paper is a hybrid of theoretical, semi-empirical and purely empirical techniques. It compares calculated data from over a thousand methods and balances the shape, accuracy and After using the cost of other factors selected. Eighty-six percent of the missile shape and flight status used for the assessment demonstrated that this method was able to achieve the desired accuracy at the preliminary design stage and that the estimates were inconsistent with the experimental values.