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本文提出一种适合于战术导弹在给定运动规律及战术技术要求的条件下.计算所需燃料重量比与推重比的方法.内容包括:计算的前提条件,数学模型建立、近似计算公式的推导及特殊情况下的应用.并通过实例计算结果,评价文中所提出的近似方法的精确度.为战术导弹初步设计阶段提供一种简便而迅速的工程设计方法.对于多种类型战术导弹都具有一定的适用性.
This paper presents a method suitable for calculating the required fuel weight ratio and thrust-to-weight ratio under the conditions of tactical and tactical requirements of the tactical missile, including the preconditions of calculation, the establishment of mathematical models and the derivation of the approximate formula And the application in special cases.And the accuracy of the approximate method proposed in this paper is evaluated through the calculation of examples.It provides a simple and rapid engineering design method for the preliminary design phase of Tactical Missile.It has some advantages for many types of tactical missiles Applicability.