前言设计一个新的导弹或大改现有的型号,先进的设计方法是按战术技术指标综合论证飞行方案、气动外形、部位安排,以及导弹在无控和有控下的动态性质,使其相互协调,达到最佳设计的目的。在方案论证中,能反映这种相互关联的设计问题的是导弹的动力系数。综合论证的目的之一就是寻求一个新导弹的合理动力系数,使飞行弹道、气动外形、部位安排和控制系统参数达到理想的要求。为此目的,在设计阶段就要不断地调整导弹的外形几何参 Foreword The design of a new missile or a large change to the existing model, the advanced design method is based on tactical and technical indicators of a comprehensive demonstration flight program, aerodynamic shape, part of the arrangement, and the missile under uncontrolled and controlled under the dynamic nature of their mutual Coordination, to achieve the best design. In the program justification, the dynamics of the missiles can be reflected in the inter-related design issues. One of the purposes of the comprehensive argument is to find a reasonable dynamic coefficient of a new missile, so that the flight trajectory, aerodynamic shape, location and control system parameters to achieve the desired requirements. For this purpose, the geometry of the missile must be constantly adjusted during the design phase