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首页> 外国专利> METHOD FOR TARGET DAMAGE BY SUPERSONIC CRUISE MISSILE AND SUPERSONIC CRUISE MISSILE FOR ITS IMPLEMENTATION

METHOD FOR TARGET DAMAGE BY SUPERSONIC CRUISE MISSILE AND SUPERSONIC CRUISE MISSILE FOR ITS IMPLEMENTATION

机译：超音速巡航导弹的目标损伤方法及超音速巡航导弹的实现

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FIELD: weapon and ammunition.;SUBSTANCE: method includes introduction into the flight control system of a pre-formed flight task containing the missile's flight path and the aiming point, information about the type of target being hit, missile launch and flight to the point with given coordinates while maintaining its supersonic speed. The flight task is formed based on the initial data on target parameters. When the missile reaches the point with the given coordinates, the speed and altitude of flight relative to the target are determined with subsequent determination of the coordinates of the separation point for the elements of additional combat equipment, separation of the additional combat equipment elements at this point, restoration of the aerodynamic contour of the cruise missile, cruise missile stabilization, maintaining of flight until the main goal is reached. The elements of additional combat equipment are stored in separate containers, from which these elements are separated. The missile contains a glider, in the instrument compartment of which blocks of the control system on-board equipment, combat equipment are located. In the front part of the missile, additional combat equipment is installed, consisting of separate elements, made in the form of statically stable modules, placed in separate containers, with a possibility of elements separation from the rocket at the calculated moment of time. In the rear of the containers, plugs are placed with a possibility of longitudinal movement along the container under the action of powder gases and fixation on the missile shell. The front part of the plug is made with a profile similar to the profile of the corresponding part of the aerodynamic circuit of the missile.;EFFECT: combat capabilities and effectiveness in the defeat of dispersed targets are increased, missile controllability is maintained until the target is achieved.;24 cl, 12 dwg
机译：领域：武器和弹药。实质：方法包括将包含导弹的飞行路径和瞄准点的预先形成的飞行任务引入飞行控制系统，有关被击中目标的类型，导弹发射和飞行到该点的信息以给定的坐标，同时保持其超音速。飞行任务是基于目标参数的初始数据形成的。当导弹到达具有给定坐标的点时，确定相对于目标的飞行速度和高度，并随后确定附加作战装备要素的分离点的坐标，在此确定附加作战装备要素的分离关键是，恢复巡航导弹的空气动力学轮廓，稳定巡航导弹，保持飞行直至达到主要目标。附加作战设备的要素存储在单独的容器中，这些要素与它们分开。导弹包含一个滑翔机，在滑翔机的机舱内装有控制系统的机载设备和战斗设备。在导弹的前部，安装了额外的作战设备，这些设备由以静态稳定模块的形式制成的单独元件组成，并放置在单独的容器中，有可能在计算出的时刻将元件与火箭分离。在容器的后部，塞子放置在粉末气体的作用下并可能沿容器纵向移动并固定在导弹壳上。插头的前部轮廓类似于导弹空气动力回路的相应轮廓。;效果：提高了打击能力和击散分散目标的效能，导弹可控性一直保持到目标达到。; 24 cl，12 dwg

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