The method of firing rockets multiple rocket launchers in a counter-battery fight

摘要

firing method rockets (PC), multiple rocket launchers (MRL) under counterbattery, consisting in bringing the launcher (PU) in a horizontal plane in the direction to the target lift guides with PC by a predetermined starting angle in the vertical plane (VP), inclusion of solid rocket motor is started and PC, followed by the flight predetermined ballistic trajectory, which deviation is eliminated by control of pitch angles and yaw PC via gas-dynamic rudders on commands from a Stem autonomous correction trajectory (saktam) PC, characterized in that before finally starting the PC by a predetermined ballistic trajectory performed PC start initially at a small angle to VI of the initial section of the flight path (TSS) PC, after the settlement PC flight time from the initial portion path whose value is introduced into saktam before starting the PC, PC transfer is performed on a new path with a large angle in the EP, the minimum value of the start angle start PC VI limited specifications PU and rele vom location placement area PU, and the maximum - the terms PC undetected in the initial part of the trajectory radar (RLS) counterbattery (HEC) enemy, then PC flight performed at a predetermined ballistic trajectory simulating launch PC from a fictitious point F, remote from the UE at a safe distance of L, excluding its defeat the enemy artillery fire on the results of radar serifs HEC starting position MLRS, the conjugation of all sections of the trajectory PC flight carried out so that the PC, moving on predetermined ballistic trajectory,