Universal vertical launching turning device

Abstract

The invention provides a universal vertical launching turning device which comprises a device shell, wherein two separated engines are arranged at the head of the device shell, a pair of gears which are coaxially and horizontally placed and have different diameters are arranged in the device shell, each gear makes contact with a brake, and an electric control set is connected between the two gears; the electric control set consists of a power supply and a sensor; a wireless receiving module and a sensor control module are integrated on the sensor; an operation module and a wireless transmitting module are mounted on a computer terminal; the sensor control module generates an on-off control signal of the sensor according to a control instruction and sends the on-off control signal to a power generator, and the power generator is started and stopped to brake the gears after receiving the on-off control signal. According to the device, a guided missile can complete steering in a vertical launching process, a gas vane can be replaced, extra space is saved, the missile body is shorter; and after steering is completed, the device is self-thrown to reduce the weight of the guided missile in the attack process, improve the impact and defense capacity of the guided missile and reduce the production cost.

Description

technical field [0001] The invention relates to the field of missiles, in particular to a throwable device for turning missiles vertically. Background technique [0002] The general vertical launching and turning device for missiles refers to the automatic device that makes the missile complete the vertical turning and throws away from the missile body through the control of preset commands in the vertical state after the missile is launched out of the barrel. At present, the missile vertical launch and steering technology used by the military forces of the United States, Russia, and China mostly uses gas rudders. The gas rudder The rudder body and the fuel it carries occupy part of the space outside the missile combat unit. With the whole process of missile launch and attack, the volume and weight of the missile body are redundant, reducing the maneuverability of the missile, and the cost is high. In order to compress the volume of the missile body, reduce the weight of th...

AI Technical Summary

Problems solved by technology

Gas rudder The rudder body and the fuel it carries occupy part of the space outside of the missile combat unit. Accompanied by the whole process of missile launch and attack, the volume and weight of the missile body are redundant, reducing the maneuverability of the missile, and the cost is high

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