A universal vertical launch turning device

Abstract

The invention proposes a universal vertical launch turning device, which includes a device housing, the head of the device housing is provided with two separate motors, and inside the device housing is a pair of coaxial horizontally placed gears with different diameters, each gear contacts one Brake, an electric control group is connected between the two gears; the electric control group is composed 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 installed on the computer terminal; The sensor control module generates an opening and closing control signal of the sensor according to the control instruction, and sends the opening and closing control signal to the generator, and the generator opens and closes to brake the gear after receiving the opening and closing control signal. The invention can not only complete the steering of the missile during the vertical launching process, but also can replace the gas rudder, save extra space, and make the missile body shorter. After the steering is completed, the device is self-thrown to reduce the weight of the missile during the rushing attack, and improve the missile strike and defense capability. ,reduce manufacturing cost.

Description

technical field [0001] The invention relates to the field of missiles, in particular to a throwable device for making a vertical launch turn of a missile. Background technique [0002] The universal vertical launch turning device of the missile is an automatic device that guides the missile to complete the vertical turn and throw it away from the missile body through the preset command control in the vertical state after the missile is launched out of the barrel. At present, the vertical launch and steering technology of missiles used by the military of the United States, Russia, and China is mostly realized by gas rudders. The gas-fired rudder body and the fuel it carries occupy part of the space outside the missile combat unit. Along with the whole process of missile launch and rushing, 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 ...

AI Technical Summary

Problems solved by technology

The gas 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.

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