FIELD: blasting operations.
SUBSTANCE: method and system are designed to control the launch and explosion of missiles. In the present invention, the power supply, communication and control of the igniters of the engine and the missile explosion are provided through the wire lines of the gun and projectile unit with a contact device between them. Before launching the missile, through communication lines with a direct current voltage of a given level, the energy storage device and the power supply of the missile devices are charged. Using the magnitude of the direct current flowing via the communication lines, the serviceability of the engine igniter and the igniter of the explosion is established. Before launching the missile, via communication lines using AC signals, information is received on the type of missile and the value of the delay time of the missile explosion after its start is entered into the program device. When the missile is launched through a non-linear device with a voltage exceeding a predetermined level, the igniter of the rocket engine is triggered. Also, the power supply of the missile devices after its launch is carried out from the energy storage device. And the firing of the missile explosion igniter takes place after the explosion lag time that is preset in the program device has elapsed.
EFFECT: invention makes it possible to improve the efficiency of launch and explosion control.
2 cl, 1 dwg
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Authors
Dates
2018-10-17—Published
2015-06-10—Filed