FIELD: weapons.
SUBSTANCE: invention concerns military technics. The device contains the power supply, an electro detonator which is a part of the device of liquidation, the first trajectory gauge, a control unit, the device of switching of the condition, the second and the third trajectory gauges, the input line and the control line. The power supply exit is connected to a control unit input, the input line and which exit is connected to the first input of the device of switching of a condition is connected to an operating which input. The operating input of the device of switching of a condition is connected to the control line, the second input - through consistently connected trajectory gauges to a power supply output. The first output of the device of switching of a condition is connected to an input of the trajectory gauge which output is connected to the second exit of the device of switching of a condition and an input of the electro detonator which is a part of the device of liquidation.
EFFECT: maintenance of self-liquidation of a rocket both at regular, and at supernumerary start-up.
1 dwg
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