FIELD: physics.
SUBSTANCE: invention is intended to control the launch and explosion of a missile. Launch and explosion control system includes a receiving circuit with a communication line. It is located at the head of the missile. There is also an explosion unit with a missile igniter, a power unit and an energy storage device. According to the invention, the communication line is made in the form of a wire line. It provides the ability to enter a flight task, obtain information about the type of missile, the power supply of the missile assemblies and the launch of engine thereof. Communication line contains a control board and a software device for timing. System also contains an additional energy storage device and a centrifugal connector. This connector is made with the possibility of closing contacts thereof during rotation of the missile after launch thereof. Connector input is connected to the energy store. Output of the connector is connected to an additional energy storage device. Additional energy storage device is made with the possibility of obtaining and storing a part of direct current energy from the energy storage device and expenditure thereof for powering missile assemblies in flight and ensuring the charge necessary to control the explosion. Output of the additional energy storage device is associated with a software device and a key device, the latter of which provides an explosion after a time reference by the software device.
EFFECT: technical result is an increase in the safety of launch and explosion of a missile.
1 cl, 1 dwg
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Authors
Dates
2019-04-19—Published
2016-02-09—Filed