FIELD: weapons and ammunition.
SUBSTANCE: fighting compartment carrier is turned until the axis of the vertically installed shot matches loading plane. Then the launcher gun and shot are turned with the help of a motor branch of a vertical homing mechanism and a drive of shot inclination at a loading angle to ensure shot gripping with the help of the loading device and additional forwarding of the shot into a channel of the launcher gun barrel. Then the launcher gun is stopped at the loading angle with the help of a motor branch of the vertical homing mechanism with the enabled arming stabiliser. The loading system of the launcher gun comprises a rotary carrier with a position sensor, a loading device, a control panel with a unit of automatics, a unit of stabiliser control, a mechanism of vertical homing of the launcher gun with motor and manual branches and a position sensor, a mechanism of launcher gun stopping. According to the first version of realisation of the system, the first inlet of the power amplifier is connected to the outlet of the stabiliser control unit, the second inlet - with the outlet of the automatics unit, the first inlet of the electromagnetic coupling is connected to the outlet of the electric drive, and the second inlet - to the unit of automatics. According to the second version of the system realisation the mechanism of vertical homing of launcher gun comprises an electric drive with an electromagnetic coupling and a power amplifier. The first inlet of the power amplifier is connected to the outlet of the stabiliser control unit, the second inlet - with the outlet of the automatics unit, and the third inlet - to the outlet of the position sensor of the launcher gun and the third inlet of the electromagnetic coupling, the first inlet of which is connected to the outlet of the electric drive, and the second inlet - to the unit of automatics.
EFFECT: reduced time required to prepare a launcher gun for firing and increased reliability of loading system operation.
3 cl, 2 dwg
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