FIELD: rocketry.
SUBSTANCE: multipurpose missile system comprises a carrier with a right and left guidance devices with lifting and rotary parts, while lifting parts have instruments with guiding channels, guides with two guided missiles, drives for transfer into combat and traveling position, weapons control device. Rotary parts are made so as to ensure limitation of rotation angles, depending on the length of the interval between axes of rotary parts, the length of the radius from the rotary part to the most remote points of the guided missile and minimum distance between guided missiles in the mode of simultaneous firing from the right and left guidance devices.
EFFECT: invention allows to increase the fire efficiency and to ensure arrangement on a wide spectrum of carriers with low carrying capacity.
3 cl, 2 dwg
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