FIELD: launch systems.
SUBSTANCE: aerostat salvo launch system contains a multi-charge launcher located on a movable platform, containing at least one vertically mounted guide in the form of a tube. A dive-planning ammunition is installed in the tube. The ammunition is equipped with folding wings with steering machines, a battery, a control unit, a radio communication module, a satellite and inertial navigation system unit, a homing head and a fuse. The ammunition is located under the folded balloon with an ejector cylinder and is connected to it through a cable with a squib. Fixation in the projectile guide is carried out by means of a spring stop. A flexible hose is connected to each of the guides, one end of which is connected through an electrovalve to a cylinder with compressed hydrogen, and the other end through an electromechanical pruner to the valve of the balloon ejector cylinder container, the ejector cylinder container is connected to the main cavity of the balloon by means of check valves.
EFFECT: providing take-off and climb of loitering ammunition by balloon method.
5 cl, 6 dwg
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