FIELD: weapons and ammunition.
SUBSTANCE: invention relates to unmanned aerial platforms based on UAVs armed with small arms. Actuation system is made in the form of an electronic unit. Element initiating the propellant charge is made in the form of an igniter. Igniter and actuation system are configured to convert electrical energy into flame force. Piston is arranged between projectile and propellant charge. Ejector channel is made on the side opposite to the muzzle end of the barrel. Recoil compensation mechanism is made in the form of a launcher. Launcher is configured to eject counterweight in direction opposite to projectile movement at the moment of firing.
EFFECT: expansion of arsenal and functional capabilities of UAV.
10 cl, 10 dwg
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