FIELD: aviation.
SUBSTANCE: invention relates to designs of unmanned aerial vehicles, devices for counteracting projectiles of surface-to-air missile systems with thermal guidance heads and methods of their operation. Hybrid reconnaissance and strike drone includes a power source, a control system with a target homing module, hull made according to “aircraft” aerodynamic configuration “tailless”, vertical keel with rudders. Under swept wing there is an armature for attachment and release of 122 mm shells for multiple-launch rocket system with a system for simultaneous start-up of their jet engines. On the upper part of the hull there are rigidly fixed a detonation pulsating air-jet engine and a device for counteracting projectiles of surface-to-air missile systems with thermal guidance heads, the latter comprises multiple-charge automatic smooth-bore firearm with barrel outlet arranged inside engine flat nozzle.
EFFECT: providing the possibility of applying several precision surgical missile-bomb strikes on enemy targets and conducting reconnaissance of the area with return to the landing site.
4 cl, 2 dwg
