FIELD: aviation.
SUBSTANCE: invention relates to aircraft engineering, particularly, to unmanned aerial vehicles intended for interception and destruction of air targets. Unmanned aerial vehicle-interceptor (UAV-I) in the form of a free-carrying monoplane comprises a fuselage and a trapezoidal wing with engines arranged on it, as well as a shooting complex. Wherein UAV-I represents a flying wing design and incorporates extra gunnery complex to make twin gunnery complex, final guidance system to be controlled at final flight stage. At that, each shooting complex is attached to airframe rail by means of front sliding attachment assembly and damping assembly forming rear attachment assembly. Technical problem solved by the claimed invention consists in increase in the UAV-I aerial targets destruction effectiveness.
EFFECT: simplified aiming and increased stability, reduced weight of UAV-I.
6 cl, 5 dwg
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Authors
Dates
2025-05-19—Published
2024-07-10—Filed