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Application filed by Национальный Авиационный УниверситетfiledCriticalНациональный Авиационный Университет
Priority to UAU201301405UpriorityCriticalpatent/UA86524U/en
Publication of UA86524UpublicationCriticalpatent/UA86524U/en
Disclosed is a training unmanned aircraft of normal aerodynamic scheme. The unmanned aircraft is equipped with a wing with advanced mechanization of leading and trailing edges and a push type power plant with a gasoline internal combustion engine located on a fuselage behind the wing, and a tricycle-equipped landing gear with a bow driven bar, which is attached to the fuselage. A fin is made T-shaped, the power plant is pulling twin-engine and is placed on the wing in special wing nacelles and the fin is classical or two-keel.