FIELD: aircraft engineering.
SUBSTANCE: proposed aircraft comprises airframe with fuselage and wings, jet lift-and-thrust units or jet lift-and-thrust engines with afterburner chambers. Said engines are arranged in one or several rows under wings or articulated at wing tips and at fuselage rudder surfaces. It includes starting engine with compressor and electrical generator, hydrocarbon fuel and conducting fluid feed pumps and pulse generators. Every jet lift-and-thrust engine has compressed air intake chamber connected with receiver arranged under working channel and damping device. Damping device comprises reflector composed of the body with one sharpened side and opposite concaved side to reflect shock waves. Combustion chamber with diverging nozzles houses combined atomizer for injection of gaseous mix of hydrocarbon fuel and conducting fluid, and nozzle. To ignite combustible mix at detonation combustion thermal dissociation products of conducting fluid are injected.
EFFECT: higher efficiency, decreased specific weight.
15 dwg
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