FIELD: aerostation; flying vehicles suitable for flying in dense atmosphere and in rarefied atmosphere.
SUBSTANCE: fuselage of proposed flying vehicle is provided with wings and stabilizers and is made in form of central disc consisting of two spherical surfaces of different curvature which are engageable with wings, stabilizers, rotating nose cone and aft arch-shaped sector forming dividing surface together with planar nozzles of engines. Upper surface is additionally provided with slotted swivel plane; central part of upper surface is rotating; it is provided with blades of centrifugal air compressor used for suction of boundary layer; aft sector is provided with inclined nozzle orifices and swivel deceleration flap.
EFFECT: simplified construction of boundary layer control system; reduced power requirements; enhanced maneuverability of flying vehicle.
4 dwg
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