1. Apparatus jet aircraft aerodynamic lift force stabilization system propulsive jet thrust aerodynamic characterized in that the working surfaces propulsors (wing, fuselage, and a parachute nozzle) combined together in a form of axisymmetrical coaxially inside each other domes, two - convexity directed upward (wing -parashyut and nozzle wall) and third - convexity downwards third fixedly connected with the second (inner) - fuselage; third - the curvature of the curvature at the top; upper (first) dome (with a curvature smaller curvature of the second) is connected to the second movable - by depreciation-damper adjustable fastening assemblies: upper node - disposed between the vertices of the first and second domes, and peripherals - are symmetrically placed in the diffuser nozzle - the gap between the first and second domes; on the extreme circles of domes symmetrically placed ailerons two rotary degrees of freedom; mass center device is positioned in the axis of symmetry ustroystva.2. Jet aircraft system device energoprivodnoy wind system according to claim 1, characterized in that for the realization of permanent autonomous flight to obtain energy from the environment into the top of the first dome-formed open ejectors inlets.; parabolic wall of the nozzle are structured as reversible MHD machine with additional features isotopic mass separator and three-dimensional paraboloid linear accelerator reactor TCB isotopes of light elements: mosaic lined active automated universal poles
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