FIELD: space.
SUBSTANCE: invention relates to aviation and space engineering, particularly, to aircrafts. Power drive system of a jet-powered vehicle system to perform independent permanent flight while obtain energy from the environment contains opening ejectors-air intakes on the top of the first dome. Parabolic nozzle walls are structurally made as a reversible MHD machine and three-dimensional paraboloid-linear accelerator-reactor. System of working surfaces of wing, fuselage, nozzle and parachute are combined together in the shape of axisymmetric coaxially placed one into another domes, two of which are convex, and third one is concave. Third dome is rigidly connected to the second one, forming a fuselage, first is movably connected to the second one with amortizing damper adjustable attachment assemblies. Method for power supply of a jet aircraft is implemented by means of AI reactions on light elements isotopes in the mode of the reactor AI accelerator.
EFFECT: higher stability and controllability of the apparatus.
3 cl, 2 dwg
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