Abstract: The group of inventions relates to the field of aircraft. In each variant, a flying object (FO) comprises a body and wings. In a first variant, an FO comprises wings mounted so as to be capable of rotating the FO. In a second variant, an FO comprises a body on which is mounted a rim with side wings. In a third variant, an FO comprises wings in the shape of a triangular prism, one side of which is fastened to the body, and the other two sides of which are spherical with arcs of different radii. In a fourth variant, the FO comprises tail wings fastened to the body such that the exhaust gases from the nozzle impinge on the wings and create a force which rotates the FO.

Abstract: The invention relates to aviation, and more particularly to designs for vertical take-off and landing aircraft. The present vertical take-off and landing aircraft comprises jet propulsion units containing compressors, overflow valves, air tanks, and a nuclear power plant. Turbines are provided with hybrid engines capable of running on electricity or liquid fuel. On the outside of the aircraft, each turbine is provided with a corrugated tip, consisting of two parts: a base and an extendable part. The bases of the tips are pivotally mounted on the turbine for rotation about their own axis and are coupled to a lateral orientation system for altering the pumping direction. The other part of the corrugated tip is coupled to an angle adjusting system, which, optionally, extends one side of the corrugated part outside the body in order to alter the pumping angle by more than 90 degrees from vertical to horizontal.