FIELD: transportation.
SUBSTANCE: aircraft comprises plate body, cabin with control panel, installed in the body centre in its upper part. Aircraft also comprises central and lateral rocket engines, nozzles of which are inverted downwards, fuel tanks installed in peripheral zone of body, and chassis. Body of apparatus is equipped with two gravitational masses that rotate in opposite directions in single plane and interacting with inclined guide of body, and drive of rotating masses is connected to central rocket engine. Lateral rocket engines are installed with the possibility of rotation around longitudinal axis of body.
EFFECT: elimination of inertial loads in vertical plane and possibility to vary speed and direction of aircraft motion depending on ambient environment.
4 cl, 1 dwg
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