FIELD: aviation technology.
SUBSTANCE: aircraft (500-1) contains hull (100) and control module (110). Hull (100) is equipped with one or more containers (300) configured to be filled with fluid under pressure. At least one of the said containers (300) has two or more outlets for releasing fluid. Each outlets is equipped with a controlled valve. The control module is connected to the controlled valves with the ability to control their state to regulate release of the fluid from the said at least one container (300) with the ability to control the movement of the aircraft through the air.
EFFECT: reduced weight and energy consumption of the aircraft.
51 cl, 13 dwg
