FIELD: aviation.
SUBSTANCE: system for jet plane vertical take-off, containing the fuselage with wings, landing gear, one or more jet engines, includes accelerator units and the device, ensuring the stability of the aircraft at takeoff. The accelerator unit consists of several solid jet engines, mounted on the aircraft. The device, that provides stability of the aircraft during takeoff, consists of four ropes, the upper ends of which are attached with possibility of simultaneous detaching to the four points at the wings and fuselage, lying in one plane and on opposite sides from the aircraft's center of gravity, and the lower ends of the ropes are coiled on a common for all cables drum, located below the deck of the carrier vessel.
EFFECT: possibility of aircraft vertical takeoff.
3 dwg
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Authors
Dates
2017-02-08—Published
2015-08-27—Filed