FIELD: aviation.
SUBSTANCE: helistat device with a bearing horizontal tail contains a shell with a carrier gas, a main rotor, a crew cabin with a payload, a rear tail unit, a marching propulsion system and a landing gear. The main rotor and the cabin are installed at the head of the helistat. The rear horizontal tail is equipped with the possibility of partial balancing the lifting-force moment of the main rotor thrust by its lifting force with respect to the gravity center.
EFFECT: reduction of the required volume of the carrier gas.
3 cl, 2 dwg
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