FIELD: aeronautical engineering. SUBSTANCE: aircraft is provided with rotating round wing 1 from which blades 2 are extended during takeoff and landing; blades 2 are controlled by servo-tabs forming main rotor; aircraft is provided with engines. Secured on fuselage 6 is horizontal tail with elevons and vertical tail with control surfaces 8 and interceptor 9 and braking system 10. EFFECT: extended field of application. 7 cl, 3 dwg
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Authors
Dates
2002-11-20—Published
2000-08-29—Filed