FIELD: aircraft engineering.
SUBSTANCE: aircraft comprises fuselage, control cabin, delta wing, tail plane, engines arranged above said wing and undercarriage. Main wing arranged above fuselage has its sharp part secured to fuselage by wedge-like prop. Cantilever wing is arranged under fuselage to support tail legs and nose wing with elevators. Said main wing is equipped with rotary valves intended for aerodynamic deceleration. Tail unit fin has cavity to accommodate fuel tank.
EFFECT: higher light, better controllability.
3 cl, 4 dwg
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Authors
Dates
2014-11-27—Published
2013-10-21—Filed