FIELD: aviation. SUBSTANCE: flying vehicle includes fuselage with convex upper part and flat lower part, landing gear, engines and aerodynamic control surface mounted in lower and upper parts of fuselage. Fuselage has form of load-bearing wing. Engines are located along trailing edge of lower part of fuselage; upper aerodynamic surface is mounted horizontally for deflection on vertical plane; its front part is connected with fuselage by means of movable rod. Lower aerodynamic surface is made in form of two horizontal planes mounted rotatably on four vertical planes secured on lower part of fuselage. EFFECT: enhanced reliability. 2 cl, 5 dwg
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Authors
Dates
1997-09-10—Published
1992-01-22—Filed