FIELD: aircraft engineering.
SUBSTANCE: canard configuration plane comprises a wing, a fuselage, a propulsion system, a chassis, a vertical fin assembly and biplane canard surfaces (CS). The plane has uniform load of a wing and PGO per unit area, at the ration of the distance between CS plans to an arithmetic average of values of chords of each plan equal to 1.2.
EFFECT: decrease of the plane sizes.
1 dwg
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