FIELD: aviation. SUBSTANCE: proposed aircraft includes fuselage, swept-forward wing with root extension, front and tail horizontal units, two-fin vertical unit, engine with changeable thrust vector, air intake and landing gear. Front and tail horizontal units are all- moving. Front horizontal unit is located on root extension. Tail horizontal unit is swept-forward. Trailing edge of front horizontal unit is located in parallel with leading edge of swept-back wing. Leading edge of tail horizontal unit is located in parallel with trailing edge of wing. Air intake located under fuselage is provided with bevel wing. EFFECT: enhanced maneuverability and combat efficiency. 7 cl, 3 dwg
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Authors
Dates
2003-09-20—Published
2002-03-15—Filed