FIELD: aircraft engineering.
SUBSTANCE: variable-thrust vector aircraft comprises fuselage, wing and gas turbine power plant comprising turbojet engine with adjustable jet nozzle that features variable thrust vector and is arranged at fuselage tail. Aforesaid nozzle consists of base, two flaps furnished with guide vanes arranged to vary gas flow direction, drive that rotates the base relative to jet nozzle and lever-and-slide mechanism designed to turn aforesaid flaps relative to base.
EFFECT: higher maneuverability.
3 cl, 11 dwg
