MULTI-PURPOSE HIGHLY MANOEUVRABLE SUPERSONIC AIRCRAFT, ITS AIRFRAME, EQUIPMENT AND SYSTEMS Russian patent published in 2003 - IPC

FIELD: manufacture of supersonic aircraft of integral aerodynamic configuration. SUBSTANCE: load- bearing case has wing deformed in center surface of panels with developed extensions, deflectable noses and flaperons smoothly changing to fuselage. Nose section of fuselage is provided with domes of radar and optical location station, extensible flying boom and two cabins provided with common hinged part of canopy; cabins are located in tandem. Arranged in center portion of fuselage are fuselage fairing with deceleration flap and air intakes of power plant mounted above and under center-wing section. Nacelles of two turbo-jet engines are connected by central beam in tail section of fuselage. Arranged on sides of nacelles are tail booms of fuselage, load-bearing fins of vertical tail and all-moving halves of stabilizer. Rapid-firing cannon is mounted in right-hand root extension of wing. Units for suspension of cargoes and ammunition are provided on lower surfaces of wing panels, center-wing section, air intakes and central beam in tail section of fuselage. Controllable front horizontal tail is mounted on root extensions of wing behind cabins. EFFECT: improved service characteristics. 42 cl, 5 dwg, 1 tbl