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  • Sukhoi Su-27 - Wikipedia
    The Sukhoi Su-27 (Russian: Сухой Су-27; NATO reporting name: Flanker) is a Soviet -origin twin-engine supersonic supermaneuverable fighter aircraft designed by Sukhoi
  • MILAVIA Aircraft - Sukhoi Su-27 Flanker Specifications
    MILAVIA Aircraft - Sukhoi Su-27 Flanker technical specifications and armament information
  • Russian Sukhoi Su-27 - Warrior Lodge
    Thrust with afterburner: 12,500 kgf (122 6 kN, 27,560 lbf) each; Leading edge sweep: 42° Performance Maximum speed: Mach 2 35 (2,500 km h, 1,550 mph) at altitude; Range: 3,530 km (2,070 mi) at altitude; (1,340 km 800 mi at sea level) Service ceiling: 19,000 m (62,523 ft) Rate of climb: 300 m s (54,000 ft min) Wing loading: 371 kg m² (76 lb
  • Su-27 Flanker Technical Data. - Fly MiG
    The Su-27's high thrust-to-weight ratio and refined aerodynamics allow superb flight characteristics at high angles of attack In addition, the Soviet Navy purchased an improved Su-27K design, later redesignated the Su-33, to operate off its first class of large aircraft carriers
  • Aerospaceweb. org | Aircraft Museum - Su-27 Flanker
    The Su-27's high thrust-to-weight ratio and refined aerodynamics allow superb flight characteristics at high angles of attack In addition, the Soviet Navy purchased an improved Su-27K design, later redesignated the Su-33, to operate off its first class of large aircraft carriers
  • Global War Birds: Sukhoi Su-27
    Thrust with afterburner: 12,500 kgf (122 6 kN, 27,560 lbf) each Leading edge sweep: 42° Performance Maximum speed: Mach 2 35 (2,500 km h, 1,550 mph) at altitude Range: 3,530 km (2,070 mi) at altitude; (1,340 km 800 mi at sea level) Service ceiling: 18,500 m (62,523 ft) Rate of climb: 300 m s (54,000 ft min) Wing loading: 371 kg m² (76 lb
  • Sukhoi Su-27 Flanker - The Trek BBS
    Two AL-31F afterburning bypass turbojet engines, each having a maximum thrust of 12,500 kgf, provide the plane with an excellent thrust-to-weight ratio and agility The engine air intakes are fitted with mesh guards, preventing the ingress of foreign matter into the engines during landing and take-off
  • Sukhoi SU-27S SU-27 (Late-Srs) - wardrawings. be
    Number built: inherited 23-28 Su-27s from USSR Powerplant: 2 × Saturn Lyulka AL-31F turbofans Dry thrust: 7670 kgf (75 22 kN) each Thrust with afterburner: 12500 kgf (122 6 kN) each: Dimensions Masses: Length: 21 9 m | Wingspan: 14 7 m | Height: 5 92 m Wing area: 62 m² | Empty weight: 16380 kg Max takeoff weight: 30450 kg
  • Architecture Myths #9: Clean Lines – misfits architecture
    The P-42 Record Flanker was an SU-27 remodelled to lower its weight for setting records Even the paint was removed, the aircraft polished and all drag-producing gaps and joints sealed The engines were pimped to increase thrust to 2,204lbs, producing a thrust-to-weight ratio of almost 2:1
  • Suchoi Sukhoi Su-27 Su-30 - Specifications - Technical Data . . .
    The Sukhoi Su-27 is a twin-engined single-seat air-superiority jet fighter aircraft developed by the Soviet Design Bureau Sukhoi, today Sukhoi JSC (Russia) The Su-30 is a two-seat multirole fighter aircraft variant





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