Su-27 Flanker
Su-27 Flanker
Role Air superiority fighter
Crew 1
Passengers 1
First flight 1977
Entered service 1984
Produced 680
Length 21.9 m
Wingspan 14.7 m
Height 5.92 m
Wing area 62 m²
Empty 16380 kg
Loaded 23430 kg
Maximum takeoff 30450 kg
Power (each)
Maximum speed Mach 2.35 (2500 km/h )
Cruising speed
Range 3530 km
Ceiling 18500 m
Rate of climb 300 m/s

The Sukhoi Su-27 Flanker is a single-seat, twin-engine Mach-2 class jet fighter originally manufactured by the Soviet Union, and designed by the Sukhoi. It was intended as a direct competitor for the large United States fourth generation fighters, with 3,530-kilometre (1,910 nmi) range, heavy armament, sophisticated avionics and high manoeuvrability. The Su-27 most often flies air superiority missions, but is able to perform almost all combat operations. Complementing the smaller MiG-29, the Su-27's closest US counterpart is the F-15 Eagle.

Developments[edit | edit source]

There are several related developments of the Su-27 design. The Su-30 is a two-seat, dual-role fighter for all-weather, air-to-air and air-to-surface deep interdiction missions. The Su-33 ‘Flanker-D’ is a navy fleet defence interceptor for use on aircraft carriers. Further versions include the side-by-side 2-seat Su-34 ‘Fullback’ strike variant and the Su-35 ‘Flanker-E’ improved air defence fighter.


  • 1 × 30 mm GSh-30-1 cannon with 150 rounds
  • 8,000 kg (17,600 lb) on 10 external pylons
  • Up to 6 × medium-range AA missiles R-27, 2 × short-range heat-seeking AA missiles R-73

Gallery[edit | edit source]

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