Modern Drawings/Air/Algeria/Fighters/Su-27SK.htm | Update: -

 

 

Export Su-27S single-seater. No additional information.

 

Type: Air-superiority fighter, multirole fighter
Crew: 1
First flight: 20 May 1977
Introduction: 22 June 1985
Number built: 809 (all variants)

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
Performances
Maximum speed: : Mach 2.35 (2500 km/h)
Service ceiling: 19000 m
Range: 3530 km at altitude; (1340 km at sea level)
Armament

Inside: 1 × 30 mm GSh-30-1 cannon with 150 rounds
Outside: Up to 6 × medium-range AA missiles R-27,
2 × short-range heat-seeking AA missiles R-73

 

 

Fighters