Type: PAK-FA / T-50
Country: Soviet Union / Russia
Function: fighter
Year: 2010 (first flight)
Crew: 1
Engines: 2 * 175 kN NPO Saturn
Wing Span: 14.20 m
Wing area: 78.8 m2
Length: 19.80 m
Height: 6.05 m
Empty weight: 18500 kg
Loaded weight: 26000 kg
Maximum Fuel weight: 10300 kg
Max. takeoff Weight: 37000 kg
Wing loading: 330 kg/m2 (normal) - 470 kg/m2 (max)
Thrust/weight: 1.19
Maximum g-load: +10.0 g
Cruise Speed: 1300-1800 km/h
Max Speed: 2600 km/h (Mach 2.45 @ 17000m)
Rate of climb: 350 m/s
Ceiling: 20000 m
Ferry range: 4000-5500 km
Armament: 1*30 mm GSh-30-1 cannon, 10 internal,6 external hardpoints for R-74M Archer and R-77M Adder missiles. Total payload 7500 kg.
Country: Soviet Union / Russia
Function: fighter
Year: 2010 (first flight)
Crew: 1
Engines: 2 * 175 kN NPO Saturn
Wing Span: 14.20 m
Wing area: 78.8 m2
Length: 19.80 m
Height: 6.05 m
Empty weight: 18500 kg
Loaded weight: 26000 kg
Maximum Fuel weight: 10300 kg
Max. takeoff Weight: 37000 kg
Wing loading: 330 kg/m2 (normal) - 470 kg/m2 (max)
Thrust/weight: 1.19
Maximum g-load: +10.0 g
Cruise Speed: 1300-1800 km/h
Max Speed: 2600 km/h (Mach 2.45 @ 17000m)
Rate of climb: 350 m/s
Ceiling: 20000 m
Ferry range: 4000-5500 km
Armament: 1*30 mm GSh-30-1 cannon, 10 internal,6 external hardpoints for R-74M Archer and R-77M Adder missiles. Total payload 7500 kg.
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