Specifications - Su-27SK (Su-30MK, Su-33) Flanker Front Line Fighter Aircraft, Russia

Key Data
Crew	1 – pilot
Dimensions
Length	21.94m
Height on Landing Gear	5.91m
Span	14.7m
Wing Area	62.04m²
Landing Gear Base	5.8m
Landing Gear Track	4.34m
Weights
Maximum Take-Off Weight	33,000kg
Normal Take-Off Weight	23,000kg
Maximum Landing Weight	21,000kg
Maximum Internal Fuel	9,400kg
Maximum Military Load	6,200kg
Engines
Engines	2 x twin-shaft augmented turbofin AL-31F
Maximum Thrust, Full Augmentation S/L, ISA	2 x 125,000kg
Maximum Thrust, Dry S/L, ISA	2 x 7,800km
Specific Fuel Consumption, kg/kg x h (At Maximum Thrust with Reheat)	1.92
Specific Fuel Consumption, kg/kg x h (At Minimum Cruise)	0.575
Performance
Maximum Speed at High Altitude	Mach 2.35
Maximum Speed Near Ground	1,400km/h
Minimum Indicated Speed	200km/h
Service Ceiling	18,500m
Rate of Climb Near Ground	330m
Radius of Turn Near Ground	450m
Maximum Limit Load Factor	+9g
Acceleration Time at h=1,000, Full Augmentation	600km/h to 1,100km/h – 14.1 seconds 1,100km/h to 1,300km/h – 9.8 seconds
Maximum Operation Range Near Ground	1,370km
Maximum Operating Range at Cruise Altitude	3,680km
Take-Off Run at Normal Take-Off Weight	400m
Landing Run with Drag Parachute	620m
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