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
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
