Basic Specification

one pilot power plant Engines
2 twin shaft augmented
turbofin AL-31F maximum
thrust, full augmentation ...
all » S/L,ISA 2 x 125,000
kg maximum thrust, dry S/L,ISA
2 x 7,800 kg specific fuel
consumption, kg/kg x h (at max
thrust with reheat) 1.92
specific fuel consumption,
kg/kg x h (at min cruis
more

Basic Specification

one pilot power plant Engines
2 twin shaft augmented
turbofin AL-31F maximum
thrust, full augmentation ...
all » S/L,ISA 2 x 125,000
kg maximum thrust, dry S/L,ISA
2 x 7,800 kg specific fuel
consumption, kg/kg x h (at max
thrust with reheat) 1.92
specific fuel consumption,
kg/kg x h (at min cruise)
0.575 Weight maximum take-off
weight 33,000 kg normal
take-off weight 23,000 kg
maximum landing weight 21,000
kg maximum internal fuel 9,400
kg maximum military load 6,200
kg Dimensions Length 21.94 m
height on landing gear 5.909 m
Span 14.70 m wing area 62.04
square m landing gear base 5.8
m landing gear track 4.34 m
flight data maximum speed at
high altitude 2.35 Mach
maximum speed near ground
1,400 km/h minimum indicated
speed 200 km/hour service
ceiling 18,500 m rate of climb
near ground 330 m radius of
turn near ground 450 m maximum
limit load factor +9g
acceleration time at h='1000',
full augmentation from speed
600 to 1100 km/hour 14.1
seconds from speed 1100 to
1300 km/hour 9.8 seconds
maximum operation range near
ground 1370 km maximum
operating range at cruise
altitude 3,680 km Take-off run
at normal take-off weight 400
m landing run with drag
parachute 620 m

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Category Autos & Vehicles

Tags Jet, aircraft