Su-30МК: Performance

Su-30МК
Take-off weight (normal/maximum), kg:
24,900 / 34,500
Fuel capacity (0.785 g/ccm). Specific weight (normal/maximum), kg:
5,270 / 9,640
Maximum flight range, km:
• near ground
• at cruise flight altitude
• with one in-flight refueling
 
1,270
3,000
5,200
Minimum take-off run at normal take-off weight (at afterburner power), m:
550
Maximum landing run at normal landing weight (with braking parachute), m:
750
Maximum speed near ground, km/h:
1,350
Maximum speed (at altitude), М:
1.9
Service ceiling, m:
17,300
Load factor limit, g:
9.0
Dimensions (length/wing span/hight), m:
21.9 / 14.7 / 6.4
Power plant: turbofan engine AL-31FP
Maximum thrust at afterburner, kg:
2 x 12,500 kgf
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