Airbus A310-300 vs. Sukhoi Su-57

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Airbus A310-300 versus Sukhoi Su-57
46.66 m 153 ft 1 in length 20.1 m 65 ft 11 in
15.8 m 51 ft 10 in height 3.8 m 12 ft 6 in
43.9 m 144 ft wingspan 14.1 m 46 ft 3 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
52,000 lb thrust per engine 107.9 kN dry and 166.8 kN after burning
104,000 lb total thrust 215.8 kN dry and 333.6 kN after burning
148,768 kg 328,000 lb MTOW 35,000 kg 77,200 lb
8,050 km 4,348 nm range 3,500 km 1,890 nm
482 knots 279 mph cruise speed Mach 2 2470 km/h
190-230 passengers capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.