Airbus A320-200 vs. Sukhoi Su-57

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Airbus A320-200 versus Sukhoi Su-57
38.7 m 127 ft 0 in length 20.1 m 65 ft 11 in
17.4 m 57 ft 1 in height 3.8 m 12 ft 6 in
35.8 m 117 ft 5 in wingspan 14.1 m 46 ft 3 in
Choice between Pratt & Whitney GTFâ„¢ and the LEAP-1A from CFM International engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
Between 21,000 - 33,000 lbf thrust per engine 107.9 kN dry and 166.8 kN after burning
Between 42,000 - 66,000 lbf total thrust 215.8 kN dry and 333.6 kN after burning
77,000 kg 169,800 lb MTOW 35,000 kg 77,200 lb
5,700 km 3,078 nm range 3,500 km 1,890 nm
530 mph 853 km/h cruise speed Mach 2 2470 km/h
Typically between 140-180 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.