McDonnell-Douglas MD-11 vs. Sukhoi Su-57

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McDonnell-Douglas MD-11 versus Sukhoi Su-57
61.20 m 200 ft 10 in length 20.1 m 65 ft 11 in
17.6 m 57 ft 9 in height 3.8 m 12 ft 6 in
51.6 m 169 ft 4 in wingspan 14.1 m 46 ft 3 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 (Izdeliye 117 or AL-41F1 augmented turbofans)
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine 107.9 kN dry and 166.8 kN after burning
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust 215.8 kN dry and 333.6 kN after burning
285,990 kg 630,400 lb MTOW 35,000 kg 77,200 lb
13,231 km 7,147 nm range 3,500 km 1,890 nm
961 km/h 597 mph cruise speed Mach 2 2470 km/h
Max 410 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.