McDonnell-Douglas MD-11 vs. Antonov An-124 Ruslan

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McDonnell-Douglas MD-11 versus Antonov An-124 Ruslan
61.20 m 200 ft 10 in length 69.10 m 226 ft 9 in
17.6 m 57 ft 9 in height 20.78 m 68 ft 2 in
51.6 m 169 ft 4 in wingspan 73.3 m 240 ft 6 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 4 x Ivchenko Progress D-18T turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 51,590 lbf
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 206,360 lbf
285,990 kg 630,400 lb MTOW 405,000 kg 893,000 lb
13,231 km 7,147 nm range 3,700 km 1,998 nm
961 km/h 597 mph cruise speed 800 km/h 497 mph
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.