McDonnell-Douglas MD-11 vs. Antonov An-225 Mriya

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McDonnell-Douglas MD-11 versus Antonov An-225 Mriya
61.20 m 200 ft 10 in length 84.0 m 275 ft 7 in
17.6 m 57 ft 9 in height 18.1 m 59 ft 5 in
51.6 m 169 ft 4 in wingspan 88.4 m 290 ft 2 in
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 6 x Ivchenko Progress D-18T turbofan engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 23,400 kgf per engine
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 140,400 kgf total
285,990 kg 630,400 lb MTOW 640,000 kg 1,411,200 lb
13,231 km 7,147 nm range 15,400 km 8,315 nm
961 km/h 597 mph cruise speed 800 km/h 497 mph
Max 410 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.