Airbus A310-300 vs. Antonov An-225 Mriya

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Airbus A310-300 versus Antonov An-225 Mriya
46.66 m 153 ft 1 in length 84.0 m 275 ft 7 in
15.8 m 51 ft 10 in height 18.1 m 59 ft 5 in
43.9 m 144 ft wingspan 88.4 m 290 ft 2 in
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines 6 x Ivchenko Progress D-18T turbofan engines
52,000 lb thrust per engine Approximately 23,400 kgf per engine
104,000 lb total thrust Approximately 140,400 kgf total
148,768 kg 328,000 lb MTOW 640,000 kg 1,411,200 lb
8,050 km 4,348 nm range 15,400 km 8,315 nm
482 knots 279 mph cruise speed 800 km/h 497 mph
190-230 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.