Antonov An-225 Mriya vs. de Havilland Canada DHC-3 Otter

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Antonov An-225 Mriya versus de Havilland Canada DHC-3 Otter
84.0 m 275 ft 7 in length 10.52 m 34 ft 6 in
18.1 m 59 ft 5 in height 3.84 m 12 ft 7 in
88.4 m 290 ft 2 in wingspan 17.68 m 58 ft
6 x Ivchenko Progress D-18T turbofan engines engines 1 x Pratt & Whitney R-1340 radial engine
Approximately 23,400 kgf per engine thrust per engine 400 to 600 horsepower (298 to 447 kW)
Approximately 140,400 kgf total total thrust 400 to 600 horsepower (298 to 447 kW)
640,000 kg 1,411,200 lb MTOW 5,670 kg 12,500 lb
15,400 km 8,315 nm range 1,296 km 700 nm
800 km/h 497 mph cruise speed 215 km/h 134 mph
based on configuration capacity 10-11 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.