Antonov An-225 Mriya vs. Canadair CL-415

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Antonov An-225 Mriya versus Canadair CL-415
84.0 m 275 ft 7 in length 19.82 m 65 ft 0 in
18.1 m 59 ft 5 in height 8.66 m 28 ft 5 in
88.4 m 290 ft 2 in wingspan 28.6 m 93 ft 1
6 x Ivchenko Progress D-18T turbofan engines engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
Approximately 23,400 kgf per engine thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
Approximately 140,400 kgf total total thrust 4,300 to 4,760 shaft horsepower
640,000 kg 1,411,200 lb MTOW 19,733 kg 43,525 lb
15,400 km 8,315 nm range 1,600 km 864 nm
800 km/h 497 mph cruise speed 290 km/h 180 mph
based on configuration 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.