de Havilland Canada DHC-2 Beaver vs. Antonov An-225 Mriya

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de Havilland Canada DHC-2 Beaver versus Antonov An-225 Mriya
13.56 m 44 ft 6 in length 84.0 m 275 ft 7 in
5 m 16 ft 5 in height 18.1 m 59 ft 5 in
16.56 m 54 ft 4 in wingspan 88.4 m 290 ft 2 in
2 x Armstrong Siddeley Double Mamba turboprop engines engines 6 x Ivchenko Progress D-18T turbofan engines
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 23,400 kgf per engine
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 140,400 kgf total
24,200 lb 10,977 kg MTOW 640,000 kg 1,411,200 lb
2,535 km 1,369 nm range 15,400 km 8,315 nm
228 mph 367 km/h cruise speed 800 km/h 497 mph
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.