Antonov An-225 Mriya vs. Lockheed Martin C-130J Super Hercules

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Antonov An-225 Mriya versus Lockheed Martin C-130J Super Hercules
84.0 m 275 ft 7 in length 34.37 m 112 ft 9 in
18.1 m 59 ft 5 in height 11.86 m 38 ft 11 in
88.4 m 290 ft 2 in wingspan 40.41 m 132 ft 7 in
6 x Ivchenko Progress D-18T turbofan engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Approximately 23,400 kgf per engine thrust per engine Approximately 4,700 hp per engine
Approximately 140,400 kgf total total thrust Approximately 18,800 hp total
640,000 kg 1,411,200 lb MTOW 76,610 kg 168,900 lb
15,400 km 8,315 nm range 4,600 km 2,485 nm
800 km/h 497 mph cruise speed 660 km/h 410 mph
based on configuration 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.