Antonov An-225 Mriya vs. lockheed C-130 hercules

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Antonov An-225 Mriya versus lockheed C-130 hercules
84.0 m 275 ft 7 in length 29.79 m 97 ft 9 in
18.1 m 59 ft 5 in height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
Approximately 23,400 kgf per engine thrust per engine Approximately 4,590 hp per engine
Approximately 140,400 kgf total total thrust Approximately 18,360 hp total
640,000 kg 1,411,200 lb MTOW 70,307 kg 155,000 lb
15,400 km 8,315 nm range 3,760 km 2,031 nm
800 km/h 497 mph cruise speed 540 km/h 335 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.