Antonov An-124 Ruslan vs. Short C-23 Sherpa

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Antonov An-124 Ruslan versus Short C-23 Sherpa
69.10 m 226 ft 9 in length 17.68 m 58 ft 0 in
20.78 m 68 ft 2 in height 6.55 m 21 ft 6 in
73.3 m 240 ft 6 in wingspan 22.76 m 74 ft 8 in
4 x Ivchenko Progress D-18T turbofan engines engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
Approximately 51,590 lbf thrust per engine Approximately 1,200 hp per engine
Approximately 206,360 lbf total thrust Approximately 2,400 hp total
405,000 kg 893,000 lb MTOW 7,484 kg 16,500 lb
3,700 km 1,998 nm range 1,048 km 566 nm
800 km/h 497 mph cruise speed 425 km/h 264 mph
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.