Lockheed Martin C-130J Super Hercules vs. Short C-23 Sherpa

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Lockheed Martin C-130J Super Hercules versus Short C-23 Sherpa
34.37 m 112 ft 9 in length 17.68 m 58 ft 0 in
11.86 m 38 ft 11 in height 6.55 m 21 ft 6 in
40.41 m 132 ft 7 in wingspan 22.76 m 74 ft 8 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
Approximately 4,700 hp per engine thrust per engine Approximately 1,200 hp per engine
Approximately 18,800 hp total total thrust Approximately 2,400 hp total
76,610 kg 168,900 lb MTOW 7,484 kg 16,500 lb
4,600 km 2,485 nm range 1,048 km 566 nm
660 km/h 410 mph cruise speed 425 km/h 264 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.