Lockheed Martin C-130J Super Hercules vs. Cessna CitationJet/M2

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Lockheed Martin C-130J Super Hercules versus Cessna CitationJet/M2
34.37 m 112 ft 9 in length 13.00 m 42 ft 7 in
11.86 m 38 ft 11 in height 4.26 m 14 ft
40.41 m 132 ft 7 in wingspan 14.39 m 47 ft 3 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 Pratt & Whitney PW615F-A
Approximately 4,700 hp per engine thrust per engine 1,900 lbf
Approximately 18,800 hp total total thrust 3,800 lbf
76,610 kg 168,900 lb MTOW 10,700 lb 4,853 kg
4,600 km 2,485 nm range 1,550 nm 2,870 km
660 km/h 410 mph cruise speed 404 kts 251 mph
based on configuration capacity 6
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.