Lockheed Martin C-130J Super Hercules vs. Cessna Citation Mustang

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Lockheed Martin C-130J Super Hercules versus Cessna Citation Mustang
34.37 m 112 ft 9 in length 12.37 m 40 ft 7 in
11.86 m 38 ft 11 in height 4.11 m 13 ft 6 in
40.41 m 132 ft 7 in wingspan 13.17 m 43 ft 2 in
4 x Rolls-Royce AE 2100D3 turboprop engines engines 2 x Pratt & Whitney Canada PW615F
Approximately 4,700 hp per engine thrust per engine 1460 lbs
Approximately 18,800 hp total total thrust 2920 lbs
76,610 kg 168,900 lb MTOW 8,625 lb 3,912 kg
4,600 km 2,485 nm range 1167 nm 2,161 km
660 km/h 410 mph cruise speed 340 kts 211 mph
based on configuration capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.