Boeing 777-200 vs. Lockheed Martin C-130J Super Hercules

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Boeing 777-200 versus Lockheed Martin C-130J Super Hercules
63.7 m 209 ft 1 in length 34.37 m 112 ft 9 in
18.6 m 61 ft height 11.86 m 38 ft 11 in
64.8 m 212 ft 7 in wingspan 40.41 m 132 ft 7 in
General Electric GE90-77B or GE90-94B, Pratt & Whitney PW4077 & PW4090, Rolls-Royce Trent 877 & Trent 895 engines 4 x Rolls-Royce AE 2100D3 turboprop engines
Up to 94,000 pounds thrust per engine Approximately 4,700 hp per engine
Up to 188,000 pounds total thrust Approximately 18,800 hp total
299,370 kg 660,000 lb MTOW 76,610 kg 168,900 lb
5,240 nm 9,711 km range 4,600 km 2,485 nm
560 mph 901 km/h cruise speed 660 km/h 410 mph
305 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.