Boeing 747-8I vs. Lockheed Martin C-130J Super Hercules

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Boeing 747-8I versus Lockheed Martin C-130J Super Hercules
76.25 m 250 ft 2 in length 34.37 m 112 ft 9 in
19.35 m 63 ft 6 in height 11.86 m 38 ft 11 in
68.45 m 224 ft 7 in wingspan 40.41 m 132 ft 7 in
4x General Electric GEnx 2B67 Turbofan engines 4 x Rolls-Royce AE 2100D3 turboprop engines
66,500 pounds thrust per engine Approximately 4,700 hp per engine
266,000 pounds total thrust Approximately 18,800 hp total
443,613 kg 977,500 lb MTOW 76,610 kg 168,900 lb
8,000 nm 14,816 km range 4,600 km 2,485 nm
Mach 0.86 1,062 km/h cruise speed 660 km/h 410 mph
467 passengers (three-class 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.