Consolidated B-24 Liberator vs. Lockheed Martin C-130J Super Hercules

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Consolidated B-24 Liberator versus Lockheed Martin C-130J Super Hercules
20.42 m 67 ft 0 in length 34.37 m 112 ft 9 in
5.49 m 18 ft height 11.86 m 38 ft 11 in
33.53 m 110 ft wingspan 40.41 m 132 ft 7 in
4 Pratt & Whitney R-1830s, 4 Pratt & Whitney R-1830 Twin Wasp radial air-cooled engines engines 4 x Rolls-Royce AE 2100D3 turboprop engines
1,200 hp, 1,200 hp each thrust per engine Approximately 4,700 hp per engine
4,800 hp (calculated from 4 engines each with 1,200 hp) total thrust Approximately 18,800 hp total
26,580 kg 58,600 lb MTOW 76,610 kg 168,900 lb
2,850 mi 2,481 nm range 4,600 km 2,485 nm
175 mph 282 km/h cruise speed 660 km/h 410 mph
8,000 pounds 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.