Brewster F2A Buffalo vs. Lockheed Martin C-130J Super Hercules

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Brewster F2A Buffalo versus Lockheed Martin C-130J Super Hercules
8.03 m 26 ft 4 in length 34.37 m 112 ft 9 in
3.66 m 12 ft height 11.86 m 38 ft 11 in
10.67 m 35 ft wingspan 40.41 m 132 ft 7 in
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 4 x Rolls-Royce AE 2100D3 turboprop engines
950 horsepower thrust per engine Approximately 4,700 hp per engine
950 horsepower total thrust Approximately 18,800 hp total
3,247 kg 7,159 lb MTOW 76,610 kg 168,900 lb
1,664 km 900 mi range 4,600 km 2,485 nm
259 km/h 161 mph cruise speed 660 km/h 410 mph
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.