Brewster F2A Buffalo vs. lockheed C-130 hercules

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Brewster F2A Buffalo versus lockheed C-130 hercules
8.03 m 26 ft 4 in length 29.79 m 97 ft 9 in
3.66 m 12 ft height 11.66 m 38 ft 3 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 Allison T56-A-15 turboprop engines
950 horsepower thrust per engine Approximately 4,590 hp per engine
950 horsepower total thrust Approximately 18,360 hp total
3,247 kg 7,159 lb MTOW 70,307 kg 155,000 lb
1,664 km 900 mi range 3,760 km 2,031 nm
259 km/h 161 mph cruise speed 540 km/h 335 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.