Brewster F2A Buffalo vs. Lockheed U-2

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Brewster F2A Buffalo versus Lockheed U-2
8.03 m 26 ft 4 in length 19.2 m 63 ft 0 in
3.66 m 12 ft height 4.8 m 15 ft 9 in
10.67 m 35 ft wingspan 32 m 105 ft
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 1 × General Electric F118-101
950 horsepower thrust per engine 17,000 lbf (76 kN)
950 horsepower total thrust 17,000 lbf (76 kN)
3,247 kg 7,159 lb MTOW 18,144 kg 40,000 lb
1,664 km 900 mi range 6,090 nm 11,278 km
259 km/h 161 mph cruise speed 475 mph 764 km/h
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.