Brewster F2A Buffalo vs. Lockheed Martin F-35 Lightning II

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Brewster F2A Buffalo versus Lockheed Martin F-35 Lightning II
8.03 m 26 ft 4 in length 15.67 m 51 ft 4 in
3.66 m 12 ft height 4.33 m 14 ft 2 in
10.67 m 35 ft wingspan 10.7 m 35 ft 1 in
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
950 horsepower thrust per engine 40,000 lb
950 horsepower total thrust 40,000 lb
3,247 kg 7,159 lb MTOW 31,800 kg 70,000 lb
1,664 km 900 mi range 1,380 mi 1,200 nm
259 km/h 161 mph cruise speed 520 kt 302 mph
capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.