Brewster F2A Buffalo vs. McDonnell Douglas F-4 Phantom II

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Brewster F2A Buffalo versus McDonnell Douglas F-4 Phantom II
8.03 m 26 ft 4 in length 19.2 m 63 ft 0 in
3.66 m 12 ft height 5.03 m 16 ft 6 in
10.67 m 35 ft wingspan 11.72 m 38 ft 5 in
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines Two General Electric J79s
950 horsepower thrust per engine 17,900 lbs
950 horsepower total thrust 35,800 lbs
3,247 kg 7,159 lb MTOW 27,965 kg 61,700 lb
1,664 km 900 mi range 3,031 km 1,636 nm
259 km/h 161 mph cruise speed Mach 2.2 2,717 km/h
capacity Up to 16,000 lbs of externally carried ordnance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.