Brewster F2A Buffalo vs. Lockheed P-2 Neptune

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Brewster F2A Buffalo versus Lockheed P-2 Neptune
8.03 m 26 ft 4 in length 30.17 m 99 ft 0 in
3.66 m 12 ft height 10.15 m 33 ft 4 in
10.67 m 35 ft wingspan 33.53 m 110 ft
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine engines 2 x Wright R-3350 radial engines
950 horsepower thrust per engine Approximately 3,700 hp
950 horsepower total thrust Approximately 7,400 hp
3,247 kg 7,159 lb MTOW 27,216 kg 60,000 lb
1,664 km 900 mi range 7,885 km 4,259 nm
259 km/h 161 mph cruise speed 300 mph 483 km/h
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.