Brewster F2A Buffalo vs. Grumman OV-1 Mohawk
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Brewster F2A Buffalo |
versus |
Grumman OV-1 Mohawk |
8.03 m |
26 ft 4 in |
length |
12.52 m |
41 ft 1 in |
3.66 m |
12 ft |
height |
3.89 m |
12 ft 9 in |
10.67 m |
35 ft |
wingspan |
14.63 m |
48 ft |
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine |
engines |
2 x Lycoming T53 turboprop engines |
950 horsepower |
thrust per engine |
Approximately 1,100 hp each |
950 horsepower |
total thrust |
Approximately 2,200 hp total |
3,247 kg |
7,159 lb |
MTOW |
14,950 lb |
6,781 kg |
1,664 km |
900 mi |
range |
1,690 km |
913 nm |
259 km/h |
161 mph |
cruise speed |
230 mph |
370 km/h |
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capacity |
Pilot and observer |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.