Brewster F2A Buffalo vs. Northrop T-38 Talon
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Brewster F2A Buffalo |
versus |
Northrop T-38 Talon |
8.03 m |
26 ft 4 in |
length |
14.1 m |
46 ft 4 in |
3.66 m |
12 ft |
height |
3.9 m |
12 ft 10 in |
10.67 m |
35 ft |
wingspan |
7.7 m |
25 ft 3 in |
1 x Wright R-1820-40 Cyclone 9 9-cyl air-cooled radial piston engine |
engines |
Two General Electric J85-GE-5A turbojet engines |
950 horsepower |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
950 horsepower |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
3,247 kg |
7,159 lb |
MTOW |
12,093 lb |
5,485 kg |
1,664 km |
900 mi |
range |
1,759 km |
950 nm |
259 km/h |
161 mph |
cruise speed |
745 kts |
1,380 km/h |
|
capacity |
Two (student and instructor) |
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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.