North American B-25 Mitchell vs. Northrop T-38 Talon
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North American B-25 Mitchell |
versus |
Northrop T-38 Talon |
16.15 m |
53 ft 0 in |
length |
14.1 m |
46 ft 4 in |
5 m |
16 ft 4 in |
height |
3.9 m |
12 ft 10 in |
20.58 m |
67 ft 6 in |
wingspan |
7.7 m |
25 ft 3 in |
2 x Wright R-2600-92 Twin Cyclone |
engines |
Two General Electric J85-GE-5A turbojet engines |
1,700 horsepower |
thrust per engine |
2,050 pounds dry thrust; 2,900 with afterburners |
3,400 horsepower |
total thrust |
4,100 pounds dry thrust; 5,800 with afterburners |
7,484 kg |
16,500 lb |
MTOW |
12,093 lb |
5,485 kg |
1,350 mi |
1,175 nm |
range |
1,759 km |
950 nm |
233 MPH |
375 km/h |
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.