Northrop T-38 Talon vs. Cessna 172
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Northrop T-38 Talon |
versus |
Cessna 172 |
14.1 m |
46 ft 4 in |
length |
8.28 m |
27 ft 2 in |
3.9 m |
12 ft 10 in |
height |
2.72 m |
8 ft 11 in |
7.7 m |
25 ft 3 in |
wingspan |
11 m |
36 ft 1 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
1 x Lycoming IO-360-L2A flat-4 piston engine |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
180 to 200 horsepower (134 to 149 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
180 to 200 horsepower (134 to 149 kW) |
12,093 lb |
5,485 kg |
MTOW |
1,040 kg |
2,293 lb |
1,759 km |
950 nm |
range |
1,056 km |
570 nm |
745 kts |
1,380 km/h |
cruise speed |
226 km/h |
140 mph |
Two (student and instructor) |
capacity |
4 |
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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.