Northrop T-38 Talon vs. Lockheed C-5 Galaxy
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Northrop T-38 Talon |
versus |
Lockheed C-5 Galaxy |
14.1 m |
46 ft 4 in |
length |
75.31 m |
247 ft 2 in |
3.9 m |
12 ft 10 in |
height |
19.84 m |
65 ft 1 in |
7.7 m |
25 ft 3 in |
wingspan |
67.89 m |
222 ft 9 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x General Electric TF39 turbofan engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
41,000 pounds of thrust (182 kilonewtons) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
164,000 pounds |
12,093 lb |
5,485 kg |
MTOW |
381,018 kg |
840,000 lb |
1,759 km |
950 nm |
range |
8,000 km |
4,320 nm |
745 kts |
1,380 km/h |
cruise speed |
908 km/h |
564 mph |
Two (student and instructor) |
capacity |
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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.