Northrop T-38 Talon vs. Airbus A380-800F
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Northrop T-38 Talon |
versus |
Airbus A380-800F |
14.1 m |
46 ft 4 in |
length |
72.73 m |
238 ft 7 in |
3.9 m |
12 ft 10 in |
height |
24.09 m |
79 ft |
7.7 m |
25 ft 3 in |
wingspan |
79.75 m |
261 ft 8 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x Engine Alliance GP7200 turbofan engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
280,000 to 320,000 pounds |
12,093 lb |
5,485 kg |
MTOW |
590,000 kg |
1,300,733 lb |
1,759 km |
950 nm |
range |
14,800 km |
7,992 nm |
745 kts |
1,380 km/h |
cruise speed |
903 km/h |
561 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.