Northrop T-38 Talon vs. Antonov An-124 Ruslan
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Northrop T-38 Talon |
versus |
Antonov An-124 Ruslan |
14.1 m |
46 ft 4 in |
length |
69.10 m |
226 ft 9 in |
3.9 m |
12 ft 10 in |
height |
20.78 m |
68 ft 2 in |
7.7 m |
25 ft 3 in |
wingspan |
73.3 m |
240 ft 6 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x Ivchenko Progress D-18T turbofan engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
Approximately 51,590 lbf |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
Approximately 206,360 lbf |
12,093 lb |
5,485 kg |
MTOW |
405,000 kg |
893,000 lb |
1,759 km |
950 nm |
range |
3,700 km |
1,998 nm |
745 kts |
1,380 km/h |
cruise speed |
800 km/h |
497 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.