Northrop T-38 Talon vs. lockheed C-130 hercules
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Northrop T-38 Talon |
versus |
lockheed C-130 hercules |
14.1 m |
46 ft 4 in |
length |
29.79 m |
97 ft 9 in |
3.9 m |
12 ft 10 in |
height |
11.66 m |
38 ft 3 in |
7.7 m |
25 ft 3 in |
wingspan |
40.41 m |
132 ft 7 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x Allison T56-A-15 turboprop engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
Approximately 4,590 hp per engine |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
Approximately 18,360 hp total |
12,093 lb |
5,485 kg |
MTOW |
70,307 kg |
155,000 lb |
1,759 km |
950 nm |
range |
3,760 km |
2,031 nm |
745 kts |
1,380 km/h |
cruise speed |
540 km/h |
335 mph |
Two (student and instructor) |
capacity |
based on configuration |
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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.