Northrop T-38 Talon vs. Douglas C-54 Skymaster
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Northrop T-38 Talon |
versus |
Douglas C-54 Skymaster |
14.1 m |
46 ft 4 in |
length |
28.60 m |
93 ft 10 in |
3.9 m |
12 ft 10 in |
height |
8.38 m |
27 ft 6 in |
7.7 m |
25 ft 3 in |
wingspan |
35.81 m |
117 ft 6 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x Pratt & Whitney R-2000 Twin Wasp radial engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
1,200 to 1,450 horsepower (895 to 1,080 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
4,800 to 5,800 horsepower |
12,093 lb |
5,485 kg |
MTOW |
29,484 kg |
65,000 lb |
1,759 km |
950 nm |
range |
6,500 km |
3,510 nm |
745 kts |
1,380 km/h |
cruise speed |
340 km/h |
211 mph |
Two (student and instructor) |
capacity |
Up to 50 passengers or 28,500 lb cargo |
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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.