Northrop T-38 Talon vs. Lockheed C-69 Constellation
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Northrop T-38 Talon |
versus |
Lockheed C-69 Constellation |
14.1 m |
46 ft 4 in |
length |
29.72 m |
97 ft 6 in |
3.9 m |
12 ft 10 in |
height |
6.02 m |
19 ft 9 in |
7.7 m |
25 ft 3 in |
wingspan |
37.49 m |
123 ft |
Two General Electric J85-GE-5A turbojet engines |
engines |
4 x Wright R-3350 Duplex-Cyclone radial engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
2,200 to 3,700 horsepower (1,640 to 2,760 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
8,800 to 14,800 horsepower |
12,093 lb |
5,485 kg |
MTOW |
44,453 kg |
98,000 lb |
1,759 km |
950 nm |
range |
5,200 km |
2,808 nm |
745 kts |
1,380 km/h |
cruise speed |
507 km/h |
315 mph |
Two (student and instructor) |
capacity |
Up to 109 passengers |
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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.