Northrop T-38 Talon vs. de Havilland Canada DHC-6 Twin Otter
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Northrop T-38 Talon |
versus |
de Havilland Canada DHC-6 Twin Otter |
14.1 m |
46 ft 4 in |
length |
15.32 m |
50 ft 3 in |
3.9 m |
12 ft 10 in |
height |
5.94 m |
19 ft 6 in |
7.7 m |
25 ft 3 in |
wingspan |
19.81 m |
65 ft |
Two General Electric J85-GE-5A turbojet engines |
engines |
2 x Pratt & Whitney Canada PT6A-27 turboprop engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
550 to 750 shaft horsepower (410 to 560 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
1100 to 1500 shaft horsepower |
12,093 lb |
5,485 kg |
MTOW |
5,670 kg |
12,500 lb |
1,759 km |
950 nm |
range |
1,389 km |
750 nm |
745 kts |
1,380 km/h |
cruise speed |
280 km/h |
174 mph |
Two (student and instructor) |
capacity |
19 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.