Northrop T-38 Talon vs. Beechcraft King Air 260
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Northrop T-38 Talon |
versus |
Beechcraft King Air 260 |
14.1 m |
46 ft 4 in |
length |
13.41 m |
43 ft 11 in |
3.9 m |
12 ft 10 in |
height |
4.57 m |
15 ft |
7.7 m |
25 ft 3 in |
wingspan |
17.39 m |
57 ft 1 in |
Two General Electric J85-GE-5A turbojet engines |
engines |
2 x Pratt & Whitney Canada PT6A turboprop |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
1050 lbs |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
2100 lbs |
12,093 lb |
5,485 kg |
MTOW |
12,500 lb |
5,670 kg |
1,759 km |
950 nm |
range |
1,720 nm |
3,185 km |
745 kts |
1,380 km/h |
cruise speed |
310 kts |
193 mph |
Two (student and instructor) |
capacity |
9 |
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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.