Northrop T-38 Talon vs. Bell 412
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Northrop T-38 Talon |
versus |
Bell 412 |
14.1 m |
46 ft 4 in |
length |
17,10 m |
56 ft 1 in |
3.9 m |
12 ft 10 in |
height |
3,48 m |
11 ft 5 in |
7.7 m |
25 ft 3 in |
wingspan |
|
|
Two General Electric J85-GE-5A turbojet engines |
engines |
2 x Pratt & Whitney Canada PT6T-3D turboshaft engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
1,800 hp |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
3,600 hp |
12,093 lb |
5,485 kg |
MTOW |
5,400 kg |
11,905 lb |
1,759 km |
950 nm |
range |
659 km |
356 nm |
745 kts |
1,380 km/h |
cruise speed |
259 km/h |
161 mph |
Two (student and instructor) |
capacity |
13 |
|
|
rotor diameter |
14.0 m |
45 ft 11 in |
|
|
rate of climb |
9.5 m/s |
1,870 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.