Northrop T-38 Talon vs. Canadair CL-415
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Northrop T-38 Talon |
versus |
Canadair CL-415 |
14.1 m |
46 ft 4 in |
length |
19.82 m |
65 ft 0 in |
3.9 m |
12 ft 10 in |
height |
8.66 m |
28 ft 5 in |
7.7 m |
25 ft 3 in |
wingspan |
28.6 m |
93 ft 1 |
Two General Electric J85-GE-5A turbojet engines |
engines |
2 x Pratt & Whitney Canada PW123AF turboprop engines |
2,050 pounds dry thrust; 2,900 with afterburners |
thrust per engine |
2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW) |
4,100 pounds dry thrust; 5,800 with afterburners |
total thrust |
4,300 to 4,760 shaft horsepower |
12,093 lb |
5,485 kg |
MTOW |
19,733 kg |
43,525 lb |
1,759 km |
950 nm |
range |
1,600 km |
864 nm |
745 kts |
1,380 km/h |
cruise speed |
290 km/h |
180 mph |
Two (student and instructor) |
capacity |
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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.