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
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.