Canadair CT-114 Tutor vs. Northrop T-38 Talon

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Canadair CT-114 Tutor versus Northrop T-38 Talon
9.75 m 32 ft 0 in length 14.1 m 46 ft 4 in
2.84 m 9 ft 4 in height 3.9 m 12 ft 10 in
11.07 m 36 ft 4 in wingspan 7.7 m 25 ft 3 in
1 Orenda J85-CAN-40 turbojet engines Two General Electric J85-GE-5A turbojet engines
2,950 lbs thrust per engine 2,050 pounds dry thrust; 2,900 with afterburners
2,950 lbs total thrust 4,100 pounds dry thrust; 5,800 with afterburners
3,331 kg 7,350 lb MTOW 12,093 lb 5,485 kg
1,520 km 821 nm range 1,759 km 950 nm
310 knots 180 mph cruise speed 745 kts 1,380 km/h
capacity Two (student and instructor)
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.