Canadair CT-114 Tutor vs. Lockheed U-2

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Canadair CT-114 Tutor versus Lockheed U-2
9.75 m 32 ft 0 in length 19.2 m 63 ft 0 in
2.84 m 9 ft 4 in height 4.8 m 15 ft 9 in
11.07 m 36 ft 4 in wingspan 32 m 105 ft
1 Orenda J85-CAN-40 turbojet engines 1 × General Electric F118-101
2,950 lbs thrust per engine 17,000 lbf (76 kN)
2,950 lbs total thrust 17,000 lbf (76 kN)
3,331 kg 7,350 lb MTOW 18,144 kg 40,000 lb
1,520 km 821 nm range 6,090 nm 11,278 km
310 knots 180 mph cruise speed 475 mph 764 km/h
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.