Canadair CT-114 Tutor vs. Lockheed Martin F-35 Lightning II

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Canadair CT-114 Tutor versus Lockheed Martin F-35 Lightning II
9.75 m 32 ft 0 in length 15.67 m 51 ft 4 in
2.84 m 9 ft 4 in height 4.33 m 14 ft 2 in
11.07 m 36 ft 4 in wingspan 10.7 m 35 ft 1 in
1 Orenda J85-CAN-40 turbojet engines Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136
2,950 lbs thrust per engine 40,000 lb
2,950 lbs total thrust 40,000 lb
3,331 kg 7,350 lb MTOW 31,800 kg 70,000 lb
1,520 km 821 nm range 1,380 mi 1,200 nm
310 knots 180 mph cruise speed 520 kt 302 mph
capacity 18,000 pounds of total ordinance
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.