BAC Jet Provost vs. Canadair CT-114 Tutor

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BAC Jet Provost versus Canadair CT-114 Tutor
10.36 m 34 ft 0 in length 9.75 m 32 ft 0 in
3.1 m 10 ft 2 in height 2.84 m 9 ft 4 in
11.25 m 36 ft 11 in wingspan 11.07 m 36 ft 4 in
1 x Bristol Siddeley Viper 201 engines 1 Orenda J85-CAN-40 turbojet
2,500 lb = 1,134 kg thrust per engine 2,950 lbs
2,500 lb = 1,134 kg total thrust 2,950 lbs
4,173 kg 9,200 lb MTOW 3,331 kg 7,350 lb
1,448 km 782 nm range 1,520 km 821 nm
440 mph 708 km/h cruise speed 310 knots 180 mph
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.