BAC Jet Provost vs. Lockheed U-2

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BAC Jet Provost versus Lockheed U-2
10.36 m 34 ft 0 in length 19.2 m 63 ft 0 in
3.1 m 10 ft 2 in height 4.8 m 15 ft 9 in
11.25 m 36 ft 11 in wingspan 32 m 105 ft
1 x Bristol Siddeley Viper 201 engines 1 × General Electric F118-101
2,500 lb = 1,134 kg thrust per engine 17,000 lbf (76 kN)
2,500 lb = 1,134 kg total thrust 17,000 lbf (76 kN)
4,173 kg 9,200 lb MTOW 18,144 kg 40,000 lb
1,448 km 782 nm range 6,090 nm 11,278 km
440 mph 708 km/h 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.