Lockheed U-2 vs. Percival Provost

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Lockheed U-2 versus Percival Provost
19.2 m 63 ft 0 in length 9.0 m 29 ft 6 in
4.8 m 15 ft 9 in height 3.02 m 9 ft 11 in
32 m 105 ft wingspan 12.19 m 40 ft
1 × General Electric F118-101 engines 1 x Alvis Leonides Major 755/1 inline engine
17,000 lbf (76 kN) thrust per engine Approximately 550 hp
17,000 lbf (76 kN) total thrust Approximately 550 hp
18,144 kg 40,000 lb MTOW 5,500 lb 2,495 kg
6,090 nm 11,278 km range 1,127 km 608 nm
475 mph 764 km/h cruise speed 175 mph 282 km/h
capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.