Lockheed U-2 vs. Westland Lysander

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Lockheed U-2 versus Westland Lysander
19.2 m 63 ft 0 in length 9.3 m 30 ft 6 in
4.8 m 15 ft 9 in height 3.51 m 11 ft 6 in
32 m 105 ft wingspan 15.24 m 50 ft
1 × General Electric F118-101 engines 1 x Bristol Mercury XII radial engine
17,000 lbf (76 kN) thrust per engine Approximately 870 hp
17,000 lbf (76 kN) total thrust Approximately 870 hp
18,144 kg 40,000 lb MTOW 7,500 lb 3,402 kg
6,090 nm 11,278 km range 966 km 522 nm
475 mph 764 km/h cruise speed 190 mph 306 km/h
capacity Pilot and observer
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.