de Havilland Venom vs. Lockheed U-2

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de Havilland Venom versus Lockheed U-2
6.71 m 22 ft 0 in length 19.2 m 63 ft 0 in
1.88 m 6 ft 2 in height 4.8 m 15 ft 9 in
12.7 m 41 ft 8 in wingspan 32 m 105 ft
1 (de Havilland Ghost 105) engines 1 × General Electric F118-101
23.6 kN thrust per engine 17,000 lbf (76 kN)
23.6 kN total thrust 17,000 lbf (76 kN)
6,945 kg 15,300 lb MTOW 18,144 kg 40,000 lb
1,730 km 935 nm range 6,090 nm 11,278 km
1030 km/h 640 mph 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.