Concorde vs. Lockheed U-2

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Concorde versus Lockheed U-2
61.66 m 202 ft 4 in length 19.2 m 63 ft 0 in
11.4 m 37 ft 5 in height 4.8 m 15 ft 9 in
25.56 m 83 ft 1 wingspan 32 m 105 ft
4 Rolls Royce/Snecma Olympus 593 turbo jet engines engines 1 × General Electric F118-101
18.7 tons (180 kN) thrust per engine 17,000 lbf (76 kN)
74.8 tons (720 kN) total thrust 17,000 lbf (76 kN)
185,000 kg 408,000 lb MTOW 18,144 kg 40,000 lb
6,580 km 3,554 nm range 6,090 nm 11,278 km
Mach 2.04 2,179 km/h cruise speed 475 mph 764 km/h
92–120 passengers 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.