Bombardier CS300 vs. Lockheed U-2

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Bombardier CS300 versus Lockheed U-2
38.0 m 124 ft 7 in length 19.2 m 63 ft 0 in
11.5 m 37 ft 9 in height 4.8 m 15 ft 9 in
35.1 m 115 ft 2 in wingspan 32 m 105 ft
2x Pratt & Whitney PurePower PW1000G engines 1 × General Electric F118-101
93.4 kN thrust per engine 17,000 lbf (76 kN)
186.8 kN total thrust 17,000 lbf (76 kN)
67,585 kg 149,000 lb MTOW 18,144 kg 40,000 lb
5,463 km 2,952 nm range 6,090 nm 11,278 km
871 km/h 541 mph cruise speed 475 mph 764 km/h
130 to 145 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.