Bombardier CS100 vs. Lockheed U-2

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Bombardier CS100 versus Lockheed U-2
35.00 m 114 ft 10 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
2 x Pratt & Whitney PurePower PW1500G engines 1 × General Electric F118-101
84.1 kN thrust per engine 17,000 lbf (76 kN)
168.2 kN total thrust 17,000 lbf (76 kN)
54,931 kg 121,100 lb MTOW 18,144 kg 40,000 lb
4,074 km 2,200 nm range 6,090 nm 11,278 km
871 km/h 541 mph cruise speed 475 mph 764 km/h
110 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.