Bombardier CRJ900 vs. Lockheed U-2

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Bombardier CRJ900 versus Lockheed U-2
36.2 m 118 ft 11 in length 19.2 m 63 ft 0 in
7.5 m 24 ft 7 in height 4.8 m 15 ft 9 in
24.9 m 81 ft 8 in wingspan 32 m 105 ft
2 Turbofans (fuselage mounted) engines 1 × General Electric F118-101
13,360 pounds force thrust per engine 17,000 lbf (76 kN)
26,720 pounds force total thrust 17,000 lbf (76 kN)
38,330 kg 84,500 lb MTOW 18,144 kg 40,000 lb
2,871 km 1,550 nm range 6,090 nm 11,278 km
515 mph 829 km/h cruise speed 475 mph 764 km/h
Up to 90 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.