Bombardier CRJ700 vs. Lockheed U-2

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Bombardier CRJ700 versus Lockheed U-2
32.51 m 106 ft 8 in length 19.2 m 63 ft 0 in
7.6 m 24 ft 11 in height 4.8 m 15 ft 9 in
23.24 m 76 ft 3 in wingspan 32 m 105 ft
2 x General Electric CF34-8C5B1 turbofans engines 1 × General Electric F118-101
13,790 pounds (61.3 kN) thrust per engine 17,000 lbf (76 kN)
27,580 pounds (122.6 kN) total thrust 17,000 lbf (76 kN)
33,113 kg 73,000 lb MTOW 18,144 kg 40,000 lb
2,655 km 1,434 nm range 6,090 nm 11,278 km
514 mph 828 km/h cruise speed 475 mph 764 km/h
Up to 78 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.