Bombardier CRJ1000 vs. Lockheed U-2

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Bombardier CRJ1000 versus Lockheed U-2
39.1 m 128 ft 5 in length 19.2 m 63 ft 0 in
7.5 m 24 ft 7 in height 4.8 m 15 ft 9 in
26.2 m 86 ft wingspan 32 m 105 ft
2 GE CF34-8C5A1 turbofans engines 1 × General Electric F118-101
13,630 lb of force or 60.6 kN at takeoff, 14,510 lb of force or 64.5 kN thrust APR Automatic Power Reserve thrust per engine 17,000 lbf (76 kN)
27,260 lb of force or 121.2 kN at takeoff, 29,020 lb of force or 129 kN thrust APR Automatic Power Reserve total thrust 17,000 lbf (76 kN)
41,640 kg 91,800 lb MTOW 18,144 kg 40,000 lb
3,004 km 1,623 nm range 6,090 nm 11,278 km
515 mph 829 km/h cruise speed 475 mph 764 km/h
100 (common) 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.