Lockheed U-2 vs. Canadair CL-415

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Lockheed U-2 versus Canadair CL-415
19.2 m 63 ft 0 in length 19.82 m 65 ft 0 in
4.8 m 15 ft 9 in height 8.66 m 28 ft 5 in
32 m 105 ft wingspan 28.6 m 93 ft 1
1 × General Electric F118-101 engines 2 x Pratt & Whitney Canada PW123AF turboprop engines
17,000 lbf (76 kN) thrust per engine 2,150 to 2,380 shaft horsepower (1,602 to 1,775 kW)
17,000 lbf (76 kN) total thrust 4,300 to 4,760 shaft horsepower
18,144 kg 40,000 lb MTOW 19,733 kg 43,525 lb
6,090 nm 11,278 km range 1,600 km 864 nm
475 mph 764 km/h cruise speed 290 km/h 180 mph
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.