Lockheed U-2 vs. Short C-23 Sherpa

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Lockheed U-2 versus Short C-23 Sherpa
19.2 m 63 ft 0 in length 17.68 m 58 ft 0 in
4.8 m 15 ft 9 in height 6.55 m 21 ft 6 in
32 m 105 ft wingspan 22.76 m 74 ft 8 in
1 × General Electric F118-101 engines 2 x Pratt & Whitney Canada PT6A-45R turboprop engines
17,000 lbf (76 kN) thrust per engine Approximately 1,200 hp per engine
17,000 lbf (76 kN) total thrust Approximately 2,400 hp total
18,144 kg 40,000 lb MTOW 7,484 kg 16,500 lb
6,090 nm 11,278 km range 1,048 km 566 nm
475 mph 764 km/h cruise speed 425 km/h 264 mph
capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.