Lockheed U-2 vs. Beechcraft King Air 350

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Lockheed U-2 versus Beechcraft King Air 350
19.2 m 63 ft 0 in length 14.27 m 46 ft 9 in
4.8 m 15 ft 9 in height 4.35 m 14 ft 3 in
32 m 105 ft wingspan 17.38 m 57 ft 1 in
1 × General Electric F118-101 engines 2 x Pratt & Whitney Canada PT6A turboprop
17,000 lbf (76 kN) thrust per engine 1050 lbs
17,000 lbf (76 kN) total thrust 2100 lbs
18,144 kg 40,000 lb MTOW 15,000 lb 6,804 kg
6,090 nm 11,278 km range 1,805 nm 3,342 km
475 mph 764 km/h cruise speed 312 kts 194 mph
capacity 9
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.