Lockheed U-2 vs. Aero Commander 500S

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Lockheed U-2 versus Aero Commander 500S
19.2 m 63 ft 0 in length 10.46 m 34 ft 4 in
4.8 m 15 ft 9 in height 3.63 m 11 ft 11 in
32 m 105 ft wingspan 13.52 m 44 ft 4 in
1 × General Electric F118-101 engines 2 x Lycoming IO-540
17,000 lbf (76 kN) thrust per engine 380 lbs
17,000 lbf (76 kN) total thrust 760 lbs
18,144 kg 40,000 lb MTOW 11,500 lb 5,216 kg
6,090 nm 11,278 km range 1,350 nm 2,500 km
475 mph 764 km/h cruise speed 230 kts 143 mph
capacity Up to 4 passengers
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.