Lockheed U-2 vs. Aero Commander 520

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Lockheed U-2 versus Aero Commander 520
19.2 m 63 ft 0 in length 11.18 m 36 ft 8 in
4.8 m 15 ft 9 in height 3.45 m 11 ft 4 in
32 m 105 ft wingspan 14.28 m 46 ft 1
1 × General Electric F118-101 engines 2 x Lycoming IO-540
17,000 lbf (76 kN) thrust per engine 400 lbs
17,000 lbf (76 kN) total thrust 800 lbs
18,144 kg 40,000 lb MTOW 8,500 lb 3,856 kg
6,090 nm 11,278 km range 850 nm 1,574 km
475 mph 764 km/h cruise speed 210 kts 130 mph
capacity 5
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.