Lockheed U-2 vs. Aero Commander 560

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Lockheed U-2 versus Aero Commander 560
19.2 m 63 ft 0 in length 10.88 m 35 ft 8 in
4.8 m 15 ft 9 in height 3.6 m 11 ft 10 in
32 m 105 ft wingspan 15.02 m 49 ft 3 in
1 × General Electric F118-101 engines 2 x Lycoming TIO-540
17,000 lbf (76 kN) thrust per engine 340 lbs
17,000 lbf (76 kN) total thrust 680 lbs
18,144 kg 40,000 lb MTOW 6,000 lb 2,722 kg
6,090 nm 11,278 km range 1,200 nm 2,222 km
475 mph 764 km/h cruise speed 210 kts 130 mph
capacity Up to 6 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.