Lockheed U-2 vs. Aero Commander 690

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Lockheed U-2 versus Aero Commander 690
19.2 m 63 ft 0 in length 12.04 m 39 ft 6 in
4.8 m 15 ft 9 in height 3.75 m 12 ft 4 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 380 lbs
17,000 lbf (76 kN) total thrust 760 lbs
18,144 kg 40,000 lb MTOW 8,000 lb 3,629 kg
6,090 nm 11,278 km range 1,600 nm 2,963 km
475 mph 764 km/h cruise speed 260 kts 162 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.