Lockheed U-2 vs. Aero Commander 1000

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Lockheed U-2 versus Aero Commander 1000
19.2 m 63 ft 0 in length 13.67 m 44 ft 10 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 Pratt & Whitney Canada PT6A-28
17,000 lbf (76 kN) thrust per engine 450 lbs
17,000 lbf (76 kN) total thrust 900 lbs
18,144 kg 40,000 lb MTOW 10,500 lb 4,763 kg
6,090 nm 11,278 km range 1,750 nm 3,241 km
475 mph 764 km/h cruise speed 282 kts 175 mph
capacity Up to 8 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.