Lockheed U-2 vs. Cirrus Vision SF50

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Lockheed U-2 versus Cirrus Vision SF50
19.2 m 63 ft 0 in length 9.36 m 30 ft 9 in
4.8 m 15 ft 9 in height 3.32 m 10 ft 11 in
32 m 105 ft wingspan 11.79 m 38 ft 8 in
1 × General Electric F118-101 engines 1 x Williams FJ33
17,000 lbf (76 kN) thrust per engine 1800 lbs
17,000 lbf (76 kN) total thrust 1800 lbs
18,144 kg 40,000 lb MTOW 6,000 lb 2,722 kg
6,090 nm 11,278 km range 1240 nm 2,296 km
475 mph 764 km/h cruise speed 300 kts 186 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.