Lockheed U-2 vs. Cessna 172

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Lockheed U-2 versus Cessna 172
19.2 m 63 ft 0 in length 8.28 m 27 ft 2 in
4.8 m 15 ft 9 in height 2.72 m 8 ft 11 in
32 m 105 ft wingspan 11 m 36 ft 1 in
1 × General Electric F118-101 engines 1 x Lycoming IO-360-L2A flat-4 piston engine
17,000 lbf (76 kN) thrust per engine 180 to 200 horsepower (134 to 149 kW)
17,000 lbf (76 kN) total thrust 180 to 200 horsepower (134 to 149 kW)
18,144 kg 40,000 lb MTOW 1,040 kg 2,293 lb
6,090 nm 11,278 km range 1,056 km 570 nm
475 mph 764 km/h cruise speed 226 km/h 140 mph
capacity 4
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.