Lockheed U-2 vs. Cessna 152

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Lockheed U-2 versus Cessna 152
19.2 m 63 ft 0 in length 7.34 m 24 ft 1 in
4.8 m 15 ft 9 in height 2.59 m 8 ft 6 in
32 m 105 ft wingspan 10.16 m 33 ft 4 in
1 × General Electric F118-101 engines 1 x Lycoming O-235-L2C flat-4 piston engine
17,000 lbf (76 kN) thrust per engine 115 horsepower (86 kW)
17,000 lbf (76 kN) total thrust 115 horsepower (86 kW)
18,144 kg 40,000 lb MTOW 757 kg 1,669 lb
6,090 nm 11,278 km range 610 km 329 nm
475 mph 764 km/h cruise speed 185 km/h 115 mph
capacity 2
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.