Lockheed U-2 vs. Polikarpov I-16

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Lockheed U-2 versus Polikarpov I-16
19.2 m 63 ft 0 in length 6.13 m 20 ft 1 in
4.8 m 15 ft 9 in height 3.25 m 10 ft 8 in
32 m 105 ft wingspan 9 m 29 ft 6 in
1 × General Electric F118-101 engines 1x Shvetsov M-25 radial engine
17,000 lbf (76 kN) thrust per engine 1000 hp
17,000 lbf (76 kN) total thrust 1000 hp
18,144 kg 40,000 lb MTOW 2,060 kg 4,540 lb
6,090 nm 11,278 km range 248 mi 216 nm
475 mph 764 km/h cruise speed 180 mph 290 km/h
capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.