Lockheed U-2 vs. Nanchang CJ-6

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Lockheed U-2 versus Nanchang CJ-6
19.2 m 63 ft 0 in length 8.48 m 27 ft 10 in
4.8 m 15 ft 9 in height 2.67 m 8 ft 9 in
32 m 105 ft wingspan 10.49 m 34 ft 5 in
1 × General Electric F118-101 engines 1 x Ivchenko AI-14RA radial engine
17,000 lbf (76 kN) thrust per engine Approximately 260 hp
17,000 lbf (76 kN) total thrust Approximately 260 hp
18,144 kg 40,000 lb MTOW 3,858 lb 1,751 kg
6,090 nm 11,278 km range 800 km 432 nm
475 mph 764 km/h cruise speed 155 mph 249 km/h
capacity Pilot and one passenger
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.