Lockheed U-2 vs. Mitsubishi A6M Zero

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Lockheed U-2 versus Mitsubishi A6M Zero
19.2 m 63 ft 0 in length 9.06 m 29 ft 9 in
4.8 m 15 ft 9 in height 3.05 m 10 ft
32 m 105 ft wingspan 12 m 39 ft 4 in
1 × General Electric F118-101 engines 1 × Nakajima NK1C Sakae-12 14-cylinder air-cooled radial piston engine
17,000 lbf (76 kN) thrust per engine 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
17,000 lbf (76 kN) total thrust 940 hp for take-off, 950 hp at 4,200 m (13,800 ft)
18,144 kg 40,000 lb MTOW 2,800 kg 6,170 lb
6,090 nm 11,278 km range 1,010 nm 1,871 km
475 mph 764 km/h cruise speed 180 knots 105 mph
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.