Lockheed U-2 vs. North American P-51 Mustang

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Lockheed U-2 versus North American P-51 Mustang
19.2 m 63 ft 0 in length 9.83 m 32 ft 3 in
4.8 m 15 ft 9 in height 4.08 m 13 ft 5 in
32 m 105 ft wingspan 11.28 m 37 ft
1 × General Electric F118-101 engines Packard Rolls Royce Merlin V-1650-7
17,000 lbf (76 kN) thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
17,000 lbf (76 kN) total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
18,144 kg 40,000 lb MTOW 5,489 kg 12,100 lb
6,090 nm 11,278 km range 2,200 km 1,188 nm
475 mph 764 km/h cruise speed 325 mph 525 km/h
capacity 2,000 pounds of bombs, or ten 5-inch rockets
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.