Lockheed Martin F-35 Lightning II vs. North American P-51 Mustang

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Lockheed Martin F-35 Lightning II versus North American P-51 Mustang
15.67 m 51 ft 4 in length 9.83 m 32 ft 3 in
4.33 m 14 ft 2 in height 4.08 m 13 ft 5 in
10.7 m 35 ft 1 in wingspan 11.28 m 37 ft
Pratt & Whitney F135 and GE Rolls-Royce Fighter Engine Team F136 engines Packard Rolls Royce Merlin V-1650-7
40,000 lb thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
40,000 lb total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
31,800 kg 70,000 lb MTOW 5,489 kg 12,100 lb
1,380 mi 1,200 nm range 2,200 km 1,188 nm
520 kt 302 mph cruise speed 325 mph 525 km/h
18,000 pounds of total ordinance 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.