Airbus A320-200 vs. North American P-51 Mustang

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Airbus A320-200 versus North American P-51 Mustang
38.7 m 127 ft 0 in length 9.83 m 32 ft 3 in
17.4 m 57 ft 1 in height 4.08 m 13 ft 5 in
35.8 m 117 ft 5 in wingspan 11.28 m 37 ft
Choice between Pratt & Whitney GTF™ and the LEAP-1A from CFM International engines Packard Rolls Royce Merlin V-1650-7
Between 21,000 - 33,000 lbf thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
Between 42,000 - 66,000 lbf total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
77,000 kg 169,800 lb MTOW 5,489 kg 12,100 lb
5,700 km 3,078 nm range 2,200 km 1,188 nm
530 mph 853 km/h cruise speed 325 mph 525 km/h
Typically between 140-180 passengers 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.