Airbus A321LR vs. North American P-51 Mustang

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Airbus A321LR versus North American P-51 Mustang
44.51 m 146 ft 0 in length 9.83 m 32 ft 3 in
11.76 m 38 ft 7 in height 4.08 m 13 ft 5 in
35.8 m 117 ft 5 in wingspan 11.28 m 37 ft
CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM engines Packard Rolls Royce Merlin V-1650-7
Over 33,000 lbs (147 kN) thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
66,000 lbs (294 kN) total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
97,000 kg 213,800 lb MTOW 5,489 kg 12,100 lb
7,400 km 4,000 nm range 2,200 km 1,188 nm
832 km/h 517 mph cruise speed 325 mph 525 km/h
180-220 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.