Airbus A321-200 vs. North American P-51 Mustang

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Airbus A321-200 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
2 GE CFM56-5B3 engines Packard Rolls Royce Merlin V-1650-7
31,600 lbs thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
63,200 lbs total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
89,000 kg 196,200 lb MTOW 5,489 kg 12,100 lb
4,000 nmi 7,408 km range 2,200 km 1,188 nm
871 km/h 541 mph cruise speed 325 mph 525 km/h
185 to 220 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.