Airbus A330-200 vs. North American P-51 Mustang

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Airbus A330-200 versus North American P-51 Mustang
58.82 m 193 ft 0 in length 9.83 m 32 ft 3 in
17.39 m 57 ft 1 in height 4.08 m 13 ft 5 in
64 m 210 ft wingspan 11.28 m 37 ft
2 Turbofans engines Packard Rolls Royce Merlin V-1650-7
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
Depends on the engine variant total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
251,000 kg 553,400 lb MTOW 5,489 kg 12,100 lb
15,094 km 8,150 nm range 2,200 km 1,188 nm
531 mph 855 km/h cruise speed 325 mph 525 km/h
220-260 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.