Airbus A310-300 vs. North American P-51 Mustang

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Airbus A310-300 versus North American P-51 Mustang
46.66 m 153 ft 1 in length 9.83 m 32 ft 3 in
15.8 m 51 ft 10 in height 4.08 m 13 ft 5 in
43.9 m 144 ft wingspan 11.28 m 37 ft
2 x General Electric CF6-80 or Pratt & Whitney JT9D then PW4000 turbofan engines Packard Rolls Royce Merlin V-1650-7
52,000 lb thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
104,000 lb total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
148,768 kg 328,000 lb MTOW 5,489 kg 12,100 lb
8,050 km 4,348 nm range 2,200 km 1,188 nm
482 knots 279 mph cruise speed 325 mph 525 km/h
190-230 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.