Airbus A300-600 vs. North American P-51 Mustang

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Airbus A300-600 versus North American P-51 Mustang
54.10 m 177 ft 6 in length 9.83 m 32 ft 3 in
16.5 m 54 ft 2 in height 4.08 m 13 ft 5 in
44.84 m 147 ft 1 in wingspan 11.28 m 37 ft
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 engines Packard Rolls Royce Merlin V-1650-7
56,000lb to 61,500lb thrust per engine 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
112,000–123,000 lb total thrust 1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP)
171,700 kg 378,600 lb MTOW 5,489 kg 12,100 lb
7,500 km 4,052 nm range 2,200 km 1,188 nm
897 km/h 557 mph cruise speed 325 mph 525 km/h
210-250 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.