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

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North American P-51 Mustang versus Airbus A300-600F
9.83 m 32 ft 3 in length 54.08 m 177 ft 5 in
4.08 m 13 ft 5 in height 17.05 m 55 ft 11 in
11.28 m 37 ft wingspan 44.84 m 147 ft 1 in
Packard Rolls Royce Merlin V-1650-7 engines 2 x General Electric CF6-80C2A5 turbofan engines
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) thrust per engine Approximately 59,000 lbf per engine
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) total thrust Approximately 118,000 lbf total
5,489 kg 12,100 lb MTOW 170,000 kg 374,786 lb
2,200 km 1,188 nm range 4,830 km 2,608 nm
325 mph 525 km/h cruise speed 860 km/h 534 mph
2,000 pounds of bombs, or ten 5-inch rockets capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.