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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.