Airbus A340-200 vs. North American P-51 Mustang
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Airbus A340-200 |
versus |
North American P-51 Mustang |
59.4 m |
194 ft 11 in |
length |
9.83 m |
32 ft 3 in |
16.8 m |
55 ft 1 in |
height |
4.08 m |
13 ft 5 in |
60.3 m |
197 ft 9 in |
wingspan |
11.28 m |
37 ft |
4 x CFM International CFM56-5C4 |
engines |
Packard Rolls Royce Merlin V-1650-7 |
34,000 lbf |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
136,000 lbf |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
275,000 kg |
606,300 lb |
MTOW |
5,489 kg |
12,100 lb |
12,400 km |
6,699 nm |
range |
2,200 km |
1,188 nm |
880 km/h |
547 mph |
cruise speed |
325 mph |
525 km/h |
Typical seating 3-class 210-250 |
capacity |
2,000 pounds of bombs, or ten 5-inch rockets |
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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.