Airbus A350-900ULR vs. North American P-51 Mustang
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Airbus A350-900ULR |
versus |
North American P-51 Mustang |
66.80 m |
219 ft 2 in |
length |
9.83 m |
32 ft 3 in |
17.05 m |
55 ft 11 in |
height |
4.08 m |
13 ft 5 in |
64.75 m |
212 ft 5 in |
wingspan |
11.28 m |
37 ft |
2 Rolls-Royce Trent XWB |
engines |
Packard Rolls Royce Merlin V-1650-7 |
84,000 lbs |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
168,000 lbs |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
280,000 kg |
617,300 lb |
MTOW |
5,489 kg |
12,100 lb |
17,964 km |
9,700 nm |
range |
2,200 km |
1,188 nm |
552 mph |
888 km/h |
cruise speed |
325 mph |
525 km/h |
300-350 passengers in three classes |
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.