Airbus A321LR vs. North American P-51 Mustang
... or view the full comparison list
here.
| Airbus A321LR |
versus |
North American P-51 Mustang |
| 44.51 m |
146 ft 0 in |
length |
9.83 m |
32 ft 3 in |
| 11.76 m |
38 ft 7 in |
height |
4.08 m |
13 ft 5 in |
| 35.8 m |
117 ft 5 in |
wingspan |
11.28 m |
37 ft |
| CFM International’s LEAP-1A or Pratt & Whitney’s PurePower PW1100G-JM |
engines |
Packard Rolls Royce Merlin V-1650-7 |
| Over 33,000 lbs (147 kN) |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
| 66,000 lbs (294 kN) |
total thrust |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
| 97,000 kg |
213,800 lb |
MTOW |
5,489 kg |
12,100 lb |
| 7,400 km |
4,000 nm |
range |
2,200 km |
1,188 nm |
| 832 km/h |
517 mph |
cruise speed |
325 mph |
525 km/h |
| 180-220 passengers |
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.
