Airbus A321neo vs. North American P-51 Mustang
... or view the full comparison list
here.
Airbus A321neo |
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 |
35,000 lb |
thrust per engine |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
70,000 lb |
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 |
828 km/h |
514 mph |
cruise speed |
325 mph |
525 km/h |
180 to 220 passengers |
capacity |
2,000 pounds of bombs, or ten 5-inch rockets |
|
|
rotor diameter |
|
|
|
|
rate of climb |
|
|
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.