North American P-51 Mustang vs. Airbus H225 Super Puma
... or view the full comparison list
here.
North American P-51 Mustang |
versus |
Airbus H225 Super Puma |
9.83 m |
32 ft 3 in |
length |
14.06 m |
46 ft 2 in |
4.08 m |
13 ft 5 in |
height |
4.38 m |
14 ft 4 in |
11.28 m |
37 ft |
wingspan |
|
|
Packard Rolls Royce Merlin V-1650-7 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
thrust per engine |
2,778 hp |
1,490 horsepower at 3,000 rpm and 1,720 horsepower at war emergency power (WEP) |
total thrust |
5,556 hp |
5,489 kg |
12,100 lb |
MTOW |
11,000 kg |
24,251 lb |
2,200 km |
1,188 nm |
range |
857 km |
463 nm |
325 mph |
525 km/h |
cruise speed |
242 km/h |
150 mph |
2,000 pounds of bombs, or ten 5-inch rockets |
capacity |
24-28 |
|
|
rotor diameter |
16.2 m |
53 ft 2 in |
|
|
rate of climb |
10.7 m/s |
2,106 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.