North American P-51 Mustang vs. Airbus H225 Super Puma

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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.