North American B-25 Mitchell vs. Airbus H225 Super Puma

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North American B-25 Mitchell versus Airbus H225 Super Puma
16.15 m 53 ft 0 in length 14.06 m 46 ft 2 in
5 m 16 ft 4 in height 4.38 m 14 ft 4 in
20.58 m 67 ft 6 in wingspan
2 x Wright R-2600-92 Twin Cyclone engines 2 x Turbomeca Makila 2A turboshaft engines
1,700 horsepower thrust per engine 2,778 hp
3,400 horsepower total thrust 5,556 hp
7,484 kg 16,500 lb MTOW 11,000 kg 24,251 lb
1,350 mi 1,175 nm range 857 km 463 nm
233 MPH 375 km/h cruise speed 242 km/h 150 mph
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.