Lockheed Ventura vs. Airbus H225 Super Puma

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Lockheed Ventura versus Airbus H225 Super Puma
15.7 m 51 ft 5 in length 14.06 m 46 ft 2 in
3.6 m 11 ft 10 in height 4.38 m 14 ft 4 in
20 m 65 ft 7 in wingspan
2 x Pratt & Whitney R-2800 radial engines engines 2 x Turbomeca Makila 2A turboshaft engines
2,000 hp thrust per engine 2,778 hp
4,000 hp total thrust 5,556 hp
15,000 kg 33,100 lb MTOW 11,000 kg 24,251 lb
2,670 km 1,440 nmi range 857 km 463 nm
230 mph 370 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.