Lockheed C-69 Constellation vs. Airbus H225 Super Puma

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Lockheed C-69 Constellation versus Airbus H225 Super Puma
29.72 m 97 ft 6 in length 14.06 m 46 ft 2 in
6.02 m 19 ft 9 in height 4.38 m 14 ft 4 in
37.49 m 123 ft wingspan
4 x Wright R-3350 Duplex-Cyclone radial engines engines 2 x Turbomeca Makila 2A turboshaft engines
2,200 to 3,700 horsepower (1,640 to 2,760 kW) thrust per engine 2,778 hp
8,800 to 14,800 horsepower total thrust 5,556 hp
44,453 kg 98,000 lb MTOW 11,000 kg 24,251 lb
5,200 km 2,808 nm range 857 km 463 nm
507 km/h 315 mph cruise speed 242 km/h 150 mph
Up to 109 passengers 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.