Douglas C-54 Skymaster vs. Airbus H225 Super Puma
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Douglas C-54 Skymaster |
versus |
Airbus H225 Super Puma |
28.60 m |
93 ft 10 in |
length |
14.06 m |
46 ft 2 in |
8.38 m |
27 ft 6 in |
height |
4.38 m |
14 ft 4 in |
35.81 m |
117 ft 6 in |
wingspan |
|
|
4 x Pratt & Whitney R-2000 Twin Wasp radial engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1,200 to 1,450 horsepower (895 to 1,080 kW) |
thrust per engine |
2,778 hp |
4,800 to 5,800 horsepower |
total thrust |
5,556 hp |
29,484 kg |
65,000 lb |
MTOW |
11,000 kg |
24,251 lb |
6,500 km |
3,510 nm |
range |
857 km |
463 nm |
340 km/h |
211 mph |
cruise speed |
242 km/h |
150 mph |
Up to 50 passengers or 28,500 lb cargo |
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.