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.