Douglas DC-8 vs. Airbus H225 Super Puma
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Douglas DC-8 |
versus |
Airbus H225 Super Puma |
57.10 m |
187 ft 4 in |
length |
14.06 m |
46 ft 2 in |
16.84 m |
55 ft 3 in |
height |
4.38 m |
14 ft 4 in |
45.24 m |
148 ft 5 in |
wingspan |
|
|
4 x Pratt & Whitney JT3D turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
Approximately 17,000 lbf per engine |
thrust per engine |
2,778 hp |
Approximately 68,000 lbf total |
total thrust |
5,556 hp |
158,760 kg |
350,000 lb |
MTOW |
11,000 kg |
24,251 lb |
11,918 km |
6,437 nm |
range |
857 km |
463 nm |
900 km/h |
559 mph |
cruise speed |
242 km/h |
150 mph |
Up to 259 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.