Douglas DC-8-61 vs. Airbus H225 Super Puma
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here.
Douglas DC-8-61 |
versus |
Airbus H225 Super Puma |
57.0 m |
187 ft 0 in |
length |
14.06 m |
46 ft 2 in |
13.1 m |
43 ft |
height |
4.38 m |
14 ft 4 in |
45.24 m |
148 ft 5 in |
wingspan |
|
|
4x P&W JT3D-3B Turbofan |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
18,000 pound-force |
thrust per engine |
2,778 hp |
72,000 pound-force |
total thrust |
5,556 hp |
147,400 kg |
325,000 lb |
MTOW |
11,000 kg |
24,251 lb |
3,200 nm |
5,926 km |
range |
857 km |
463 nm |
483 knots |
282 mph |
cruise speed |
242 km/h |
150 mph |
180 to 220 passengers in a mixed-class seating |
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.