Boeing 747-8F vs. Airbus H225 Super Puma
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Boeing 747-8F |
versus |
Airbus H225 Super Puma |
76.25 m |
250 ft 2 in |
length |
14.06 m |
46 ft 2 in |
19.33 m |
63 ft 5 in |
height |
4.38 m |
14 ft 4 in |
68.4 m |
224 ft 6 in |
wingspan |
|
|
4 x General Electric GEnx-2B67 turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
Approximately 66,500 lbf |
thrust per engine |
2,778 hp |
Approximately 266,000 lbf |
total thrust |
5,556 hp |
442,253 kg |
975,000 lb |
MTOW |
11,000 kg |
24,251 lb |
8,130 km |
4,390 nm |
range |
857 km |
463 nm |
919 km/h |
571 mph |
cruise speed |
242 km/h |
150 mph |
|
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.