Airbus A350-1000 vs. Airbus H225 Super Puma
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Airbus A350-1000 |
versus |
Airbus H225 Super Puma |
73.79 m |
242 ft 1 in |
length |
14.06 m |
46 ft 2 in |
17.08 m |
56 ft |
height |
4.38 m |
14 ft 4 in |
64.75 m |
212 ft 5 in |
wingspan |
|
|
2 Trent XWB-97 turbofan engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
97,000 lb |
thrust per engine |
2,778 hp |
194,000 lb |
total thrust |
5,556 hp |
319,000 kg |
703,300 lb |
MTOW |
11,000 kg |
24,251 lb |
16,100 km |
8,695 nm |
range |
857 km |
463 nm |
1,099 km/h |
683 mph |
cruise speed |
242 km/h |
150 mph |
350 to 410 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.