Boeing 787-10 vs. Airbus H225 Super Puma
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Boeing 787-10 |
versus |
Airbus H225 Super Puma |
68.0 m |
223 ft 2 in |
length |
14.06 m |
46 ft 2 in |
17 m |
55 ft 9 in |
height |
4.38 m |
14 ft 4 in |
60 m |
196 ft 1 |
wingspan |
|
|
2x Rolls-Royce Trent 1000 or General Electric GEnx-1B |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
76,000 N |
thrust per engine |
2,778 hp |
2 x 76,000 N |
total thrust |
5,556 hp |
254,000 kg |
560,000 lb |
MTOW |
11,000 kg |
24,251 lb |
11,910 km |
6,430 nmi |
range |
857 km |
463 nm |
652 mph |
1,050 kph |
cruise speed |
242 km/h |
150 mph |
330 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.