Boeing 787-8 vs. Airbus H225 Super Puma
... or view the full comparison list
here.
Boeing 787-8 |
versus |
Airbus H225 Super Puma |
57.0 m |
187 ft 0 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 |
|
|
GEnx-1B / Trent 1000 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
265.1 kN (59600 lbf) for Trent 1000-E, 321.6 kN (72300 lbf) for GEnx-1B70 |
thrust per engine |
2,778 hp |
2 * 265.1 kN (59600 lbf) for Trent 1000-E, 2 * 321.6 kN (72300 lbf) for GEnx-1B70 |
total thrust |
5,556 hp |
227,930 kg |
502,500 lb |
MTOW |
11,000 kg |
24,251 lb |
13,530 km |
7,305 nmi |
range |
857 km |
463 nm |
652 mph |
1,050 kph |
cruise speed |
242 km/h |
150 mph |
248 |
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.