Airbus H225 Super Puma vs. Boeing CH-47 Chinook
... or view the full comparison list
here.
| Airbus H225 Super Puma |
versus |
Boeing CH-47 Chinook |
| 14.06 m |
46 ft 2 in |
length |
15.88 m |
51 feet 2 inches |
| 4.38 m |
14 ft 4 in |
height |
5.68 m |
18 feet 7.8 inches |
|
|
wingspan |
|
|
| 2 x Turbomeca Makila 2A turboshaft engines |
engines |
2 x Honeywell T55-GA-714A turboshaft engines |
| 2,778 hp |
thrust per engine |
4,868 hp |
| 5,556 hp |
total thrust |
9,736 hp |
| 11,000 kg |
24,251 lb |
MTOW |
22,680 kg |
50,000 lb |
| 857 km |
463 nm |
range |
370 km |
200 nm |
| 242 km/h |
150 mph |
cruise speed |
259 km/h |
161 mph |
| 24-28 |
capacity |
33-55 |
| 16.2 m |
53 ft 2 in |
rotor diameter |
18.3 m |
60 ft |
| 10.7 m/s |
2,106 ft/min |
rate of climb |
10.2 m/s |
2,008 ft/min |
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.
