Airbus A321-200 vs. Airbus H225 Super Puma
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Airbus A321-200 |
versus |
Airbus H225 Super Puma |
44.51 m |
146 ft 0 in |
length |
14.06 m |
46 ft 2 in |
11.76 m |
38 ft 7 in |
height |
4.38 m |
14 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
|
|
2 GE CFM56-5B3 |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
31,600 lbs |
thrust per engine |
2,778 hp |
63,200 lbs |
total thrust |
5,556 hp |
89,000 kg |
196,200 lb |
MTOW |
11,000 kg |
24,251 lb |
4,000 nmi |
7,408 km |
range |
857 km |
463 nm |
871 km/h |
541 mph |
cruise speed |
242 km/h |
150 mph |
185 to 220 |
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.