Auster AOP.6 vs. Airbus H225 Super Puma
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Auster AOP.6 |
versus |
Airbus H225 Super Puma |
7.24 m |
23 ft 9 in |
length |
14.06 m |
46 ft 2 in |
2.55 m |
8 ft 4 in |
height |
4.38 m |
14 ft 4 in |
10.97 m |
36 ft |
wingspan |
|
|
1× de Havilland Gipsy Major 7 inline piston |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
145 hp (108 kW) |
thrust per engine |
2,778 hp |
145 hp (108 kW) |
total thrust |
5,556 hp |
2,160 lb |
980 kg |
MTOW |
11,000 kg |
24,251 lb |
507 km |
274 nm |
range |
857 km |
463 nm |
174 km/h |
108 mph |
cruise speed |
242 km/h |
150 mph |
|
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.