Lockheed Ventura vs. Airbus H225 Super Puma
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Lockheed Ventura |
versus |
Airbus H225 Super Puma |
15.7 m |
51 ft 5 in |
length |
14.06 m |
46 ft 2 in |
3.6 m |
11 ft 10 in |
height |
4.38 m |
14 ft 4 in |
20 m |
65 ft 7 in |
wingspan |
|
|
2 x Pratt & Whitney R-2800 radial engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
2,000 hp |
thrust per engine |
2,778 hp |
4,000 hp |
total thrust |
5,556 hp |
15,000 kg |
33,100 lb |
MTOW |
11,000 kg |
24,251 lb |
2,670 km |
1,440 nmi |
range |
857 km |
463 nm |
230 mph |
370 km/h |
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.