Lockheed Model 18 Lodestar vs. Airbus H225 Super Puma
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Lockheed Model 18 Lodestar |
versus |
Airbus H225 Super Puma |
13.61 m |
44 ft 8 in |
length |
14.06 m |
46 ft 2 in |
3.63 m |
11 ft 11 in |
height |
4.38 m |
14 ft 4 in |
19.96 m |
65 ft 6 in |
wingspan |
|
|
2 x Wright R-1820 Cyclone radial engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1,200 to 1,350 horsepower (895 to 1,007 kW) |
thrust per engine |
2,778 hp |
2,400 to 2,700 horsepower |
total thrust |
5,556 hp |
9,979 kg |
22,000 lb |
MTOW |
11,000 kg |
24,251 lb |
2,500 km |
1,350 nm |
range |
857 km |
463 nm |
300 km/h |
186 mph |
cruise speed |
242 km/h |
150 mph |
14 passengers |
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.