Lockheed P-38 Lightning vs. Airbus H225 Super Puma
... or view the full comparison list
here.
Lockheed P-38 Lightning |
versus |
Airbus H225 Super Puma |
11.53 m |
37 ft 10 in |
length |
14.06 m |
46 ft 2 in |
3.91 m |
12 ft 10 in |
height |
4.38 m |
14 ft 4 in |
15.85 m |
52 ft |
wingspan |
|
|
Engines: Two Allison V-1710-111/113 V-12 supercharged 4-stroke liquid-cooled engines |
engines |
2 x Turbomeca Makila 2A turboshaft engines |
1,425 hp |
thrust per engine |
2,778 hp |
2,850 hp |
total thrust |
5,556 hp |
9,798 kg |
21,600 lb |
MTOW |
11,000 kg |
24,251 lb |
1,100 nm |
2,037 km |
range |
857 km |
463 nm |
239 knots |
139 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.