Lockheed P-38 Lightning vs. Airbus H225 Super Puma

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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.