Lockheed P-2 Neptune vs. Airbus H225 Super Puma

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Lockheed P-2 Neptune versus Airbus H225 Super Puma
30.17 m 99 ft 0 in length 14.06 m 46 ft 2 in
10.15 m 33 ft 4 in height 4.38 m 14 ft 4 in
33.53 m 110 ft wingspan
2 x Wright R-3350 radial engines engines 2 x Turbomeca Makila 2A turboshaft engines
Approximately 3,700 hp thrust per engine 2,778 hp
Approximately 7,400 hp total thrust 5,556 hp
27,216 kg 60,000 lb MTOW 11,000 kg 24,251 lb
7,885 km 4,259 nm range 857 km 463 nm
300 mph 483 km/h cruise speed 242 km/h 150 mph
based on configuration 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.