Lockheed P-2 Neptune vs. Airbus A380-800F

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Lockheed P-2 Neptune versus Airbus A380-800F
30.17 m 99 ft 0 in length 72.73 m 238 ft 7 in
10.15 m 33 ft 4 in height 24.09 m 79 ft
33.53 m 110 ft wingspan 79.75 m 261 ft 8 in
2 x Wright R-3350 radial engines engines 4 x Engine Alliance GP7200 turbofan engines
Approximately 3,700 hp thrust per engine 70,000 to 80,000 pounds of thrust (311 to 356 kilonewtons)
Approximately 7,400 hp total thrust 280,000 to 320,000 pounds
27,216 kg 60,000 lb MTOW 590,000 kg 1,300,733 lb
7,885 km 4,259 nm range 14,800 km 7,992 nm
300 mph 483 km/h cruise speed 903 km/h 561 mph
based on configuration capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.