Airbus A380-800 vs. Lockheed P-2 Neptune

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Airbus A380-800 versus Lockheed P-2 Neptune
72.72 m 238 ft 7 in length 30.17 m 99 ft 0 in
24.09 m 79 ft height 10.15 m 33 ft 4 in
79.75 m 261 ft 8 in wingspan 33.53 m 110 ft
4 engines 2 x Wright R-3350 radial engines
70000lbs thrust per engine Approximately 3,700 hp
280000lbs total thrust Approximately 7,400 hp
560,000 kg 1,234,600 lb MTOW 27,216 kg 60,000 lb
14,800 km 8,000 nm range 7,885 km 4,259 nm
1,050 km/h 652 mph cruise speed 300 mph 483 km/h
525-853 passengers capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.