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 |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.