Airbus A321-200 vs. Lockheed P-2 Neptune
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Airbus A321-200 |
versus |
Lockheed P-2 Neptune |
44.51 m |
146 ft 0 in |
length |
30.17 m |
99 ft 0 in |
11.76 m |
38 ft 7 in |
height |
10.15 m |
33 ft 4 in |
35.8 m |
117 ft 5 in |
wingspan |
33.53 m |
110 ft |
2 GE CFM56-5B3 |
engines |
2 x Wright R-3350 radial engines |
31,600 lbs |
thrust per engine |
Approximately 3,700 hp |
63,200 lbs |
total thrust |
Approximately 7,400 hp |
89,000 kg |
196,200 lb |
MTOW |
27,216 kg |
60,000 lb |
4,000 nmi |
7,408 km |
range |
7,885 km |
4,259 nm |
871 km/h |
541 mph |
cruise speed |
300 mph |
483 km/h |
185 to 220 |
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.