Airbus A330-200 vs. Lockheed P-2 Neptune
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Airbus A330-200 |
versus |
Lockheed P-2 Neptune |
58.82 m |
193 ft 0 in |
length |
30.17 m |
99 ft 0 in |
17.39 m |
57 ft 1 in |
height |
10.15 m |
33 ft 4 in |
64 m |
210 ft |
wingspan |
33.53 m |
110 ft |
2 Turbofans |
engines |
2 x Wright R-3350 radial engines |
GE CF6-80E1A3: 304.7 kN / 68500 lbf, PW4170: 311.4 kN / 70000 lbf, RR Trent 772C-60: 316.3 kN / 71100 lbf |
thrust per engine |
Approximately 3,700 hp |
Depends on the engine variant |
total thrust |
Approximately 7,400 hp |
251,000 kg |
553,400 lb |
MTOW |
27,216 kg |
60,000 lb |
15,094 km |
8,150 nm |
range |
7,885 km |
4,259 nm |
531 mph |
855 km/h |
cruise speed |
300 mph |
483 km/h |
220-260 |
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.