Airbus A340-600 vs. Lockheed P-2 Neptune
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Airbus A340-600 |
versus |
Lockheed P-2 Neptune |
75.36 m |
247 ft 3 in |
length |
30.17 m |
99 ft 0 in |
17.93 m |
58 ft 10 in |
height |
10.15 m |
33 ft 4 in |
63.45 m |
208 ft 2 in |
wingspan |
33.53 m |
110 ft |
4 x Rolls-Royce Trent 556 |
engines |
2 x Wright R-3350 radial engines |
56,000 lbs |
thrust per engine |
Approximately 3,700 hp |
224,000 lbs |
total thrust |
Approximately 7,400 hp |
380,000 kg |
837,800 lb |
MTOW |
27,216 kg |
60,000 lb |
14,450 km |
7,804 nm |
range |
7,885 km |
4,259 nm |
890 km/h |
553 mph |
cruise speed |
300 mph |
483 km/h |
320-370 |
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.