Lockheed P-2 Neptune vs. Airbus A300-600F

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Lockheed P-2 Neptune versus Airbus A300-600F
30.17 m 99 ft 0 in length 54.08 m 177 ft 5 in
10.15 m 33 ft 4 in height 17.05 m 55 ft 11 in
33.53 m 110 ft wingspan 44.84 m 147 ft 1 in
2 x Wright R-3350 radial engines engines 2 x General Electric CF6-80C2A5 turbofan engines
Approximately 3,700 hp thrust per engine Approximately 59,000 lbf per engine
Approximately 7,400 hp total thrust Approximately 118,000 lbf total
27,216 kg 60,000 lb MTOW 170,000 kg 374,786 lb
7,885 km 4,259 nm range 4,830 km 2,608 nm
300 mph 483 km/h cruise speed 860 km/h 534 mph
based on configuration capacity
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.