Lockheed P-2 Neptune vs. Antonov An-124 Ruslan

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Lockheed P-2 Neptune versus Antonov An-124 Ruslan
30.17 m 99 ft 0 in length 69.10 m 226 ft 9 in
10.15 m 33 ft 4 in height 20.78 m 68 ft 2 in
33.53 m 110 ft wingspan 73.3 m 240 ft 6 in
2 x Wright R-3350 radial engines engines 4 x Ivchenko Progress D-18T turbofan engines
Approximately 3,700 hp thrust per engine Approximately 51,590 lbf
Approximately 7,400 hp total thrust Approximately 206,360 lbf
27,216 kg 60,000 lb MTOW 405,000 kg 893,000 lb
7,885 km 4,259 nm range 3,700 km 1,998 nm
300 mph 483 km/h cruise speed 800 km/h 497 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.