Lockheed P-2 Neptune vs. Antonov An-225 Mriya

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Lockheed P-2 Neptune versus Antonov An-225 Mriya
30.17 m 99 ft 0 in length 84.0 m 275 ft 7 in
10.15 m 33 ft 4 in height 18.1 m 59 ft 5 in
33.53 m 110 ft wingspan 88.4 m 290 ft 2 in
2 x Wright R-3350 radial engines engines 6 x Ivchenko Progress D-18T turbofan engines
Approximately 3,700 hp thrust per engine Approximately 23,400 kgf per engine
Approximately 7,400 hp total thrust Approximately 140,400 kgf total
27,216 kg 60,000 lb MTOW 640,000 kg 1,411,200 lb
7,885 km 4,259 nm range 15,400 km 8,315 nm
300 mph 483 km/h cruise speed 800 km/h 497 mph
based on configuration capacity based on configuration
rotor diameter
rate of climb
Please note that these values are indicative and actual values can vary based on specific engine models and configurations.