Boeing 747-8I vs. Lockheed P-2 Neptune

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Boeing 747-8I versus Lockheed P-2 Neptune
76.25 m 250 ft 2 in length 30.17 m 99 ft 0 in
19.35 m 63 ft 6 in height 10.15 m 33 ft 4 in
68.45 m 224 ft 7 in wingspan 33.53 m 110 ft
4x General Electric GEnx 2B67 Turbofan engines 2 x Wright R-3350 radial engines
66,500 pounds thrust per engine Approximately 3,700 hp
266,000 pounds total thrust Approximately 7,400 hp
443,613 kg 977,500 lb MTOW 27,216 kg 60,000 lb
8,000 nm 14,816 km range 7,885 km 4,259 nm
Mach 0.86 1,062 km/h cruise speed 300 mph 483 km/h
467 passengers (three-class 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.