Douglas DC-8-61 vs. Lockheed P-2 Neptune

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Douglas DC-8-61 versus Lockheed P-2 Neptune
57.0 m 187 ft 0 in length 30.17 m 99 ft 0 in
13.1 m 43 ft height 10.15 m 33 ft 4 in
45.24 m 148 ft 5 in wingspan 33.53 m 110 ft
4x P&W JT3D-3B Turbofan engines 2 x Wright R-3350 radial engines
18,000 pound-force thrust per engine Approximately 3,700 hp
72,000 pound-force total thrust Approximately 7,400 hp
147,400 kg 325,000 lb MTOW 27,216 kg 60,000 lb
3,200 nm 5,926 km range 7,885 km 4,259 nm
483 knots 282 mph cruise speed 300 mph 483 km/h
180 to 220 passengers in a mixed-class seating 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.