McDonnell-Douglas DC-9-30 vs. Lockheed P-2 Neptune

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McDonnell-Douglas DC-9-30 versus Lockheed P-2 Neptune
36.36 m 119 ft 3 in length 30.17 m 99 ft 0 in
8.5 m 27 ft 11 in height 10.15 m 33 ft 4 in
28.44 m 93 ft 4 in wingspan 33.53 m 110 ft
2x Pratt & Whitney JT8D engines 2 x Wright R-3350 radial engines
15,000 pound-force thrust per engine Approximately 3,700 hp
30,000 pound-force (2 engines) total thrust Approximately 7,400 hp
54,885 kg 121,000 lb MTOW 27,216 kg 60,000 lb
2,632 km 1,422 nm range 7,885 km 4,259 nm
898 km/h 558 mph cruise speed 300 mph 483 km/h
Up to 139 passengers 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.