McDonnell-Douglas DC-10-30 vs. Lockheed P-2 Neptune

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McDonnell-Douglas DC-10-30 versus Lockheed P-2 Neptune
55.35 m 181 ft 8 in length 30.17 m 99 ft 0 in
17.8 m 58 ft 5 in height 10.15 m 33 ft 4 in
50.39 m 165 ft 4 in wingspan 33.53 m 110 ft
3x GE CF6-50C Turbofan engines 2 x Wright R-3350 radial engines
54,000 lbf thrust per engine Approximately 3,700 hp
162,000 lbf total thrust Approximately 7,400 hp
251,744 kg 555,000 lb MTOW 27,216 kg 60,000 lb
9,630 km 5,200 nm range 7,885 km 4,259 nm
507 knots 939 km/h cruise speed 300 mph 483 km/h
Up to 380 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.