McDonnell-Douglas MD-11 vs. Lockheed P-2 Neptune

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McDonnell-Douglas MD-11 versus Lockheed P-2 Neptune
61.20 m 200 ft 10 in length 30.17 m 99 ft 0 in
17.6 m 57 ft 9 in height 10.15 m 33 ft 4 in
51.6 m 169 ft 4 in wingspan 33.53 m 110 ft
3 (General Electric CF6-80C2D1F or Pratt & Whitney PW4460 or PW4462) engines 2 x Wright R-3350 radial engines
273.1 kN (GE CF6-80C2D1F) or 266.9 kN (PW4460) thrust per engine Approximately 3,700 hp
819.3 kN (GE CF6-80C2D1F) or 800.7 kN (PW4460) total thrust Approximately 7,400 hp
285,990 kg 630,400 lb MTOW 27,216 kg 60,000 lb
13,231 km 7,147 nm range 7,885 km 4,259 nm
961 km/h 597 mph cruise speed 300 mph 483 km/h
Max 410 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.