de Havilland Canada DHC-2 Beaver vs. Lockheed P-2 Neptune

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de Havilland Canada DHC-2 Beaver versus Lockheed P-2 Neptune
13.56 m 44 ft 6 in length 30.17 m 99 ft 0 in
5 m 16 ft 5 in height 10.15 m 33 ft 4 in
16.56 m 54 ft 4 in wingspan 33.53 m 110 ft
2 x Armstrong Siddeley Double Mamba turboprop engines engines 2 x Wright R-3350 radial engines
Approximately 3,100 hp (2,312 kW) each thrust per engine Approximately 3,700 hp
Approximately 6,200 hp (4,624 kW) total total thrust Approximately 7,400 hp
24,200 lb 10,977 kg MTOW 27,216 kg 60,000 lb
2,535 km 1,369 nm range 7,885 km 4,259 nm
228 mph 367 km/h cruise speed 300 mph 483 km/h
Pilot and Observer, plus various configurations for reconnaissance, anti-submarine warfare, and aerial refueling 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.