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  • Lockheed P-2 Neptune

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    Description

    The Lockheed P-2 Neptune (designated P2V by the United States Navy prior to September 1962) was a maritime patrol and anti-submarine warfare (ASW) aircraft.

    General Information

    The Neptune was developed for the US Navy by Lockheed to replace the Lockheed PV-1 Ventura and PV-2 Harpoon, and was replaced in turn by the Lockheed P-3 Orion. Designed as a land-based aircraft, the Neptune never made a carrier landing, but a small number were converted and deployed as carrier-launched, stop-gap nuclear bombers that would have to land on shore or ditch. The type was successful in export, and saw service with several armed forces.

     

    Beginning with the P2V-5F model, the Neptune became one of the first operational aircraft fitted with both piston and jet engines.

     

    Neptunes were operated by RAAF Squadrons 10 and 11 from RAAF Edinburgh, South Australia.

     

    For full details on the Neptune P-2 and its variants, click here.

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    lockheed-neptune-nearing-touchdown-ymav-20150301.jpg_thumb.7d1d0c87cd283376dde7b8524d36dcf1.jpg

    lockheed-p2v-7-neptune-a89-273-side-on-ymav-20110306.jpg_thumb.c200b24ffe2936c7265b777027ab98cb.jpg

    lockheed-p2v-7-neptune-a89-273-ymav-20110306.jpg_thumb.49c68b91db5da6a411599aab2c88bf9e.jpg

    Specifications

    Seats:
    Crew: 7–9
    Length:
    91 ft 8 in (27.94 m)
    Wingspan:
    103 ft 10 in (31.65 m)
    Height:
    29 ft 4 in (8.94 m)
    Wing Area:
    1,000 ft² (92.9 m²)
    Empty Weight:
    49,935 lb (22,650 kg)
    MTOW:
    79,895 lb (35,240 kg)
    Powerplant:
    2 × Westinghouse J34-WE-34 turbojet, 3,400 lbf (15.1 kN) each; 2 × Wright R-3350-32W Cyclone Turbo-compound radial engine, 3,700 hp (2,759 kW) wet each
    Vne:
    Maximum speed: 316 kn (363 mp/h) (586 km/h) (all engines)
    Cruise Speed:
    180 kn (207 mp/h) (333 km/h) (max)
    Range:
    1,912 nmi (2,157 mi) (3,540 km)

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