Lockheed
P-2 / P2V
Neptune
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P2V-7
 Photo: Robert Deering 1986
National Museum of Naval Aviation
NAS Pensacola (NPA)
Pensacola, Florida
The Lockheed P-2 Neptune (designated P2V by the United States Navy prior to September 1962) is a maritime patrol and anti-submarine warfare (ASW) aircraft. It 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 (using JATO assist), 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.

Variants

Lockheed produced seven main variants of the P2V. In addition, Kawasaki built the turboprop-powered P-2J in Japan.

XP2V-1
Prototype, two built. Powered by two 2,300 horsepower (1,700 kW) Wright R-3350-8 engines with four-bladed propellers, with armament of two .50 in machine guns in nose, tail and dorsal turrets, and 8,000 pounds (3,600 kg) of stores in an internal bomb bay.
P2V-1
First production model with R-3350-8A engine. Provision for 16 5-inch (127 mm) HVAR or 4 11.75 -inch (300 mm) Tiny Tim rockets underwing; 14 built.|
P2V-2
Second production model, powered by two 2,800 horsepower (2,100 kW) R-3350-24W engines driving three-bladed propellers. Nose turret replaced by "attack" nose fitted with six fixed 20 mm cannon. First eight aircraft retained Bell tail turret fitted with twin .50 (12.7 mm) machine guns, with remaining aircraft using Emerson tail turret with twin 20 mm cannon. 80 built.
P2V-3
Improved patrol bomber with 3,200 horsepower (2,400 kW) R-3350-26W engines with jet stack engine exhausts. 53 built.
P2V-4
Improved anti-submarine aircraft. Fitted with AN/APS-20 search radar and provision for dropping sonobuoys with additional dedicated sonobuoy operator. Underwing tip-tanks added, with searchlight in nose of starboard tip tank. Gun Turrets in tail and dorsal position. First 25 aircraft powered by 3,200 horsepower (2,400 kW) R-3350-26WA engines, with remaining 27 powered by 3,250 horsepower (2,420 kW) Wright R-3350-30W turbo-compound engines. 52 built in total. Surviving aircraft redesignated P-2D in 1962.
P2V-5
Fitted with Emerson nose turret with two 20 mm cannon replacing solid nose of earlier versions, while retaining dorsal and tail turrets. New, larger, jettisonable tip tanks, with traversable searchlight slaved to nose turret in front of starboard tip-tank and AN/APS-8 radar in nose of port tip-tank. AN/APS-20 search radar under fuselage. Later aircraft featured glazed observation nose and MAD gear in place of nose and tail turrets, and revised crew accommodation, with many earlier aircraft refitted. Dorsal turret often removed. 424 built.
P2V-6
Multi-role version with lengthened weapons bay and provision for aerial minelaying and photo-reconnaissance. Smaller AN/APS-70 radar instead of AN/APS-20. Initially fitted with gun turrets as P2V-5, though retaining the ability to be refitted with glazed nose. A total of 67 were built for the US Navy and France. Redesignated P-2F in 1962.
P2V-7
Last Neptune variant produced by Lockheed, powered by R-3350-32W and J-34 engines. Fitted with lower drag wingtip tanks, AN/APS-20 search radar in a revised radome and a bulged cockpit canopy. Early aircraft were fitted with defensive gun turrets but these were removed as for the P2V-5. 287 were built, including 48 assembled by Kawasaki in Japan. Redesignated P-2H in 1962.

P2V-1 "Truculent Turttle"
 Photo: Robert Deering 1986
National Museum of Naval Aviation
Pensacola, Florida
 

P2V-7
Photo: Robert Deering 1971
 Will Rogers World Airport (OKC)
Oklahoma City, Oklahoma
 
 
 
Design and Development

Development of a new land-based patrol bomber began early in World War II, with design work starting at Lockheed's Vega subsidiary as a private venture on 6 December 1941. At first, the new design was considered a low priority compared to other aircraft in development at the time, with Vega also developing and producing the PV-2 Harpoon patrol bomber. On 19 February 1943, the U.S. Navy signed a letter of intent for two prototype XP2Vs, which was confirmed by a formal contract on 4 April 1944 with a further 15 aircraft being ordered 10 days later. It was not until 1944 that the program went into full swing. A major factor in the design was ease of manufacture and maintenance, and this may have been a major factor in the type's long life and worldwide success. The first aircraft flew in May 1945. Production began in 1946, and the aircraft was accepted into service in 1947. Potential use as a bomber led to successful launches from aircraft carriers.

Beginning with the P2V-5F model, the Neptune became one of the first operational aircraft fitted with both piston and jet engines. The Convair B-36, several Boeing C-97 Stratofreighter, Fairchild C-123 Provider, North American AJ Savage, and Avro Shackleton aircraft were also so equipped. To save weight and complexity of two separate fuel systems, the Westinghouse J34 jet engines on P2Vs burned the 115–145 Avgas fuel of the piston engines, instead of jet fuel. The jet pods were fitted with intake doors that remained closed when the J-34s were not running. This prevented windmilling, allowing for economical piston-engine-only long-endurance search and patrol operations. In normal US Navy operations, the jet engines were run at full power (97%) to assure takeoff, then shut down upon reaching a safe altitude. The jets were also started and kept running at flight idle during low-altitude (500-foot (150 m) during the day and 1,000-foot (300 m) at night) anti-submarine and/or anti-shipping operations as a safety measure should one of the radials develop problems.

Normal crew access was via a ladder on the aft bulkhead of the nosewheel well to a hatch on the left side of the wheel well, then forward to the observer nose, or up through another hatch to the main deck. There was also a hatch in the floor of the aft fuselage, near the sonobuoy chutes.

SOURCE: Wikipedia
SPECIFICATIONS: PERFORMANCE:
Span:  103 ft., 10 in. Maximum speed:  345 M.P.H. at 10,000 ft
Length:  91 ft., 4 in. Cruising speed:  
Height:  29 ft., 4 in.| Range:  2,200 miles
Empty Weight:  47,456lb Service ceiling:  22,000 ft
Gross Weight:  75,500 lb.  
Crew:  9-10
Engines:  Two 3,500 horsepower R-3350-32W engines and two 3,400 lb. J34-WE-34 turbojets
Armament: 
   
SOURCE:  National Museum of Naval Aviation  
   
1959 DOD Aircraft
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