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Martin P5M Marlin

martinmarlin

 

As a new US Navy patrol flying-boat, Martin developed the Model 237 design, combining the wing and upper hull of the Mariner with the new lower hull structure. A PBM-5 Mariner served as the prototype XP5M-1 which, when ordered into production, was given the name Marlin.

The modified hull of the XP5M-1 incorporated radar-directed nose and tail turrets, as well as a power-operated dorsal turret, and power was provided by two 2424kW Wright R-3350 radial engines.

This prototype flew for the first time on 30 May 1948, but it was not until two years later that the P5M-1 was ordered into production, the first of these series aircraft being flown on 22 June 1951.

Initial deliveries, to US Navy Squadron VP-44, began on 23 April 1952 and the type remained in service until the mid-1960s.

 

 Martin-P5M
Martin P5M-1

 

In addition to those operated by the US Navy, 12 of the later P5M-2 version were supplied to France under the American MAP for use by the Aeronavale in 1959. In the French Aeronavale, where they were used for maritime patrol out of Dakar, West Africa, until 1964, after which they were returned to the Navy. The P5M-2 Marlin could carry up to 8,000 lb (3,629 kg) of assorted weapons. The P5M-1 has a low mounted " dihedral " tailplane, different hull shape and lower-powered engines, compared to the P5M-2.

The first of 28 P5M-2 Marlins to undertake a modernisation program was delivered to the US Navy in 1959.

Martin aircraft production ceased December 20,1960 when the last P5M- 2 Marlin was handed over to U.S. Navy.

 

  Martin-P5M-2

 

Claiming high operational costs, the Coast Guard turned over all of its P5Ms to the Navy in 1961. Lacking most military equipment, they were used as crew trainers as P5M-1T and P5M-2Ts.

In September 1962, when all American military forces adopted the tri-service designation scheme, the P5M-1 became the P-5A, the P5M-1S the SP-5A, the P5M-1T the TP-5A, the P5M-2 the P-5B, the P5M-2S and P5M-2T the PT-2B.

 

 Martin-SP5
SP-5B / P5M2

 

In 1964, in an attempt to boost take-off power, one SP-3B was tested with a tail mounted 3000 lb.st Pratt & Whitney turbojet engine. They were not adopted for service.

No Marlins went to the reserves. As they were retired, they were stored until sold as scrap. A Navy SP-5B of VP-40 made the last operationsl flight on 6 November 1967.

 

 Martin-270
Model 270

 

The XP5M-1 prototype was later used (as the model 270) to test the 15:1 hull configuration for the P4M SeaMaster.


P5M
Engines: 2 x Wright R-3350-32WA Turbo-Compound, 2573kW
Max take-off weight: 38555 kg / 85000 lb
Empty weight: 22900 kg / 50486 lb
Wingspan: 36.02 m / 118 ft 2 in
Length: 30.66 m / 100 ft 7 in
Wing area: 130.62 sq.m / 1405.98 sq ft
Max. speed: 404 km/h / 251 mph
Ceiling: 7300 m / 23950 ft
Range: 3300 km / 2051 miles
Armament: 3600kg of weapons
Crew: 11

P5M-2 Marlin

Naval patrol bomber flying boat
Engines: 2x3, Wright R3350-32W Turbo-Cyclone, 3450 h.p
Wingspan: 118 ft. 2in (36.02 m)
Length: 100 ft. 7in (30.66 m)
Height: 32 ft 8.5 in (9.97 m).
Max TO wt: 85,000 lb (38,555 kg).
Loaded weight: 73,055 lb.
Max. speed: 262 m.p.h.
Ceiling: 22,400 ft.
Range: 3,600 miles
Armament: 2 x tail mounted guns
Bombload: 16,000 lb
Crew: 7

 

Martin-P5M2-ld
P5M-2 Marlin

 

 


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