Martin P6M Sea Master

1955

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Martin P6M Sea Master

To meet a US Navy requirement for a high-performance multi-role flying-boat, the company offered its very advanced Martin Model 275 design. This had an all-metal hull of high length/beam ratio, mounting a cantilever high-set sharply-swept wing incorporating so much anhe-dral that the stabilising floats at the wirwg-tips could be attached permanently; the tail unit was of T-tail configuration with all-swept surfaces. Above the wing, to minimise spray ingestion, were mounted four Allison turbojet engines, and pressurised accommodation was provided for a crew of five. The first XP6M-1 prototype was flown on 14 July 1955, the second following on 18 May 1956, and Martin received orders for six pre-production YP6M-1 boats powered by Allison J71 turbojets each developing a maximum 5897kg afterburning thrust. Successful flight testing led to an order for 24 production P6M-2 aircraft named SeaMaster, which differed primarily by having 7711kg thrust non-afterburning Pratt & Whitney J75-P-2 turbojet engines. However, the contract was cancelled on 21 August 1959 after only three had been built and these, together with the YP6M-1s, were scrapped at a later date. They were the fastest flying-boats ever built.

FACTS AND FIGURES

© The cockpit glazing was modified on later models to give a much better overhead and side view.

© Ejection seats were fitted to the second and subsequent aircraft. These proved useful when the second SeaMaster pitched up, went into a loop and disintegrated.

© The intakes were mounted above the wing to keep them clear of the water spray.

© A beaching cradle allowed the SeaMaster to taxi in and out of the water under its own power.

© The P6M used a rotary bomb bay (as used on Martin's licence-built Canberras and the XB-51). This permitted weapons release at high speeds without the drag of conventional bomb doors.

© The original position of the engine exhausts caused stress on the rear fuselage which resulted in structural damage. The angle of the exhausts was adjusted after testing.

Martin P6M Sea Master on YOUTUBE

Martin P6M Sea Master

Specification 
 MODELP6M
 CREW4
 ENGINE4 x Pratt & Whitney J75-P-2 turbojets, 7938kg
 WEIGHTS
  Take-off weight72575 kg160001 lb
  Payload13600kg29983 lb
 DIMENSIONS
  Wingspan30.48 m100 ft 0 in
  Length40.84 m134 ft 0 in
  Height9.45 m31 ft 0 in
 PERFORMANCE
  Max. speed965 km/h600 mph
  Ceiling12200 m40050 ft
  Range4830 km3001 miles
 ARMAMENT6 x 12.7mm machine-guns, 1800kg of weapons

Comments1-20 21-40
Rick Cotton, e-mail, 03.05.2008 21:18

I briefly flew the P6M in 1954-55 as the Chief Production Test Pilot at The Glenn L. Martin Company in Baltimore. We were preparing a Training Program for our Navy Customer when,over a period of several months,two Test A /C were lost(I was chasing the first one in a borrowed USAF B-57 which had much longer legs than the FJ-2 that he Navy had provided). This and other more Political factors ended the program. It was quite an experiance and a uniquely advanced concept.

reply

Paul, e-mail, 19.07.2007 02:51

Any comments on the P6M's resemblance to the "Caspian Sea Monster?"

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1-20 21-40

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