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Martin P6M SeaMaster

Jet-Powered Flying Boat

Martin P6M SeaMaster

Jet-Powered Flying Boat

OVERVIEW
SPECIFICATIONS
ARMAMENT
VARIANTS
HISTORY
MEDIA
OVERVIEW



Only twelve examples of the Martin P6M SeaMaster jet-powered flying boat were eventually realized.
National Flag Graphic
ORIGIN: United States
YEAR: 1955
MANUFACTURER(S): Glenn L. Martin Company - USA
PRODUCTION: 12
OPERATORS: United States
SPECIFICATIONS



Unless otherwise noted the presented statistics below pertain to the Martin P6M SeaMaster model. Common measurements, and their respective conversions, are shown when possible.
CREW: 4
LENGTH: 133.99 feet (40.84 meters)
WIDTH: 102.92 feet (31.37 meters)
HEIGHT: 32.41 feet (9.88 meters)
WEIGHT (EMPTY): 91,271 pounds (41,400 kilograms)
WEIGHT (MTOW): 119,050 pounds (54,000 kilograms)
ENGINE: 4 x Pratt & Whitney J75-P-2 turbojet engines developing 17,500 lb of thrust each.
SPEED (MAX): 628 miles-per-hour (1010 kilometers-per-hour; 545 knots)
RANGE: 1,988 miles (3,200 kilometers; 1,728 nautical miles)
CEILING: 39,370 feet (12,000 meters; 7.46 miles)




ARMAMENT



STANDARD:
2 x 20mm cannons in tail turret

OPTIONAL:
Up to 4,000 lb of internal ordnance carried.
VARIANTS



Series Model Variants
• P6M "SeaMaster" - Base Series Designation
• XP6M-1 - Prototype model designation; two completed.
• YP6M-1 - Pre-production model designation; six completed.
• P6M-1 - Main production model designation; eight completed.


HISTORY



Detailing the development and operational history of the Martin P6M SeaMaster Jet-Powered Flying Boat.  Entry last updated on 1/5/2015. Authored by Staff Writer. Content ©www.MilitaryFactory.com.
The Cold War (1947-1991) period was one of technological advancement whose momentum was driven by developments during World War 2 (1939-1945). In the early 1950s, the United States Navy worked in concert with the Glenn L. Martin Company aviation firm to produce a new jet-powered, nuclear-capable flying boat of considerable performance and capabilities. The aircraft would retain its aircraft qualities about her while also incorporate a boat-like hull/fuselage which would allow it to land and take-off from water. In this way, the USN could now field its own fighting force of nuclear-carrying strategic bombers without reliance on the fleet being managed by the United States Air Force. Flying boats promised tactical flexibility in the field and could prove more mobile than land-based bombers - able to undertake surprise attacks against the heart of the Soviet Empire in short order.

The formal requirement for the aircraft came in April of 1951. It called for a jet-powered aircraft capable of top-flight speeds over water with a 1,500 mile operating range. Its internal payload carrying capacity would be in the 30,000lbs range.

The USN entertained submissions from both Martin and competing Convair and elected with the former's design. A contract then followed calling for a pair of prototypes to be constructed for testing. The prototypes were designated "XP6M" with the initial mark being "XP6M-1". The USN ultimately envisioned a complete fleet of twenty-four jet-powered flying boats by program's end - a total never to be realized. The aircraft carried the name of "SeaMaster".

The Martin design showcased a deep fuselage approach for the necessary hull shape and internal bomb load. The flight deck sat high at the frontal section with a single vertical fin at the tail. The horizontal tailplanes were high-mounted and produced the classic "T" style tail unit. Wings were shoulder-mounted assemblies to supply the necessary clearance on water as well as provide inherent lifting qualities. The wings were given considerable sweepback and displayed a noticeable droop when at rest. Engineers focused on a pair of Curtiss-Wright ramjets at first thought their complexity soon resulted in the selection of 4 x Allison J71-A-4 turbojets instead. These engines were then mounted above aircraft wingroots as paired nacelles. Despite it being a water-borne system, the aircraft was still given a retractable wheeled undercarriage to allowed it to land on prepared runways - in effect doubling its in-theater value.




Prototype XP6M-1 made its first flight on July 14th, 1955 and resulting data collected forced changes to the engine placement. This prototype was then lost on December 7th, 1955, when the aircraft disintegrated mid-flight with the loss of all four crew aboard due to a failure in the tail unit. The second prototype then followed in a first flight recorded on May 18th, 1956. It too, however, suffered a catastrophic failure in the tail unit. In this case, all four crew exited the aircraft safely.

Undeterred, the USN SeaMaster program continued and resulted in the YP6M-1 pre-production model of 1957. The example began its testing phase the following year which ultimately revealed several major shortcomings of the design as a whole. The aircraft was of a heavy configuration and this was coupled to poor controls and underpowered engines unsuitable for on-water/over-water operation. Five additional airframes were ordered and changes instituted for the better: the Allison engines were given up in favor of 4 x Pratt & Whitney J75 turbojets which promised more power and vision out-of-the-cockpit was improved as was the avionics suite. An in-flight refueling probe was added to help increase the operational reach of the aircraft.

This revised design emerged as the "P6M-2" and eight total airframes followed. By this time, however, the bloated and oft-delayed program has met its end - cancelled before operational service was reached. The USN elected to fund its ballistic missile submarine program instead and all remaining SeaMaster airframes were scrapped and lost to naval aviation history.

As completed, P6M-2 featured an overall length of 134 feet, a wingspan of 103 feet and a height of 32 feet, 5 inches. Its operating crew was four including two pilots. Primary armament was a 4,000lb bomb load while point-defense was handled by a 2 x 20mm cannon arrangement in a tail turret. The aircraft weighed 91,300lbs when empty and showcased a Maximum Take-Off Weight (MTOW) of 176,400lbs. Power from the finalized 4 x Pratt & Whitney J75-P-2 turbojets outputted at 17,500lbs thrust each and allowed for a maximum speed of 630 miles per hour, a range out to 2,000 miles and a service ceiling up to 40,000 feet.




MEDIA









Our Data Modules allow for quick visual reference when comparing a single entry against contemporary designs. Areas covered include general ratings, speed assessments, and relative ranges based on distances between major cities.

Image of collection of graph types

Relative Maximum Speed Rating
Hi: 750mph
Lo: 375mph
    This entry's maximum listed speed (628mph).

    Graph average of 562.5 miles-per-hour.
City-to-City Ranges
NYC
 
  LDN
LDN
 
  PAR
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  BER
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  MSK
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  TKY
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  SYD
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  LAX
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  NYC
Graph showcases the Martin P6M SeaMaster's operational range (on internal fuel) when compared to distances between major cities.
Aviation Era
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Pie graph section
Pie graph section
Pie graph section
Pie graph section
Useful in showcasing the era cross-over of particular aircraft/aerospace designs.
Unit Production Comparison
Comm. Market HI*: 44,000 units
Military Market HI**: 36,183 units
12
12

  * Commercial Market High belongs to Cessna 172.

  ** Military Market High belongs to Ilyushin Il-2.


Altitude Visualization
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Supported Roles
A2A
Interception
UAV
Ground Attack
CAS
Training
ASW
Anti-Ship
AEW
MEDEVAC
EW
Maritime/Navy
SAR
Aerial Tanker
Utility/Transport
VIP
Passenger
Business
Recon
SPECOPS
X-Plane/Development
A2A=Air-to-Air; UAV=Unmanned; CAS=Close Support; ASW=Anti-Submarine; AEW=Airborne Early Warning; MEDEVAC=Medical Evac; EW=Electronic Warfare; SAR=Search-Rescue
Supported Arsenal
Graphical image of an aircrat automatic cannon
Commitments / Honors
Military lapel ribbon for Operation Allied Force
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Military lapel ribbon for the Golden Age of Flight
Military lapel ribbon for the 1991 Gulf War
Military lapel ribbon for the Indo-Pak Wars
Military lapel ribbon for the Iran-Iraq War
Military lapel ribbon for the Korean War
Military lapel ribbon for the 1982 Lebanon War
Military lapel ribbon for the Malayan Emergency
Military lapel ribbon representing modern aircraft
Military lapel ribbon for the attack on Pearl Harbor
Military lapel ribbon for the Six Day War
Military lapel ribbon for the Soviet-Afghan War
Military lapel ribbon for the Spanish Civil War
Military lapel ribbon for the Suez Crisis
Military lapel ribbon for the Vietnam War
Military lapel ribbon for Warsaw Pact of the Cold War-era
Military lapel ribbon for the WASP (WW2)
Military lapel ribbon for the World War 1
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Military lapel ribbon for the Yom Kippur War
Military lapel ribbon for experimental x-plane aircraft
* Ribbons not necessarily indicative of actual historical campaign ribbons. Ribbons are clickable to their respective campaigns/operations.