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Martin P4M Mercator


Maritime Patrol Bomber Aircraft


United States | 1950



"Martin developed the P4M Mercator to contend for the USN long-range maritime patrol bomber role - it lost to the Lockheed Neptune design."



Authored By: Staff Writer | Last Edited: 01/16/2019 | Content ©www.MilitaryFactory.com | The following text is exclusive to this site; No A.I. was used in the generation of this content.
Flag of Image from the Public Domain.
Firepower
Performance
Survivability
Versatility
Impact
During the later stages of World War 2 (1939-1945), the United States Navy (USN) began an active search for a new long-ranged maritime patrol bomber to succeed an aging fleet of Consolidated PB4Y "Privateer" aircraft in same role. Two potential candidates emerged from the competing firms of the Glenn L. Martin Company (Martin) and Lockheed and these became the P4M "Mercator" and P2V "Neptune", respectively. In the end, however, the latter was selected for serial production and frontline service while the P4M was taken only into limited service to satisfy a long-ranged electronic reconnaissance role for the USN - this resulted in just nineteen aircraft being built.

The aircraft that would become the "Mercator" was known in-house as the "Model 219" and work began as soon as 1944 on the type (World War 2 ended in 1945). In its prototype form the aircraft recorded a first-flight on October 20th, 1946 and flew with 2 x Pratt & Whitney R-4360-4 "Wasp Major" air-cooled radial piston engines providing necessary power and performance to go along with the range required of maritime types (often operating over swathes of uninhabited, landless terrain).

At this stage during the "age of the jet engine", it proved somewhat common for American warplanes to feature a "combination" propulsion scheme so 2 x Allison J33 series turbojets were added to augment performance for the aircraft - either to reduce the runway take-off length required or escape from pursuing enemy interceptors. The jet systems relied on the same fuel as the prop-driven radials so only a common fuel supply was necessary.

Standard installed armament became 2 x 20mm autocannons in the nose, an additional 2 x 20mm autocannons at the tail, and 2 x 0.50 caliber Heavy Machine Guns (HMGs) in a dorsal turret. In this fashion, the aircraft would defend itself from most any position an enemy was approaching from (save the underside). The optional bomb load could be made up of conventional drop bombs, naval mines, depth charges, or torpedoes up to a 12,000lb total war load.

The aircraft was given a very slim top-down profile, its fuselage glazed at both nose and tail. The cockpit was seated aft and above the nose section as in a typical "stepped" arrangement so this elevated position could improve pilot vision over the aircraft and towards each engine. The engines were underslung at each mainplane, extending noticeably forward from the leading edges. The bomb bay buried within the fuselage was equal in length to the engines. Instead of fitting the main landing gear into the engines, the legs were positioned outboard of the nacelles and recessed into the wings (folding outwards from centerline). The nosewheel was positioned under the mass of the nose section to complete the tricycle arrangement needed for ground-running. The tail unit incorporated an elegantly-shaped single rudder fin with low-mounted, upward-canted horizontal planes. The wing mainplanes were situated directly at midships and were slim in their own right, tapering from centerline to wing tip along both the leading and trailing edges.

Two prototypes were ultimately built to the "XP4M-1" standard and these flew with R-4360-4 engines followed by the production-standard "P4M-1" models of which nineteen were built and these carried 2 x R-4360-20A series engines into service. The "P4M-1Q" designation was used to mark P4M-1 airframes converted as radar countermeasures platforms (SIGnals INTelligence = "SIGINT").

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As finalized, the P4M-1 would go one to carry a complete crew of nine and, structurally, it had an overall length of 85.1 feet, a wingspan of 114 feet and a height of 26 feet. Empty weight was 48,535lb with a Maximum Take-Off Weight (MTOW) of 88,380 feet. Power was from 2 x Pratt & Whitney R-4360 "Wasp Major" air-cooled radial piston engines of 3,250 horsepower each and these were aided by 2 x Allison J33-A-23 turbojet engines of 4,600 thrust each. Performance included a maximum speed of 410 miles-per-hour, a range out to 2,850 miles, and a service ceiling up to 35,000 feet. The aircraft was fitted with the AN/APS-33 search radar.

Even as Lockheed's Neptune design went on to win the original USN requirement, the value of the Mercator was not overlooked by authorities as a mine-laying platform so a production order for the design followed in 1947 leading to service entry in 1950. As soon as 1951, the fleet was converted for the SIGINT role and operated under the aforementioned P4M-1Q designation - these flew with additional mission support equipment and more crewmembers for the revised role.

In this guise, Mercators undertook daring, often dangerous, spying missions around communist territories near the likes of the Soviet Union, China, North Korea, and Vietnam. On August 22nd, 1956, a Mercator was shot down by Chinese interceptors, killing all aboard, and another such incident followed with the Soviet Union over Mediterranean waters after the Mercator was caught near Ukraine. Similarly, North Korean interceptors met a Mercator with gunfire though the American warplane managed to survive the encounter and limp home.

Once their useful service lives were over (and pure jet aircraft took over in full), the Mercator line was given up in favor of the Douglas A-3 "Skywarrior" through its "EA-3B" guise. Unlike the Mercator, the Skywarrior was compact enough to be operated from, and be stored below, the decks of American carriers of the period. The last Mercator was retired in 1960 and none of the surviving airframes were spared.

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Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Martin P4M Mercator Maritime Patrol Bomber Aircraft.
2 x Pratt & Whitney R-4360 "Wasp Major" air-cooled radial piston engines developing 3,250 horsepower; 2 x Allison J33-A-23 turbojet engines developing 4,600lb of thrust each.
Propulsion
410 mph
660 kph | 356 kts
Max Speed
34,449 ft
10,500 m | 7 miles
Service Ceiling
2,840 miles
4,570 km | 2,468 nm
Operational Range
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).
NYC
 
  LON
LON
 
  PAR
PAR
 
  BER
BER
 
  MOS
MOS
 
  TOK
TOK
 
  SYD
SYD
 
  LAX
LAX
 
  NYC
Structure
The nose-to-tail, wingtip-to-wingtip physical qualities of the Martin P4M Mercator Maritime Patrol Bomber Aircraft.
9
(MANNED)
Crew
85.3 ft
26.00 m
O/A Length
114.8 ft
(35.00 m)
O/A Width
26.2 ft
(8.00 m)
O/A Height
48,535 lb
(22,015 kg)
Empty Weight
88,405 lb
(40,100 kg)
MTOW
Design Balance
The three qualities reflected below are altitude, speed, and range. The more full the box, the more balanced the design.
RANGE
ALT
SPEED
Armament
Available supported armament and special-mission equipment featured in the design of the Martin P4M Mercator Maritime Patrol Bomber Aircraft .
STANDARD:
2 x 20mm automatic cannons in nose turret.
2 x 20mm automatic cannons in tail turret.
2 x 0.50 caliber (12.7mm) heavy machine guns in dorsal turret.

OPTIONAL:
Up to 12,000lb of conventional drop stores including bombs, torpedoes, depth charges and naval mines.
Variants
Notable series variants as part of the Martin P4M Mercator family line.
P4M "Mercator" - Base Series Designation
XP4M-1 - Prototype aircraft with 2 x R-4360-4 series engines fitted; two examples completed.
P4M-1 - Production-quality aircraft; fitted with 2 x R-4360-20A series engines; 19 examples completed.
P4M-1Q - Radar CounterMeasures (CM) conversion model; based on existing P4M-1 framework.
Operators
Global customers who have evaluated and/or operated the Martin P4M Mercator. Nations are displayed by flag, each linked to their respective national aircraft listing.

Total Production: 21 Units

Contractor(s): Glenn L. Martin Company - USA
National flag of the United States

[ United States ]
Relative Max Speed
Hi: 500mph
Lo: 250mph
Aircraft Max Listed Speed (410mph).

Graph Average of 375 MPH.
Era Crossover
Pie graph section
Showcasing Aircraft Era Crossover (if any)
Max Alt Visualization
Small airplane graphic
Production Comparison
21
36183
44000
Entry compared against Ilyushin IL-2 (military) and Cessna 172 (civilian) total production.
MACH Regime (Sonic)
Sub
Trans
Super
Hyper
HiHyper
ReEntry
RANGES (MPH) Subsonic: <614mph | Transonic: 614-921 | Supersonic: 921-3836 | Hypersonic: 3836-7673 | Hi-Hypersonic: 7673-19180 | Reentry: >19030
Aviation Timeline
EarlyYrs
WWI
Interwar
WWII
ColdWar
Postwar
Modern
Future
1 / 1
Image of the Martin P4M Mercator
Image from the Public Domain.

Mission Roles
Some designs are single-minded in their approach while others offer a more versatile solution to airborne requirements.
GROUND ATTACK
MARITIME / NAVY
RECONNAISSANCE
Recognition
Some designs stand the test of time while others are doomed to never advance beyond the drawing board; let history be their judge.
Going Further...
The Martin P4M Mercator Maritime Patrol Bomber Aircraft appears in the following collections:
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