Military Wiki
P4M Mercator
United States Navy P4M-1
Role Patrol bomber
National origin United States
Manufacturer Martin
First flight 20 October 1946
Introduction 1950
Retired 1960
Status Retired
Primary user United States Navy
Number built 21

The Martin P4M Mercator was a maritime reconnaissance aircraft built by the Glenn L. Martin Company. The Mercator was an unsuccessful contender for a United States Navy requirement for a long-range maritime patrol bomber, with the Lockheed P2V Neptune chosen instead. It saw a limited life as a long-range electronic reconnaissance aircraft. Its most unusual feature was that it was powered by a combination of piston engines and turbojets, the latter being in the rear of the engine nacelles.

Design and development

Work began on the Model 219 in 1944, as a replacement for the PB4Y Privateer long range patrol bomber, optimised for long range minelaying missions, with the first flight being on 20 October 1946.[1] A large and complicated aircraft, it was powered by two Pratt & Whitney R4360 Wasp Major 28-cylinder radial engines. To give a boost during takeoff and combat, two Allison J33 turbojets were fitted in the rear of the two enlarged engine nacelles, the intakes being beneath and behind the radial engines.[2] The jets, like those on most other piston/jet hybrids, burned gasoline, not jet fuel.

A tricycle undercarriage was fitted, with the nosewheel retracting forwards. The single-wheel main legs into coverless fairings in the wings, so that the sides of the wheels could be seen even when retracted. The wings themselves, unusually, had a different airfoil cross-section on the inner wings than the outer.

Heavy defensive armament was fitted, with two 20 mm (.79 in) cannons in an Emerson nose turret and a Martin tail turret, and two 0.5 in (12.7 mm) machine guns in a Martin dorsal turret. The bomb-bay was, like British practice, long and shallow rather than the short and deep bay popular in American bombers. This gave greater flexibility in payload, including long torpedoes, bombs, mines, depth charges or extended-range fuel tanks.[3]

Operational history

P4M-1 of patrol squadron VP-21

The US Navy chose the smaller, simpler, cheaper and better performing P2V Neptune for the maritime patrol requirement, but nineteen aircraft were ordered in 1947 for high-speed minelaying purposes. The P4M entered service with Patrol Squadron 21 (VP-21) in 1950, the squadron deploying to Port Lyautey (now Kenitra) in French Morocco.[4] It remained in use with VP-21 until February 1953.[5] From 1951, the 18 surviving production P4Ms were modified for the electronic reconnaissance (or SIGINT, for signals intelligence) mission as the P4M-1Q, to replace the PB4Y-2 Privateer. The crew was increased to 14 and later 16 to operate all the surveillance gear, and the aircraft was fitted with a large number of different antennas.[6]

P4M-1Q Mercator of VQ-2 electronics reconnaissance squadron in September 1956 - note extra radar 'bulges' on this variant

Starting in October 1951, electronic surveillance missions were flown from U.S. Naval Station Sangley Point in the Philippines (and, later from the Naval Air Station Iwakuni, Japan, and later Naval Air Station Atsugi, Japan, by a secretive unit that eventually gained the designation [first as Electronic Countermeasures Squadron ONE, later as Fleet Air Reconnaissance Squadron ONE (VQ-1). Long missions were flown along the coast (about 30 NM of shore) of Viet Nam, China, North Korea and the eastern Soviet Union, and were of a highly secret nature; the aircraft some times masqueraded as regular P2V Neptunes in radio communications, and often flew with false serial numbers (Bureau Numbers) painted under the tail. Operational missions were always flown at night, the dark of the moon and with no external running lights. serial numbers.[7]

One Mercator was shot down near Shanghai by Chinese fighters on August 22, 1956, with its crew of 16 all killed. Also see New York Times August 1956.[8] Another P4M-1Q was attacked by two North Korean MiG-17s on June 16, 1959 with heavy damage and serious injury to the tail gunner.[9] The aircraft were also operated out of Morocco by VQ-2, where one aircraft was intercepted near Ukrainian airspace by Soviet MiG's. It escaped by flying under jet power but ran out of fuel and crashed into Mediterranean Sea with the loss of all crew. Another, in 1952, ditched north of Cyprus at night, out of fuel, no power, losing ony the Aircraft Commander/pilot after they were in the water (See United States Naval Institute, Naval History, March/April 1997).

The Mercators were replaced by the EA-3B Skywarrior, which being carrier-based had a greater degree of flexibility and the larger Lockheed WV-2Q Warning Star. Final withdrawal from service was in 1960, and all of the remaining P4Ms were scrapped.[10]


Two prototype aircraft with two R-4360-4 engines.
Production aircraft with two R-4360-20A engines, 19 built.
P4M-1s redesignated when modified for radar countermeasures.


United States

Specifications (P4M Mercator)

Martin P4M-1 Mercator

General characteristics

  • Crew: 9
  • Length: 85 ft 2 in (26.0 m)
  • Wingspan: 114 ft 0 in (34.7 m)
  • Height: 26 ft 1 in (8.0 m)
  • Wing area: 1,311 ft² (122 m²)
  • Empty weight: 48,536 lb (22,016 kg)
  • Loaded weight: 88,378 lb (40,088 kg)
  • Max. takeoff weight: lb (kg)
  • Powerplant:
    • 2 × Allison J33-A-23 turbojets, 4,600 lbf (20 kN) each
    • 2 × Pratt & Whitney R-4360 Wasp Major radial engines, 3,250 hp (2,420 kW) each


  • Maximum speed: 410 mph (660 km/h)
  • Range: 2,840 mi (4,570 km)
  • Service ceiling: 34,600 ft (10,500 m)
  • Rate of climb: ft/min (m/s)
  • Wing loading: lb/ft² (kg/m²)


  • 4 × 20 mm (.79 in) cannons in nose and tail turrets
  • 2 × .50 in (12.7 mm) machine guns in dorsal turret
  • Up to 12,000 lb (5,400 kg) of bombs, mines, depth charges, or torpedoes
  • Avionics

    • AN/APS-33 search radar

    See also


    1. Lake and Dorr 2000, p.139.
    2. Lake and Dorr 2000, pp. 138–139.
    3. Dorr and Burgess 1993, pp. 216–217.
    4. Dorr and Burgess 1993, p.217.
    5. Roberts 2000, p.125.
    6. Lake and Dorr 2000, pp. 141–142.
    7. Dorr and Burgess 1993, pp. 217, 220.
    8. Dorr and Burgess 1993, pp. 220–221.
    9. Dorr and Burgess 1993, pp. 221–222.
    10. Dorr and Burgess 1993, p.222.

    External links

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