Martin PBM Mariner

Patrol bomber flying boat introduced in 1940

Overview

Glenn L. Martin United States ICAO: PBM 1940–1949

The Martin PBM Mariner was developed and produced by Glenn L. Martin Company as a patrol bomber flying boat during the Second World War and the early period of the Cold War. The PBM Mariner was built in addition to the flying boats in service during the time such as the Consolidated PBY Catalina and the PB2Y Coronado. On February 18, 1939, the aircraft took its maiden flight and in September 1940, it entered into service.

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Specifications

Units
Engine
2 × Wright R-2600-6
Engine type
Piston
Power
2 × 1,600 hp · 1,193 kW
Avionics
Wing tips
No winglets
Seats
7
Crew
Cabin width
Cabin height
Cabin length
Exterior length
77 ft 1 in  ·  23.50 m
Tail height
27 ft 6 in  ·  8.38 m
Fuselage diameter
9 ft 2 in  ·  2.80 m
Wing span
118 ft 1 in  ·  36.00 m
Baggage volume
Gross weight
Empty weight
Max takeoff weight
58,000 lb  ·  26,300 kg
Max landing weight
48,000 lb  ·  21,800 kg
Max payload
2,600 lb  ·  1,200 kg
Fuel capacity
2,700 gal · 10,200 L · 7,400 kg (AvGas)
Max cruise speed
178 kt  ·  205 mph  ·  330 km/h
Maximum speed
Cruise speed
Approach speed
72 kt  ·  83 mph  ·  133 km/h
Range
2,600 nm  ·  2,990 mi  ·  4,820 km
Fuel burn
Ceiling
19,800 ft  ·  6,000 m
Rate of climb
800 ft/min  ·  4 m/s
Takeoff distance
Landing distance
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U.S. Navy Martin PBM-3R Mariner transport aircraft taking off in water.

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Flight Airline Reg Alt Speed Heading V/S

Operational Context

In 1937, a new flying boat powered by twin engines designated as the Model 162 was developed by the Glenn L. Martin Company. It was to take the place of the Consolidated P2Y and was built to be in addition to the PBY Catalina and PB2Y Coronado. On June 30, 1937, an order for a single prototype designated as XPBM-1 was placed. On December 28, 1937, the first production order for twenty-one PBM-1 was received.

The initial production version PBM-1 has an external length of 23.50 meters, an external height of 5.8 meters, and a width of 2.8 meters. It has a tail height of 8.38 meters and a wheelbase of 11.3 meters. The wingspan is 36 meters and the wing area is 131 square meters. The aircraft could accommodate up to seven crew members in flight. The PBM-1 has an empty weight of 15,048 kg and a gross weight of 25,425 kg. The maximum takeoff and landing weights are 26,300 kg and 21,768 kg, respectively. It has a maximum payload of 1,180 kg and a fuel tank capacity of 2,700 US gallons.

The aircraft is powered by two Wright R-2600 also called Twin Cyclone. It is a fourteen-cylinder, supercharged, air-cooled, two-row radial engine which produces a maximum power of 1,600 hp each. It has two pushrod-actuated valves per cylinder with a sodium-cooled exhaust valve, a single-stage two-speed centrifugal-type supercharger, a Stromberg downdraft carburetor with automatic mixture control, a dry-sump with one pressure pump and two scavenge pumps oil system and an air-cooling system.

The PBM-1 has a maximum speed of 178 knots and a travel range of 2,600 nautical miles. It can fly up to 19,800 feet and can climb at a rate of 800 feet per minute. The patrol bomber could be loaded with eight 12.7 mm M2 Browning heavy machine guns located in the nose, tail turrets, and blisters amidships, and 1,800 kg of aerial bombs or depth charges or two Mark 13 torpedoes.