Nakajima A6M2-N Airplane Videos and Airplane Pictures

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Nakajima A6M2-N Aircraft Information

Nakajima A6M2-N

A6M2-N

Warbird Picture - A6M2-N

Picture - A6M2-N

Role: Interceptor/Fighter-bomber
Manufacturer: Nakajima Aircraft Company
Introduced: 1942
Primary user: Imperial Japanese Navy Air Service
Number built: 327
Developed from: A6M Zero

The Nakajima A6M2-N (Navy Type 2 Interceptor/Fighter-Bomber) is a single-crew float seaplane based on the Mitsubishi A6M Zero Model 11. The Allied reporting name for the aircraft was Rufe.

Design and development

The A6M2-N floatplane was developed from the Mitsubishi A6M Zero Type 0, for the purpose of supporting amphibian operations and defending remote bases. It was based on the A6M-2 Model 11 fuselage, with a modified tail and added floats. This aircraft was the brainchild of Shinobu Mitsutake, Nakajima Aircraft Company's Chief Engineer, and Atsushi Tajima, one of the company's designers. A total of 327 were built, including the original prototype.

The aircraft was deployed in 1942, referred to as the "Suisen 2" ("Hydro fighter type 2"), and was only utilized in defensive actions in the Aleutians and Solomon Islands operations. Such seaplanes were effective at night in harassing American PT boats, and they were very difficult to detect, even with primitive radar. Close misses killed officers and crew of boats such as PT 105. They would also drop flares to illuminate the PTs which were vulnerable to destroyer gunfire, and depended on cover of darkness. Since the boats left a phosphorescent wake which was visible from the air, they would leave their engines in idle to minimize this wake. It was primarily for this reason that John F. Kennedy's PT 109 was caught off guard in idle and rammed by the destroyer Amagiri, unable to maneuver out of the way in time.

Airplane Picture - A6M2-Ns at Attu, Alaska.

Picture - A6M2-Ns at Attu, Alaska.

The seaplane also served as an interceptor for protecting fueling depots in Balikpapan and Avon Bases (Dutch East Indies) and reinforced the Shumushu base (North Kuriles) in the same period. Such fighters served aboard seaplane carriers Kamikawa Maru in the Solomons and Kuriles areas and aboard Japanese raiders Hokoku Maru and Aikoku Maru in Indian Ocean raids. In the Aleutian Campaign this fighter engaged with Lockheed P-38 Lightning fighters and Boeing B-17 Flying Fortress bombers. The aircraft was used for interceptor, fighter-bomber, and short reconnaissance support for amphibious landings, among other uses.

Later in the conflict the Otsu Air Group utilized the A6M2-N as an interceptor alongside Kawanishi N1K1 Kyofu ("Rex") aircraft based in Biwa lake in the Honshū area.

The last A6M2-N in military service was a single example recovered by the French forces in Indochina after the end of World War II. It crashed shortly after being overhauled by the French.

The large float and wing pontoons of the A6M2-N degraded its performance by about 20%, enough that the Rufe was not usually a match for even the first generation of Allied fighters.

Operators

Airplane Picture - Japanese pilots at a A6M2-N plane anchorage.

Picture - Japanese pilots at a A6M2-N plane anchorage.

Japan

Imperial Japanese Navy Air Service
Yokohama Air Group
Toko Air Group
Otsu Air Group
Yokosuka Air Group (technical evaluation unit)
11th Air Fleet
5th Air Fleet
36th Air Fleet
452nd Air Fleet
934th Air Fleet

Specifications (Nakajima A6M2-N)

Airplane Picture - Salvaged wreck of an A6M2-N at a U.S. base in 1943.

Picture - Salvaged wreck of an A6M2-N at a U.S. base in 1943.

Data from Japanese Aircraft of the Pacific War

General characteristics

Length: 10.10 m (33ft 1⅝ in)
Wingspan: 12.00 m (39 ft 4⅜ in)
Height: 4.30 m (14ft 1⅜ in)
Wing area: 22.44 m² (251.4 sq ft)
Empty weight: 1,912 kg (4,235 lb)
Loaded weight: 2,460 kg (5,423 lb)
Max takeoff weight: 2,880 kg (6,349 lb)
Powerplant: 1x— Nakajima NK1C Sakae 12 air cooled 14 cylinder radial engine, 950 hp (709 kW) at 4,200 m (13,800 ft)

Performance

Maximum speed: 436 km/h (235 knots, 270.5 mph) at 5,000 m (16,400 ft)
Cruise speed: 296 km/h (160 knots, 184 mph)
Range: 1,782 km (963 nmi, 1,107 mi)
Service ceiling: 10,000 m (32,800 ft)
Climb to 5,000 m (16,400 ft): 6 min 43 s

Armament

Guns:
2 x— 7.7 mm Type 97 machine guns in forward fuselage
2 x—20 mm Type 99 cannons -fixed in outer wings
Bombs: 2 x— 60 kg (132 lb) bombs

Related development

Mitsubishi A6M Zero

Bibliography

Dorr, Robert F. and Chris Bishop. Vietnam Air War Debrief. London:Aerospace |Publishing, 1996. ISBN 1 874023 78 6.
Francillon, R.J. Japanese Aircraft of the Pacific War. London:Putnam, 1970. ISBN 0 370 00033 1.
Green, William. War Planes of the Second World War, Volume Six: Floatplanes. London: Macdonald & Co., (Publishers) Ltd., 1962.
Jackson, Robert. Combat Legend: Mitsubishi Zero. Ramsbury, Marlborough, Wiltshire, UK: Airlife Publishing, 2003. ISBN 1-84037-398-9.
Janowicz, Krzystof. Mitsubishi A6M2-N Rufe (Kagero Famous Airplanes 4) (in Polish/English). Lublin, Poland: Kagero, 2004. ISBN 83-89088-42-8.
Mikesh, Robert C. Warbird History: Zero, Combat & Development History of Japan's Legendary Mitsubishi A6M Zero Fighter. Osceola, Wisconsin: Motorbooks International, 1994. ISBN 0-87938-915-X.
Sakaida, Henry. Imperial Japanese Navy Aces, 1937-45. Botley, Oxford, UK: Osprey Publishing Ltd., 1999. ISBN 1-85532-727-9.
Gunston,Bill. The Illustrated Encyclopedia of Combat Aircraft of World War II. London, UK: Salamander Books Ltd., 1978 ISBN 0-89673-000-x

Nakajima A6M2-N Pictures

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Source: WikiPedia

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