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Nakajima B3N

From Wikipedia, the free encyclopedia
Japanese carrier-based torpedo bomber prototype
B3N
General information
TypeTorpedo bomber
National originJapan
ManufacturerNakajima Aircraft Company
StatusPrototype
Number built2
History
First flight1933

TheNakajima B3N was a prototypeJapanesecarrier-basedtorpedo-bomber aircraft of the 1930s. A single-enginedbiplane with a crew of three, it was unsuccessful, only two being built.

Development and design

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In April 1932, theImperial Japanese Navy placed orders withMitsubishi andNakajima for prototypes of three-seat torpedo-bombers to replace the relatively unsuccessfulMitsubishi B2M and the earlierMitsubishi B1M aboard Japan's aircraft carriers.[1] Nakajima's design was a single-enginedbiplane with a slender circular section fuselage of steel tube construction. It hadsingle-bay metal and fabric wings, with both the upper and lower wingsgulled to meet the fuselage, with the upper wings gulled normally and the lower wings in an inverted gull arrangement, forming an X shape. It had atailwheel undercarriage, with the main wheels attached to the lower wing where the gulled section joined the main wing. The new 700 hp (522 kW)Nakajima Hikari engine was chosen to power the aircraft, driving a three-bladed fixed-pitch metal propeller.[2]

Nakajima built two prototypes in 1933, with the internal designationNakajima Y3B, as theExperimental 7-Shi Carrier Attack Aircraft, with theshort designationB3N1 but the prototype Hikari engines proved unreliable, and the type was not accepted by the Navy.[2] Mitsubishi's competing 7-Shi design, theRolls-Royce Buzzard powered3MT10 was also a failure, the sole prototype crashing on take-off in 1934,[3] with the design from the Navy's ownAir Technical Arsenal atYokosuka, which was started later than the competing designs from Mitsubishi and Nakajima and therefore managed to avoid some of their flaws, being ordered into production as theYokosuka B3Y.[4]

Specifications (B3N1)

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Data fromJapanese Aircraft 1910-41[2]

General characteristics

  • Crew: 3 (pilot, navigator/bomb aimer and gunner)
  • Length: 10 m (32 ft 10 in)
  • Wingspan: 14 m (45 ft 11 in)
  • Height: 3.80 m (12 ft 6 in)
  • Wing area: 50.0 m2 (538 sq ft)
  • Empty weight: 2,000 kg (4,409 lb)
  • Gross weight: 3,800 kg (8,378 lb)
  • Powerplant: 1 ×Nakajima Hikari 2 9-cylinderradial engine, 520 kW (700 hp)
  • Propellers: 3-bladed

Performance

  • Maximum speed: 220 km/h (140 mph, 120 kn)
  • Stall speed: 93 km/h (58 mph, 50 kn)
  • Endurance: 6 hr
  • Service ceiling: 5,500 m (18,000 ft)
  • Time to altitude: 12 minutes to 3,000 m (9,800 ft)

Armament

  • Guns: 1 × flexibly mounted 7.7 mm machine gun
  • Bombs: 1 × 800 kg (1,760 lb) torpedo,or 1 × 800 kg bomb,or 2 × 250 kg bombs

See also

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Aircraft of comparable role, configuration, and era

References

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  1. ^Mikesh and Abe 1990, pp. 230–231.
  2. ^abcMikesh and Abe 1990, p.231.
  3. ^Mikesh and Abe 1990, p.170.
  4. ^Mikesh and Abe 1990, pp. 280–281.
  • Mikesh, Robert C. and Abe, Shorzoe.Japanese Aircraft 1910-1941. London:Putnam, 1990.ISBN 0-85177-840-2.

External links

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Nakajima aircraft
Imperial Japanese Navy types
Carrier fighters
Carrier Torpedo Bombers
Reconnaissance aircraft
Dive bombers
Reconnaissance floatplanes
Land-based Attack Bombers
Interceptors
Transports
Floatplane fighter
Other
Imperial Japanese Army types
Army manufacturer type code system
Army type-year
Kitai (airframe #)
WW2 Allied reporting names
Fighters (A)
Torpedo bombers (B)
Shipboard reconnaissance (C)
Dive bombers (D)
Reconnaissance seaplanes (E)
Observation seaplanes (F)
Land-based bombers (G)
Flying Boats (H)
Land-based Fighters (J)
Trainers (K)
Transports (L)
Special-purpose (M)1
Floatplane fighters (N)
Land-based bombers (P)
Patrol (Q)
Land-based reconnaissance (R)
Night fighters (S)
1 X as second letter is for experimental aircraft or imported technology demonstrators not intended for service,2 Hyphenated trailing letter (-J, -K, -L, -N or -S) denotes design modified for secondary role,3 Possibly incorrect designation, but used in many sources
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