Nakajima J5N

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Nakajima J5N
Nakajima Ki-84 Hayate
Type: Fighter plane
Design country:

JapanJapan Japan

Manufacturer:

Nakajima Hikōki

First flight:

July 13, 1944

Number of pieces:

6th

The Nakajima J5N (nickname 天雷, Tenrai, German " Heavenly Thunder ") was a twin-engine high - altitude interceptor of the Imperial Japanese Naval Air Force in World War II .

development

In the spring of 1943, the Imperial Japanese Navy Air Force requested a single-seat, twin-engine interceptor that was to be able to simultaneously reach a top speed of 666 km / h at an altitude of 6,000 meters. The aircraft manufacturer Nakajima Hikōki developed the prototype Nakajima J5N1 on this . The machine was based on the earlier Nakajima J1N1 , a three-seater night fighter . The armament of the Nakajima J5N consisted of two 30 mm and two 20 mm cannons as well as a 250 kg bomb , with which the US armed forces were to be inflicted heavy losses. The maiden flight of a still unarmed Nakajima J5N on July 13, 1944 was disappointing. The prototype could not reach the required top speed with only 597 km / h.

A total of six Nakajima J5N machines were completed, but not a single one was used in the war. Of the six completed aircraft, four were lost in crashes or on the ground.

Technical specifications

Parameter Data from the Nakajima J5N1
crew 1
length 11.46 m
span 14.00 m
height 2.38 m
Wing area 32.00 m²
Empty mass 5,195 kg
Max. Takeoff mass 7,350 kg
Best climb 900 m / min
Top speed 619 km / h
Engines two 18-cylinder double radial engines of the type Nakajima Homare 21, each with 1,990 hp (1,485 kW)
Armament two 30 mm cannons, two 20 mm cannons and a 250 kg bomb

See also

Web links

Commons : Nakajima J5N Tenrai  - Collection of pictures, videos and audio files

Individual evidence

  1. ^ A b cf. Kenneth Munson: The World War II Aircraft - All Aircraft of the Warring Powers. Motorbuch Verlag, Stuttgart 1977, p. 439.