Ishikawajima Ne-20

The Ishikawajima Ne-20 (Template:Langx) was Japan's first turbojet engine. It was developed during World War II in parallel with the nation's first military jet, the Nakajima Kikka.

Design and development

The decision to manufacture this engine came about because of the unsuitability of two earlier powerplants selected for the Kikka, the Tsu-11 and the Ne-12.

Only a small number of these engines, perhaps fifty, were produced before the end of the war. Two of them were used to power the Kikka on its only flight on August 7, 1945. Only a few of the engines under construction survived. It was also planned to use the engine to power a version of the Ohka kamikaze weapon, but this was not implemented before the end of the war.

Variants

Ne-20

Standard production engines

Ne-20-Kai

Up-rated version

Engines on display

File:Ne20 turbojet.png

Ishikawajima Ne-20 turbojet on display at Steven F. Udvar-Hazy Center

Three Ne-20s have been preserved to the present day, one at Ishikawajima-Harima's internal company museum in Tanashi, and two at the Smithsonian's National Air and Space Museum in Washington, DC.

Specifications (Ne-20)

Data from Turbojet History and Development 1930–1960 Volume 2:USSR, USA, Japan, France, Canada, Sweden, Switzerland, Italy and Hungary

General characteristics

• Type: Turbojet engine
• Length: 2700 mm
• Diameter: 620 mm
• Dry weight: 470 kg

Components

• Compressor: 8-stage Axial compressor
• Combustors: Annular combustion chamber
• Turbine: 1-stage axial turbine

Performance

• Maximum thrust: 475 kgf (4.66 kN, 1,047 lbf) at 11,000 rpm
• Specific fuel consumption: 1.5 lb/(lb h)
• Thrust-to-weight ratio: 1.01

See also

Comparable engines

• BMW 003
• Junkers Jumo 004
• Heinkel HeS 006 — later, more common designation: Heinkel HeS 30

Related lists

• List of aircraft engines

External links

• Kugisho Ne-20, Naval Air Technical Arsenal, Turbojet Engine Template:Webarchive -National Air and Space Museum

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