Nakajima Hikari

Type: 9-cylinder air-cooled radial aircraft piston engine
Bore: 160 mm (6.30 in)
Stroke: 180 mm (7.09 in)
Displacement: 32.57 L (1,987.7 in 3 )

From Wikipedia, the free encyclopedia

The Nakajima Hikari (Japanese: 光 "Light") was a nine-cylinder, air-cooled, radial aircraft engine developed in Japan for Navy use during World War II by the Nakajima Aircraft Company. It was a development of the Nakajima Kotobuki and Wright Cyclone.

Variants

v t e Nakajima aircraft engines

Piston engines	Ha-1 Kotobuki Ha-5 Ha-8 Hikari Ha-103 Mamoru Sakae Ha-45 Homare

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