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Nakajima Hikari : ウィキペディア英語版 | Nakajima Hikari
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. In Army use it was known as the Ha-20. ==Variants==
* Hikari 3 - 770 hp (574 kW) * Hikari 1 - 820 hp (611 kW)
抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)』 ■ウィキペディアで「Nakajima Hikari」の詳細全文を読む
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