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.

Variants

 * Hikari 3 - 770 hp (574 kW)
 * Hikari 1 - 820 hp (611 kW)

Applications

 * Aichi D1A
 * Aichi D3A (prototype only)
 * Mitsubishi F1M
 * Nakajima A4N
 * Nakajima B5N1 (B5N1 only)
 * Nakajima C3N
 * Yokosuka B4Y