- Nakajima Hikari
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Hikari Type Piston aircraft engine Manufacturer Nakajima Aircraft Company Major applications Aichi D1A Developed from Nakajima Kotobuki 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.
Contents
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
Specifications
General characteristics
- 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 in3)
Components
- Cooling system: Air-cooled
Performance
- Power output: 611 kW (820 hp)
See also
- Related development
- Related lists
References
Nakajima aircraft engines Piston engines Ha-1 Kotobuki · Ha-5 · Ha-8 Hikari · Ha-103 Mamoru · Sakae · Ha-45 Homare
Lists relating to aviation General Aircraft (manufacturers) · Aircraft engines (manufacturers) · Airlines (defunct) · Airports · Civil authorities · Museums · Registration prefixes · Rotorcraft (manufacturers) · TimelineMilitary Accidents/incidents Records Categories:- Radial engines
- Aircraft piston engines 1930-1939
- Nakajima aircraft engines
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