Titan Missile Museum
 

Nakajima NK9K-S Homare 22

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Developed by the Japanese Army from the Sakae engine. Engine used steel crankcase, water injection and dynamic crankshaft balancers. Only used in two aircraft types.

All photographs and text copyright Arizona Aerospace Foundation, 2009 and may not be used in any way without express written permission.

Technical Specifications
Model NK9K-S
Cylinders 18
Displacement/ Compressions 1,940 cu in
Rated Output 2,000 hp max
Commonly Used On Mitsubishi A7M1 Reppu, Aichi S1A Denko


Location: Hangar 4