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Allison V-1710

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Resulted from U.S. Army development program dating back to 1930's. Engine was liquid cooled. Engine continued to be improved during WW-II. Engine shown above mounted on a Curtiss P-40N.

Technical Specifications
Cylinders 12
Displacement/ Compressions 1,700 cu in/6.65 to 1
Rated Output 1,325 hp at 3,000 r.p.m.
Dry Weight 1,620 lbs
Commonly Used On YFM-1, P-38, P-39, P-40, early P-51, P-63


Location: Hangar 4