Titan Missile Museum
 

Shvetsov ASh-62

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This engine design was a Russian re-engineered version of the Wright R-1820.

All photographs and text copyright Arizona Aerospace Foundation, 2006 and may not be used in any way without express written permission.

Technical Specifications
Cylinders 9
Rated Output 1,000 hp at 2,000 r.p.m.
Dry Weight 1,200 lbs
Commonly Used On An-2, An-2M


Location: Hangar 1 North