Brief illustrated description of radial engine rated 165 hp at 2100 rpm and 175 hp at 2250 rpm for take-off; bore 4.625 in.; stroke 4.25 in.; compression ratio 6.4:1; dual ignition. (See also Aero Digest v 35 n 1 July 1939 p 110)


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    Title :

    Warner 7-cylinder 165 hp super-scarab


    Additional title:

    Aviation


    Published in:

    Aviation ; 38 , n 8


    Publication date :

    1939


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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    Engineering Index Backfile | 1929


    The Warner Scarab aircraft engine

    Engineering Index Backfile | 1929


    The Warner Scarab aircraft engine

    Engineering Index Backfile | 1929



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