4-cyl in-line, air-cooled, direct-drive engine; 95 mm bore; 127 mm stroke; normal bhp 70 at 2400 rpm; weight 210 lb; fuel consumption 0.54 pt per hp-hr at normal rpm. (Similar description) (See also - Aeroplane v 48 n 1240 Feb 27 1935 p 241-3)


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    Title :

    Cirrus minor


    Additional title:

    Flight


    Published in:

    Flight ; 27 , n 1366


    Publication date :

    1935


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Cirrus minor

    Engineering Index Backfile | 1935


    "Cirrus" minor II aero-engine

    Engineering Index Backfile | 1945


    "Cirrus" minor II aero-engine

    Engineering Index Backfile | 1945


    "Cirrus" minor II aero-engine

    Engineering Index Backfile | 1945


    "Cirrus" minor II aero-engine

    Engineering Index Backfile | 1945