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. (see also similar description in Flight v 27 n 1366 Feb 28 1935 p 218-9)


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    Title :

    Cirrus minor


    Additional title:

    Aeroplane


    Published in:

    Aeroplane ; 48 , n 1240


    Publication date :

    1935


    Size :

    3 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