Details of static radical aircooled 7-cylinder 4-cycle engine developing 122 hp. at 1950 r.p.m.; weight 270 lb.; fuel consumption 6 to 8 gal. per hr.; bore 4.25 in.; stroke 4.25 in.; compression ratio 5.2 to 1; displacement 422 cu. in. (See also Airway Age vol. 10, no. 1, Jan. 1929 pp. 82-83, 2 figs; Aero Digest, vol. 14, no. 2, Feb. 1929, pp. 114 and 116, 4 figs.)


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    Title :

    The Warner Scarab aircraft engine


    Additional title:

    Aviation Eng


    Published in:

    Publication date :

    1929


    Size :

    2 pages


    Remarks:

    1 Fig.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




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