Description of 6-cylinder inverted in-line air-cooled engine; good forward vision is afforded by position of engine in respect to line of thrust; bore 4 1/8 in.; stroke 5 1/2 in.; piston displacement 441 cu. in.; weight 345 lb.; 2 valves per cylinder; underhead camshaft; pressure feed lubrication. (See also West. Flying vol. 6, no. 4, Oct. 1929 pp. 68 and 142, 1 fig; Aviation Eng., vol. 10, no. 2, Oct. 1929, p. 44, 1 fig.; Airway Age, vol. 10, no. 12, Dec. 1929, p. 1988, 2 figs)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Curtiss crusader


    Additional title:

    Aero Digest


    Published in:

    Aero Digest ; 15 , n 5


    Publication date :

    1929


    Remarks:

    4 Figs.


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English




    Curtiss crusader

    Engineering Index Backfile | 1929


    Curtiss crusader

    Engineering Index Backfile | 1929


    Curtiss crusader

    Engineering Index Backfile | 1929


    Curtiss. Curtiss P-6 Hawk

    Engineering Index Backfile | 1930


    Curtiss ascender

    Perry, H.W. | Engineering Index Backfile | 1945