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)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Curtiss crusader


    Weitere Titelangaben:

    Aero Digest


    Erschienen in:

    Aero Digest ; 15 , n 5


    Erscheinungsdatum :

    1929


    Anmerkungen:

    4 Figs.


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    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 controllable

    Engineering Index Backfile | 1937