Design and performance of Ryan's X-13 Vertijet powered by 10,000-lb thrust Rolls-Royce Avon turbojet; X-13 is without either undercarriage or flaps, which simplifies design, and results in weight saving of 10%; for takeoff, it is suspended clear of ground, hooked to short length of cable, to which it returns at hover when landing.


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    Titel :

    Development for VTOL jet fighter


    Weitere Titelangaben:

    Aeroplane


    Erschienen in:

    Aeroplane ; 93 , n 2415 ; p 891-893


    Erscheinungsdatum :

    1957


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Dispersed Site VTOL Fighter-Bomber Design Study

    by christenson / hutchinson | NTIS | 1956


    CTOL, STOVL, and VTOL FIGHTER DESIGN COMPARISONS

    WILSON, III, S. / ESKEY, M.A. / ZOLA, C.L. | AIAA | 1985



    Free-flight model investigation of a vertical-attitude VTOL fighter

    Newsom, W. A., Jr. / Anglin, E. L. | NTRS | 1975