Missile 36D was tested at the Sycamore Canyon Captive Test Site, from 28 October 1959 through 9 February 1960. The purpose of the test program was to study missile tank skin strain characteristics during the thrust build-up transient for both wet and dry engine start configurations. (Author)


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    Titel :

    Effects of Engine Thrust Transients on XSM-65D Missiles


    Beteiligte:
    D. F. Foreman (Autor:in)

    Erscheinungsdatum :

    1960


    Format / Umfang :

    151 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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