One of design conditions for solid propellant rocket motors is that of inertia loading due to long term storage at 1 g, or acceleration in short time to high g; paper investigates structural integrity for inertia loading of long, bonded, thick-walled cylinder, and includes parametric considerations of rocket diameter, web fraction, inertia g-level, and reduced burnout time, as well as employing typical propellant properties and allowing for various burning rates of eroding boundary; by assuming maximum shear strain failure criterion, design envelope is obtained expressing interaction among various parameters.


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    Titel :

    Structural integrity of ablating rocket subjected to axial acceleration


    Weitere Titelangaben:

    AIAA J


    Beteiligte:
    Lindsey, G.H. (Autor:in) / Williams, M.L. (Autor:in)

    Erschienen in:

    AIAA Journal ; 3 , n 2 ; p 258-262


    Erscheinungsdatum :

    1965


    Format / Umfang :

    5 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :