Internal insulation in a solid rocket motor is defined as a layer of heat barrier material placed between the internal surface of the case propellant. The primary purpose is to prevent the case from reaching temperatures that endanger its structural integrity. Secondary functions of the insulation are listed and guidelines for avoiding critical problems in the development of internal insulation for rocket motors are presented.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Solid rocket motor internal insulation


    Beteiligte:

    Erscheinungsdatum :

    1976-12-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Elastomeric insulation for solid propellant rocket motor cases

    Burnett, C. R. / Mclaughlin, W. J. | NTRS | 1962



    Segmented solid rocket motor internal flow simulations

    TON, V. / WANG, J. / WIDHOPF, G. | AIAA | 1990