An extensive program has been conducted to evaluate the performance of a broad spectrum of heatshield materials in the near-field exhaust regions of solid propellant rocket motors. Environmental emphasis focused on motors which produce a high concentration of alumina particles in the exhaust flow field. Testing was performed using various tactical missile motors and specially-designed solid propellant rocket motor simulators. Specimens surveyed included a wide variety of commercially available and specialty heatshield materials. Materials were evaluated from a weight and cost basis, as well as from a relative erosion standpoint.


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    Titel :

    Performance of Materials in Solid Propellant Rocket Motor Exhaust Environments


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Intersociety Conference on Environmental Systems ; 1984



    Erscheinungsdatum :

    01.07.1984




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    SOLID PROPELLANT ROCKET MOTOR

    W. L. Dowler / J. I. Shafer / J. W. Behm et al. | NTIS | 1971


    Solid propellant rocket motor

    Dowler, W. L. / Shafer, J. I. / Behm, J. W. et al. | NTRS | 1973


    Solid Propellant Rocket Motor

    W. L. Dowler / J. I. Shafer / J. W. Behm et al. | NTIS | 1973