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.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Performance of Materials in Solid Propellant Rocket Motor Exhaust Environments


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    Intersociety Conference on Environmental Systems ; 1984



    Publication date :

    1984-07-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




    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