A multi-phase investigation was conducted to quantify the thermal insult produced by the burning of unspent solid rocket propellant in a missile hit scenario. The objectives of this multi-phase investigation were to; identify the thermal conditions produced in the compartment during the missile fuel burning stage, identify the likelihood for ignition of Class A materials in the space and bound the transition time for the ensuring compartment fire. This report summarizes the results of the third and final phase of this investigation.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Propellant Fires in a Simulated Shipboard Compartments: Project HULVUL Phase III


    Beteiligte:
    F. W. Williams (Autor:in) / G. G. Back (Autor:in) / R. L. Darwin (Autor:in) / J. L. Scheffey (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    42 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Modeling Missile Propellant Fires In Shipboard Compartments

    P. A. Tatem / F. W. Williams / D. A. White et al. | NTIS | 2000


    Post-Flashover Fires in Simulated Shipboard Compartments. Phase 1 - Small Scale Studies

    J. T. Leonard / C. R. Fulper / R. L. Darwin et al. | NTIS | 1991


    Electrical cables in shipboard fires

    Codega, L. | Tema Archiv | 1975


    Fuelling fires in vehicle engine compartments

    British Library Online Contents | 1993