SOLROCK

    Projekter: ProjektForskning

    Projektdetaljer

    Beskrivelse

    The goal of this project was to develop a procedure for reliable structural analysis and service life
    estimation of a solid rocket motor grain.
    I did structural stress analyses of a full-scale model of a solid propellant rocket motor under actual
    loading histories. An accurate material model of propellant was verified with including material ageing.

    Funding 300.000 Euro
    StatusAfsluttet
    Effektiv start/slut dato01/01/200731/12/2010