Advanced, burn-rate, propellant modeling is critical for developing new rocket missile and gun propellants for Future Combat Systems and for providing a fundamental screening tool that can result in substantial cost savings compared to missile and gun firings. In this paper, we report the detailed chemical kinetics and burn rate prediction of tri-aminoguanidinium azotetrazolate (TAGzT) and nitrocellulose (NC).


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Burn-Rate Modeling and Combustion Diagnostics for Environmentally Friendly, Solid Rocket Propellants


    Contributors:

    Publication date :

    2006


    Size :

    5 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Environmentally Compatible Solid Rocket Propellants

    Jacox, J. L. / Bradford, D. J. / United States; National Aeronautics and Space Administration | British Library Conference Proceedings | 1995




    New Ferrocenes for Burn Rate Modification of Composite Rocket Propellants

    Menke, K. / Bohnlein-Mauss, J. / Brehler, K.-P. et al. | British Library Conference Proceedings | 1995


    SOLID ROCKET PROPELLANTS

    Mama, Horrrluz P. | Online Contents | 1996