A composite propellant composition and process are disclosed for reducing the reactive violence during cook-off and to improve the performance of a potassium perchlorate/ammonium perchlorate propellant composition wherein 0.25-2.0%, by weight, of iron oxide replaces 0.25-2.0% by weight, of potassium perchlorate in the composition.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Desensitized Solid Rocket Propellant Formulation


    Beteiligte:
    A. N. Duong (Autor:in) / G. B. Wilmot (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Solid-Propellant Rocket Engines

    A. M. Vinitskii | NTIS | 1974


    Solid propellant rocket motor

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


    Solid propellant rocket motors

    Smith, E.T.B. | Engineering Index Backfile | 1957


    Fast Desensitized Optimal Control for Rocket Powered Descent and Landing

    Robbiani, Tommaso / Sagliano, Marco / Topputo, Francesco et al. | AIAA | 2024


    Solid-Propellant Rocket Motors

    Greatrix, David R. | Springer Verlag | 2012