This study focused on the mechanical properties and ablation properties of liner insulation in rocket motors for improving rocket performance by means of tensile strength, elongation, ablation rate and density. The following parameters were varied: amount of zinc oxide, antimony trioxide and carbon black (N550). It was found that the insulation of the rocket motors with antimony trioxide and carbon black provided higher the elongation and ablation rate. Thus, it was able to endure more heat from hot gas in combustion chamber. The result suggests that use of antimony trioxide and carbon black as filler in liner insulation can improve the thermal insulators and case-bonded in rocket motor between the solid propellant and the rocket motor tube.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Effect of Antimony Trioxide and Carbon Black on the Mechanical Properties and Ablation Properties of Liner Insulation in Rocket Motors



    Erschienen in:

    Erscheinungsdatum :

    2021-03-29


    Format / Umfang :

    6 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





    Propellant-liner bonding in colloidal propellant rocket motors

    Cunliffe, A. V. / Tod, D. A. / Wylie, P. | British Library Conference Proceedings | 2004


    Cumulative-damage concept for propellant-liner bonds in solid rocket motors

    Bills, Jr., K.W. / Svob, G.J. / Planck, R.W. et al. | Engineering Index Backfile | 1966


    PRECURSOR COMPOSITIONS FOR AN INSULATION AND INSULATED ROCKET MOTORS

    GAJIWALA HIMANSU M / HALL STEVEN B | Europäisches Patentamt | 2021

    Freier Zugriff

    Precursor compositions for an insulation and insulated rocket motors

    GAJIWALA HIMANSU M / HALL STEVEN B | Europäisches Patentamt | 2022

    Freier Zugriff