A precursor formulation comprising, before curing, a hydroxyl-terminated polybutadiene (HTPB) prepolymer or a hydroxyl-terminated polyether (HTPE) prepolymer, an oxidizer, a dimer fatty diol, and an isocyanate curative. A solid propellant comprising a reaction product of the HTPB prepolymer or HTPE prepolymer, the dimer fatty diol, and the isocyanate curative is also disclosed, as is a rocket motor comprising a case and a solid propellant in the case, the solid propellant comprising the reaction product and an oxidizer. A method of reducing a burn rate of a solid propellant is also disclosed.


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    Titel :

    PRECURSOR FORMULATIONS OF A SOLID PROPELLANT, SOLID PROPELLANTS INCLUDING A REACTION PRODUCT OF THE PRECURSOR FORMULATION, ROCKET MOTORS INCLUDING THE SOLID PROPELLANT, AND RELATED METHODS


    Beteiligte:
    LARSON ROBERT S (Autor:in) / BEAL ROYCE (Autor:in)

    Erscheinungsdatum :

    17.01.2019


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64G Raumfahrt , COSMONAUTICS / F02K JET-PROPULSION PLANTS , Strahltriebwerke / C06B EXPLOSIVE OR THERMIC COMPOSITIONS , Sprengstoffe oder thermische Gemische




    Solid propellant rocket motors

    Maxwell, W.R. / Young, G.H.S. | Engineering Index Backfile | 1961


    Testing solid-propellant rocket motors

    Klient, R.E. / McCown, R.D. | Engineering Index Backfile | 1960



    VORTICES IN SOLID PROPELLANT ROCKET MOTORS

    SOTTER, G. / SWITHENBANK, J. | AIAA | 1963