Carbide-based fuel assembly includes outer structural member of ceramic matrix composite material (e.g., SiC—SiC composite), insulation layer of porous refractory ceramic material (e.g., zirconium carbide with open-cell foam structure or fibrous zirconium carbide), and interior structural member of refractory ceramic-graphite composite material (e.g., zirconium carbide-graphite or niobium carbide-graphite). Spacer structures between various layers provide a defined and controlled spacing relationship. A fuel element bundle positioned between support meshes includes a plurality of distributively arranged fuel elements or a solid, unitary fuel element with coolant channels, each having a fuel composition including high assay, low enriched uranium (HALEU). Fuel assemblies are distributively arranged in a moderator block and the upper end of the outer structural member is attached to a metallic inlet tube for hydrogen propellant and the lower end of the outer structural member is interfaced with a support plate, forming a NTP reactor.


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    Title :

    CARBIDE-BASED FUEL ASSEMBLY FOR THERMAL PROPULSION APPLICATIONS


    Additional title:

    CARBIDBASIERTES BRENNSTOFFBÜNDEL FÜR WÄRMEANTRIEBSANWENDUNGEN
    ASSEMBLAGE COMBUSTIBLE À BASE DE CARBURE POUR APPLICATIONS DE PROPULSION THERMIQUE


    Contributors:

    Publication date :

    2024-03-20


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS / G21C NUCLEAR REACTORS , Kernreaktoren / G21D NUCLEAR POWER PLANT , Kernkraftwerke



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