A thruster designed to produce thrust by introducing a propellant to a catalyst layer from a propellant valve via a propellant introduction member and spurting out a gas resulting from decomposition of the propellant occurring on the catalyst layer, wherein the thruster comprises a chamber of an Ni alloy for holding the catalyst layer inside, the propellant introduction member is made of an Ni alloy and connects the propellant valve and the chamber, and a propellant valve flange of a Ti alloy with a plurality of columns of a Ti alloy is arranged between the chamber and the propellant valve to support the chamber by the columns.


    Zugriff

    Download


    Exportieren, teilen und zitieren



    Titel :

    Thruster and spacecraft


    Beteiligte:
    NAGAO TORU (Autor:in) / MORITA NAOKI (Autor:in)

    Erscheinungsdatum :

    28.06.2016


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F02K JET-PROPULSION PLANTS , Strahltriebwerke / B64G Raumfahrt , COSMONAUTICS



    Gimballing Spacecraft Thruster

    Pickens, Tim / Bossard, John | NTRS | 2010




    Mach‐Lorentz Thruster Spacecraft Applications

    March, Paul | American Institute of Physics | 2007


    Spacecraft thruster voltage measurement unit

    MARCOPULOS THEODORE | Europäisches Patentamt | 2025

    Freier Zugriff