Operation of Hall thrusters with bismuth propellant has been shown to be a promising path for development of high-power (140 kW per thruster), high performance (8000s I(sub sp at >70% efficiency) electric propulsion systems.


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    Titel :

    Flow Control of Liquid Metal Propellants for In-Space Electric Propulsion Systems


    Beteiligte:
    Bonds, Kevin W. (Autor:in) / Polzin, Kurt A. (Autor:in)

    Kongress:

    40th Fluid Dynamics Conference and Exhibit ; 2010 ; Chicago, IL, United States


    Erscheinungsdatum :

    28.06.2010


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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