Current theory and experimental data on propellant utilization in electron-bombardment ion thrusters are reviewed. Because the majority of investigations have been conducted with mercury, the presentation emphasizes that propellant. The results are presented in as general a form as possible to facilitate use in areas other than space propulsion.


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    Titel :

    Maximum propellant utilization in an electron-bombardment thruster.


    Beteiligte:
    Kaufman, H. R. (Autor:in) / Cohen, A. J. (Autor:in)

    Kongress:

    American Physical Society and Brookhaven National Laboratory, Symposium on Ion Sources and Formation of Ion Beams ; 1971 ; Upton, NY


    Erscheinungsdatum :

    01.10.1971


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :





    Ion-Thruster Propellant Utilization

    H. R. Kaufman | NTIS | 1971


    Ion-thruster propellant utilization

    Kaufmann, Harold R. | TIBKAT | 1971