The current status of technology and the developmental trends in the field of ion propulsion systems and components for primary and auxiliary applications in advanced earth-orbital and interplanetary missions are reviewed. Particular attention is given to the (electrostatic) 30-cm electron bombardment ion thruster being developed with the aim of achieving an overall efficiency of 73% at full power (2.75 kW) and 64% at half power.


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    Titel :

    Current NASA ion propulsion technology


    Beteiligte:
    Finke, R. C. (Autor:in)

    Kongress:

    European Electric Propulsion Conference ; 1974 ; Hinterzarten


    Erscheinungsdatum :

    01.01.1974


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch




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