Plasma source neutralizes electrical charge on spacecraft. When triggered by command from spacecraft potential monitor or from control system, plasma apparatus responds within about 1 s, generating charged plasma of required polarity. Discharging system to be tested on Air Force Geophysics Laboratory BERT-1 (Beam Emission Rocket Test) sounding rocket.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Plasma Source for Charge Control


    Beteiligte:
    Aston, G. (Autor:in) / Pless, L. C. (Autor:in) / Deininger, W. D. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1986-06-01



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Hollow cathode plasma source for active spacecraft charge control

    Deininger, W.D. / Ashton, G. / Pless, L.C. | Tema Archiv | 1987



    Charge Loss of Proton Flux as an Additional Source of Plasma in F~2 Region

    Kozelov, B. V. / Kozelova, T. V. / Committee on Space Research; Scientific Commission C | British Library Conference Proceedings | 1995


    Active Charge Control Using an Electron Beam and Ultraviolet Light Source

    Walker, James D. / Schaub, Hanspeter | AIAA | 2024


    Quiet Plasma Source

    Leung, P. L. | NTRS | 1986