Spacecraft charging can occur when a spacecraft vehicle is subject to space plasma environments and varying sunlit conditions. The trajectory of the spacecraft will determine the specific impinging environment while the spacecraft geometry and material properties determine the susceptibility to various charging issues. In general, spacecraft charging is separated into two categories, surface charging (~<100 keV) and internal charging (~>100keV).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Spacecraft Charging during Docking Operations in the Outer Radiation Belt


    Beteiligte:

    Kongress:

    Applied Space Environments Conference ; 2019 ; Los Angeles, CA, United States


    Erscheinungsdatum :

    14.05.2019


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Internal Charging of Spacecraft in Jupiter's Radiation Belt

    Leung, P. / Garrett, H. / Whittlesey, A. | NTRS | 1996


    Artemis IV Docking in Radiation Belt Charging Environment

    Matthew Mccollum / Emily Willis / Anne Diekmann | NTRS


    Outer Radiation Belt Variations during 1995

    Desorgher, L. / Buehler, P. / Zehnder, A. et al. | British Library Conference Proceedings | 1998


    Outer Radiation Belt Variations during 1995

    Desorgher, L. | Online Contents | 1998


    EMI from Spacecraft Docking Systems Spacecraft Charging - Plasma Contact Potentials

    Norgard, John D. / Scully, Robert / Musselman, Randall | NTRS | 2012