A number of phenomena observed on the first orbiting Meteosat satellite attributed to spacecraft charging effects are considered. Design analysis, correlation of anomalies with space environmental data, on ground tests with an engineering model spacecraft, tests on the validity of improvements, and installation of suitable monitors for the second improved flight satellite are discussed.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Meteosat spacecraft charging investigation


    Beteiligte:
    Hoge, D. G. (Autor:in)


    Erscheinungsdatum :

    1980-10-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Meteosat

    Kendal, B. / McDermott, M. | Tema Archiv | 1985


    Meteosat Second Generation: CFRP-Structures for High Precision Optical Spacecraft Instruments

    Seibel, M. / Huchler, M. / European Space Agency | British Library Conference Proceedings | 1999



    Meteosat First Generation Spacecraft Power System Design Evolution & In-Orbit Performance Features

    Levins, D. P. / European Space Agency | British Library Conference Proceedings | 1998


    Meteosat Earth station

    Christieson, M.L. | Tema Archiv | 1979