This paper will highlight the electrical power system topology and basic performance of the SOHO mission during the first two years of its operation. It will go on to relate the chronology of spacecraft and power system events that occurred from the initial loss of SOHO contact in June 1998, up until the time of its attitude recovery some three months later. It will describe the operational modes of the power system during this critical period and the fundamental lessons learnt, which could enhance recovery prospects in the event that other missions experience a similar anomaly.


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    Titel :

    Power System Performance of the SOHO Spacecraft During the 1998 Attitude Recovery


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Fiebrich, H. (Autor:in) / Haines, J. E. (Autor:in) / Perol, P. (Autor:in) / Rumle, P. (Autor:in)

    Kongress:

    34th Intersociety Energy Conversion Engineering Conference ; 1999



    Erscheinungsdatum :

    02.08.1999




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :



    The SOHO Mission L~1 Halo Orbit Recovery from the Attitude Control Anomalies of 1998

    Roberts, C.E. | British Library Conference Proceedings | 2003


    SOHO spacecraft thermal control aspects

    Poinas, P. / Cande, J. | British Library Online Contents | 1997


    SOHO spacecraft thermal control aspects

    Poinas, P. / Cande, J. / European Space Agency | British Library Conference Proceedings | 1997