On-orbit anomalies related to the deployment of spacecraft appendage and possible causes of such failures are considered. The discussion covers mechanical launch loading, on-orbit thermal and solar concerns, reliability of spacecraft pyrotechnics, and practical limitations of ground-based deployment testing. Lessons learned from the successful recovery of the Telesat Canada Anik-E2 satellite in 1991 are examined.<>


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    Titel :

    Spacecraft on-orbit deployment anomalies: What can be done?


    Beteiligte:
    Freeman, M.T. (Autor:in)


    Erscheinungsdatum :

    1993-04-01


    Format / Umfang :

    2045994 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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