Compliance with the United Nations recommended 25-year maximum orbital lifetime requirement will restrict future standard CubeSat nanosatellite deployments to altitudes below 600 km. This paper describes a deployable aerodynamic drag device that can be incorporated in basic CubeSat satellite units that can meet the 25-year orbital lifetime constraint for initial orbit perigees of up to 900 km.


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    Titel :

    A de-orbit system design for CubeSat payloads


    Beteiligte:
    Lokcu, E. (Autor:in) / Ash, R. L. (Autor:in)


    Erscheinungsdatum :

    01.06.2011


    Format / Umfang :

    1306300 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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