The purpose of the CubeSat development is to define a standard bus that can be used by anyone needing a simple picosatellite. Defining a standard bus, developing standard hardware components using commercial off the shelf components and a standard spacecraft frame will simplify the development of picosatellites. The CubeSat development will provide a standard spacecraft frame, a spacecraft controller, radio transceiver, attitude determination and control, solar cells, batteries, and an interface for a payload. The developer needs only to concentrate on the payload.


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    Titel :

    CubeSat: developing a standard bus for picosatellites


    Beteiligte:
    Galysh, Ivan (Autor:in) / Doherty, Kevin (Autor:in) / McGuire, James (Autor:in) / Heidt, Hank (Autor:in) / Niemi, David (Autor:in) / Dutchover, G. (Autor:in)

    Kongress:

    Small Payloads in Space ; 2000 ; San Diego,CA,United States


    Erschienen in:

    Proc. SPIE ; 4136 ; 64


    Erscheinungsdatum :

    07.11.2000





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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