The mission of the Micro-sized Microwave Atmospheric Satellite (MicroMAS) is to collect useful atmospheric images using a miniature passive microwave radiometer payload hosted on a low-cost CubeSat platform. In order to collect this data, the microwave radiometer payload must rotate to scan the ground-track perpendicular to the satellite's direction of travel. A custom motor assembly was developed to facilitate the rotation of the payload while allowing the spacecraft bus to remained fixed in the local-vertical, local-horizontal (LVLH) frame for increased pointing accuracy. This paper describes the mechanism used to enable this dual-spinning operation for CubeSats, and the lessons learned during the design, fabrication, integration, and testing phases of the mechanism's development lifecycle.


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    Titel :

    Design and Functional Validation of a Mechanism for Dual-Spinning CubeSats


    Beteiligte:
    Peters, Eric (Autor:in) / Dave, Pratik (Autor:in) / Kingsbury, Ryan (Autor:in) / Marinan, Anne (Autor:in) / Wise, Evan (Autor:in) / Pong, Chris (Autor:in) / Prinkey, Meghan (Autor:in) / Cahoy, Kerri (Autor:in) / Miller, David W. (Autor:in) / Sklair, Devon (Autor:in)


    Erscheinungsdatum :

    2014-05-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


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