NanoSail-D unfurled January 20th, 2011 and successfully demonstrated the deployment and deorbit capability of a solar sail in low Earth orbit. The orbit was strongly perturbed by solar radiation pressure, aerodynamic drag, and oblate gravity which were modeled using STK HPOP. A comparison of the ballistic coefficient history to the orbit parameters exhibits a strong relationship between orbital lighting, the decay rate of the mean semi-major axis and mean eccentricity.


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    Titel :

    NanoSail:D Orbital and Attitude Dynamics


    Weitere Titelangaben:

    Springer Praxis Books (formerly: Springer-Praxis Series)


    Beteiligte:
    Macdonald, Malcolm (Herausgeber:in) / Heaton, Andrew F. (Autor:in) / Faller, Brent F. (Autor:in) / Katan, Chelsea K. (Autor:in)


    Erscheinungsdatum :

    2014-02-04


    Format / Umfang :

    19 pages




    Medientyp :

    Aufsatz/Kapitel (Buch)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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