This paper discusses application of computerassisted design system to development of a solar sail powered spacecraft. Minimum orbit altitude is calculated; also non-linear static analysis for frame-type solar sail is performed in finite elements simulation system. Moreover, mathematical model of small solar sail spacecraft motion is considered. Finally, the analysis of this motion is performed.


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    Titel :

    The project of the small frame-type solar sail spacecraft


    Beteiligte:


    Erscheinungsdatum :

    01.06.2015


    Format / Umfang :

    646208 byte




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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