The development and ground testing of a scalable solar sail configuration to address NASA's future space propulsion needs were discussed. The baseline design in development and testing was optimized around the 1 Au solar sentinel mission. The use of striped sail architecture, net/membrane sail design and L'Garde's conical boom depolyment technique allows scalability without high mass penalties. The fabricated masses and structural test results of our beam components have met predictions and no changes to the mass estimates have been identified, which added great credibility to the design.


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    Titel :

    Development and ground testing of a compactly stowed scalable inflatably deployed solar sail


    Beteiligte:
    Lichodziejewski, David (Autor:in) / Derbes, Billy (Autor:in) / Reinert, Rich (Autor:in) / Belvin, Keith (Autor:in) / Slade, Kara (Autor:in) / Mann, Troy (Autor:in)


    Erscheinungsdatum :

    2004


    Format / Umfang :

    16 Seiten, 9 Quellen


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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    Lichodziejewski, David / Derbes, Billy / Reinert, Rich et al. | NTRS | 2004


    Development and Ground Testing of a Compactly Stowed Inflatably Deployed Solar Sail

    Lichodziejewski, David / West, John / Reinert, Richard et al. | AIAA | 2004


    AIAA-2004-1507 Development and Ground Testing of a Compactly Stowed Inflatably Deployed Solar Sail

    Lichodziejewski, D. / West, J. / Reinert, R. et al. | British Library Conference Proceedings | 2004


    Ground Testing A 20-Meter Inflation Deployed Solar Sail

    Mann, Troy / Behun, Vaughn / Lichodziejewski, David et al. | NTRS | 2006