The paper considers the solar sail principle as an effective means of space propulsion. The heliogyro configuration is discussed including the hub structures, the flap-hinge brace assembly, and the blade. The material requirements of the sail film made of metallized polymers, the tendons produced from a polymer-graphite fiber composite, and battens constructed of graphite/epoxy tubings are considered, noting that not all of these materials were readily available. It was concluded that the primary material problems are the environmental degradation of polymer films, the meteoroid hazard, and the production capacity for large polymer film quantities.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Material problems in solar sail development


    Beteiligte:
    Steurer, W. H. (Autor:in)

    Kongress:

    Aerospace Sciences Meeting ; 1980 ; Pasadena, CA


    Erscheinungsdatum :

    01.01.1980


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Solar Sail Spacecraft Development

    Danielle R DaCosta | NTRS



    Solar Sail Propulsion Technology Development

    Jenkins, Christopher H. M. | AIAA | 2006


    Spacecraft solar sail processing method and solar sail

    REN ZHONGJING / LI CHENGYANG / XIE KECAI et al. | Europäisches Patentamt | 2023

    Freier Zugriff