A method is described for placing a large, STS-compatible platform on orbit utilizing a construction method employing both deployable and erectable structures. A multifunctional mechanism is used for deployable structures and an on-orbit assembly is used for erectable structures. Also analyses are discussed which assess the thermal distortion of a simple open truss and a more complex truss.


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    Titel :

    Structural/thermal considerations for design of large space platform structures


    Beteiligte:
    Barclay, D. L. (Autor:in) / Brogren, E. W. (Autor:in) / Skoumal, D. E. (Autor:in)


    Erscheinungsdatum :

    01.01.1978


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch




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