Design studies involving weight and cost were carried out for several structural concepts applicable to space shuttle disposable tankage. An effective design, a honeycomb stabilized pressure vessel, was chosen. A test model was designed and fabricated.


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    Titel :

    Composite reinforced propellant tanks


    Beteiligte:
    Brown, L. D. (Autor:in) / Martin, M. J. (Autor:in) / Aleck, B. J. (Autor:in) / Landes, R. (Autor:in)

    Erscheinungsdatum :

    1975-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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