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. (Author)


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    Titel :

    Composite Reinforced Propellant Tanks


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

    Erscheinungsdatum :

    1975


    Format / Umfang :

    203 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Composite reinforced propellant tanks

    Brown, L. D. / Martin, M. J. / Aleck, B. J. et al. | NTRS | 1975


    COMPOSITE OVERWRAP POSITIVE EXPULSION PROPELLANT TANKS

    Sanscrainte, W. A. / West, L. K. / United States | British Library Conference Proceedings | 1990


    Design of Propellant Tanks

    Huang, David H. / Huzel, Dieter K. | AIAA | 1992


    Propellant Condensation Prediction in Tanks

    Jallade, S. / Ounougha, L. | British Library Online Contents | 1997


    Propellant management in toroidal tanks

    DOMINICK, S. / TEGART, J. | AIAA | 1985