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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    Title :

    Composite reinforced propellant tanks


    Contributors:
    Brown, L. D. (author) / Martin, M. J. (author) / Aleck, B. J. (author) / Landes, R. (author)

    Publication date :

    1975-02-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Composite Reinforced Propellant Tanks

    L. D. Brown / M. J. Martin / B. J. Aleck et al. | NTIS | 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