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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Composite Reinforced Propellant Tanks


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

    Publication date :

    1975


    Size :

    203 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




    Composite reinforced propellant tanks

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


    Propellant Condensation Prediction in Tanks

    Jallade, S. / Ounougha, L. | British Library Conference Proceedings | 1997


    Propellant management in toroidal tanks

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



    Propellant Condensation Prediction in Tanks

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