Conceptual tank with replaceable liner holds liquid propellant and is suitable for reuse in spacecraft propulsion systems. Main components are: composite outer shell for containment of pressure, replaceable membrane liner, and foam-filled honeycomb sandwich bonded to inside of tank to insulate and stabilize wall of tank. Concept maximizes potential of filament-wound composite pressure shells with strength-to-density ratios five times those of comparable aluminum shells. Reduction in weight as much as 50 percent.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Reusable Cryogenic-Liquid Tank With Replaceable Liner



    Erschienen in:

    Erscheinungsdatum :

    01.07.1992



    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Reinforcing Liner For Composite Cryogenic Tank

    Burgeson, John E. | NTRS | 1990


    Aerostat launching system with replaceable liner

    SLOCUM JONATHAN T / SLOCUM ALEXANDER H | Europäisches Patentamt | 2025

    Freier Zugriff

    Developments on Cryogenic Tank Insulation for Reusable Launchers

    Denaro, A. / Ritter, H. / Society of Automotive Engineers | British Library Conference Proceedings | 2004


    Developments on Cryogenic Tank Insulation for Reusable Launchers

    Denaro, A. / Ritter, H. | SAE Technical Papers | 2004