An unlined reusable filament wound composite cryogenic tank was tested at the Marshall Space Flight Center using LH2 cryogen and pressurization to 320 psig. The tank was fabricated by Phillips Laboratory and Wilson Composite Group, Inc., using an EnTec five-axis filament winder and sand mandrels. The material used was IM7/977-2 (graphite/epoxy).


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing


    Beteiligte:
    A. W. Murphy (Autor:in) / R. E. Lake (Autor:in) / C. Wilkerson (Autor:in)

    Erscheinungsdatum :

    1999


    Format / Umfang :

    12 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




    Cryogenic Glass-Filament-Wound Tank Evaluation

    E. E. Morris / R. E. Landes | NTIS | 1971


    Filament-Wound, Fiberglass Cryogenic Tank Supports

    J. S. Carter / T. E. Timberlake | NTIS | 1971


    Filament-wound, fiberglass cryogenic tank supports

    Carter, J. S. / Timberlake, T. E. | NTRS | 1971


    REUSEABLE ROCKET RENAISSANCE

    Debra Werner | Online Contents | 2015


    Test of Filament Wound Prototype for Cryogenic Propellant Tank of Space Plane

    Shimoda, Takayuki / He, Jianmei / Mizutani, Yoshihiro et al. | AIAA | 2002