Shuttle systems ablator and insulation materials underwent water soak with subsequent water desorption in vacuum. Water accumulation in these materials after a soak for 24 hours ranged from +1.1% for orbiter tile to +161% for solid rocket booster MSA-1. After 1 minute in vacuum, water retention ranged from none in the orbiter tile to +70% for solid rocket booster cork.


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    Titel :

    Water absorption and desorption in shuttle ablator and insulation materials


    Beteiligte:
    Whitaker, A. F. (Autor:in) / Smith, C. F. (Autor:in) / Wooden, V. A. (Autor:in) / Cothren, B. E. (Autor:in) / Gregory, H. (Autor:in)

    Erscheinungsdatum :

    1982-02-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    Apollo composite ablator material used on Space Shuttle

    TARTAGLIONE, L. / MAZZOLA, J. | AIAA | 1982


    Origin and Development of Ablator for Space Shuttle External Tank

    Ronquillo, Leon | SAE Technical Papers | 1985


    ABLATOR, AND METHOD FOR MANUFACTURING ABLATOR

    KUBOTA YUKI / SUZUKI TOSHIYUKI / ISHIDA YUICHI et al. | Europäisches Patentamt | 2019

    Freier Zugriff