This presentation focuses on the tank history, test objectives, failure description, investigation and conclusions. The test objectives include verify structural integrity at 105% expected flight load limit varying the following parameters: cryogenic temperature; internal pressure; and mechanical loading. The Failure description includes structural component of the aft body, quad-lobe design, and sandwich - honeycomb graphite epoxy construction.


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    Titel :

    X-33 LH2 Tank Failure Investigation Findings


    Beteiligte:

    Kongress:

    Aerospace Materials, Processes and Environmental Technology ; 2000 ; Huntsville, AL, United States


    Erscheinungsdatum :

    2000-01-01


    Medientyp :

    Preprint


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :




    X33 Hydrogen Tank Failure

    James Reeder | NTRS



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