The technique of mixing argon with air was used to simulate the temperature-time trajectory experienced by space shuttle vehicle insulation panels. Gap heating appears to be highly dependent upon gap design, it is relatively low for interlocking and tapered panel designs and significantly higher for a wider, unfilled gap design. The heating rate appears to be significantly higher at the windward facing edges of flush tiles and is aggravated at forward facing steps. This heating, however, is highly dependent on step heights relative to some characteristic thickness of the boundary layer.


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    Titel :

    Aerodynamic simulation tests of RSI panels


    Beteiligte:


    Erscheinungsdatum :

    01.09.1973


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :



    On aerodynamic instability of thin panels

    Miles, J.W. | Engineering Index Backfile | 1956


    Postflight Apollo command module aerodynamic simulation tests

    Griffith, B.J. / Boylan, D.E. | Engineering Index Backfile | 1968