Model information and data are presented from wind tunnel tests conducted on 0.01-scale models of the space shuttle orbiter and external tank. These tests were conducted in a hypersonic shock tunnel to determine heating rates on ascent and reentry configurations at various Reynolds numbers, Mach numbers, and angles of attack.


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    Titel :

    Heat transfer tests on a 0.01-scale Rockwell configuration 3 space shuttle orbiter and tank (37-OT) in the Calspan 48-inch hypersonic shock tunnel (OH12/IH21), volume 1


    Beteiligte:
    Kotch, M. (Autor:in)

    Erscheinungsdatum :

    1975-10-01


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch