Results of investigation conducted in Langley 8-ft transonic pressure tunnel on vehicle designed to use heat sink and blunt shape to alleviate effects of heating encountered during reentry of earth's atmosphere.


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    Title :

    Wind-tunnel investigation at mach numbers from 0.40 to 1.14 of static aerodynamic characteristics of nonlifting vehicle suitable for reentry


    Additional title:

    NASA -- Memo


    Contributors:


    Publication date :

    1959


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :