The results are reported of the phase-change paint tests conducted at Mach 8, to determine the aerodynamic heat transfer distributions on the McDonnell Douglas delta wing orbiter. Model details, test conditions, and reduced heat transfer data are presented.


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    Title :

    Space Shuttle Heat Transfer Rate Distributions on Mcdonnell-Douglas delta Wing Orbiter Determined by Phase-Change Paint Technique for Nominal Mach Number of 8


    Contributors:

    Publication date :

    1972


    Size :

    358 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English