The development and demonstration of practical thermal scale modeling techniques applicable to systems involving radiation, conduction, and convection with emphasis on cabin atmosphere/cabin wall thermal interface are discussed. The Apollo spacecraft environment is used as the model. Four possible scaling techniques were considered: (1) modified material preservation, (2) temperature preservation, (3) scaling compromises, and Nusselt number preservation. A thermal mathematical model was developed for use with the Nusselt number preservation technique.


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    Title :

    A thermal scale modeling study for Apollo and Apollo applications, volume 2


    Contributors:

    Publication date :

    1972-06-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English


    Keywords :