The results of a program to design and fabricate an unshielded actively cooled structural panel for a hypersonic aircraft are presented. The design is an all-aluminum honeycomb sandwich with embedded cooling passages soldered to the inside of the outer moldline skin. The overall finding is that an actively cooled structure appears feasible for application on a hypersonic aircraft, but the fabrication process is complex and some material and manufacturing technology developments are required. Results from the program are summarized and supporting details are presented.


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    Title :

    High Heat Flux Actively Cooled Honeycomb Sandwich Structural Panel for a Hypersonic Aircraft


    Contributors:
    L. C. Koch (author) / L. L. Pagel (author)

    Publication date :

    1978


    Size :

    172 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English