A method for the conceptual design of a capsule type re-entry vehicle was investigated aerodynamically and aerothermodynamically. The purpose of this investigation was to find a method for determining the optimum thermal protection thickness under arbitrary constraints such as decelaration rate, down range, and so forth.


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    Title :

    Method for Aerodynamic and Aerothermodynamic Conceptual Design of Capsule Type Re-entry Vehicle


    Contributors:
    S. Nomura (author)

    Publication date :

    1983


    Size :

    80 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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