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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    Titel :

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


    Beteiligte:
    S. Nomura (Autor:in)

    Erscheinungsdatum :

    1983


    Format / Umfang :

    80 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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