Preliminary selection of basic materials for flight vehicles is based on Mach number-altitude orientation, which includes turbulent flow to laminar flow location and effects. Structural weights and materials as a function of temperature are presented for both protected and unprotected primary structures. Design considerations and material selections for other pertinent items such as inlets, nose cones, leading edges, and transparencies are also considered.


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    Title :

    Effects of Subsonic, Supersonic, Hypersonic, and Orbital Environments on Structures


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    National Aeronautic and Space Engineering and Manufacturing Meeting ; 1966



    Publication date :

    1966-02-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :