Study shows weight comparison or trend data between different vehicles and heat protection schemes; application is to lifting and ballistic-type entry vehicles undertaking satellite and circumlunar missions; structural cooling methods examined include radiation, ablation, and combinations of these methods.


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    Title :

    Parametric weight study of manned space entry vehicle


    Additional title:

    Aerospace Eng


    Contributors:

    Published in:

    Aerospace Engineering ; 19 , n 10 ; p 40-49 + 77


    Publication date :

    1960


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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