Linearized thermal balance equations of two-nodes system, in which radiative heat dissipation to outer space from each node and heat transfer between them are counted, are analytically solved for several special cases which closely relate to real situations in spacecraft; new method of thermal analysis of spacecraft is proposed, which is essentially experimental analysis of simplified thermal model; construction of this model and data reduction process are shown with example; using this method, thermal character of spacecraft can be determined with minimum simulator time and without lengthy numerical computation. (08545)


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    Title :

    Analytical approach to thermal design of spacecrafts


    Additional title:

    Inst Space Aeronaut Sci, Univ Tokyo, Rep


    Contributors:
    Oshima, K. (author) / Oshima, Y. (author)


    Publication date :

    1968


    Size :

    39 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


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