Many requirements must be satisfied in order to achieve a successful spacecraft mission. One very pervasive requirement is that every spacecraft component must be maintained within either operating or survival temperature limits at all times. This is a very difficult requirement to satisfy because of the many boundary conditions.


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    Title :

    Radiant Heat Transfer in Reflector Systems


    Contributors:


    Publication date :

    1971-01-01


    Size :

    22 pages




    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English






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