Theoretical studies made prior to launching of satellites and examples of relationships presented in graphs; thermal control was based on analysis of all influencing parameters; it is shown that temperature of satellites can be controlled can be passive means; on-board instrument temperatures can be kept between 0 and 65 C during operating time of 60 to 90 days; temperature variations of skin can be kept between -- 30 and 90 C. (see also IRE -- Trans on Military Electronics v MIL-4 n 2-3 Apr-July 1960 p 98-112)


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    Title :

    Thermal control of explorer satellites


    Additional title:

    ARS -- J


    Contributors:

    Published in:

    ARS Journal ; 30 , n 4


    Publication date :

    1960


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :