Explorer 40 satellite mathematical model and verification testing for close spacecraft flight temperature predictions


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    Title :

    Generalized approach to the thermal analysis of orbiting spacecraft.


    Contributors:

    Conference:

    SOCIETY OF AUTOMOTIVE ENGINEERS, INTERNATIONAL AUTOMOTIVE ENGINEERING CONGRESS ; 1969 ; DETROIT, MICH.


    Publication date :

    1969-01-01


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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