A discussion of the unique problems associated with the integration of radioisotope thermoelectric systems and various types of satellites is presented. The effect of the device upon spacecraft thermal balance, mechanical integrity and configuration, mission interference, and electrical compatibility are explored. Aerospace safety and its dominant role in the practicable use of the device are considered.


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    Title :

    The Integration of Radioisotope Thermoelectric Systems and Spacecraft


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    SAE World Congress & Exhibition ; 1964



    Publication date :

    1964-01-01




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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