This paper describes the processes and evolution of the design and verification of the thermal control subsystem of the Rosetta spacecraft. In particular, it describes the testing, both at component-level and spacecraft-level, that was necessary and the subsequent correlation activities that were required to understand the thermal behaviour of the spacecraft and thus develop a thermal model that portrayed this correctly.


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    Title :

    Characterising the Thermal Performance of the European Comet Chaser ROSETTA


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    International Conference On Environmental Systems ; 2003



    Publication date :

    2003-07-07




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English


    Keywords :


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