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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    Titel :

    Characterising the Thermal Performance of the European Comet Chaser ROSETTA


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Stramaccioni, D. (Autor:in) / Kerner, R. (Autor:in) / Tuttle, S. L. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 2003



    Erscheinungsdatum :

    07.07.2003




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Characterising the Thermal Performance of the European Comet Chaser ROSETTA

    Tuttle, S. L. / Kerner, R. / Stramaccioni, D. et al. | British Library Conference Proceedings | 2003



    US Rosetta Project: NASA's Contribution to ESA's Comet Chaser

    Chmielewski, Arthur B. / Alexander, Claudia J. | NTRS | 2011


    The New Mission of ‘Rosetta’ Comet Chaser and In-Orbit First Temperature Results

    Stramaccioni, D. / Kerner, R. / Tuttle, S. | SAE Technical Papers | 2004


    The New Mission of Rosetta Comet Chaser and In-Orbit First Temperature Results

    Stramaccioni, D. / Kerner, R. / Tuttle, S. et al. | British Library Conference Proceedings | 2004