The design and development of the louvre for the ROSETTA spacecraft in the scope of its thermal qualification process are presented. In the first section the design and its development are described. The analytical prediction considering effective emittance and absorbtance of this design are presented in the following section. Tests at unit as well as spacecraft level have been conducted in order to verify the thermal design.


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    Titel :

    Thermal Design and Test of ROSETTA Platform Louvres*


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Stramaccioni, D. (Autor:in) / Pérez, F.J. (Autor:in) / Härtel, K. (Autor:in) / Reichenberger, K. (Autor:in) / Morgenroth, L. (Autor:in) / Domingo, M. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 2000



    Erscheinungsdatum :

    10.07.2000




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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    Wind-tunnel tests of air intake louvres

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