We have use CORATHERM (Aérospatiale Cannes thermal software) capabilities to build a Thermal -> Mechanical interface and then to provide thermo-elastic inputs. Spacecraft thermal control CORATHERM model and spacecraft mechanical finite element mesh are the inputs of the interface. Temperature distribution calculation for finite element thermal loading does not come from a simple conductive interpolation but is the result of a method (“Equivale method”) which complies with thermal equations (radiative and conductive coupling).We have used this interface for a whole spacecraft (ARABSAT III) and we get temperature distribution for all panels and webs, on both sides, for various orbital positions.


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    Titel :

    Application of Thermal Software CORATHERM to Provide Thermo-Elastic Inputs


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    International Conference On Environmental Systems ; 1998



    Erscheinungsdatum :

    13.07.1998




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Application of Thermal Software CORATHERM to Provide Thermo-Elastic Inputs

    Rossi, F. N. / Pelletier, L. / SAE | British Library Conference Proceedings | 1998


    Applications of Thermal Software Coratherm to Provide Spacecraft Thermo-Elastic Inputs

    Basset, T. / Dudon, J.-P. / Vernay, C. et al. | British Library Conference Proceedings | 2001


    Applications of Thermal Software Coratherm to Provide Spacecraft Thermo-Elastic Inputs

    Vernay, Christophe / Dudon, Jean-Paul / Basset, Thierry | SAE Technical Papers | 2001


    Thermo-elastic similarity

    Sobey, A.J. | Engineering Index Backfile | 1954


    Thermo-Elastic Similarity

    Sobey, A.J. | Emerald Group Publishing | 1954