For the long duration mission intended for the COLUMBUS pressurized modules (i.e. APM & PM2) the Environmental Control and Life Support System (ECLSS) as used in former applications like Spacelab had to be advanced.The development encompasses modifications of assemblies/functions which have been part of existing systems (e.g the cooling air loops) as well as the implementation of new features like for example the trace gas contamination monitoring assembly.AH functions which form a part of one of the two ECLS systems are listed and described with their status at the beginning of Phase C/D. Special emphasis is given to the air loops.


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    Titel :

    Design of the Environmental Control & Life Support Systems for the Columbus Pressurized Modules


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Kring, G. (Autor:in) / Hlenerwadel, K.-O. (Autor:in)

    Kongress:

    Intersociety Conference on Environmental Systems ; 1989



    Erscheinungsdatum :

    1989-07-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Active Thermal Control Design of COLUMBUS Pressurized Modules

    Dodd, Charles / Trichilo, Michele / Dolce, Silvio | SAE Technical Papers | 1989


    Thermal Control Definition of COLUMBUS Pressurized Modules

    Racca, Giuseppe D. / Costamagna, Lazzaro | SAE Technical Papers | 1987


    Thermal Design and Analysis of Columbus Pressurized Modules

    Dodd, Charles / Ciampolini, Francesca / Dolce, Silvio | SAE Technical Papers | 1990


    Air Coolant Circuits in the Columbus Pressurized Modules

    Honnen, Karl / Huchler, Markus | SAE Technical Papers | 1992


    Atmosphere Trace Gas Contamination Management for the Columbus Pressurized Modules

    Abele, Hermann / Franzen, Jochen / Ammann, Klaus | SAE Technical Papers | 1990