This paper describes testing of four-bed molecular sieve (4BMS) development hardware in support of future operations of the International Space Station (ISS) Carbon Dioxide Removal Assembly (CDRA). During 1998, testing of a MSFC 4BMS included operations with the 4BMS inlet air drawn directly from the cabin atmosphere instead of the baseline air source downstream of a Condensing Heat Exchanger (CHX), operating with high carbon dioxide (CO2) loading, and long duration operation in a power save mode. Additionally, testing with increased coolant water temperature was performed to determine effects on the systems CO2 removal performance.


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    Titel :

    Performance Enhancement, Power Reduction, and other Flight Concerns - Testing of the CO2 Removal Assembly for ISS


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Howard, David F. (Autor:in) / Knox, James C. (Autor:in)

    Kongress:

    International Conference On Environmental Systems ; 1999



    Erscheinungsdatum :

    1999-07-12




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




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