The International Space Station (ISS) Environmental Control and Life Support (ECLS) system includes regenerative and non-regenerative technologies which provide the basic life support functions to support the crew, while maintaining a safe and habitable shirt-sleeve environment. Significant progress has been made over the past year including initial assembly flights of the Functional Cargo Block (FGB) and Node 1 modules. The remaining Phase 2 elements have completed significant element integration testing with ECLS hardware deliveries complete, while the Phase 3 elements and regenerative ECLS design activities have continued. This paper provides a summary of the U.S. Environmental Control and Life Support (ECLS) system activities over the past year.


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    Title :

    International Space Station Environmental Control and Life Support System Status: 1998-1999


    Additional title:

    Sae Technical Papers


    Contributors:

    Conference:

    International Conference On Environmental Systems ; 1999



    Publication date :

    1999-07-12




    Type of media :

    Conference paper


    Type of material :

    Print


    Language :

    English




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