The International Space Station (ISS) Pressurized Mating Adapters (PMAs) Environmental Control and Life Support (ECLS) System is comprised of three subsystems: Atmosphere Control and Supply (ACS), Temperature and Humidity Control (THC), and Water Recovery and Management (WRM). PMA 1 and PMA 2 flew to ISS on Flight 2A and PMA 3 flew to ISS on Flight 3A. This paper provides a summary of the PMAs ECLS design and the detailed Element Verification methodologies utilized during the Qualification phase for the PMAs.


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    Title :

    International Space Station Environmental Control and Life Support System: Verification for the Pressurized Mating Adapters


    Contributors:

    Publication date :

    2007


    Size :

    10 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English