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). PMAs 1 and 2 flew to ISS on Flight 2A and Pressurized Mating Adapter (PMA) 3 flew to ISS on Flight 3A. This paper provides a summary of the PMAs ECLS design and a detailed discussion of the ISS ECLS Acceptance Testing methodologies utilized for the PMAs.


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    Titel :

    International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters


    Beteiligte:

    Kongress:

    International Conference on Environmental Systems ; 2008 ; San Francisco, CA, United States


    Erscheinungsdatum :

    01.01.2008


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch