International Space Station Environmental Control and Life Support System - Verification for the Pressurized Mating Adapters | Zendy

David E. Williams | Zendy

Open Access

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

Author(s) -

David E. Williams

Publication year - 2007

Publication title -

sae technical papers on cd-rom/sae technical paper series

Language(s) - English

Resource type - Conference proceedings

SCImago Journal Rank - 0.295

H-Index - 107

eISSN - 1083-4958

pISSN - 0148-7191

DOI - 10.4271/2007-01-3103

Subject(s) - mating , life support system , international space station , computer science , space (punctuation) , control (management) , environmental science , engineering , aeronautics , operating system , ecology , aerospace engineering , biology , artificial intelligence

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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