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International Space Station Environmental Control and Life Support System: Verification for the Pressurized Mating AdaptersThe 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.
Document ID
20070019851
Document Type
Conference Paper
Authors
Williams, David E. (NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 23, 2013
Publication Date
July 9, 2007
Subject Category
Man/System Technology and Life Support
Meeting Information
37th International Conference on Environmental Systems(Chicago, IL)
Funding Number(s)
WBS: WBS 401769.06.01.01.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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