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.
International Space Station Environmental Control and Life Support System - Verification for the Pressurized Mating Adapters
Sae Technical Papers
International Conference On Environmental Systems ; 2007
2007-07-09
Aufsatz (Konferenz)
Englisch
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