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.
International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters
Sae Technical Papers
International Conference On Environmental Systems ; 2008
29.06.2008
Aufsatz (Konferenz)
Englisch
British Library Conference Proceedings | 2008
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