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International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters NASA, Johnson Space Center
- Format:
- Conference/Event
- Author/Creator:
- Williams, David E., author.
- Conference Name:
- International Conference On Environmental Systems (2008-06-29 : San Francisco, California, United States)
- Language:
- English
- Physical Description:
- 1 online resource
- Place of Publication:
- Warrendale, PA SAE International 2008
- Summary:
- 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
- Notes:
- Vendor supplied data
- Publisher Number:
- 2008-01-2182
- Access Restriction:
- Restricted for use by site license
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