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International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters
Technical Paper
2008-01-2182
ISSN: 0148-7191, e-ISSN: 2688-3627
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Language:
English
Abstract
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.
Authors
Citation
Williams, D., "International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters," SAE Technical Paper 2008-01-2182, 2008, https://doi.org/10.4271/2008-01-2182.Also In
References
- Williams, D. E. “International Space Station Environmental Control and Life Support System - Verification for the Pressurized Mating Adapters” SAE 2007-01-3103 37 th International Conference on Environmental Systems Chicago, Il. July 2007
- “Prime Item Development Specification for Pressurized Mating Adapter” August 24 2004
- “Space Station Program Fluid Procurement and Use Control Specification” September 29 2004
- “Element Acceptance Test Drawing Acceptance Test Requirements” June 23 1997
- “PMA 2/3 Element Acceptance Test Requirements” August 19 1998
- “Test Report PMA 2 - PMA 2 O2/N2 Resupply Lines Verification - 1F92500-P0207-B;” June 1 1998
- “Test Report Node 1/PMA 2 Oxygen System Testing - 1F00400-P1900 New;” May 5 1998
- “Test Report PMA 3 - PMA 3 O2/N2 Resupply Lines Verification - 1F93000-P0307-A;” June 22 1998