International Space Station Environmental Control and Life Support System Acceptance Testing for the Pressurized Mating Adapters 2008-01-2182
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.
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. Download Citation
Author(s):
David E. Williams
Affiliated:
NASA, Johnson Space Center
Pages: 12
Event:
International Conference On Environmental Systems
ISSN:
0148-7191
e-ISSN:
2688-3627
Related Topics:
Life support systems
Spacecraft
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