International Space Station Environmental Control and Life Support System - Verification for the Pressurized Mating Adapters 2007-01-3103
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.
Citation: Williams, D., "International Space Station Environmental Control and Life Support System - Verification for the Pressurized Mating Adapters," SAE Technical Paper 2007-01-3103, 2007, https://doi.org/10.4271/2007-01-3103. Download Citation
Author(s):
David E. Williams
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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