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Impacts of Reduced Pressure Atmospheres on Environmental Control and Life Support Systems (ECLSS) ArchitecturesThe study found that while nine subsystems are viable without modification at 10.2 psia, only three remain acceptable at 8.2 psia. Material flammability presents the most critical hurdle in the 8.2 psia/34-40% O2 environment, where 70% of the assessed subsystems will require material replacements, many of which have yet to be developed. Ultimately, adapting ISS heritage hardware to these exploration conditions will introduce varied mass, power (e.g., increased fan speeds), and significant schedule impacts driven by the need for extensive testing, redesign, and recertification. The report concludes with specific recommendations for targeted analysis and testing to quantify these impacts and guide necessary design modifications.
Document ID
20260003925
Acquisition Source
Langley Research Center
Document Type
Technical Memorandum (TM)
Authors
Morgan B Abney
(Langley Research Center Hampton, United States)
Robert M. Bagdigian
(NASA Retired Redstone Arsenal, Alabama, United States)
Chase Hopkins
(University of South Florida Tampa, United States)
Ariel V Macatangay
(Johnson Space Center Houston, United States)
Holly A Cagle
(NASA Retired Houston, Texas, United States)
Michael D Pedley
(Johnson Space Center Houston, United States)
James Knox
(Dynetics, Inc. Huntsville, AL, United States)
Date Acquired
May 6, 2026
Publication Date
May 1, 2026
Publication Information
Subject Category
Man/System Technology and Life Support
Report/Patent Number
NESC-RP-20-01610
Funding Number(s)
WBS: 869021.01.23.01.01
Distribution Limits
Public
Copyright
Public Use Permitted.
Technical Review
NASA Peer Committee
Keywords
Environmental Control and Life Support Systems
Exploration Atmospheres
Flammability
Reduced Pressure
High Oxygen Concentration
Material Selection
Thermal Control
ISS Heritage Hardware
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