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Trace chemical contaminant generation rates for spacecraft contamination control system designA spacecraft presents a unique design challenge with respect to providing a comfortable environment in which people can live and work. All aspects of the spacecraft environmental design including the size of the habitable volume, its temperature, relative humidity, and composition must be considered to ensure the comfort and health of the occupants. The crew members and the materials selected for outfitting the spacecraft play an integral part in designing a habitable spacecraft because material offgassing and human metabolism are the primary sources for continuous trace chemical contaminant generation onboard a spacecraft. Since these contamination sources cannot be completely eliminated, active control processes must be designed and deployed onboard the spacecraft to ensure an acceptably clean cabin atmosphere. Knowledge of the expected rates at which contaminants are generated is very important to the design of these processes. Data from past spacecraft missions and human contaminant production studies have been analyzed to provide this knowledge. The resulting compilation of contaminants and generation rates serve as a firm basis for past, present, and future contamination control system designs for space and aeronautics applications.
Document ID
19960003343
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Perry, J. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1995
Subject Category
Man/System Technology And Life Support
Report/Patent Number
NASA-TM-108497
NAS 1.15:108497
Accession Number
96N13352
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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