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The environmental control and life support system for a lunar base - What drives its designIt is noted that no single ECLSS is uniquely applicable to a mission of given crew size and duration; all mission parameters, together with details of other systems, must accordingly be factored into the lunar base ECLSS design process that is presently discussed. Experience to date with ECLSS design tasks indicates that mission planners and systems engineers should refrain from emphasizing the 'closed loop' aspects of such systems, since even the best regenerative processes will involve expendable materials that must be resupplied; resupply logistics will accordingly constitute a considerable effort of lunar base operation. Technology development status for processes and subsystems is identified as a major ECLSS design driver.
Document ID
19880051458
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hypes, Warren D.
(Bionetics Corp. Hampton, VA, United States)
Hall, John B., Jr.
(NASA Langley Research Center Hampton, VA, United States)
Date Acquired
August 13, 2013
Publication Date
April 1, 1988
Subject Category
Man/System Technology And Life Support
Accession Number
88A38685
Distribution Limits
Public
Copyright
Other

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