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Technical Paper

A Strategy of System Synthesis for Developing Integrated Regenerative Life Support Systems

1998-07-13
981719
This paper considers one of the possible approaches to the synthesis of technologies for developing future Integrated Regenerative Life Support Systems (IRLSS) for space vehicle crews. The solution of technology synthesis task involves the following phases: (a) the efficiency model structuring for technical decision making process; (b) presentation of a discrete set of alternative technologies and their formal description; (c) the decision making task introduction. Modified efficiency model under consideration is based on use of local efficiency criteria set, reflecting designed system and its subsystems properties, space vehicle properties for which this system is intended. For the local criteria after verification of the independence terms quantitative and qualitative efficiency factors are applied. The qualitative efficiency factors were evaluated on the scale of order. The consideration of uncertainty in criteria values is based on a fuzzy set theory.
Technical Paper

Total Organic Carbon Analyzer For ISS

1998-07-13
981765
On the International Space Station (ISS), atmospheric humidity condensate and other waste waters will be recycled and treated to produce potable water for use by the crews. Space Station requirements include an on-orbit capability for real-time monitoring of key water quality parameters, such as total organic carbon (TOC), total inorganic carbon (TIC), total carbon (TC), pH, and conductivity, to ensure that crew health is protected during consumption of reclaimed water. The Crew Health Care System (CHeCS) for ISS includes an analyzer that has been designed to meet this requirement. The analyzer is adapted from commercially successful technology, and it measures TOC and TIC throughout the range from 1 to 50,000 μg/L, and TC from 1 to 100,000 μg/L. It measures pH between 2.0 and 12.0 pH units, and conductivity from 0.1 to 300 μmho/cm. The analyzer is scheduled for launch to ISS on mission 2A.1.
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