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Exergy Based Analysis for the Environmental Control and Life Support Systems of the International Space StationWhen optimizing the performance of complex systems, a logical area for concern is improving the efficiency of useful energy. The energy available for a system to perform work is defined as a system's energy content. Interactions between a system's subsystems and the surrounding environment can be accounted for by understanding various subsystem energy efficiencies. Energy balance of reactants and products, and enthalpies and entropies, can be used to represent a chemical process. Heat transfer energy represents heat loads, and flow energy represents system flows and filters. These elements allow for a system level energy balance. The energy balance equations are developed for the subsystems of the Environmental Control and Life Support (ECLS) system aboard the International Space Station (ISS). The use of these equations with system information would allow for the calculation of the energy efficiency of the system, enabling comparisons of the ISS ECLS system to other systems as well as allows for an integrated systems analysis for system optimization.
Document ID
20160012079
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Clem, Kirk A.
(Alabama Univ. Huntsville, AL, United States)
Nelson, George J.
(Alabama Univ. Huntsville, AL, United States)
Mesmer, Bryan L.
(Alabama Univ. Huntsville, AL, United States)
Watson, Michael D.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Perry, Jay L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
October 7, 2016
Publication Date
September 13, 2016
Subject Category
Space Transportation And Safety
Man/System Technology And Life Support
Report/Patent Number
M16-5542
Report Number: M16-5542
Meeting Information
Meeting: AIAA Space 2016 Conference
Location: Long Beach, CA
Country: United States
Start Date: September 13, 2016
End Date: September 16, 2016
Sponsors: American Inst. of Aeronautics and Astronautics
Distribution Limits
Public
Copyright
Public Use Permitted.
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