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Heating-Rate-Coupled Model for Hydrogen Reduction of JSC-1AA previously developed and validated model for hydrogen reduction of JSC-1A for a constant reaction-bed temperature is extended to account for reaction during the bed heat-up period. A quasisteady approximation is used wherein an expression is derived for a single average temperature of reaction during the heat-up process by employing an Arrhenius expression for regolith conversion. Subsequently, the regolith conversion during the heat-up period is obtained by using this representative temperature. Accounting for the reaction during heat-up provides a better estimate of the reaction time needed at the desired regolith-bed operating temperature. Implications for the efficiency of the process, as measured by the energy required per unit mass of oxygen produced, are also indicated.
Document ID
20100017327
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Hegde, U.
(National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Balasubramaniam, R.
(National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Gokoglu, S. A.
(NASA Glenn Research Center Cleveland, OH, United States)
Date Acquired
August 24, 2013
Publication Date
April 1, 2010
Subject Category
Lunar And Planetary Science And Exploration
Report/Patent Number
NASA/TM-2010-216256
AIAA Paper 2010-1546
E-17242
Report Number: NASA/TM-2010-216256
Report Number: AIAA Paper 2010-1546
Report Number: E-17242
Meeting Information
Meeting: 48th Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2010
End Date: January 7, 2010
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
CONTRACT_GRANT: NNC08BA08B
WBS: WBSW 387498.04.01.05.02.03
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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