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Hydrogen Reduction of Lunar Regolith Simulants for Oxygen ProductionHydrogen reduction of the lunar regolith simulants JSC-1A and LHT-2M is investigated in this paper. Experiments conducted at NASA Johnson Space Center are described and are analyzed utilizing a previously validated model developed by the authors at NASA Glenn Research Center. The effects of regolith sintering and clumping, likely in actual production operations, on the oxygen production rate are studied. Interpretations of the obtained results on the basis of the validated model are provided and linked to increase in the effective particle size and reduction in the intra-particle species diffusion rates. Initial results on the pressure dependence of the oxygen production rate are also presented and discussed
Document ID
20110008404
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
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)
Rogers, K.
(NASA Johnson Space Center Houston, TX, United States)
Reddington, M.
(NASA Johnson Space Center Houston, TX, United States)
Oryshchyn, L.
(NASA Johnson Space Center Houston, TX, United States)
Date Acquired
August 25, 2013
Publication Date
March 1, 2011
Subject Category
Engineering (General)
Report/Patent Number
E-17632
NASA/TM-2011-216993
AIAA Paper 2011-0608
Meeting Information
Meeting: 49th Aerospace Sciences Meeting
Location: Orlando, FL
Country: United States
Start Date: January 4, 2011
End Date: January 7, 2011
Sponsors: American Inst. of Aeronautics and Astronautics
Funding Number(s)
WBS: WBS 387498.04.01.05.02.03
Distribution Limits
Public
Copyright
Public Use Permitted.
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