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Modeling of Melt Growth During Carbothermal Processing of Lunar RegolithThe carbothermal processing of lunar regolith has been proposed as a means to produce carbon monoxide and ultimately oxygen to support human exploration of the moon. In this process, gaseous methane is pyrolyzed as it flows over the hot surface of a molten zone of lunar regolith and is converted to carbon and hydrogen. Carbon gets deposited on the surface of the melt, and mixes and reacts with the metal oxides in it to produce carbon monoxide that bubbles out of the melt. Carbon monoxide is further processed in other reactors downstream to ultimately produce oxygen. The amount of oxygen produced crucially depends on the amount of regolith that is molten. In this paper we develop a model of the heat transfer in carbothermal processing. Regolith in a suitable container is heated by a heat flux at its surface such as by continuously shining a beam of solar energy or a laser on it. The regolith on the surface absorbs the energy and its temperature rises until it attains the melting point. The energy from the heat flux is then used for the latent heat necessary to change phase from solid to liquid, after which the temperature continues to rise. Thus a small melt pool appears under the heated zone shortly after the heat flux is turned on. As time progresses, the pool absorbs more heat and supplies the energy required to melt more of the regolith, and the size of the molten zone increases. Ultimately, a steady-state is achieved when the heat flux absorbed by the melt is balanced by radiative losses from the surface. In this paper, we model the melting and the growth of the melt zone with time in a bed of regolith when a portion of its surface is subjected to a constant heat flux. The heat flux is assumed to impinge on a circular area. Our model is based on an axisymmetric three-dimensional variation of the temperature field in the domain. Heat transfer occurs only by conduction, and effects of convective heat transport are assumed negligible. Radiative heat loss from the surface of the melt and the regolith to the surroundings is permitted. We perform numerical computations to determine the shape and the mass of the melt at steady state and its time evolution. We first neglect the volume change upon melting, and subsequently perform calculations including it. Predictions from our model are compared to test data to determine the effective thermal conductivities of the regolith and the melt that are compatible with the data
Document ID
20120008556
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Balasubramaniam, R. (National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Gokoglu S. (NASA Glenn Research Center Cleveland, OH, United States)
Hegde, U. (National Center for Space Exploration Research on Fluids and Combustion Cleveland, OH, United States)
Date Acquired
August 25, 2013
Publication Date
May 1, 2012
Subject Category
Engineering (General)
Report/Patent Number
NASA/TM-2012-217440
E-18171
AIAA Paper 2012-0638
Meeting Information
Meeting: 50th Aerospace Science Conference
Location: Nashville, TN
Country: United States
Start Date: January 9, 2012
End Date: January 12, 2012
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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