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Optimization of a Wcl6 CVD System to Coat UO2 Powder with TungstenIn order to achieve deep space exploration via Nuclear Thermal Propulsion (NTP), Marshall Space Flight Center (MSFC) is developing W-UO2 CERMET fuel elements, with focus on fabrication, testing, and process optimization. A risk of fuel loss is present due to the CTE mismatch between tungsten and UO2 in the W-60vol%UO2 fuel element, leading to high thermal stresses. This fuel loss can be reduced by coating the spherical UO2 particles with tungsten via H2/WCl6 reduction in a fluidized bed CVD system. Since the latest incarnation of the inverted reactor was completed, various minor modifications to the system design were completed, including an inverted frit sublimer. In order to optimize the parameters to achieve the desired tungsten coating thickness, a number of trials using surrogate HfO2 powder were performed. The furnace temperature was varied between 930 C and 1000degC, and the sublimer temperature was varied between 140 C and 200 C. Each trial lasted 73-82 minutes, with one lasting 205 minutes. A total of 13 trials were performed over the course of three months, two of which were re-coatings of previous trials. The powder samples were weighed before and after coating to roughly determine mass gain, and Scanning Electron Microscope (SEM) data was also obtained. Initial mass results indicated that the rate of layer deposition was lower than desired in all of the trials. SEM confirmed that while a uniform coating was obtained, the average coating thickness was 9.1% of the goal. The two re-coating trials did increase the thickness of the tungsten layer, but only to an average 14.3% of the goal. Therefore, the number of CVD runs required to fully coat one batch of material with the current configuration is not feasible for high production rates. Therefore, the system will be modified to operate with a negative pressure environment. This will allow for better gas mixing and more efficient heating of the substrate material, yielding greater tungsten coating per trial.
Document ID
20150006887
Acquisition Source
Marshall Space Flight Center
Document Type
Abstract
Authors
Belancik, Grace A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Barnes, Marvin W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Mireles, Omar
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hickman, Robert
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
April 29, 2015
Publication Date
February 23, 2015
Subject Category
Propellants And Fuels
Report/Patent Number
M15-4296
Meeting Information
Meeting: Nuclear and Emerging Technologies for Space (NETS) 2015
Location: Albuquerque, NM
Country: United States
Start Date: February 23, 2015
End Date: February 26, 2015
Sponsors: American Nuclear Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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