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Development Status of a CVD System to Deposit Tungsten onto UO2 Powder via the WCI6 ProcessNuclear Thermal Propulsion (NTP) is under development for deep space exploration. NTP's high specific impulse (> 850 second) enables a large range of destinations, shorter trip durations, and improved reliability. W-60vol%UO2 CERMET fuel development efforts emphasize fabrication, performance testing and process optimization to meet service life requirements. Fuel elements must be able to survive operation in excess of 2850 K, exposure to flowing hydrogen (H2), vibration, acoustic, and radiation conditions. CTE mismatch between W and UO2 result in high thermal stresses and lead to mechanical failure as a result UO2 reduction by hot hydrogen (H2) [1]. Improved powder metallurgy fabrication process control and mitigated fuel loss can be attained by coating UO2 starting powders within a layer of high density tungsten [2]. This paper discusses the advances of a fluidized bed chemical vapor deposition (CVD) system that utilizes the H2-WCl6 reduction process.
Document ID
20140008754
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Mireles, O. R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Kimberlin, A.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Broadway, J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Hickman, R.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
July 8, 2014
Publication Date
February 24, 2014
Subject Category
Inorganic, Organic And Physical Chemistry
Metals And Metallic Materials
Report/Patent Number
M14-3225
Meeting Information
Meeting: Nuclear & Emerging Technologies for Space (NETS) Conference
Location: Stennis Space Center, MS
Country: United States
Start Date: February 24, 2014
End Date: February 26, 2014
Sponsors: American Nuclear Society
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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