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Design Evolutuion of Hot Isotatic Press Cans for NTP Cermet Fuel FabricationNuclear Thermal Propulsion (NTP) is under consideration for potential use in deep space exploration missions due to desirable performance properties such as a high specific impulse (> 850 seconds). Tungsten (W)-60vol%UO2 cermet fuel elements are under development, with efforts emphasizing fabrication, performance testing and process optimization to meet NTP service life requirements [1]. Fuel elements incorporate design features that provide redundant protection from crack initiation, crack propagation potentially resulting in hot hydrogen (H2) reduction of UO2 kernels. Fuel erosion and fission product retention barriers include W coated UO2 fuel kernels, W clad internal flow channels and fuel element external W clad resulting in a fully encapsulated fuel element design as shown.
Document ID
20140008753
Acquisition Source
Marshall Space Flight Center
Document Type
Conference Paper
Authors
Mireles, O. R.
(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
Metals And Metallic Materials
Report/Patent Number
M14-3224
Report Number: M14-3224
Meeting Information
Meeting: Nuclear & Emerging Technologies for Space (NETS) Conference
Location: NASA Stennis Space Ctr. 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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