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Development and Evaluation of Mixed Uranium-Refractory Carbide/Refractory Carbide Cer-Cer Fuels, Phase I

Completed

Description

A new carbon-based fuel is introduced with outstanding potential to eliminate the loss of uranium, minimize the loss of carbon, and retain fission products for many hours of operation in hydrogen environment at temperatures in excess of 3,200K. The proposed fuel is a Cer-Cer made of mixed uranium-refractory carbide particles such as (U, Zr)C or (U, Zr, Nb)C dispersed in a refractory carbide matrix such as ZrC. For efficient operation in NTR applications for Isp of 1000 sec. or more, a fuel temperature of 3000 K or greater is necessary. Various fuel materials have been tested for NTR applications with most based on carbide fuel technology because of their improved thermal properties enabling the design of very small, high power density cores. Fuel designs from dispersed microspheres in graphite, to composite mixed carbides with graphite, to solid solution mixed carbides have been tested. Fuels bearing graphite are not tenable because of the high reactivity of free carbon with the hot hydrogen propellant. Solid solution, mixed carbides are most often brittle but otherwise perform well under the high temperature flowing hot hydrogen environment. The life limiting phenomenon for their use in NTR applications is the loss of uranium due to vaporization from the fuel surface at temperatures in excess of 2800 K. Though the proposed Cer-Cer fuel is relatively at lower level of technology maturity, its unique potential for elimination of uranium loss and retention of fission fragments at very high operational temperatures would amply justify the proposed research program.

Details

Technology areaPropulsion Systems > Aero Propulsion > Alternative Low-Carbon Jet Fuel
ProgramSmall Business Innovation Research/Small Business Tech Transfer (SBIR/STTR)
Lead organizationGlenn Research Center, Cleveland, OH
Start date2006-01-20
End date2006-07-24

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