A logical approach for zero-rupture Fully Ceramic Microencapsulated (FCM) fuels via pressure-assisted sintering route

Caen Ang, Lance Snead, Yutai Kato

Research output: Contribution to journalArticlepeer-review

21 Scopus citations

Abstract

A pathway to Fully Ceramic Microencapsulated (FCM™) fuel pellets showing absence of sintering-derived “rupture” has been demonstrated. In the typical FCM manufacturing process, TRistructral ISOtropic (TRISO) particles show statistically significant rupture, caused by contact of particles during the axial shrinkage of fuel pellet that accompanies pressure-assisted sintering. To solve this, template SiC powder discs were fabricated to host planes of TRISO particles, and the disks were stacked to form a cylindrical “green” pellet. After sintering, up to ∼34% packing fraction of particles (Vp) was physically feasible without contact between planes. Sintering was shown to reduce the axial displacement between planes of TRISO particles, and X-ray Computed Tomography (XCT) showed planes separated by a displacement of ∼100 μm. XCT, optical microscopy and SEM showed the very limited radial displacement of particles. However, the relative density of the FCM pellet was limited to ∼95%. The current results support the zero-rupture concept as viable, but perturbations to TRISO arrangements and limited matrix density require further investigation to improve FCM fuel uniformity and microstructure.

Original languageEnglish
Article number151987
JournalJournal of Nuclear Materials
Volume531
DOIs
StatePublished - Apr 1 2020
Externally publishedYes

Funding

David Sprouster (Stony Brook University) conducted XCT analysis of the prototypes. The authors would like to thank J. O. Kiggans (Oak Ridge National Laboratory) for contributions and useful discussion. M. Koehler, J. Dunlap, M. S. Scott and W. S. Emert (UTK) contributed to the experimental investigations. The work presented in this paper was supported by NASA Contract No. 80MSFC18C0011 supporting Versatile NTP.

FundersFunder number
National Aeronautics and Space Administration80MSFC18C0011

    Keywords

    • FCM fuel
    • Inert matrix fuel
    • Processing
    • SiC
    • TRISO

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