Doctoral Dissertations
Keywords and Phrases
Carbides; Cermets; Mechanical Properties; NTP; Thermal Properties; ZrC
Abstract
This research focuses on the processing and properties of zirconium carbide-based materials to promote their use in extreme environment aerospace applications, including nuclear thermal propulsion and hyper sonics. Several carbide systems including ZrC, ZrC-Mo cermets, (Zr, Nb)C, and a high entropy carbide were developed. The ZrC-Mo cermet was studied extensively to understand the effect of starting carbide grain size on the final microstructure, composition, elastic moduli, hardness, fracture toughness, room and elevated temperature flexural strength, thermal diffusivity, electrical resistivity, thermal expansion coefficient, and thermal conductivity. It was shown that heat transport in the cermets was dominated by the ZrC phase as well as several compositional interactions. Two methods were employed to sinter the ZrC-Mo and (Zr, Nb)C with integral cooling channels using fugitive materials in an effort to reduce required post process machining as the matrix material is a surrogate for fissile fuel. One method involved inserting a Mo loaded thermoplastic rod while the other method consisted of pouring loose powder around graphite pins in an array before densifying. The Mo rod worked best with the cermet composition with limited cracking, while the graphite pins worked with the (Zr, Nb)C due to thermal mismatch leading to radial cracking of the incompatible materials. A carbothermal reduction process was used to synthesize both ZrC and a high entropy carbide in an effort to produce high purity, nominally dense, carbides. After hot pressing, the ZrCx stoichiometry was estimated and the room temperature mechanical properties of the ZrC and HEC were measured to compare both the difference between monocarbides and high entropy systems as well as commercial versus synthesized carbides.
Advisor(s)
Hilmas, Greg
Committee Member(s)
Emdadi, Arezoo
Lonergan, Jason
Watts, Jeremy Lee, 1980-
Chandrashekhara, K.
Department(s)
Materials Science and Engineering
Degree Name
Ph. D. in Ceramic Engineering
Publisher
Missouri University of Science and Technology
Publication Date
Spring 2026
Journal article titles appearing in thesis/dissertation
Paper I, found on pages 35-67, has been published in Ceramics International.
Paper II, found on pages 68-99, is intended for submission to Ceramics International.
Paper III, found on pages 100-135, is intended for submission to International Journal of Applied Ceramic Technology.
Paper IV, found on pages 136-164, is intended for submisstion to Journal of the American Ceramic Society.
Pagination
xiii, 185 pages
Note about bibliography
Includes_bibliographical_references_(pages 171-184)
Rights
© 2026 Nathaniel Hyman Blatt , All Rights Reserved
Document Type
Dissertation - Open Access
File Type
text
Language
English
Thesis Number
T 12586
Recommended Citation
Blatt, Nathaniel Hyman, "Zirconium Carbide Based Materials For Extreme Aerospace Environments" (2026). Doctoral Dissertations. 3455.
https://scholarsmine.mst.edu/doctoral_dissertations/3455
