NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Extrusion-based Additive Manufacturing of Zirconium Carbide for Nuclear Fuel Cell StructuresNuclear thermal propulsion relies on heating hydrogen propellant using nuclear fuel to generate thrust for spacecraft propulsion. Ceramic fuel elements like zirconium carbide (ZrC) offer advantages over metals due to their high melting points and high temperature stability. The primary function of ZrC in this context is to provide structural integrity and stability to the nuclear fuel, especially under high-temperature and high-radiation conditions. Vanadium carbide (VC), a nonradioactive surrogate with similar properties, has also emerged for research purposes. Recent advancements include utilizing VC as a sintering additive for ZrC, enhancing densification and mechanical properties. Traditional ZrC fabrication methods struggle with intricate geometries, but additive manufacturing (AM), specifically extrusion-based methods, revolutionizes ceramic fabrication by offering material flexibility, multi-material printing, minimal waste, and rapid prototyping. This study explores extrusion-based AM for the fabrication of ZrC nuclear fuel cell structures. Experimental findings highlight the impact of Nano Crystalline Cellulose (NCC) and VC additives on 3D-printed ZrC ceramics: higher NCC concentrations improves ink recovery and reduces deformation during the printing process but excessive NCC leading to increased porosity after sintering process; VC additives mitigate decreased mechanical properties caused by higher NCC content, emphasizing the crucial role of ink composition and additive selection in achieving desired material properties for broader applications. These insights pave the way for innovative approaches in AM structures for nuclear propulsion and other high-performance applications. The integration of AM technologies with advanced materials like ZrC and tailored additives represents a significant step towards efficient and sustainable propulsion systems for future space exploration missions.
Document ID
20250002730
Acquisition Source
Marshall Space Flight Center
Document Type
Accepted Manuscript (Version with final changes)
Authors
Guang Yang
(Kansas State University Manhattan, United States)
Yuhui Xiang
(Oregon State University Corvallis, United States)
Thomas Poirier
(Kansas State University Manhattan, United States)
Narges Malmir
(Kansas State University Manhattan, United States)
Tiankai Yao
(Idaho National Laboratory Idaho Falls, United States)
Nikhil Churi
(Utah Valley University Orem, United States)
Brian Taylor
(Marshall Space Flight Center Redstone Arsenal, United States)
James H Edgar
(Kansas State University Manhattan, United States)
Dong Lin
(Oregon State University Corvallis, United States)
Shuting Lei
(Kansas State University Manhattan, United States)
Date Acquired
March 17, 2025
Publication Date
December 24, 2024
Publication Information
Publication: Ceramics International
Publisher: Elsevier
Volume: 51
Issue: 1
Issue Publication Date: January 1, 2025
ISSN: 0272-8842
e-ISSN: 1873-3956
Subject Category
Propellants and Fuels
Engineering (General)
Funding Number(s)
CONTRACT_GRANT: 80NSSC22M0221
CONTRACT_GRANT: 2309995
CONTRACT_GRANT: KS-80NSSC22M0261
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
Single Expert
Keywords
zironium carbide
additive manufacturing
three-interval thixotropy test
No Preview Available