Date of Award
December 2025
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Space Studies
First Advisor
Marcos M. Fernandez-Tous
Abstract
Nuclear fusion propulsion represents a promising solution for future interplanetarymissions due to its high energy density and potential for continuous power generation. However, existing fusion propulsion systems face significant limitations, particularly in achieving stable plasma confinement. The Polywell concept, introduced by physicist Robert Bussard in 1985, offers advantages through its compact, polyhedral geometry that is wellsuited for spacecraft applications where mass and volume constraints are critical. Despite these advantages, Polywell designs have encountered stability challenges in maintaining the electric potential well over time. Plasma instabilities induced by magnetic fields disrupt containment and reduce fusion efficiency, limiting overall performance and scalability for space propulsion applications. This research also addresses the regulatory frameworks applicable to Polywell technology development, including compliance with international space law and nuclear safety standards. The outcome of the research, with neutron radiation values, reinforces the need to develop a legal framework for fusion-based space propulsion systems.
Recommended Citation
Nair, Preeti, "A Space Propulsion Concept Based On Inertial Confinement: Exploring Nuclear Fusion Utilizing Polywell Geometry" (2025). Theses and Dissertations. 8237.
https://commons.und.edu/theses/8237