Date of Graduation
8-2017
Document Type
Thesis
Degree Name
Master of Science in Microelectronics-Photonics (MS)
Degree Level
Graduate
Department
Microelectronics-Photonics
Advisor/Mentor
Huang, Po-Hao Adam
Committee Member
El-Shenawee, Magda O.
Second Committee Member
Harter, William G.
Third Committee Member
Wise, Rick L.
Keywords
Advanced Propulsion; Computational Modeling; COMSOL; Heat Transfer; Microwaves; Miniaturization
Abstract
A gedankenexperiment was considered to compare a hypothetical thruster that used no reaction mass to propulsion methods currently in use. A brief discussion of previous research work done on closed resonant cavity thrust devices was conducted. Using the previous work as a template, a simulation plan was devised. Computational models of resonant microwave cavities were constructed and investigated using COMSOL software. These COMSOL simulations were verified against known analytical solutions using Matlab software as a computational tool. Multiphysics simulations were created to study the microwave heating environment of the resonant cavities. From the COMSOL study outputs, the electromagnetic field magnitude, temperature, surface resistive losses, volume resistive losses, quality factor, and energy contained in the electric field were presented and discussed. The disagreements between the computational model and real-world resonant cavities were also presented and discussed.
Citation
Pennington, J. S. (2017). Optimization of Miniaturized Resonant Microwave Cavities for Use in Q-Thrusters. Graduate Theses and Dissertations Retrieved from https://scholarworks.uark.edu/etd/2473
Included in
Electromagnetics and Photonics Commons, Systems Engineering and Multidisciplinary Design Optimization Commons
