
Electronic Theses and Dissertations
Date
2024
Document Type
Thesis
Degree Name
Master of Science
Department
Mechanical Engineering
Committee Chair
Jeffrey Marchetta
Committee Member
Alexander Headley
Committee Member
Daniel Foti
Abstract
Previous studies have determined that a magnetically susceptible fluid can be influenced by a magnetic field of sufficient strength in low gravity conditions. The use of magnetic positive positioning to manipulate magnetically susceptible fluids has potential uses in both specifying location and reducing the thermal heat leak as a means of effective positive positioning. A computational simulation is used to model the phase separation in cryogenic propellant tanks as in previous studies, while an analytic model is created to represent the magnetic field of a real permanent magnet. Previous studies have focused on the cryogenic propellant, liquid oxygen, which is attracted to regions with high magnetic field intensity. This study will focus on liquid hydrogen, which is repelled from these regions, in hopes to move the fluid away from the tank wall at points of high heat leak, such as tank supports. Using the validated computational simulation software and the validated analytic equation for the magnetic field intensity, the effectiveness of which a permanent magnet can reduce heat leak will be analyzed. Simulation results are presented to show the effectiveness of magnetic positive positioning in various states of low gravity and zero gravity.
Library Comment
Dissertation or thesis originally submitted to ProQuest.
Notes
Open Access
Recommended Citation
Hughes, Emma Kate, "Feasibility of LH2 Magnetic Positive Positioning to Minimize Spacecraft Propellant Tank Heat Leak" (2024). Electronic Theses and Dissertations. 3656.
https://digitalcommons.memphis.edu/etd/3656
Comments
Data is provided by the student.