Date of Award
Summer 2014
Document Type
Thesis
Degree Name
Master of Science (MS)
Department
Electrical & Computer Engineering
Program/Concentration
Electrical and Computer Engineering
Committee Director
Ravindra P. Joshi
Committee Member
Vishnukumar K. Lakdawala
Committee Member
Duc T. Nguyen
Call Number for Print
Special Collections LD4331.E55 F896 2014
Abstract
A goal of the National Aeronautics and Space Administration (NASA) has been to develop technologies that will enable deep space explorations. Such missions include a prolonged stay on the Moon and the ability to sustain a long duration of travel time to Mars and beyond. Long-term human exposures to radiation are a crucial concern. Recent research has taken focus on active and passive shielding methods as a way of eliminating the hazard posed by radiation particles. Passive shielding involves the use of materials that has the ability to withstand radiation particles and reduce the dose by stopping or slowing the incoming charged particles. Active shielding, on the other hand, uses electrostatic or magnetostatic fields as a means for deflecting various ions. Each has its unique advantages and disadvantages.
The goal of this thesis is to show the advantages of using an active shielding method by utilizing a hybrid configuration which consists of both electrostatic and magnetostatic fields for particle protection. This configuration will utilize a modified electrostatic coil arrangement along with a superconducting coil for creating a magnetic field. This setup will show improved advantages over the standard hybrid configurations that have been previously presented. Improvements to the standard hybrid configuration are shown: (i) to have a much lower magnetic field present in a protected region, (ii) to provide greater shielding and repulsion of the transmission of incident ions from both Solar Particle Events (SPE) and Galactic Cosmic Rays (GCR), (iii) reduce the power requirement for re-charging the electrostatic sub-system, and (iv) require fewer coils which would lead to savings on costs for material and fuel.
The results will further show that the effects of SPE and GCR can almost be eliminated by the modified hybrid configurations and that advances in technology and design could fu1ther reduce the transmission percentage of particles. The power needed to replenish the electrostatic charges due to particle strikes from the GCR and SPE radiation will also be shown be small and insignificant.
Rights
In Copyright. URI: http://rightsstatements.org/vocab/InC/1.0/ This Item is protected by copyright and/or related rights. You are free to use this Item in any way that is permitted by the copyright and related rights legislation that applies to your use. For other uses you need to obtain permission from the rights-holder(s).
DOI
10.25777/yef4-zy32
Recommended Citation
Fung, Leroy A..
"The Study of Electrostatic and Magnetostatic Active Space Radiation Shielding for Deep Space Missions"
(2014). Master of Science (MS), Thesis, Electrical & Computer Engineering, Old Dominion University, DOI: 10.25777/yef4-zy32
https://digitalcommons.odu.edu/ece_etds/327
Included in
Electrical and Electronics Commons, Electromagnetics and Photonics Commons, Space Vehicles Commons