Scholars' Mine Masters Theses Student Theses and Dissertations Fall 2019 Small satellite earth-to-moon direct transfer trajectories using the CR3BP Garrett Levi McMillan Follow this and additional works at: https://scholarsmine.mst.edu/masters_theses Part of the Aerospace Engineering Commons Department: Recommended Citation McMillan, Garrett Levi, "Small satellite earth-to-moon direct transfer trajectories using the CR3BP" (2019). Masters Theses. 7920. https://scholarsmine.mst.edu/masters_theses/7920 This thesis is brought to you by Scholars' Mine, a service of the Missouri S&T Library and Learning Resources. This work is protected by U. S. Copyright Law. Unauthorized use including reproduction for redistribution requires the permission of the copyright holder. For more information, please contact
[email protected]. SMALL SATELLITE EARTH-TO-MOON DIRECT TRANSFER TRAJECTORIES USING THE CR3BP by GARRETT LEVI MCMILLAN A THESIS Presented to the Graduate Faculty of the MISSOURI UNIVERSITY OF SCIENCE AND TECHNOLOGY In Partial Fulfillment of the Requirements for the Degree MASTER OF SCIENCE in AEROSPACE ENGINEERING 2019 Approved by: Dr. Henry Pernicka, Advisor Dr. David Riggins Dr. Serhat Hosder Copyright 2019 GARRETT LEVI MCMILLAN All Rights Reserved iii ABSTRACT The CubeSat/small satellite field is one of the fastest growing means of space exploration, with applications continuing to expand for component development, commu- nication, and scientific research. This thesis study focuses on establishing suitable small satellite Earth-to-Moon direct-transfer trajectories, providing a baseline understanding of their propulsive demands, determining currently available off-the-shelf propulsive technol- ogy capable of meeting these demands, as well as demonstrating the effectiveness of the Circular Restricted Three Body Problem (CR3BP) for preliminary mission design.