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Start Over Year 2014 Thesis Supervisor David Bradley Spencer Keyword Jacobi Integral

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Author:: Al Jaberi, Saeed
Title:: Low Thrust Trajectories From Low Earth Orbits to the Moon
Area of Honors:: Aerospace Engineering
Keywords:: Astrodynamics
the Three Body Problem
CR3BP
Low Thrust
Jacobi Integral
File:: Download thesis_Aljaberi___SHC.pdf
Thesis Supervisors:: Robert Graham Melton, Thesis Supervisor
David Bradley Spencer, Faculty Reader
Dr. George A Lesieutre, Faculty Reader
Robert Graham Melton, Thesis Honors Advisor

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