She did. Now I'm done!
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In performing this examination, two results were selected for further analysis. These
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results are outlined in Table~\ref{results_table}. As can be seen in the table, both
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resulting trajectories have trade-offs in mission length, launch energy, fuel usage, and
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more. However, both results show very interesting trajectories that could indicate some
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favorable possibilities for such a mission profile. Each of these trajectories should be
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within the capabilities of existing launch vehicles in terms of $C_3$.
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\section{Recommendations for Future Work}\label{improvement_section}
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more. Each of these trajectories appear to be within the capabilities of existing launch
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vehicles in terms of $C_3$.
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In the course of producing this algorithm, a large number of improvement possibilities were
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noted. This work was based, in large part, on the work of Jacob Englander in a number of
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