Abort Trajectories for Manned Lunar Missions

Abort Trajectories for Manned Lunar Missions is final year project for Aerospace Engineering students.This is an astrodynamic model for lunar transfer which has been developed to allow for characterization of the abort feasibility envelope for conceivable transfer orbits. You can also Subscribe to FINAL YEAR PROJECT'S by Email for more such Projects and Seminar.
In addition the model allows for several trade studies involving differently executed abort options, factoring in fuel margins. Two optimization schemes were utilized; one to expedite return via any fuel in excess of that required for the abort, and one to explore the boundary region of direct abort infeasibility envelope searching for plausible abort trajectories.

Author:-Beksinski Jr, Edward David
Source:- DRUM


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