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Apr 19, 2024
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AE 142 - Astrodynamics 3 units Two-body problem analysis and orbit design; Kepler’s Laws; Single-impulse orbit transfers; Hohmann transfers; Circularization; Plane changes; Kepler’s Equation; Planetary sphere of influence; Vector mechanics and relative motion of interplanetary flight; Patched conic trajectory model; Gravity-assist trajectories; Case studies; Restricted three-body problem.
Prerequisite(s): AE 138 , AE 165 Grading: Graded
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