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AERO 3240

Orbital Mechanics

0.5 credit · Undergraduate

Review of translational kinematics and dynamics. Keplerian two-body problem: Kepler's laws, orbital elements, orbit determination. Orbital perturbations: oblateness of the Earth, atmospheric drag. Orbital maneuvers and interplanetary flights. Advanced topics.

Prerequisites & course information

Prerequisite(s): MAAE 2101 . Lectures three hours per week, tutorial one hour per week.

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