AERO 624

Celestial Mechanics

Texas A&M University · UGRD · Fall 2026

1 section

Catalog description

Credits 3. 3 Lecture Hours. Analytical and numerical methods for computing spacecraft orbits under the influence of gravitational, aerodynamic, thrust and other forces; Keplerian two-body problem, perturbation methods, orbit determination, navigation and guidance for aerospace vehicles. Prerequisite: AERO 423 or equivalent.

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Class #texas_am-0205Fall 2026UGRD

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