MAE 3304

ASTRONAUTICS I.

University of Texas at Arlington · UGRD · Fall 2026

1 section

Catalog description

Introduction to astronautics, the solar system, and the two-body problem. Orbit shaping and orbit transfers. Patched conic approximations for interplanetary transfers. Introduction to the three-body problem and relative motion. Rigid spacecraft equation of motion. Active and passive attitude stabilization techniques for spacecraft. Prerequisite: Must be in the professional ME or AE program and C or better in each of the following: MATH 3330 (or MATH 3319 ), PHYS 1443 , PHYS 1444 , and MATH 2326 ; or student group.

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Class #texas_arlington-4183Fall 2026UGRD3 credits

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