AE 110 - Space Systems Engineering

3 unit(s)
Introduction to design, analysis and operation of spacecraft power, communications, attitude determination/control, structures, propulsion, thermal management systems. Typical payload systems design and operation, including remote Earth sensors. System integration issues. Lab experiments.

Lecture 2 hours/Lab 3 hours.

Prerequisite(s): C or better in AE 100 or AE 165, or graduate standing.
Grading: Letter Graded

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