Spacecraft Electric Propulsion
Lecture
Main Campus
Course Description
The fundamentals of electric propulsion for spacecraft, which exists at the junction of traditional fluid dynamics, plasma physics, and aerospace engineering. The design and physics of electrothermal, electrostatic, and electromagnetic propulsion devices. Prerequisites: prior familiarity and experience with electromagnetism (Maxwell's equations, Ohm's law); fluid dynamics (fluid equations, choked flow, nozzles, Mach number); chemistry (stoichiometry, heat of formation, heat of reaction); and orbital dynamics (rocket equation, thrust, specific impulse, delta-v).
AA 204
Units: 3
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Typically Offered
Not Available
Grading Basis
Letter (ABCD/NP)
Class Level
Graduate
Instructional Mode
In Person
Gen Ed Requirement(s)
None
