Spacecraft Electric Propulsion
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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).
Grading Basis
RLT - Letter (ABCD/NP)
Min
3
Max
3
Course Repeatable for Degree Credit?
No
Course Component
Lecture
Enrollment Optional?
No
Does this course satisfy the University Language Requirement?
No
Programs
AA204
is a
completion requirement
for: