AE 402
Fall 2014 All Classes
All Classes
Credit: 3 OR 4 hours.
Analysis of orbits in an inverse-square gravitational field; elementary rocket dynamics, impulsive orbit transfer and rendezvous, and Lambert's Theorem with applications; patched-conic trajectories, planetary gravity-assist maneuvers, and linearized orbit theory with application to simplified analytical models; perturbations.
3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 202.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
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29794
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Lecture-Discussion
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A
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2:00PM
-3:20PM
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TR
|
Engineering Hall
|
Coverstone, V
Kroeker, E |
|
|
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63683
|
Online
|
ONL
|
ARRANGED
|
n.a.
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n.a.
|
Coverstone, V
|
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