AE 402
Fall 2005 Part of Term 1
Part of Term 1
Aug 24-Dec 9
Aug 24-Dec 9
Credit: 3 OR 4 hours.
(A A E 306) 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 302 or consent of instructor.
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
|
A
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11:00AM
-11:50AM
|
MWF
|
Everitt Laboratory
|
Prussing, J
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