AE 508
Spring 2006 All Classes
All Classes
Credit: 4 hours.
Optimal rocket trajectories in inverse-square and linearized gravitational fields; orbital transfer, intercept, and rendezvous; high-thrust (impulsive) and low-thrust (continuous) trajectories; primer vector theory and applications; cooperative rendezvous.
Prerequisite: Credit or concurrent registration in AE 504 or equivalent; or consent of instructor.
Section Status updates every 10 minutes.
| CRN | Type | Section | Time | Day | Location | Instructor | Section Details | |
|---|---|---|---|---|---|---|---|---|
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30029
|
Lecture-Discussion
|
A
|
1:00PM
-1:50PM
|
MWF
|
Talbot Laboratory
|
Prussing, J
|
|