AEM4301
AEM 4301 - Orbital Mechanics (3 Cr.)
Aerospace Engineering & Mechanics (11090)
TIOT - College of Science and Engineering
AEM 4301 - Orbital Mechanics (3 Cr.)
Course description
The two-body problem. Earth-satellite operations, rocket performance, reentry dynamics, space environments, interplanetary trajectories. Numerical simulations. Design project.
prereq: [2012 or equiv], [MATH 2373 or equiv], [CSE upper div or grad student]
prereq: [2012 or equiv], [MATH 2373 or equiv], [CSE upper div or grad student]
Minimum credits
3
Maximum credits
3
Is this course repeatable?
No
Grading basis
AFV - A-F or Audit
Lecture
Requirements
001545
Fulfills the writing intensive requirement?
No
Typically offered term(s)
Every Fall