AEM4301: Orbital Mechanics

3 Credits

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]

View on University Catalog

All Instructors

B+ Average (3.475)Most Common: A (37%)

This total also includes data from semesters with unknown instructors.

669 students
SNWFDCBA

  • 4.86

    /6

    Recommend

  • 4.62

    /6

    Effort

  • 5.29

    /6

    Understanding

  • 4.94

    /6

    Interesting

  • 4.95

    /6

    Activities
      Contribute on our Github

      Gopher Grades is maintained by Social Coding with data from Summer 2017 to Summer 2025 provided by the University in response to a public records request

      Not affiliated with the University of Minnesota

      Privacy Policy