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]

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A- Average (3.518)Most Common: A (38%)

This total also includes data from semesters with unknown instructors.

579 students
SNWFDCBA

  • 3.68

    /5

    Recommend

  • 3.41

    /5

    Effort

  • 4.14

    /5

    Understanding

  • 3.78

    /5

    Interesting

  • 3.84

    /5

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