MAE 3010

Astronautics

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Course Description

Pre-Requisite(s): MAE 2320

Discussion of the Keplerian two-body problem; elliptic, parabolic, and hyperbolic orbits; solution of Kepler's equation and analogs; the classical orbital elements; orbit determination; prediction of future position and velocity; orbital perturbations; Lambert's problem.


  • Carl Knospe

     Rating

    3.26

     Difficulty

    4.11

     GPA

    3.26

     Sections

    Last Taught

    Spring 2025

  • Kathryn Thornton

     Rating

    3.67

     Difficulty

    3.50

     GPA

    2.87

     Sections

    Last Taught

    Spring 2018

  • Faculty Staff

     Rating

     Difficulty

     GPA

     Sections

    Last Taught

    Spring 2022

  • To Announced

     Rating

     Difficulty

     GPA

     Sections

    Last Taught

    Spring 2023

  • Dale Arney

     Rating

     Difficulty

     GPA

    3.29

     Sections

    Last Taught

    Spring 2022