AE 202

fall 2013
 
All Classes

Credit: 3 hours.

Fundamental principles of aerospace flight mechanics applied to spacecraft and aircraft. Orbital mechanics, rocket propulsion, and dynamics and control applied to spacecraft design. Aerodynamics, maneuvering, stability and flight performance applied to aircraft design. MATLAB examples and assignments. Prerequisite: Credit or concurrent registration in TAM 212.

Closed
Section Status Closed
Open
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Pending
Section Status Pending
Open (Restricted)
Section Status Open (Restricted)
Unknown
Section Status Unknown
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