AE 434

spring 2024
 
All Classes

Credit: 3 OR 4 hours.

Basic principles of chemical rocket propulsion and performance, rocket component design, liquid rockets, solid rocket motors, combustion processes, combustion instability.

3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 312.

Closed
Section Status Closed
Open
Section Status Open
Pending
Section Status Pending
Open (Restricted)
Section Status Open (Restricted)
Unknown
Section Status Unknown
Detail Status CRN Type Section Time Day Location Instructor