View reviews for professors for this course View On Testudo

ENPM684

Rocket Propulsion

Review of basic rocket propulsion principles including performance, design, analysis, nozzle theory, and thermodynamic relationships. Students will conduct performance analyses of solid, liquid, and hybrid rocket motors. Design projects will be focused to allow students to develop a basic understanding for the challenges associated with the design of chemical rocket engines/motors. We will examine the classification of solid and liquid propellants/fuels/oxidizers and their combustion characteristics.

0 reviews
Average rating: Not yet rated

0 reviews
Average rating: Not yet rated

Average GPA: 3.20 between 51 students

"W"s are considered to be 0.0 quality points. "Other" grades are not factored into the average GPA calculation.