16.512 Rocket Propulsion

Class Info

Chemical rocket propulsion systems for launch, orbital, and interplanetary flight. Modeling of solid, liquid-bipropellant, and hybrid rocket engines. Thermochemistry, prediction of specific impulse. Nozzle flows including real gas and kinetic effects. Structural constraints. Propellant feed systems, turbopumps. Combustion processes in solid, liquid, and hybrid rockets. Cooling; heat sink, ablative, and regenerative.

This class has 16.50 as a prerequisite.

16.512 will not be offered this semester. It will be available in the Fall semester, and will be instructed by P. C. Lozano.

Lecture occurs 9:30 AM to 11:00 AM on Tuesdays and Thursdays in 33-418.

This class counts for a total of 12 credits.

You can find more information on MIT OpenCourseWare at the Rocket Propulsion site or on the 16.512 Stellar site.

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