Course Name: AS5610 : Rocket Propulsion

Description: (Prereq. AS 493) Chemical rocket performance: Thermochemical calculations. Liquid propellant rockets: Droplet combustion, feed system and ignition, injector design, combustion chamber geometry and cooling, nozzle design, thrust vector control. Solid propellant rockets: Combustion mechanisms, grain design, two phase flow, case fabrication problems. Combustion instability.

Slot: G

RoomNo: CR2

Instructor: Ramakrishna P A

Period: JAN-MAY 2013

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