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AE662A - Rocket Engine Design

IITK

Prerequisites:

2-0-3-7

Course Contents

Introduction to rocket propulsion, Types of rocket engines, Elements of combustion, Chemical propellants and their burning characteristics, Aero thermodynamic de-signanalysis of solid propellant rocket engine, Liquid propellant rocket engine, Design of thrust chamber, Design of cooling system; Design of rocket Nozzle. 


 

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