Hypersonic Rocket Nozzle Essay
INVESTIGATION OF THERMAL CHARACTERISTICS IN SOLID ROCKET NOZZLE WITH INSULATE USING CAD/CAE
V. Jayakumar1*, S.Madhu2, A. Muniappan3, K. Shanmuganandam4 and Sattu Naveen Kumar5
1,3,4,5Department of Mechanical Engineering, Saveetha School of Engineering, Saveetha University, Chennai, Tamilnadu, India.
2Department of Automobile Engineering, Saveetha School of Engineering, Saveetha University, Chennai, Tamilnadu, India.
*E-mail: jkmails2k2@yahoo.com
ABSTRACT
Rocket engine nozzle is a propelling nozzle used to expand and accelerate the combustion gases produced by burning propellants so that the exhaust gases exit the nozzle at hypersonic velocities. In this work rocket nozzle designed using CATIA software. Due to high temperature from nozzle
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