Propulsion – II Syllabus for B.Tech 5th sem is covered here. This gives the details about credits, number of hours and other details along with reference books for the course.<\/p>\n
The detailed syllabus for Propulsion – II B.Tech (R13) fifthsem is as follows<\/p>\n
OBJECTIVES:<\/strong><\/p>\n To impart knowledge in non air-breathing and hypersonic propulsion methods to students so that\u00a0they are familiar with various propulsion technologies associated with space launch vehicles,\u00a0missiles and space probes.<\/p>\n UNIT I : HYPERSONIC AIRBREATHING PROPULSION<\/strong> \u00a0 \u00a0[8 hours] UNIT II : FUNDAMENTALS OF CHEMICAL ROCKET PROPULSION<\/strong> \u00a0 \u00a0[9 hours] UNIT III : SOLID ROCKET PROPULSION<\/strong> \u00a0 \u00a0[10 hours]
\nIntroduction to hypersonic air breathing propulsion, hypersonic vehicles and supersonic combustion- need for supersonic combustion for hypersonic propulsion \u2013 salient features of scramjet engine and\u00a0its applications for hypersonic vehicles \u2013 problems associated with supersonic combustion \u2013engine\/airframe integration aspects of hypersonic vehicles \u2013 various types scramjet combustors \u2013 fuel\u00a0injection schemes in scramjet combustors \u2013 one dimensional models for supersonic combustion using\u00a0method of influence coefficients.<\/p>\n
\nOperating principle \u2013 specific impulse of a rocket \u2013 internal ballistics \u2013 performance considerations of\u00a0rockets \u2013 types of igniters- preliminary concepts in nozzle-less propulsion \u2013 air augmented rockets \u2013\u00a0pulse rocket motors \u2013 static testing of rockets & instrumentation \u2013safety considerations<\/p>\n
\nSalient features of solid propellant rockets \u2013 selection criteria of solid propellants \u2013 estimation of solid\u00a0propellant adiabatic flame temperature – propellant grain design considerations \u2013 erosive burning in\u00a0solid propellant rockets \u2013 combustion instability \u2013 strand burner and T-burner \u2013 applications and\u00a0advantages of solid propellant rockets.<\/p>\n