Anna University Syllabus - Anna University ME Syllabus
AO7016 ADVANCED PROPULSION SYSTEMS Syllabus | Anna University ME Aerospace Technology & Satellite Technology streams Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology & Satellite Technology streams, Textbooks, Reference books, Exam portions, Question Bank, Previous year question papers, Model question papers, Class notes, Important 2 marks, 8 marks, 16 marks topics.
It is applicable for all students admitted in the Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AO7016 ADVANCED PROPULSION SYSTEMS L T P C
3 0 0 3
OUTCOME:
Upon completion of the course, students will learn in detail about gas turbines, ramjet, fundamentals
of rocket propulsion and chemical rockets.
UNIT I THERMODYNAMIC CYCLE ANALYSIS OF AIR-BREATHING PROPULSION
SYSTEMS 8
Air breathing propulsion systems like Turbojet, turboprop, ducted fan, Ramjet and Air augmented
rockets – Thermodynamic cycles – Pulse propulsion – Combustion process in pulse jet engines – inlet
charging process – Subcritical, Critical and Supercritical charging.
UNIT II RAMJETS AND AIR AUGMENTED ROCKETS 8
Preliminary performance calculations – Diffuser design with and without spike, Supersonic inlets –
combustor and nozzle design – integral Ram rocket.
UNIT III SCRAMJET PROPULSION SYSTEM 12
Fundamental considerations of hypersonic air breathing vehicles – Preliminary concepts in engine
airframe integration – calculation of propulsion flow path – flowpath integration – Various types of
supersonic combustors – fundamental requirements of supersonic combustors – Mixing of fuel jets in
supersonic cross flow – performance estimation of supersonic combustors.
UNIT IV NUCLEAR PROPULSION 9
Nuclear rocket engine design and performance – nuclear rocket reactors – nuclear rocket nozzles –
nuclear rocket engine control – radioisotope propulsion – basic thruster configurations – thruster
technology – heat source development – nozzle development – nozzle performance of radiosotope
propulsion systems.
UNIT V ELECTRIC AND ION PROPULSION 8
Basic concepts in electric propulsion – power requirements and rocket efficiency – classification of
thrusters – electrostatic thrusters – plasma thruster of the art and future trends – Fundamentals of ion
propulsion – performance analysis – ion rocket engine.
TOTAL: 45 PERIODS
REFERENCES
1. G.P. Sutton, “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York,1998.
2. William H. Heiser and David T. Pratt, Hypersonic Airbreathing propulsion, AIAA Education Series,
2001.
3. Fortescue and Stark, Spacecraft Systems Engineering, 1999.
4. Cumpsty, Jet propulsion, Cambridge University Press, 2003.
AO7016 ADVANCED PROPULSION SYSTEMS L T P C
3 0 0 3
OUTCOME:
Upon completion of the course, students will learn in detail about gas turbines, ramjet, fundamentals
of rocket propulsion and chemical rockets.
UNIT I THERMODYNAMIC CYCLE ANALYSIS OF AIR-BREATHING PROPULSION
SYSTEMS 8
Air breathing propulsion systems like Turbojet, turboprop, ducted fan, Ramjet and Air augmented
rockets – Thermodynamic cycles – Pulse propulsion – Combustion process in pulse jet engines – inlet
charging process – Subcritical, Critical and Supercritical charging.
UNIT II RAMJETS AND AIR AUGMENTED ROCKETS 8
Preliminary performance calculations – Diffuser design with and without spike, Supersonic inlets –
combustor and nozzle design – integral Ram rocket.
UNIT III SCRAMJET PROPULSION SYSTEM 12
Fundamental considerations of hypersonic air breathing vehicles – Preliminary concepts in engine
airframe integration – calculation of propulsion flow path – flowpath integration – Various types of
supersonic combustors – fundamental requirements of supersonic combustors – Mixing of fuel jets in
supersonic cross flow – performance estimation of supersonic combustors.
UNIT IV NUCLEAR PROPULSION 9
Nuclear rocket engine design and performance – nuclear rocket reactors – nuclear rocket nozzles –
nuclear rocket engine control – radioisotope propulsion – basic thruster configurations – thruster
technology – heat source development – nozzle development – nozzle performance of radiosotope
propulsion systems.
UNIT V ELECTRIC AND ION PROPULSION 8
Basic concepts in electric propulsion – power requirements and rocket efficiency – classification of
thrusters – electrostatic thrusters – plasma thruster of the art and future trends – Fundamentals of ion
propulsion – performance analysis – ion rocket engine.
TOTAL: 45 PERIODS
REFERENCES
1. G.P. Sutton, “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York,1998.
2. William H. Heiser and David T. Pratt, Hypersonic Airbreathing propulsion, AIAA Education Series,
2001.
3. Fortescue and Stark, Spacecraft Systems Engineering, 1999.
4. Cumpsty, Jet propulsion, Cambridge University Press, 2003.
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