IC 9254 SPACE PROPULSION SYLLABUS | ANNA UNIVERSITY ME INTERNAL COMBUSTION ENGINEERING ELECTIVES SYLLABUS REGULATION 2009 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY M.E INTERNAL COMBUSTION ENGINEERING DEPARTMENT ELECTIVES SYLLABUS, 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 YEAR 2011 2012-2013 (ANNA UNIVERSITY CHENNAI, TRICHY, MADURAI, TIRUNELVELI, COIMBATORE), 2009 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2010
IC 9254 SPACE PROPULSION L T P C
3 0 0 3
OBJECTIVE:
To gain insight on the working principle of rocket engines, different feed systems,
propellants and their properties and dynamics of rockets.
UNIT I GAS DYNAMICS 8
Wave motion - Compressible fluid flow through variable area devices – Stagnation
state and properties – Normal shock and oblique shock waves – Rayleigh and Fanno
Flow.
UNIT II THERMODYNAMICS OF AIRCRAFT ENGINES 9
Theory of Aircraft propulsion – Thrust – Various efficiencies – Different propulsion
systems – Turboprop – Ram Jet – Turbojet, Turbojet with after burner, Turbo fan and
Turbo shaft.
11
UNIT III PERFORMANCE CHARACTERISTICS OF AIRCRAFT ENGINES 9
Engine - Aircraft matching – Design of inlets and nozzles – Performance
characteristics of Ramjet, Turbojet, Scramjet and Turbofan engines.
UNIT IV ROCKET PROPULSION 9
Theory of rocket propulsion – Rocket equations – Escape and Orbital velocity – Multistaging
of Rockets – Space missions – Performance characteristics – Losses and
efficiencies.
UNIT V ROCKET THRUST CHAMBER 10
Combustion in solid and liquid propellant rockets – Classification of propellants and
Propellant Injection systems – Non-equilibrium expansion and supersonic
combustion – Propellant feed systems – Reaction Control Systems - Rocket heat
transfer.
TOTAL : 45 PERIODS
TEXT BOOKS:
1. Philip G. Hill and Carl R.Peterson, Mechanics and Thermodynamics of
Propulsion, Second Edition, Addition – Wesley Publishing Company, New York,
1992.
2. Zucrow N.J. Principles of Jet Propulsion and Gas Turbines, John Wiley and
Sons Inc, New York, 1970.
3. Zucrow N.J. Aircraft and Missile Propulsion , Vol. I and Vol. II, John Wiley and
Sons Inc, New York, 1975.
REFERENCES :
1. Bonney E.A. Zucrow N.J. Principles of Guided Missile Design, Van Nostranc
Co., 1985.
2. . S.M.Yahya, Fundamentals of Compressible Flow.
IC 9254 SPACE PROPULSION L T P C
3 0 0 3
OBJECTIVE:
To gain insight on the working principle of rocket engines, different feed systems,
propellants and their properties and dynamics of rockets.
UNIT I GAS DYNAMICS 8
Wave motion - Compressible fluid flow through variable area devices – Stagnation
state and properties – Normal shock and oblique shock waves – Rayleigh and Fanno
Flow.
UNIT II THERMODYNAMICS OF AIRCRAFT ENGINES 9
Theory of Aircraft propulsion – Thrust – Various efficiencies – Different propulsion
systems – Turboprop – Ram Jet – Turbojet, Turbojet with after burner, Turbo fan and
Turbo shaft.
11
UNIT III PERFORMANCE CHARACTERISTICS OF AIRCRAFT ENGINES 9
Engine - Aircraft matching – Design of inlets and nozzles – Performance
characteristics of Ramjet, Turbojet, Scramjet and Turbofan engines.
UNIT IV ROCKET PROPULSION 9
Theory of rocket propulsion – Rocket equations – Escape and Orbital velocity – Multistaging
of Rockets – Space missions – Performance characteristics – Losses and
efficiencies.
UNIT V ROCKET THRUST CHAMBER 10
Combustion in solid and liquid propellant rockets – Classification of propellants and
Propellant Injection systems – Non-equilibrium expansion and supersonic
combustion – Propellant feed systems – Reaction Control Systems - Rocket heat
transfer.
TOTAL : 45 PERIODS
TEXT BOOKS:
1. Philip G. Hill and Carl R.Peterson, Mechanics and Thermodynamics of
Propulsion, Second Edition, Addition – Wesley Publishing Company, New York,
1992.
2. Zucrow N.J. Principles of Jet Propulsion and Gas Turbines, John Wiley and
Sons Inc, New York, 1970.
3. Zucrow N.J. Aircraft and Missile Propulsion , Vol. I and Vol. II, John Wiley and
Sons Inc, New York, 1975.
REFERENCES :
1. Bonney E.A. Zucrow N.J. Principles of Guided Missile Design, Van Nostranc
Co., 1985.
2. . S.M.Yahya, Fundamentals of Compressible Flow.
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