CY9016 CRYOGENIC ROCKET PROPULSION SYLLABUS | ANNA UNIVERSITY ME CRYOGENIC ENGINEERING ELECTIVES SYLLABUS REGULATION 2009 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY M.E CRYOGENIC 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
CY9016 CRYOGENIC ROCKET PROPULSION L T P C
3 0 0 3
UNIT I 9
Chemical rocket propulsion, Definitions and fundamentals; thrust, total impulse, mixture ratio,
bulk density, characteristics velocity, thrust to weight ratio, exhaust velocity, mass ratio,
multistaging.
UNIT II 9
Types of chemical propellants; solid, liquid, hybrid, physical properties of common earth storable
propellants, semi- cryo and cryogenic propellants.
UNIT III 9
Pressure fed system – sources of pressurizing gas, pump fed systems – engine operating
cycles, pumps and turbines –general configuration, fluid circuits of vibration of cryogenic
engines and semi –cryogenic engines.
24
UNIT IV 9
Design of regenerative cooled combustion chamber, film cooling, dump cooling transpiration
cooling and radiation cooling. Design of expansion nozzle – characteristics, design of injector
hydraulic characteristics; Engine thrust and mixture ratio control, igniters, Propellant tanks.
UNIT V 9
Valves: Shut off value, flow control valves, check valve, isolation valve, relief valves, common
materials used in cryogenic propulsion; problems in storage and handling of cryogenic
propellants: safety aspects, Thermal protection systems for stage tanks, Thermal stratificationdesertification,
Geysering effect – geysering elimination, Zero “g” problems- restart mechanism.
TOTAL: 45 PERIODS
CY9016 CRYOGENIC ROCKET PROPULSION L T P C
3 0 0 3
UNIT I 9
Chemical rocket propulsion, Definitions and fundamentals; thrust, total impulse, mixture ratio,
bulk density, characteristics velocity, thrust to weight ratio, exhaust velocity, mass ratio,
multistaging.
UNIT II 9
Types of chemical propellants; solid, liquid, hybrid, physical properties of common earth storable
propellants, semi- cryo and cryogenic propellants.
UNIT III 9
Pressure fed system – sources of pressurizing gas, pump fed systems – engine operating
cycles, pumps and turbines –general configuration, fluid circuits of vibration of cryogenic
engines and semi –cryogenic engines.
24
UNIT IV 9
Design of regenerative cooled combustion chamber, film cooling, dump cooling transpiration
cooling and radiation cooling. Design of expansion nozzle – characteristics, design of injector
hydraulic characteristics; Engine thrust and mixture ratio control, igniters, Propellant tanks.
UNIT V 9
Valves: Shut off value, flow control valves, check valve, isolation valve, relief valves, common
materials used in cryogenic propulsion; problems in storage and handling of cryogenic
propellants: safety aspects, Thermal protection systems for stage tanks, Thermal stratificationdesertification,
Geysering effect – geysering elimination, Zero “g” problems- restart mechanism.
TOTAL: 45 PERIODS
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