AE2033 ROCKETS AND MISSILES SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 8TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY 8TH SEMESTER B.E AERONAUTICAL ENGINEERING DEPARTMENT 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), 2008 REGULATION OF ANNA UNIVERSITY CHENNAI AND STUDENTS ADMITTED IN ANNA UNIVERSITY CHENNAI DURING 2009
AE2033 ROCKETS AND MISSILES L T P C
3 0 0 3
OBJECTIVE
To introduce basic concepts of design and trajectory estimation of rocket and missiles
UNIT I ROCKET MOTION IN FREE SPACE AND GRAVITATIONAL FIELD 10
One Dimensional and Two Dimensional rocket Motions in Free Space and Homogeneous
Gravitational Fields – description of Vertical, Inclined and Gravity Turn Trajectories –
Determination of range and Altitude Simple Approximations to Burnout Velocity.
UNIT II STAGING AND CONTROL OF ROCKETS AND MISSILES 10
Multistaging of rockets – Vehicle Optimization – Stage Separation Dynamics – Separation
Techniques.
Rocket Thrust Vector Control Methods.
UNIT III AERODYNAMICS OF ROCKETS AND MISSILES 10
Airframe Components of Rockets and Missiles – Forces Acting on a Missile While Passing
Through Atmosphere – Classification of Missiles – methods of Describing Aerodynamic
Forces and Moments – Lateral Aerodynamic Moment – Lateral Damping Moment and
Longitudinal Moment of a Rocket – lift and Drag Forces – Drag Estimation.
UNIT IV ROCKET PROPULSION SYSTEMS 10
Ignition System in rockets – types of Igniters – Igniter Design Considerations – Design
Consideration of liquid Rocket Combustion Chamber, Injector Propellant Feed Lines,
Valves, Propellant Tanks Outlet and Helium Pressurized and Turbine feed Systems –
Propellant Slash and Propellant Hammer – Elimination of Geysering Effect in Missiles –
Combustion System of Solid Rockets.
UNIT V MATERIALS FOR ROCKETS AND MISSILES 5
Selection of Materials – Special Requirements of Materials to Perform under Adverse
Conditions.
TOTAL: 45 PERIODS
TEXT BOOKS
1. Sutton, G.P., et al., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York,
1993.
REFERENCES
1. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”,
Standard Publishers, New Delhi 1998.
2. Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W., Freeman & Co. Ltd.,
London, 1982.
3. Parker, E.R., “Materials for Missiles and Spacecraft”, McGraw-Hill Book Co. Inc., 1982.
AE2033 ROCKETS AND MISSILES L T P C
3 0 0 3
OBJECTIVE
To introduce basic concepts of design and trajectory estimation of rocket and missiles
UNIT I ROCKET MOTION IN FREE SPACE AND GRAVITATIONAL FIELD 10
One Dimensional and Two Dimensional rocket Motions in Free Space and Homogeneous
Gravitational Fields – description of Vertical, Inclined and Gravity Turn Trajectories –
Determination of range and Altitude Simple Approximations to Burnout Velocity.
UNIT II STAGING AND CONTROL OF ROCKETS AND MISSILES 10
Multistaging of rockets – Vehicle Optimization – Stage Separation Dynamics – Separation
Techniques.
Rocket Thrust Vector Control Methods.
UNIT III AERODYNAMICS OF ROCKETS AND MISSILES 10
Airframe Components of Rockets and Missiles – Forces Acting on a Missile While Passing
Through Atmosphere – Classification of Missiles – methods of Describing Aerodynamic
Forces and Moments – Lateral Aerodynamic Moment – Lateral Damping Moment and
Longitudinal Moment of a Rocket – lift and Drag Forces – Drag Estimation.
UNIT IV ROCKET PROPULSION SYSTEMS 10
Ignition System in rockets – types of Igniters – Igniter Design Considerations – Design
Consideration of liquid Rocket Combustion Chamber, Injector Propellant Feed Lines,
Valves, Propellant Tanks Outlet and Helium Pressurized and Turbine feed Systems –
Propellant Slash and Propellant Hammer – Elimination of Geysering Effect in Missiles –
Combustion System of Solid Rockets.
UNIT V MATERIALS FOR ROCKETS AND MISSILES 5
Selection of Materials – Special Requirements of Materials to Perform under Adverse
Conditions.
TOTAL: 45 PERIODS
TEXT BOOKS
1. Sutton, G.P., et al., “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York,
1993.
REFERENCES
1. Mathur, M., and Sharma, R.P., “Gas Turbines and Jet and Rocket Propulsion”,
Standard Publishers, New Delhi 1998.
2. Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W., Freeman & Co. Ltd.,
London, 1982.
3. Parker, E.R., “Materials for Missiles and Spacecraft”, McGraw-Hill Book Co. Inc., 1982.
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