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AE1451 ROCKETS AND MISSILES Syllabus - Anna university
Posted Date: 13 Aug 2008 Resource Type: Articles/Knowledge Sharing Category: Syllabus
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Posted By: Ramkumar Member Level: Diamond Rating: Points: 2
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AE1451 ROCKETS AND MISSILES 3 0 0 100
OBJECTIVE To introduce basic concepts of design and trajectory estimation of rocket and missiles 1. ROCKETS SYSTEM 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.
2. AERODYNAMICS OF ROCKETS AND MISSILES 13 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 – Body Upwash and Downwash in Missiles – Rocket Dispersion – Numerical Problems.
3. 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. 4. STAGING AND CONTROL OF ROCKETS AND MISSILES 7 Rocket Vector Control – Methods – Thrust determination – SITVC – Multistaging of rockets – Vehicle Optimization – Stage Separation Dynamics – Separation Techniques.
5. MATERIALS FOR ROCKETS AND MISSILES 5 Selection of Materials – Special Requirements of Materials to Perform under Adverse Conditions.
TOTAL : 45 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. Parket, E.R., “ Materials for Missiles and Spacecraft”, McGraw-Hill Book Co. Inc., 1982.
For more details, visit http://www.annauniv.edu/academics/index.html/
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