Rockets and Missiles Aero 8th Sem Syllabus for BE 2017 Regulation Anna Univ (Professional Elective IV) detail syllabus for Aeronautical Engineering (Aero), 2017 regulation is collected from the Anna Univ official website and presented for students of Anna University. The details of the course are: course code (AE8013), Category (PE), Contact Periods/week (3), Teaching hours/week (3), Practical Hours/week (0). The total course credits are given in combined syllabus.
For all other aero 8th sem syllabus for be 2017 regulation anna univ you can visit Aero 8th Sem syllabus for BE 2017 regulation Anna Univ Subjects. For all other Professional Elective IV subjects do refer to Professional Elective IV. The detail syllabus for rockets and missiles is as follows.
Course Objective:
- To give revelation on basic concepts of rocket motion, rocket aerodynamics, staging and control of rockets, materials and propulsion systems of rockets and missiles to students to augment their knowledge in the region of rockets and missile flight.
Unit I
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Unit II
Rocket Motion in Free Space and Gravitational Field
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 and altitudeestimation of culmination time and altitude.
Unit III
Aerodynamics of Rockets and Missiles
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
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Unit V
Rocket Propulsion Systems and Materials for Rockets and Missiles
Ignition System in rockets – types of Igniters- Design Consideration of liquid Rocket Combustion Chamber, Injector Propellant Feed Lines, Valves, Propellant Tanks Outlet and propellant feed Systems – Propellant Slash and Propellant Hammer – Elimination of Geysering Effect in Missiles -Selection of Materials – Special Requirements of Materials to Perform under Adverse Conditions.
Course Outcome:
- To be able to know about the current scenario of rockets and missiles.
- To gain knowledge about the trajectory motion of rockets and missiles.
- Gaining information on aerodynamic characteristics of rockets and missiles.
- To expand the ability to design the staging and control of own rockets.
- Basic knowledge about the propulsion systems and materials used in rockets and missiles.
Text Books:
- Cornelisse, J.W., Rocket Propulsion and Space Dynamics, J.W., Freeman and Co. Ltd., London, 1982.
- Sutton, G.P., et al., Rocket Propulsion Elements, John Wiley and Sons Inc., New York, 1993.
References:
- Mathur, M., and Sharma, R.P., Gas Turbines and Jet and Rocket Propulsion, Standard Publishers, New Delhi 1998.
- Parker, E.R., Materials for Missiles and Spacecraft, McGraw-Hill Book Co. Inc., 1982.
For detail syllabus of all other subjects of BE Aero, 2017 regulation do visit Aero 8th Sem syllabus for 2017 Regulation.
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