Anna University Syllabus - Anna University ME Syllabus
AO7018 ROCKETRY AND SPACE MECHANICS Syllabus. Anna University ME Aerospace Technology Second Semester Syllabus Regulation 2013. Below is the Anna University 2013 Regulation Syllabus for 2nd Semester for ME Aerospace Technology(Launch Vehicle Technology), 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 Academic year 2013-2014 onwards for all its Affiliated institutions in Tamil Nadu.
Anna University Chennai Syllabus
AO7018 ROCKETRY AND SPACE MECHANICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will have an idea about solar system, basic concepts of
orbital mechanics with particular emphasis on interplanetary trajectories.
UNIT I ORBITAL MECHANICS 9
Description of solar system – Kepler’s Laws of planetary motion – Newton’s Law of Universal
gravitation – Two body and Three-body problems – Jacobi’s Integral, Librations points - Estimation of
orbital and escape velocities
14
UNIT II SATELLITE DYNAMICS 9
Geosynchronous and geostationary satellites- factors determining life time of satellites – satellite
perturbations – methods to calculate perturbations- Hohmann orbits – calculation of orbit parameters
– Determination of satellite rectangular coordinates from orbital elements
UNIT III ROCKET MOTION 10
Principle of operation of rocket motor - thrust equation – one dimensional and two dimensional rocket
motions in free space and homogeneous gravitational fields – Description of vertical, inclined and
gravity turn trajectories determinations of range and altitude – simple approximations to burnout
velocity.
UNIT IV ROCKET AERODYNAMICS 9
Description of various loads experienced by a rocket passing through atmosphere – drag estimation –
wave drag, skin friction drag, form drag and base pressure drag – Boat-tailing in missiles –
performance at various altitudes – conical and bell shaped nozzles – adapted nozzles – rocket
dispersion – launching problems.
UNIT V STAGING AND CONTROL OF ROCKET VEHICLES 8
Need for multistaging of rocket vehicles – multistage vehicle optimization – stage separation dynamics
and separation techniques- aerodynamic and jet control methods of rocket vehicles - SITVC.
TOTAL: 45 PERIODS
REFERENCES
1. G.P. Sutton, “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 5th Edition, 1986.
2. J.W. Cornelisse, “Rocket Propulsion and Space Dynamics”, J.W. Freeman & Co., Ltd., London,
1982
3. Van de Kamp, “Elements of astromechanics”, Pitman Publishing Co., Ltd., London, 1980.
4. E.R. Parker, “Materials for Missiles and Spacecraft”, McGraw-Hill Book Co., Inc., 1982.
AO7018 ROCKETRY AND SPACE MECHANICS L T P C 3 0 0 3
OUTCOME:
Upon completion of the course, students will have an idea about solar system, basic concepts of
orbital mechanics with particular emphasis on interplanetary trajectories.
UNIT I ORBITAL MECHANICS 9
Description of solar system – Kepler’s Laws of planetary motion – Newton’s Law of Universal
gravitation – Two body and Three-body problems – Jacobi’s Integral, Librations points - Estimation of
orbital and escape velocities
14
UNIT II SATELLITE DYNAMICS 9
Geosynchronous and geostationary satellites- factors determining life time of satellites – satellite
perturbations – methods to calculate perturbations- Hohmann orbits – calculation of orbit parameters
– Determination of satellite rectangular coordinates from orbital elements
UNIT III ROCKET MOTION 10
Principle of operation of rocket motor - thrust equation – one dimensional and two dimensional rocket
motions in free space and homogeneous gravitational fields – Description of vertical, inclined and
gravity turn trajectories determinations of range and altitude – simple approximations to burnout
velocity.
UNIT IV ROCKET AERODYNAMICS 9
Description of various loads experienced by a rocket passing through atmosphere – drag estimation –
wave drag, skin friction drag, form drag and base pressure drag – Boat-tailing in missiles –
performance at various altitudes – conical and bell shaped nozzles – adapted nozzles – rocket
dispersion – launching problems.
UNIT V STAGING AND CONTROL OF ROCKET VEHICLES 8
Need for multistaging of rocket vehicles – multistage vehicle optimization – stage separation dynamics
and separation techniques- aerodynamic and jet control methods of rocket vehicles - SITVC.
TOTAL: 45 PERIODS
REFERENCES
1. G.P. Sutton, “Rocket Propulsion Elements”, John Wiley & Sons Inc., New York, 5th Edition, 1986.
2. J.W. Cornelisse, “Rocket Propulsion and Space Dynamics”, J.W. Freeman & Co., Ltd., London,
1982
3. Van de Kamp, “Elements of astromechanics”, Pitman Publishing Co., Ltd., London, 1980.
4. E.R. Parker, “Materials for Missiles and Spacecraft”, McGraw-Hill Book Co., Inc., 1982.
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