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Friday, December 28, 2012

AE2023 SPACE MECHANICS SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 6TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013

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AE2023 SPACE MECHANICS SYLLABUS | ANNA UNIVERSITY BE AERONAUTICAL ENGINEERING 6TH SEMESTER SYLLABUS REGULATION 2008 2011 2012-2013 BELOW IS THE ANNA UNIVERSITY SIXTH 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

AE2023 SPACE MECHANICS L T P C
3 0 0 3
OBJECTIVE
To study the basic concepts of orbital Mechanics with particular emphasis on
interplanetary trajectories
UNIT I BASIC CONCEPTS 4
The Solar System – References Frames and Coordinate Systems – The Celestial Sphere
– The Ecliptic – Motion of Vernal Equinox – Sidereal Time – Solar Time – Standard Time –
The Earth’s Atmosphere.
UNIT II THE GENERAL N-BODY PROBLEM 10
The many body Problem – Lagrange – Jacobian Identity –The Circular Restricted Three
Body Problem – Libration Points- Relative Motion in the N-body Problem –Two –Body
Problem – Satellite Orbits – Relations Between Position and Time – Orbital Elements.
72
UNIT III SATELLITE INJECTION AND SATELLITE ORBIT PERTURBATIONS 12
General Aspects of satellite Injections – Satellite Orbit Transfer –Various Cases – Orbit
Deviations Due to Injection Errors – Special and General Perturbations – Cowell’s Method
– Encke’s Method – Method of vibrations of Orbital Elements – General Perturbations
Approach.
UNIT IV INTERPLANETARY TRAJECTORIES 6
Two Dimensional Interplanetary Trajectories –Fast Interplanetary Trajectories – Three
Dimensional Interplanetary Trajectories – Launch if Interplanetary Spacecraft –Trajectory
about the Target Planet.
UNIT V BALLISTIC MISSILE TRAJECTORIES AND MATERIALS 13
The Boost Phase – The Ballistic Phase –Trajectory Geometry- Optimal Flights – Time of
Flight – Re – entry Phase – The Position of the Impact Point – Influence Coefficients.
Space Environment – Peculiarities – Effect of Space Environment on the Selection of
Spacecraft Material.
TOTAL: 45 PERIODS
TEXT BOOK
1. Cornelisse, J.W., “Rocket Propulsion and Space Dynamic”, W.H. Freeman & Co.,
1984.
REFERENCES
1. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley, 1993.
2. Van de Kamp, P., “Elements of Astro-mechanics”, Pitman, 1979.
3. Parker E.R., “Materials for Missiles and Spacecraft”, McGraw-Hill Book Co. Inc.,
1982.

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