In this article, we are glad to provide the syllabus of the code AS3502 of Anna University awarding the B.E Aerospace Engineering Syllabus based on regulation 2021. Let’s what we have here.
We tried our best to provide the detailed syllabus unit-wise for the subject code AS3502 – Space Mechanics Semester V. We also include the required textbooks and references from the expert faculty regarding the syllabus. Along with it assists the students to become more aware of the topics. And can easily make preparation strategies as per the syllabus to make your move for examinations. Hope this information is useful. Comment below if you need anything relevant to the syllabus. We’ll try to answer your questions. Don’t forget to share with your classmates.
If you want to know more about the B.E Aerospace Engineering Syllabus connected to an affiliated institution’s four-year undergraduate degree program. We provide you with a detailed Year-wise, semester-wise, and Subject-wise syllabus in the following link B.E Aerospace Engineering Syllabus Regulation 2021 Anna University.
Aim Of Concept:
To familiarize students with
- Concepts of satellite injection and satellite perturbations
- Trajectory computation
- Interplanetary travel and
- Flight of ballistic missiles
- Fundamental concepts of orbital mechanics
AS3502 – Space Mechanics Syllabus
Unit I: Space Environment
Peculiarities of space environment and its description– effect of space environment on materials of spacecraft structure and astronauts- manned space missions – effect on satellite life time
Unit II: Basic Concepts And The General N- Body Problem
The solar system – reference frames and coordinate systems – terminology related to the celestial sphere and its associated concepts – Kepler’s laws of planetary motion and proof of the laws – Newton’s universal law of gravitation – many body problem – Lagrange-Jacobi identity – circular restricted three body problem – libration points – general N-body problem – two body problem – relations between position and time.
Unit III: Satellite Injection And Satellite Perturbations
General aspects of satellite injection – satellite orbit transfer – various cases – orbit deviations due to injection errors – special and general perturbations – Cowell’s method and Encke’s method – method of variations of orbital elements – general perturbations approach.
Unit IV: Interplanetary Trajectories
Two-dimensional interplanetary trajectories – fast interplanetary trajectories – three-dimensional interplanetary trajectories – launch of interplanetary spacecraft – trajectory estimation about the target planet – concept of sphere of influence – Lambert’s theorem
Unit V: Ballistic Missile Trajectories
Introduction to ballistic missile trajectories – boost phase – ballistic phase – trajectory geometry – optimal flights – time of flight – re-entry phase – position of impact point – influence coefficients.
Text Books:
- Cornelisse, J.W., “Rocket Propulsion and Space Dynamics”, J.W. Freeman & Co., Ltd, London, 1982
- Parker, E.R., “Materials for Missiles and Spacecraft”, Mc.Graw Hill Book Co. Inc., 1982.
Reference:
- Sutton, G.P., “Rocket Propulsion Elements”, Wiley, New York, 9th Ed., 2017.
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