BAE052

Space Flight Mechanics

L-T-P3-0-0 Credits3 Session2024-25 TypeTheory
Appears in 1 semester

B.Tech Aeronautical Engineering · Sem 5 (Departmental Elective-I)

Syllabus

5 units · 41 lecture hours
Unit1

Unit 1

8 hrs

Basic Concepts 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. 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 proofs of the laws –Newton’s universal law of gravitation - the many body problems, the celestial Sphere.

Unit2

Unit 2

9 hrs

The General N-Body Problem The Ecliptic Motion of Vernal Equinox – Sidereal Time – Solar Time -Standard Time – The Earth’s Atmosphere. Study the basic concepts of orbital Mechanics with particular emphasis on interplanetary trajectories. 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.

Unit3

Unit 3

8 hrs

Satellite Injection and Satellite Orbit Perturbations General Aspects of satellite Injections, Satellite Orbit Transfer, Various Cases – Orbit Deviations Due to Injection – Errors – Special and General Perturbations – Cowbell’s Method- Neck’s Method - Method of vibrations of Orbital Elements- General Perturbations Approach.

Unit4

Unit 4

8 hrs

Interplanetary Trajectories Two Dimensional Interplanetary Trajectories – Fast Interplanetary Trajectories – Three Dimensional Interplanetary Trajectories – 3-Dimensional Interplanetary Trajectories – Launch if Interplanetary Spacecraft – Trajectory estimation about the Target Planet, Concept of the sphere of influence, Lambert’s theorem.

Unit5

Unit 5

8 hrs

Ballistic Missile Trajectories and Materials 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, the Selection of Spacecraft Material.

Course Outcomes (COs)5 outcomes

After completion of the course student will be able to:

  1. CO1description– effect of space environment on materials of spacecraft structure. Understand the different terminologies related to space flight. TheK2
  2. CO2K2 Newton’s universal law of gravitation - the many body problems. Apply the concept of the different laws of planetary motion and the different
  3. CO3K3 types of satellites and missile systems. Apply the concept of the different phases of satellite and missile launching
  4. CO4and their trajectory and the various techniques of satellite injection and further maneuvering. Apply the concept of the natural means to navigate accurately to theK3
  5. CO5destination and analyze the chart reading and problem occurring on dead reckoning.K3

Books and Reference

  1. Cornelisse, J.W. “Rocket Propulsion and Space Dynamic”, W.H. Freeman & Co., 1984.
  2. Sutton, G.P., “Rocket Propulsion Elements”, John Wiley, 1993.
  3. Parker E.R., “Material for Missiles and Spacecraft”, McGraw – Hill Book Co.

Official AKTU syllabus

This subject is on page 14, 15 of the original AKTU PDF.

Official AKTU syllabus PDF ↗