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  • 1:21 AM, Wednesday, 13 Aug 2025


Course Undergraduate
Semester Sem. VII
Subject Code AE411
Subject Title Rocket Propulsion

Syllabus

Introduction to rocket propulsion systems – rocket propulsion engines – types of rocket nozzles and thrust vector control – propellants – combustion in rocket engines – parameters for chemical rockets – elements of liquid propulsion systems – thrust chambers – turbo pumps – non conventional propulsion techniques – solid rocket motors – grain configuration – hybrid rockets – rocket testing and performance evaluation – selection of rocket motors.

Text Books
  • Sutton, G. P. and Biblarz, O., Rocket Propulsion Elements, 7th ed., John Wiley (2000).

References
  1. Hill, P. G. and Peterson, C. R., Mechanics and Thermodynamics of Propulsion, 2nd ed., Pearson Education (2009).

  2. Ramamurthi, K., Rocket Propulsion, Macmillan (2010).

Course Outcomes (COs):

CO1: Knowledge about the different types of rocket propulsion systems.

CO2: Knowledge about the different parameters that influence the performance of chemical rock- ets.

CO3: Obtain detailed knowledge about the different components and working of the chemical rocket propulsion systems.

CO4: Obtain knowledge about the different types of propellants used for chemical propulsion and the factors affecting their performance.

CO5: Knowledge about the processes and criteria followed in the selection of propulsion system for a mission.

CO6: Knowledgeable about contemporary research in rocket propulsion related disciplines.

CO7: Ability to disseminate knowledge in rocket propulsion research through presentation of scientific talks.