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