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IIT Guwahati - Introduction to Rocket Propulsion 

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Introduction to Rocket Propulsion
 at 
NPTEL 
Overview

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Duration

12 weeks

Total fee

Free

Mode of learning

Online

Difficulty level

Beginner

Official Website

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Credential

Certificate

Introduction to Rocket Propulsion
 at 
NPTEL 
Highlights

  • Start instantly and learn at your own schedule.
  • Earn a certificate of learning on course completion
  • Enroll for free
  • Pay only for getting a certificate of completion
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Introduction to Rocket Propulsion
 at 
NPTEL 
Course details

Skills you will learn
More about this course
  • This is an introductory course on rocket propulsion. The objective of this course is to impart knowledge about rocket propulsion to both UG and PG students. In this course, fundamentals aspects of rocket propulsion namely Solid, Liquid and Hydride rocket engines are to be covered extensively. Besides this, performance of rocket engine and heat transfer aspects of various components are to be covered briefly.

Introduction to Rocket Propulsion
 at 
NPTEL 
Curriculum

Week 1: Introduction, Types of Rocket Engines, Applications of Rocket Engines

Week 2: Aerothermodynamics of Rocket Engines, Fundamentals of Aerodynamics, Elements of thermodynamics

Week 3: Combustion, Ideal Rocket Engine

Week 4: Thrust Equation, Rocket Engine parameters, Rocket Engine Nozzles

Week 5: Space Flight Performance, Rocket Propellant

Week 6: Introduction to Solid Propellant Rocket Engine, Components of SPRE, Regression rate relation

Week 7: Liquid Propellant Rocket Engine, Injector, Feed system

Week 8: Hybrid rocket Engine, Rocket Heat transfer

Week 9: Liquid Propellant Rocket Engine, Types of liquid rocket engines, Combustion of liquid propellant

Week 10:Combustion Chamber Geometry, Types of liquid rocket engines, Injectors,Feed system

Week 11:Combustion Instability, Ignition System, Hybrid rocket Engine

Week 12:Rocket Heat transfer, Types of Cooling System

Introduction to Rocket Propulsion
 at 
NPTEL 
Entry Requirements

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  • Not mentioned

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Introduction to Rocket Propulsion
 at 
NPTEL 

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