Rocket Propulsion NPTEL
Online Free Online Course by
World Mentoring Academy
Online
/ Free Online Course
Details
Resources: OpenCourseware from NPTEL (India), Sheridan College, MIT, UC
Berkeley, Stanford & many other of the World's finest University's.
Berkeley, Stanford & many other of the World's finest University's.
Language: English
Professors: Michael Williams
Units: 41
Lesson content
- Lec-01 Introduction
- Lec-02 Motion in Space
- Lec-03 Rotational Frame of Reference and Orbital Velocities
- Lec-04 Velocity Requirements
- Lec-05 Theory of Rocket Propulsion
- Lec-06 Rocket Equation and Staging of Rockets
- Lec-07 Review of Rocket Principles: Propulsion Efficiency
- Lec-08 Examples Illustrating Theory of Rocket Propulsion and Introduction to Nozzles
- Lec-09 Theory of Nozzles
- Lec-10 Nozzles Shapes
- Lec-11 Area Ratio of Nozzles:Under-expansion and Over-expansion
- Lec-12 Characteristic Velocity and Thrust Coefficient
- Lec-13 Divergence Loss in Conical Nozzles and the Bell Nozzle
- Lec-14 Unconventional Nozzles and Problems in Nozzles
- Lec-15 Criterion for Choice of Chemical Propellants
- Lec-16 Choice of Fuel-Rich Propellants
- Lec-17 Performance Prediction Analysis
- Lec-18 Dissociation of Products of Combustion
- Lec-19 Shifting Equilibrium and Frozen Flow in Nozzles
- Lec-20 Factors Influencing Choice of Chemical Propellants
- Lec-21 Low Energy Liquid Propellants and Hybrid Propellants
- Lec-22 Introduction to Solid Propellant Rockets
- Lec-23 Burn Rate of Solid Propellants and Equilibrium pressure in Solid Propellants Rockets
- Lec-24 Design Aspects of Solid Propellant Rockets
- Lec-25 Burning Surface Area of Solid Propellant Grains
- Lec-26 Ignition of Solid Propellant Rockets
- Lec-27 Review of Solid Propellant Rockets
- Lec-28 Feed Systems for Liquid Propellant Rockets
- Lec-29 Feed System Cycles for Pump Fed Liquid Propellant Rockets
- Lec-30 Analysis of Gas Generator and Staged Combustion Cycles and Introduction to
- Lec-31Injectors,Cooling of Chamber and Mixture Ratio Distribution
- Lec-32 Efficiencies due to Mixture Ratio Distribution and Incomplete Vaporization
- Lec-33 Pumps and Turbines; Propellant Feed System at Zero "g" Conditions
- Lec-34 Review of Liquid Bi-propellant Rockets and Introduction to Mono-propellant Rockets
- Lec-35 Introduction to Hybrid Rockets and a Simple Illustration of Combustion Instability
- Lec-36 Combustion Instability in Solid Propellant and Liquid Propellant Rockets
- Lec-37 Wave models of Oscillation
- Lec-38 Mechanisms Causing Instabilities and Strategies for Avoiding Combustion Instability
- Lec-39 Electric and Magnetic Fields and the Electrostatic Thruster
- Lec-40 Electrical Thrusters
- Lec-41 Advances in Rocket Propulsion
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