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Course Co-ordinated by
IIT madras
NPTEL
>>
Courses
>>
Mechanical Engineering
>> Rocket Propulsion (Video) >>
Introduction
Question in Lecture
Rocket Propulsion
Introduction
Motion in Space
Rotational Frame of Reference and Orbital Velocities
Velocity Requirements
Theory of Rocket Propulsion
Rocket Equation and Staging of Rockets
Review of Rocket Principles; Propulsion Efficiency
Examples Illustrating Theory of Rocket Propulsion and Introduction to Nozzles
Theory of Nozzles
Nozzle Shape
Area Ratio of Nozzles; Under-expansion and Over-expansion
Characteristic Velocity and Thrust Coefficient
Divergence Loss in Conical Nozzles and the Bell Nozzle
Unconventional Nozzles and Problems in Nozzles
Criterion for Choice of Chemical Propellants
Choice of Fuel-Rich Propellants
Performance Prediction Analysis
Dissociation of Products of Combustion
Shifting Equilibrium and Frozen Flow in Nozzles
Factors Influencing Choice of Chemical Propellants
Low Energy Liquid Propellants and Hybrid Propellants
Introduction to Solid Propellant Rockets
Burn Rate of Solid Propellants and Equilibrium Pressure in Solid Propellant Rockets
Design Aspects of Solid Propellant Rockets
Burning Surface Area of Solid Propellant Grains
Ignition of Solid Propellant Rockets
Review of Solid Propellant Rockets
Feed Systems for Liquid Propellant Rockets
Feed System Cycles for Pump Fed Liquid Propellant Rockets
Analysis of Gas Generator and Staged Combustion Cycles and Introduction to Injectors
Injectors, Cooling of Chamber and Mixture Ratio Distribution
Efficiencies due to Mixture Ratio Distribution and Incomplete Vaporization
Pumps and Turbines; Propellant Feed System at Zero “g” Conditions
Review of Liquid Bi-propellant Rockets and Introduction to Mono-propellant Rockets
Introduction to Hybrid Rockets and a Simple Illustration of Combustion Instability in Liquid Propellant Rockets
Combustion Instability in Solid Propellant and Liquid Propellant Rockets – Bulk and Wave Modes
Wave modes of Oscillation
Mechanisms Causing Instabilities and Strategies for Avoiding Combustion Instability
Electric and Magnetic Fields and the Electrostatic Thruster
Electrical Thrusters
Advances in Rocket Propulsion
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Question:
Can we use de-laval nozzle in aircraft? what would be its impact?
By:
Ravi Thakur
Date:
2013-02-26
The co-ordinator will post his answer
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