K. Ramamurthi: Rocket Propulsion (IIT Madras)

# playlist of the 40 videos (click the up-left corner of the video)

source: nptelhrd    2012年6月24日
Mechanical - Rocket Propulsion by Prof. K. Ramamurthi, Department of Mechanical Engineering, IIT Madras. For more details on NPTEL visit http://nptel.iitm.ac.in

01 Introduction 57:30
Mod-01 Lec-02 Motion in Space 45:02
03 Rotational Frame of Reference and Orbital Velocities 41:32
04 Velocity Requirements 52:20
05 Theory of Rocket Propulsion 50:43
06 Rocket Equation and Staging of Rockets 55:21
07 Review of Rocket Principles: Propulsion Efficiency 59:45
08 Examples Illustrating Theory of Rocket Propulsion and Introduction to Nozzles 54:18
09 Theory of Nozzles 51:31
10 Nozzles Shapes 52:17
11 Area Ratio of Nozzles:Under-expansion and Over-expansion 55:09
12 Characteristic Velocity and Thrust Coefficient 54:23
13 Divergence Loss in Conical Nozzles and the Bell Nozzle 50:59
14 Unconventional Nozzles and Problems in Nozzles 54:21
15 Criterion for Choice of Chemical Propellants 53:40
16 Choice of Fuel-Rich Propellants 56:24
17 Performance Prediction Analysis 57:06
18 Dissociation of Products of Combustion 51:43
19 Shifting Equilibrium and Frozen Flow in Nozzles 52:45
20 Factors Influencing Choice of Chemical Propellants 51:34
21 Low Energy Liquid Propellants and Hybrid Propellants 55:16
22 Introduction to Solid Propellant Rockets 52:44
23 Burn Rate of Solid Propellants and Equilibrium pressure in Solid Propellants Rockets 53:49
24 Design Aspects of Solid Propellant Rockets 57:06
25 Burning Surface Area of Solid Propellant Grains 54:32
26 Ignition of Solid Propellant Rockets 55:11
27 Review of Solid Propellant Rockets 54:44
28 Feed Systems for Liquid Propellant Rockets 53:06
29 Feed System Cycles for Pump Fed Liquid Propellant Rockets 52:19
30 Analysis of Gas Generator and Staged Combustion Cycles and Introduction to Injectors 56:12
31 Injectors,Cooling of Chamber and Mixture Ratio Distribution 51:42
32 Efficiencies due to Mixture Ratio Distribution and Incomplete Vaporization 54:05
33 Pumps and Turbines; Propellant Feed System at Zero "g" Conditions 52:52
34 Review of Liquid Bi-propellant Rockets and Introduction to Mono-propellant Rockets 53:59
35 Introduction to Hybrid Rockets and a Simple Illustration of Combustion Instability 52:34
36 Combustion Instability in Solid Propellant and Liquid Propellant Rockets 48:36
37 Wave models of Oscillation 55:15
38 Mechanisms Causing Instabilities and Strategies for Avoiding Combustion Instability 59:10
39 Electric and Magnetic Fields and the Electrostatic Thruster 48:06
40 Electrical Thrusters 54:10