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Fundamentals of Rocket Propulsion [Kõva köide]

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(Indian Institute of Technology, Kanpur, Uttar Pradesh, India)
  • Formaat: Hardback, 462 pages, kõrgus x laius: 234x156 mm, kaal: 1040 g, 18 Tables, black and white; 24 Line drawings, color; 110 Line drawings, black and white
  • Ilmumisaeg: 02-Aug-2017
  • Kirjastus: CRC Press Inc
  • ISBN-10: 1498785352
  • ISBN-13: 9781498785358
Teised raamatud teemal:
Fundamentals of Rocket PropulsionSuurem pilt
  • Formaat: Hardback, 462 pages, kõrgus x laius: 234x156 mm, kaal: 1040 g, 18 Tables, black and white; 24 Line drawings, color; 110 Line drawings, black and white
  • Ilmumisaeg: 02-Aug-2017
  • Kirjastus: CRC Press Inc
  • ISBN-10: 1498785352
  • ISBN-13: 9781498785358
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781498785358.html
Märksõnad:

The book follows a unified approach to present the basic principles of rocket propulsion in concise and lucid form. This textbook comprises of ten chapters ranging from brief introduction and elements of rocket propulsion, aerothermodynamics to solid, liquid and hybrid propellant rocket engines with chapter on electrical propulsion. Worked out examples are also provided at the end of chapter for understanding uncertainty analysis. This book is designed and developed as an introductory text on the fundamental aspects of rocket propulsion for both undergraduate and graduate students. It is also aimed towards practicing engineers in the field of space engineering. This comprehensive guide also provides adequate problems for audience to understand intricate aspects of rocket propulsion enabling them to design and develop rocket engines for peaceful purposes.

Key Features:

• Book presents an integrated approach including mechanics, modeling, manufacture and design of composite components including theory and practice.

• Exhaustive discussion on analysis and analytical methods for composite beams, columns and plates, and the basic procedure of the finite element method.

• Principles of composite manufacturing, common manufacturing methods and selection of manufacturing methods are presented in depth.

• Presents concept of design and composite design process, along with several representative design examples.

• Includes fully-solved examples with solutions manual and high quality illustrative figures

Arvustused

"The main focus of the book is thermochemical rocket propulsion systems and the introductory chapters include a useful review of key aerothermodynamic principles. Subsequent chapters cover key performance parameters for thermochemical systems and details of nozzle flow as well as a chapter covering spacecraft flight analysis, including atmospheric launch vehicle analysis and basic orbit mechanics relating to propulsion. Overall this is a very good undergraduate level text book covering basics of thermochemical rocket propulsion elements and introducing key principles of other rocket propulsion systems." The Aeronautical Journal November 2018 Issue

Preface xvii
Author xix
Chapter 1 Introduction
1(20)
1.1 Introduction
1(1)
1.2 Basic Principle Of Propulsion
2(1)
1.3 Brief History Of Rocket Engines
2(5)
1.4 Classification Of Propulsive Devices
7(2)
1.4.1 Comparison of Air-Breathing and Rocket Engines
8(1)
1.5 Types Of Rocket Engines
9(6)
1.5.1 Chemical Rocket Engines
9(1)
1.5.1.1 Solid-Propellant Rocket Engines
9(3)
1.5.1.2 Liquid Propellant Rocket Engines
12(1)
1.5.1.3 Hybrid Propellant Rocket Engines
13(2)
1.5.2 Nonchemical Rocket Engines
15(1)
1.6 Applications Of Rocket Engines
15(6)
1.6.1 Space Launch Vehicle
15(1)
1.6.2 Spacecraft
16(1)
1.6.3 Missile
17(1)
1.6.4 Other Civilian Applications
18(1)
Review Questions
18(1)
References And Suggested Readings
18(3)
Chapter 2 Aerothermochemistry of Rocket Engines
21(48)
2.1 Introduction
21(1)
2.2 Basic Principles Of Chemical Thermodynamics
21(1)
2.2.1 Basic Definitions
22(1)
2.3 Thermodynamic Laws
22(5)
2.3.1 First Law of Thermodynamics
23(1)
2.3.2 First Law for Control Volume
24(1)
2.3.3 Second Law of Thermodynamics
24(3)
2.4 Reacting System
27(20)
2.4.1 Stoichiometry
27(4)
2.4.2 Ideal Gas Mixture
31(3)
2.4.3 Heats of Formation and Reaction
34(3)
2.4.4 Adiabatic Flame Temperature
37(3)
2.4.5 Chemical Equilibrium
40(5)
2.4.5.1 Evaluation of Equilibrium Composition of Simultaneous Reactions
45(2)
2.5 Basic Principles Of Gas Dynamics
47(22)
2.5.1 Conservation Equations
48(1)
2.5.2 Steady Quasi-One-Dimensional Flow
48(2)
2.5.3 Isentropic Flow through Variable Area Duct
50(1)
2.5.4 Mass Flow Parameter
51(3)
2.5.5 Normal Shocks
54(6)
2.5.6 Oblique Shocks
60(5)
Review Questions
65(1)
Problems
66(1)
References And Suggested Readings
67(2)
Chapter 3 Elements of Rocket Propulsion
69(22)
3.1 Introduction
69(1)
3.2 Ideal Rocket Engine
70(1)
3.3 Thrust Equation Of Rocket Engines
71(5)
3.3.1 Effective Exhaust Velocity
72(1)
3.3.2 Maximum Thrust
73(1)
3.3.3 Variation of Thrust with Altitude
74(1)
3.3.4 Effect of Divergence Angle on Thrust
74(2)
3.4 Rocket Performance Parameters
76(15)
3.4.1 Total Impulse and Specific Impulse
77(1)
3.4.2 Specific Impulse Efficiency
78(1)
3.4.3 Volumetric Specific Impulse
79(1)
3.4.4 Mass Flow Coefficient
80(1)
3.4.5 Thrust Coefficient
80(1)
3.4.6 Specific Propellant Consumption
81(1)
3.4.7 Characteristic Velocity
81(1)
3.4.8 Impulse-to-Weight Ratio
82(2)
3.4.9 Energy Balance and Efficiencies
84(1)
3.4.9.1 Propulsive Efficiency
85(1)
3.4.9.2 Thermal Efficiency
86(1)
3.4.9.3 Overall Efficiency
87(1)
Review Questions
88(1)
Problems
89(1)
References And Suggested Reading
90(1)
Chapter 4 Rocket Nozzle
91(38)
4.1 Introduction
91(1)
4.2 Basics Of CD Nozzle Flow
91(13)
4.2.1 Exhaust Velocity
93(4)
4.2.2 Mass Flow Rate and Characteristics of Velocity
97(5)
4.2.3 Expansion Area Ratio
102(2)
4.3 CD Nozzle Geometry
104(2)
4.4 Effect Of Ambient Pressure
106(4)
4.4.1 Underexpansion in CD Nozzle
107(1)
4.4.2 Overexpansion in CD Nozzle
108(2)
4.5 Advanced Rocket Nozzle
110(3)
4.5.1 Extendible Nozzle
110(1)
4.5.2 Dual Bell-Shaped Nozzle
111(1)
4.5.3 Expansion-Deflection Nozzle
112(1)
4.5.4 Aerospike Nozzle
113(1)
4.6 Thrust-Vectoring Nozzles
113(3)
4.7 Losses In Rocket Nozzle
116(1)
4.8 Performance Of Exhaust Nozzle
117(3)
4.8.1 Isentropic Efficiency
118(1)
4.8.2 Discharge Coefficient
119(1)
4.8.3 Mass Flow Coefficient
119(1)
4.9 Thrust Coefficient
120(9)
Review Questions
123(1)
Problems
124(3)
References And Suggested Readings
127(2)
Chapter 5 Spacecraft Flight Performance
129(32)
5.1 Introduction
129(1)
5.2 Forces Acting On A Vehicle
130(3)
5.2.1 Aerodynamic Forces
130(2)
5.2.2 Gravity
132(1)
5.2.3 Atmospheric Density
132(1)
5.3 The Rocket Equation
133(7)
5.3.1 Burnout Distance
138(1)
5.3.2 Coasting Height
138(1)
5.3.3 Flight Trajectory
139(1)
5.4 Space Flight And Its Orbit
140(7)
5.4.1 Elliptic Orbit
142(2)
5.4.2 Geosynchronous Earth Orbit
144(1)
5.4.3 Requisite Velocity to Reach an Orbit
144(2)
5.4.4 Escape Velocity
146(1)
5.5 Interplanetary Transfer Path
147(1)
5.6 Single-Stage Rocket Engines
148(4)
5.7 Multistage Rocket Engines
152(9)
5.7.1 Multistaging
153(3)
Review Questions
156(2)
Problems
158(2)
References And Suggested Readings
160(1)
Chapter 6 Chemical Rocket Propellants
161(34)
6.1 Introduction
161(1)
6.2 Classification Of Chemical Propellants
162(1)
6.3 General Characteristics Of Propellants
163(1)
6.4 Solid Propellants
164(11)
6.4.1 Homogeneous Solid Propellants
165(3)
6.4.2 Heterogeneous Propellants
168(1)
6.4.2.1 Solid Fuel (Binder)
168(3)
6.4.2.2 Solid Oxidizer
171(2)
6.4.2.3 Composite Modified Double-Base Propellant
173(1)
6.4.2.4 Advanced Propellants
173(2)
6.5 Liquid Propellants
175(13)
6.5.1 Liquid Fuels
176(1)
6.5.1.1 Hydrocarbon Fuels
176(2)
6.5.1.2 Hydrazine (N2H4)
178(1)
6.5.1.3 Liquid Hydrogen
179(1)
6.5.1.4 Hydroxyl Ammonium Nitrate (NH2OH*NO3)
180(1)
6.5.2 Liquid Oxidizers
180(2)
6.5.2.1 Hydrogen Peroxide (H2O2)
182(1)
6.5.2.2 Nitrogen Tetraoxide (N204)
182(1)
6.5.2.3 Nitric Acid (HNO3)
183(1)
6.5.2.4 Liquid Oxygen
184(1)
6.5.2.5 Liquid Fluorine
184(1)
6.5.3 Physical and Chemical Properties of Liquid Propellants
185(1)
6.5.4 Selection of Liquid Propellants
186(2)
6.6 Gel Propellants
188(3)
6.6.1 Common Gel Propellants and Gellants
189(1)
6.6.2 Advantages of Gel Propellants
189(1)
6.6.2.1 Safety Aspects
190(1)
6.6.2.2 Performance Aspects
190(1)
6.6.2.3 Storage Aspects
190(1)
6.6.3 Disadvantages of Gel Propellants
191(1)
6.7 Hybrid Propellants
191(4)
Review Questions
192(1)
References And Suggested Readings
193(2)
Chapter 7 Solid-Propellant Rocket Engines
195(66)
7.1 Introduction
195(2)
7.2 Basic Configuration
197(1)
7.3 Physical Processes Of Solid-Propellant Burning
198(1)
7.4 Burning Mechanism Of Solid Propellants
199(4)
7.4.1 Double-Base Propellants
199(2)
7.4.2 Composite Propellant Combustion
201(2)
7.5 Measurement Of Propellant Burning/Regression Rate
203(15)
7.5.1 Effect of Chamber Pressure on Burning Rate
206(3)
7.5.2 Effects of Grain Temperature on Burning Rate
209(2)
7.5.3 Effect of Gas Flow Rate
211(3)
7.5.4 Effects of Transients on Burning Rate
214(1)
7.5.5 Effects of Acceleration on Burning Rate
215(1)
7.5.6 Other Methods of Augmenting Burning Rate
216(1)
7.5.6.1 Particle Size Effects
217(1)
7.5.6.2 Burning Rate Modifiers
218(1)
7.6 Thermal Model For Solid-Propellant Burning
218(2)
7.7 Solid-Propellant Rocket Engine Operation
220(5)
7.7.1 Ignition of a Solid Propellant
220(3)
7.7.2 Action Time and Burn Time
223(2)
7.8 Internal Ballistics Of SPRE
225(6)
7.8.1 Stability of SPRE Operation
230(1)
7.9 Propellant Grain Configuration
231(2)
7.10 Evolution Of Burning Surface
233(10)
7.10.1 Star Grain
236(4)
7.10.1.1 Three-Dimensional Grains
240(3)
7.11 Ignition System
243(6)
7.11.1 Pyrotechnic Igniter
246(2)
7.11.2 Pyrogen Igniter
248(1)
7.12 Modeling Of Flow In A Side Burning Grain Of Rocket Engine
249(12)
Review Questions
254(2)
Problems
256(3)
References
259(2)
Chapter 8 Liquid-Propellant Rocket Engines
261(48)
8.1 Introduction
261(1)
8.2 Basic Configuration
262(2)
8.3 Types Of Liquid-Propellant Rocket Engines
264(3)
8.3.1 Monopropellant Rocket Engines
264(1)
8.3.2 Bipropellant Rocket Engines
265(2)
8.4 Combustion Of Liquid Propellants
267(7)
8.4.1 Hypergolic Propellant Combustion
272(1)
8.4.1.1 Nonhypergolic Propellant Combustion
273(1)
8.5 Combustion Chamber Geometry
274(6)
8.6 Combustion Instabilities In LPRE
280(10)
8.6.1 Analysis of Bulk Mode Combustion Instability
283(4)
8.6.2 Control of Combustion Instability
287(1)
8.6.2.1 Chemical Method
287(1)
8.6.2.2 Aerodynamic Method
287(1)
8.6.2.3 Mechanical Method
288(2)
8.7 Ignition Systems
290(4)
8.8 Cooling Systems
294(3)
8.8.1 Regenerative Cooling
294(1)
8.8.2 Film/Sweat Cooling
295(1)
8.8.3 Ablative Cooling
296(1)
8.9 Heat Transfer Analysis For Cooling Systems
297(12)
Review Questions
304(2)
Problems
306(1)
References
307(2)
Chapter 9 Hybrid Propellant Rocket Engine
309(24)
9.1 Introduction
309(1)
9.2 Combustion Chamber
310(1)
9.3 Propellants For HPRE
311(1)
9.4 Grain Configuration
312(1)
9.5 Combustion Of Hybrid Propellants
313(12)
9.5.1 Effects of Thermal Radiation on Hybrid Propellant Combustion
322(3)
9.6 Ignition Of Hybrid Propellants
325(1)
9.7 Combustion Instability In HPRE
326(7)
9.7.1 Feed System-Coupled Instabilities
326(1)
9.7.2 Chuffing
327(1)
9.7.3 Intrinsic Low-Frequency Instabilities
328(2)
Review Questions
330(1)
Problems
330(1)
References
331(2)
Chapter 10 Liquid-Propellant Injection System
333(64)
10.1 Introduction
333(1)
10.2 Atomization Process
334(3)
10.3 Injector Elements
337(8)
10.3.1 Types of Injectors
338(1)
10.3.1.1 Nonimpinging Injectors
338(2)
10.3.1.2 Impinging Injectors
340(4)
10.3.1.3 Other Types of Injectors
344(1)
10.4 Design Of Injector Elements
345(6)
10.5 Performance Of Injector
351(4)
10.5.1 Droplet Size Distribution
351(2)
10.5.2 Mass Distribution
353(1)
10.5.3 Quality Factor
354(1)
10.6 Injector Distributor
355(1)
10.7 Injector Manifold
356(1)
10.8 Liquid-Propellant Feed System
357(15)
10.8.1 Gas Pressure Feed System
358(2)
10.8.1.1 Cold Gas Pressure Feed System
360(3)
10.8.1.2 Hot Gas Pressure Feed System
363(1)
10.8.1.3 Chemically Generated Gas Feed System
364(8)
10.9 Turbo-Pump Feed System
372(25)
10.9.1 Types of Turbo-Pump Feed System
372(3)
10.9.1.1 Propellant Turbo-Pumps
375(1)
10.9.2 Propellant Pumps
375(7)
10.9.2.1 Cavitation
382(4)
10.9.2.2 Propellant Turbines
386(5)
Review Questions
391(1)
Problems
392(3)
References
395(2)
Chapter 11 Nonchemical Rocket Engine
397(42)
11.1 Introduction
397(1)
11.2 Basic Principles Of Electrical Rocket Engine
398(7)
11.2.1 Classifications of Electrical Rockets
398(1)
11.2.2 Background Physics of Electrical Rockets
399(1)
11.2.2.1 Electrostatic and Electromagnetic Forces
399(4)
11.2.2.2 Ionization
403(1)
11.2.2.3 Electric Discharge Behavior
403(2)
11.3 Electrothermal Thrusters
405(8)
11.3.1 Resistojets
405(6)
11.3.2 Arcjets
411(2)
11.4 Electrostatic Thrusters
413(10)
11.4.1 Basic Principles of Electrostatic Thrusters
415(5)
11.4.2 Propellant Choice
420(1)
11.4.3 Performance of Ion Thruster
420(3)
11.5 Electromagnetic Thruster
423(7)
11.5.1 Basic Principles of Electromagnetic Thruster
423(1)
11.5.2 Types of Plasma Thruster
424(1)
11.5.2.1 Magnetoplasmadynamic Thrusters
425(2)
11.5.2.2 Pulsed Plasma Thruster
427(1)
11.5.2.3 Hall Effect Thruster
428(2)
11.6 Nuclear Rocket Engines
430(3)
11.7 Solar Energy Rockets
433(6)
Review Questions
435(1)
Problems
436(2)
References
438(1)
Appendices 439(12)
Index 451
Dr. D.P. Mishra is a professor in the Department of Aerospace Engineering at Indian Institute of Technology (IIT) Kanpur, Kanpur, India where he was instrumental in establishing a combustion laboratory. He currently holds the Indian Oil Golden Jubilee Professional Chair in IIT Kanpur. He was a Visiting Professor in 2002 at the Tokyo-Denki University, Japan. His areas of research interest include combustion, computational fluid dynamics, atomization, etc. He is the recipient of the Young Scientist Award in 1991 from the Ministry of New and Renewable Energy, Government of India. He was conferred the INSA-JSPS Fellowship in 2002. In recognition of his research, Dr. Mishra received the Sir Rajendranath Mookerjee Memorial Award from the Institution of Engineers (India). Dr. Mishra is a recipient of the Samanta Chadrasekhar Award for his contributions to science and technology. For technological contribution for the common people, he has been conferred with the Vikash Prerak Sanman in 2010. Currently he is serving as an Assistant Editor, International Journal of Hydrogen Energy, Elsevier, USA. Besides this, he also serves as an editorial board member of Journal of the Chinese Institute of Engineers, Taylor & Francis, and International Journal of Turbo and Jet engines. Dr. Mishra has six Indian patents and around 200 research papers in refereed Journals and in conference proceedings to his credit. He has authored a textbook titled "Fundamentals of Combustion", published by Prentice Hall of India, New Delhi. Two other text books on "Experimental Combustion" and "Engineering Thermodynamics" have been published by Taylor and Francis, USA and Cengage India Pvt Ltd., New Delhi, respectively. He has published a text book titled as "Gas turbine propulsion" (MV Learning, New Delhi/London). He is also serving as a managing trustee of the International Foundation of Humanistic Education.