Mishra Fundamentals of Rocket Propulsion

1. Auflage 2017
ISBN: 978-1-4987-8536-5
Verlag: CRC Press
Format: PDF
Kopierschutz: Adobe DRM (»Systemvoraussetzungen)

E-Book, Englisch, 482 Seiten

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

Autoren/Hrsg.

Mishra, DP

Fachgebiete

• Technische Wissenschaften Maschinenbau | Werkstoffkunde Maschinenbau

Inhaltsverzeichnis

Chapter 1: Introduction
1.1 Introduction
1.2 Basic Principle of Propulsion:

1.3 Brief History of Rocket Engine:

1.4 Classification of Propulsive Devices
1.5 Types of Rocket Engine

1.6 Applications of Rocket Engine
1.7 Review Questions
1.8 References and Suggested Readings

Chapter 2 Aerothermochemistry of Rocket Engine
2.1 Introduction
2.2 Basic Principles of Chemical Thermodynamics
2.3 Thermodynamic Laws
2.4 Reacting System
2.5 Basic Principles of Gas Dynamics

2.6 Review Questions
2.7 Problems
2.8 References and Suggested Readings

Chapter 3 Elements of Rocket Propulsion
3.1 Introduction
3.2 Ideal Rocket Engine
3.3 Thrust Equation of Rocket Engine
3.4 Rocket Performance Parameters
3.5 Review Questions
3.6 Problems
3.7 References

Chapter 4 Rocket Nozzle
4.1 Introduction
4.2 Basics of CD Nozzle Flow
4.3 CD Nozzle Geometry
4.4 Effect of Ambient Pressure
4.5 Advanced Rocket Nozzle
4.6 Thrust Vectoring Nozzles

4.7 Losses in Rocket Nozzle
4.8 Performance of Exhaust Nozzle

4.9 Thrust Coefficient
4.10 Review Questions
4.11 Problems
4.12 References and Suggested Readings

Chapter 5 Spacecraft Flight Performance
5.1 Introduction
5.2 Forces Acting on Vehicle
5.3 The Rocket Equation
5.4 Space Flight and its Orbit
5.5 Interplanetary Transfer Path

5.6 Single Stage Rocket
5.7 Multistage Rocket Engine
5.8 Review Questions
5.9 Problems
5.10 References and Suggested Readings

Chapter 6: Chemical Rocket Propellants
6.1 Introduction
6.2 Classification of Chemical Propellant
6.3 General Characteristics of Propellant
6.4 Solid Propellant
6.5 Liquid Propellants

6.6 Gel Propellants
6.7 Hybrid Propellants
6.8 Review Questions
6.9 References and Suggested Readings

Chapter 7: Solid Propellant Rocket Engine
7.1 Introduction
7.2 Basic Configuration

7.3 Physical Processes of Solid Propellant Burning
7.4 Burning Mechanism of Solid Propellant
7.5 Measurement of Propellant Burning/Regression Rate
7.6 Thermal Model for Solid Propellant Burning
7.7 Solid Propellant Rocket Engine Operation
7.8 Internal Ballistics of SPR Engine
7.9 Propellant Grain Configuration
7.10 Evolution of Burning Surface

7.11 Ignition System

7.12 Modeling of Flow in a Side Burning Grain of Rocket Engine

Chapter 8: Liquid Propellant Rocket Engine
8.1 Introduction
8.2 Basic Configuration

8.3 Types of Liquid Propellant Rocket (LPR) Engines

8.4 Combustion of Liquid Propellant

8.5 Combustion Chamber Geometry

8.6 Combustion Instabilities in LPRE
8.7 Ignition System
8.8 Cooling System

8.9 Heat Transfer Analysis for Cooling System

8.10 Review Questions
8.11 Problems

Chapter 9: Hybrid Propellant Rocket Engine

9.1 Introduction
9.2 Combustion Chamber
9.3 Propellants for HPRE
9.4 Grain Configuration
9.5 Combustion of Hybrid Propellant
9.6 Ignition of Hybrid Propellant

9.7 Combustion Instability in HPRE
9.8 Review Questions

9.9 Problems

Chapter 10: Liquid Propellant Injection System
10.1 Introduction
10.2 Atomization Process
10.3 Injector Elements
10.4 Design of Injector Elements
10.5 Performance of Injector
10.6 Injector Distributor
10.7 Injector Manifold
10.8 Liquid Propellant Feed System
10.9 Turbo-pump Feed System
10.10 Review Questions
10.11 Problems

Chapter 11: Non-chemical Rocket Engine
11. 1 Introduction

11.2 Basic Principles of Electrical Rocket Engine
11.3 Electrothermal Thrusters
11.4 Electrostatic Thrusters
11.5 Electromagnetic Thruster
11.6 Nuclear Rocket Engine
11.7 Solar Energy Rockets
11.8 Review Questions
11.9 Problems

Über Autor(innen)

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.