Modern Engineering for Design of Liquid-Propellant Rocket Engines
Author: Dieter K. Huzel
Publisher: AIAA
Published: 1992
Total Pages: 452
ISBN-13: 9781600864001
DOWNLOAD EBOOK →Author: Dieter K. Huzel
Publisher: AIAA
Published: 1992
Total Pages: 452
ISBN-13: 9781600864001
DOWNLOAD EBOOK →Author: Alessandro de Iaco Veris
Publisher: Springer Nature
Published: 2020-09-26
Total Pages: 747
ISBN-13: 3030547043
DOWNLOAD EBOOK →This book is intended for students and engineers who design and develop liquid-propellant rocket engines, offering them a guide to the theory and practice alike. It first presents the fundamental concepts (the generation of thrust, the gas flow through the combustion chamber and the nozzle, the liquid propellants used, and the combustion process) and then qualitatively and quantitatively describes the principal components involved (the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements). The book includes extensive data on existing engines, typical values for design parameters, and worked-out examples of how the concepts discussed can be applied, helping readers integrate them in their own work. Detailed bibliographical references (including books, articles, and items from the “gray literature”) are provided at the end of each chapter, together with information on valuable resources that can be found online. Given its scope, the book will be of particular interest to undergraduate and graduate students of aerospace engineering.
Author: George Paul Sutton
Publisher: AIAA
Published: 2006
Total Pages: 936
ISBN-13: 9781563476495
DOWNLOAD EBOOK →Liquid propellant rocket engines have propelled all the manned space flights, all the space vehicles flying to the planets or deep space, virtually all satellites, and the majority of medium range or intercontinental range ballistic missiles.
Author: Vigor Young
Publisher: AIAA
Published: 1995
Total Pages: 606
ISBN-13: 9781600864186
DOWNLOAD EBOOK →Annotation Since the invention of the V-2 rocket during World War II, combustion instabilities have been recognized as one of the most difficult problems in the development of liquid propellant rocket engines. This book is the first published in the United States on the subject since NASA's Liquid Rocket Combustion Instability (NASA SP-194) in 1972. In this book, experts cover four major subject areas: engine phenomenology and case studies, fundamental mechanisms of combustion instability, combustion instability analysis, and engine and component testing. Especially noteworthy is the inclusion of technical information from Russia and China--a first.
Author: Dr Jim Ras
Publisher: Lulu.com
Published: 2016-09-20
Total Pages: 414
ISBN-13: 9781365409332
DOWNLOAD EBOOK →This book intends to build a bridge for the student and the young engineer: to link the rocket propulsion fundamentals and elements (which are well covered in the literature) with the actual rocket engine design and development work as it is carried out in industry (which is very little, if at all covered in literature). The book attempts to further the understanding of the realistic application of liquid rocket propulsion theories, and to help avoid or at least reduce time and money consuming errors and disappointments. In so doing, it also attempts to digest and consolidate numerous closely related subjects, hitherto often treated as separate, bringing them up to date at the same time.
Author: James R.
Publisher: Noah Books
Published: 1969-01-02
Total Pages: 468
ISBN-13: 9781948117944
DOWNLOAD EBOOK →This book intends to build a bridge for the student and the young engineer: to link the rocket propulsion fundamentals and elements with the actual rocket engine design and development work as it is carried out in the industry. The book attempts to further the understanding of the realistic application of liquid rocket propulsion theories, and to help avoid or at least reduce time and money consuming errors and disappointments. This book was written "on the job" for use by those active in all phases of engine systems, design, development, and application, in industry.
Author: DP Mishra
Publisher: CRC Press
Published: 2017-07-20
Total Pages: 313
ISBN-13: 1351708414
DOWNLOAD EBOOK →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.