Fundamental Concepts of Liquid-Propellant Rocket Engines

This book is a comprehensive guide to the theory and practice of liquid-propellant rocket engines for students and engineers. It covers fundamental concepts, components, and data, with examples and bibliographical references. It is particularly useful for undergraduate and graduate students in aerospace engineering.

Format: Paperback / softback
Length: 747 pages
Publication date: 28 September 2021
Publisher: Springer Nature Switzerland AG

This comprehensive book is meticulously crafted to cater to students and engineers engaged in the design and development of liquid-propellant rocket engines. It serves as a valuable guide, offering both theoretical insights and practical applications in this field. The book begins by introducing the fundamental concepts that underpin the operation of rocket engines, including thrust generation, gas flow through the combustion chamber and nozzle, the utilization of liquid propellants, and the combustion process. It then delves into a detailed qualitative and quantitative analysis of the key components involved, encompassing the combustion chamber, nozzle, feed systems, control systems, valves, propellant tanks, and interconnecting elements.

To enhance the reader's understanding, the book provides extensive data on existing engines, encompassing typical values for design parameters and illustrative examples showcasing how the discussed concepts can be applied to real-world scenarios. Furthermore, each chapter concludes with a comprehensive list of bibliographical references, encompassing books, articles, and valuable resources available online. Given the broad scope of the book, it holds immense appeal to undergraduate and graduate students pursuing aerospace engineering, providing them with a comprehensive foundation for their studies and future careers.

Weight: 1145g
Dimension: 235 x 155 (mm)
ISBN-13: 9783030547066
Edition number: 1st ed. 2021