Modern Engineering for Design of Liquid Propellant Rocket Engines: An American Institute of Aeronautics and Astronautics Series

By Dieter K Huzel
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"Modern Engineering for Design of Liquid Propellant Rocket Engines" by Dieter K. Huzel provides an in-depth exploration of the engineering principles and design techniques crucial in the development of liquid propellant rocket engines.

This comprehensive guide begins with an overview of the historical background and evolution of rocket engines, setting the stage for understanding the contemporary methodologies discussed throughout the book.

Readers will gain a deep understanding of critical elements such as combustion processes, heat transfer, and thermodynamics involved in the design of rocket engines. The author elucidates the fundamental principles of propellants and their behavior, encompassing the intricate aspects of fluid dynamics.

The book covers a wide array of design considerations, including propellant selection, combustion chamber design, turbopumps, nozzles, and ignition systems. It explores the practical aspects of liquid rocket engine design, providing insights into materials selection, fabrication techniques, and assembly processes.

Furthermore, Huzel methodically discusses performance analysis and optimization methods, equipping readers with the necessary tools to evaluate and refine their designs.

This book also examines thrust chamber cooling techniques, injector design, and turbopump performance, addressing the challenges and innovations in these areas.

With its emphasis on reliability and efficiency, "Modern Engineering for Design of Liquid Propellant Rocket Engines" is an invaluable resource for engineers, researchers, and students involved in the field of rocket propulsion. Huzel's authoritative approach and meticulous analysis make this book an essential reference for those seeking to advance their knowledge and skills in liquid propellant rocket engine design.
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