"Fundamentals of Hybrid Rocket Combustion and Propulsion" is the first text to offer a comprehensive treatment of hybrid rockets. In this book, editors have pooled together some of the most respected minds in the field, each providing their very special insight and expertise to the text. The content is therefore as up-to-date as it is broad. Each chapter offers an expert account of every aspect of hybrid rocket propulsion, including fundamental aspects of hybrid combustion, numerical and theoretical approaches, and various applications. All chapters are enhanced with more than 25 to 35 graphical elements - including tables, figures and photographs. Making for an easy and informative read, this book is a must-have resource for anyone currently working in or studying rocket propulsion.
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About the Author
Martin J. Chiaverini is a Principal Propulsion Engineer at Orbital Technologies Corporation (ORBITEC). He earned a B.S. in Aerospace Engineering and a B.S. in English from the University of Notre Dame, as well as an M.S. in Aerospace Engineering, an M.S. in Mechanical Engineering, and a Ph.D. in Mechanical Engineering from The Pennsylvania State University.
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3 of 3 people found the following review helpful:
5.0 out of 5 stars
THE work on Hybrid Rocket Propulsion,
This review is from: Fundamentals of Hybrid Rocket Combustion and Propulsion (Progress in Astronautics and Aeronautics) (Hardcover)
An outstanding assembly of work in this field. Deeply technical, this book covers every aspect of the art from science to speculation.
Highly recommended for University Libraries, Engineering Libraries and for students of reaction propulsion.
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