Description: Fundamental Concepts of Liquid-Propellant Rocket Engines, Hardcover by Veris, Alessandro De Laco, ISBN 3030547035, ISBN-13 9783030547035, Brand New, Free shipping in the US
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). Th 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, th will be of particular interest to undergraduate and graduate students of aerospace engineering.
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Book Title: Fundamental concepts of Liquid Propellant Rocket Engines
Number of Pages: IX, 747 Pages
Language: English
Publisher: Springer International Publishing A&G
Topic: Engineering (General), Machinery, Aeronautics & Astronautics
Publication Year: 2020
Illustrator: Yes
Genre: Technology & Engineering
Item Weight: 45.8 Oz
Item Length: 9.3 in
Author: Alessandro De Iaco Veris
Book Series: Springer Aerospace Technology Ser.
Item Width: 6.1 in
Format: Hardcover
