Skip to main content

Fundamental Concepts of Liquid-Propellant Rocket Engines

DESCRIPTION

(Springer Aerospace Technology) 1st ed. 2021 Edition 

by Alessandro de Iaco Veris (Author) 

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.

DETAILS:

Year: 2021
Pages: 755
Language: English
Format: PDF
Size: 36 MB
Publisher: Springer
ISBN-10: 3030547035
ISBN-13: 978-3030547035
ASIN: B08K761MHN
Tag: Download Book Fundamental Concepts of Liquid-Propellant Rocket Engines