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Название: Fundamental Concepts of Liquid-Propellant Rocket Engines
Автор: Alessandro de Iaco Veris
Издательство: Springer
Год: 2021
Формат: PDF
Страниц: 755
Размер: 35,94 МБ
Язык: English
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).