Electronic Resource

Fundamental Concepts of Liquid-Propellant Rocket Engines

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Penilaian

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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.

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Availability

Inventory Code	Barcode	Call Number	Location	Status
1908000470	EB0000970	621.435 6 Ver f	Central Library (OPAC)	Available

Detail Information

Series Title

Springer Aerospace Technology

Call Number

621.435 6 Ver f

Publisher

Switzerland : Springer Cham., 2020

Collation

ix, 747p.:Ill

Language

English

ISBN/ISSN

978-3-030-54704-2

Classification

621.435 6

Content Type

Ebook

Media Type

-

Carrier Type

online resource

Edition

-

Subject(s)

Liquid propellant rocket engines

Specific Detail Info

-

Statement of Responsibility

BRF

Other version/related

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