Articles liés à Fundamental Concepts of Liquid-Propellant Rocket Engines
Synopsis
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.
Les informations fournies dans la section « Synopsis » peuvent faire référence à une autre édition de ce titre.
À propos de l?auteur
Alessandro de Iaco Veris holds degrees in civil engineering and aerospace engineering, both from the University of Rome. He has also completed specialist training, including a high-level professional course on "Projet, calcul et emploi des fusées spatiales" at the Ecole Nationale Supérieure de l'Aéronautique et de l'Espace (ENSAE) and a course on "Dynamics of Controlled Structures" at Massachusetts Institute of Technology (MIT). He is a strong proponent of the application of mathematics for practical purposes and in particular for the solution of problems arising in engineering. His expertise is in the fields of mathematical models and numerical methods for aerodynamics, space flight mechanics, system studies, and mission analysis. His professional interests include numerical integration methods used to predict the motion of space vehicles and Earth satellites subject to perturbations.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
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Fundamental Concepts of Liquid
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Springer, 2020
ISBN 10 : 3030547035
ISBN 13 : 9783030547035
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Fundamental Concepts of Liquid-Propellant Rocket Engines
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ISBN 10 : 3030547035
ISBN 13 : 9783030547035
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Includes extensive data on current engines and worked-out examples with their numerical resultsIntended for aerospace engineers, particularly those who design liquid-propellant enginesUses only the metric system (SI) Written in a hig. N° de réf. du vendeur 448684451
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Fundamental Concepts of Liquid-Propellant Rocket Engines (Springer Aerospace Technology)
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Fundamental Concepts of Liquid-Propellant Rocket Engines
Edité par
Springer International Publishing, 2020
ISBN 10 : 3030547035
ISBN 13 : 9783030547035
Neuf
Couverture rigide
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
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Buch. Etat : Neu. Druck auf Anfrage Neuware - Printed after ordering - Thisbook 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. N° de réf. du vendeur 9783030547035
Quantité disponible : 1 disponible(s)
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Fundamental Concepts of Liquid-Propellant Rocket Engines
Edité par
Springer International Publishing Sep 2020, 2020
ISBN 10 : 3030547035
ISBN 13 : 9783030547035
Neuf
Couverture rigide
Vendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Évaluation du vendeur 5 sur 5 étoiles
Buch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Thisbook 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. 760 pp. Englisch. N° de réf. du vendeur 9783030547035
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Fundamental Concepts of Liquid-Propellant Rocket Engines (Springer Aerospace Technology)
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Fundamental Concepts of Liquid-Propellant Rocket Engines
ISBN 10 : 3030547035
ISBN 13 : 9783030547035
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Vendeur : buchversandmimpf2000, Emtmannsberg, BAYE, Allemagne
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Buch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -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.Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg 760 pp. Englisch. N° de réf. du vendeur 9783030547035
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Fundamental Concepts of Liquid-Propellant Rocket Engines
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Fundamental Concepts of Liquid-Propellant Rocket Engines
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Fundamental Concepts of Liquid-Propellant Rocket Engines
Edité par
Springer, 2020
ISBN 10 : 3030547035
ISBN 13 : 9783030547035
Ancien ou d'occasion
Couverture rigide
Vendeur : GreatBookPricesUK, Woodford Green, Royaume-Uni
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Etat : As New. Unread book in perfect condition. N° de réf. du vendeur 42076410
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