Springer Aerospace Technology
cover

Fundamental Concepts of Liquid Propellant Rocket Engines

Authors: de Iaco Veris, Alessandro

  • Includes extensive data on current engines and worked-out examples with their numerical results
  • Intended for aerospace engineers, particularly those who design liquid-propellant engines
  • Uses only the metric system (SI)
  • Written in a highly readable style
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書籍の購入

イーブック ¥5,719
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • イーブック版は、まもなく発売予定です。
  • 予定日: December 20, 2020
  • ISBN 978-3-030-54704-2
  • ウォーターマーク付、 DRMフリー
  • ファイル形式:
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥7,149
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: December 20, 2020
  • ISBN 978-3-030-54703-5
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
  • Immediate ebook access, if available*, with your print order
この教本について

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.


著者について

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.

書籍の購入

イーブック ¥5,719
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • イーブック版は、まもなく発売予定です。
  • 予定日: December 20, 2020
  • ISBN 978-3-030-54704-2
  • ウォーターマーク付、 DRMフリー
  • ファイル形式:
  • どの電子書籍リーダーからでもすぐにお読みいただけます。
ハードカバー ¥7,149
価格の適用国: Japan (日本円価格は個人のお客様のみ有効) (小計)
  • 予定日: December 20, 2020
  • ISBN 978-3-030-54703-5
  • 個人のお客様には、世界中どこでも配送料無料でお届けします。
  • Immediate ebook access, if available*, with your print order
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書誌情報

Bibliographic Information
Book Title
Fundamental Concepts of Liquid Propellant Rocket Engines
Authors
Series Title
Springer Aerospace Technology
Copyright
2021
Publisher
Springer International Publishing
Copyright Holder
The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerland AG
イーブック ISBN
978-3-030-54704-2
DOI
10.1007/978-3-030-54704-2
ハードカバー ISBN
978-3-030-54703-5
Series ISSN
1869-1730
Edition Number
1
Number of Pages
X, 768
Number of Illustrations
401 b/w illustrations, 54 illustrations in colour
Topics

*immediately available upon purchase as print book shipments may be delayed due to the COVID-19 crisis. ebook access is temporary and does not include ownership of the ebook. Only valid for books with an ebook version. Springer Reference Works and instructor copies are not included.