| 书目名称 | Fundamental Concepts of Liquid-Propellant Rocket Engines | | 编辑 | Alessandro de Iaco Veris | | 视频video | | | 概述 | 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 | | 丛书名称 | Springer Aerospace Technology | | 图书封面 |  | | 描述 | .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.. | | 出版日期 | Textbook 2021 | | 关键词 | Textbook in aerospace engineering; Spacecraft propulsion; Rocket engines; Liquid-propellant rockets; liq | | 版次 | 1 | | doi | https://doi.org/10.1007/978-3-030-54704-2 | | isbn_softcover | 978-3-030-54706-6 | | isbn_ebook | 978-3-030-54704-2Series ISSN 1869-1730 Series E-ISSN 1869-1749 | | issn_series | 1869-1730 | | copyright | The Editor(s) (if applicable) and The Author(s), under exclusive license to Springer Nature Switzerl |
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发表于 2025-3-21 18:10:50
