Fluidic Nozzle Throats in Solid Rocket Motors
This book focuses on the performance and application of fluidic nozzle throats for solid rocket motors, discussing their flow details and characterization performance, as well as the influence of the particle phase on their performance. It comprehensively
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luidic Nozzle Throats in Solid Rocket Motors
Fluidic Nozzle Throats in Solid Rocket Motors
Kan Xie Xinmin Chen Junwei Li Yu Liu •
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Fluidic Nozzle Throats in Solid Rocket Motors
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Kan Xie Jet Propulsion Lab, School of Aerospace Engineering Beijing Institute of Technology Beijing, China Junwei Li School of Aerospace Engineering Beijing Institute of Technology Beijing, China
Xinmin Chen China Academy of Launch Vehicle Technology Beijing, China Yu Liu Beihang University Beijing, China
Funded by B&R Book Program ISBN 978-981-13-6438-9 ISBN 978-981-13-6439-6 https://doi.org/10.1007/978-981-13-6439-6
(eBook)
Jointly published with National Defense Industry Press, Beijing, China The print edition is not for sale in China Mainland. Customers from China Mainland please order the print book from National Defense Industry Press. Library of Congress Control Number: 2019932829 © Springer Nature Singapore Pte Ltd. and National Defense Industry Press 2019 This work is subject to copyright. All rights are reserved by the Publishers, whether the whole or part of the material is concerned, specifically the rights of translation, reprinting, reuse of illustrations, recitation, broadcasting, reproduction on microfilms or in any other physical way, and transmission or information storage and retrieval, electronic adaptation, computer software, or by similar or dissimilar methodology now known or hereafter developed. The use of general descriptive names, registered names, trademarks, service marks, etc. in this publication does not imply, even in the absence of a specific statement, that such names are exempt from the relevant protective laws and regulations and therefore free for general use. The publishers, the authors and the editors are safe to assume that the advice and information in this book are believed to be true and accurate at the date of publication. Neither the publishers nor the authors or the editors give a warranty, express or implied, with respect to the material contained herein or for any errors or omissions that may have been made. The publishers remain neutral with regard to jurisdictional claims in published maps and institutional affiliations. This Springer imprint is published by the registered company Springer Nature Singapore Pte Ltd. The registered company address is: 152 Beach Road, #21-01/04 Gateway East, Singapore 189721, Singapore
Preface
It is a worldwide trend to develop solid-rocket engines with the trust being able to adjustwithin a broad range in real time. This key technology is under great and urgent demands in many national defense technologies even for many developed countries during these years. For example, these technologies include missile defense systems, solid rocket-ramjet engines, avoidance maneuver of warheads, buffer systems for landers (reentry capsules), multi-mission missiles, energy management technology for wide flight profiles, etc. During the past few decades, researchers have done a great deal of theoretical and experimental work of the thrust-controlled rocket eng
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