Micro Newton Thruster Development Direct Thrust Measurements and Thr
Franz Georg Hey summarises the development and testing of a micro-Newton thrust balance, as well as the downscaling of a High Efficiency Multistage Plasma Thruster to micro-Newton thrust levels. The balance is tailored to fully characterise thruster candi
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Micro Newton Thruster Development Direct Thrust Measurements and Thruster Downscaling
Micro Newton Thruster Development
Franz Georg Hey
Micro Newton Thruster Development Direct Thrust Measurements and Thruster Downscaling
Franz Georg Hey Friedrichshafen, Germany Dissertation, Dresden University of Technology, 2017 with the title “Development and Test of a Micro-Newton Thruster Test Facility and Micro-Newton HEMPTs”
ISBN 978-3-658-21208-7 ISBN 978-3-658-21209-4 (eBook) https://doi.org/10.1007/978-3-658-21209-4 Library of Congress Control Number: 2018935282 Springer Vieweg © Springer Fachmedien Wiesbaden GmbH 2018 This work is subject to copyright. All rights are reserved by the Publisher, 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 publisher, 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 publisher 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 publisher remains neutral with regard to jurisdictional claims in published maps and institutional affiliations. Printed on acid-free paper This Springer Vieweg imprint is published by Springer Nature The registered company is Springer Fachmedien Wiesbaden GmbH The registered company address is: Abraham-Lincoln-Str. 46, 65189 Wiesbaden, Germany
Acknowledgements This work has been performed in the Laboratory for Enabling Technologies of Airbus in Friedrichshafen in close collaboration with the Dresden University of Technology and the University of Bremen / DLR Bremen. Therefore, I want to thank my colleagues at Airbus, in particular Ulrich Johann, Dennis Weise, Noah Saks, Karlheinz Eckert, Ewan Fitzsimons, Hans Reiner Schulte, Andreas Keller, Harald Kögel, Oliver Mandel, Max Vaupel and Marjetka Kastner. From the Dresden University of Technology, I want to thank Martin Tajmar. I would like to acknowledge the support of Martin Gohlke, Thilo Schuldt, Tim Brandt and Claus Braxmaier in Bremen. The Radio Frequency Ion Thruster tested has been provided by the ArianeGroup, thanks go to Christian Altmann and Hans Leiter, Marcel Berger. My special acknowledgement goes to Günter Kornfeld, whose idea it was to use a cusp structured magnetic field as a thruster. Lastly, I would like to thank Karolin and my family for t
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