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Micro Newton Thruster Development: Direct Thrust Measurements and Thruster Downscaling PDF

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Franz Georg Hey 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 ThisworkhasbeenperformedintheLaboratoryforEnablingTechnologiesofAirbus inFriedrichshafeninclosecollaborationwiththeDresdenUniversityofTechnology andtheUniversityofBremen/DLRBremen. Therefore,IwanttothankmycolleaguesatAirbus,inparticularUlrichJohann, DennisWeise,NoahSaks,KarlheinzEckert,EwanFitzsimons,HansReinerSchulte, AndreasKeller,HaraldKögel,OliverMandel,MaxVaupelandMarjetkaKastner. FromtheDresdenUniversityofTechnology,IwanttothankMartinTajmar. IwouldliketoacknowledgethesupportofMartinGohlke,ThiloSchuldt,Tim BrandtandClausBraxmaierinBremen. TheRadioFrequencyIonThrustertestedhasbeenprovidedbytheArianeGroup, thanksgotoChristianAltmannandHansLeiter,MarcelBerger. MyspecialacknowledgementgoestoGünterKornfeld,whoseideaitwastousea cuspstructuredmagneticfieldasathruster. Lastly,IwouldliketothankKarolinandmyfamilyfortheirsupport. FranzGeorgHey Contents 1 Introduction 1 1.1 MissionsforMicro-NewtonThrusterApplications . . . . . . . . . 1 1.2 MicroPropulsionThrustersOverview . . . . . . . . . . . . . . . 7 1.3 MicroNewtonTestFacilitiesinEurope . . . . . . . . . . . . . . . 9 1.4 AirbusDevelopmentApproach . . . . . . . . . . . . . . . . . . . 11 2 ElectricPropulsionFundamentals 15 2.1 BasicEquations. . . . . . . . . . . . . . . . . . . . . . . . . . . . 16 2.2 BasicPlasmaPhysics . . . . . . . . . . . . . . . . . . . . . . . . . 18 2.3 ElectricPropulsionThrusterTypes . . . . . . . . . . . . . . . . . 22 2.3.1 FieldEmissionElectricPropulsion . . . . . . . . . . . . . 23 2.3.2 RadioFrequencyIonThruster . . . . . . . . . . . . . . . 24 2.3.3 HighEfficiencyMultistagePlasmaThruster . . . . . . . . 26 2.4 ThrusterCharacterisation . . . . . . . . . . . . . . . . . . . . . . 29 2.4.1 DirectThrustMeasurement . . . . . . . . . . . . . . . . . 30 2.4.2 IndirectThrustMeasurement . . . . . . . . . . . . . . . . 36 3 Micro-NewtonThrusterTestFacility 43 3.1 VacuumFacility . . . . . . . . . . . . . . . . . . . . . . . . . . . 45 3.2 PlasmaDiagnosticSetup . . . . . . . . . . . . . . . . . . . . . . . 52 3.2.1 FaradayCup . . . . . . . . . . . . . . . . . . . . . . . . . 54 3.2.2 RetardingPotentialAnalyser . . . . . . . . . . . . . . . . 57 3.2.3 PlasmaDiagnosticCalibration . . . . . . . . . . . . . . . 60 3.3 AirbusMicro-NewtonThrustBalance . . . . . . . . . . . . . . . 61 3.3.1 MechanicalBalanceSetup. . . . . . . . . . . . . . . . . . 64 3.3.2 OpticalBalanceReadout . . . . . . . . . . . . . . . . . . 70 3.3.3 ThrustBalanceControllingandDataAcquisition . . . . . 75 3.3.4 BalanceCalibrationandUncertaintyAnalysis . . . . . . . 79 3.3.5 ThrustBalanceCharacterisation,TestingandAnalysis . . 85 3.4 TestFacilityRealThrusterMeasurementResultsandAnalysis . . . 92 4 MicroHighEfficiencyMultistagePlasmaThrusterDevelopment 105 4.1 NextGenerationμHEMPTDevelopmentApproach . . . . . . . . 108 VIII Contents 4.2 TheNextGenerationμHEMPT . . . . . . . . . . . . . . . . . . . 114 4.2.1 FullSizeNG-μHighEfficiencyMultistagePlasmaThruster (HEMPT) . . . . . . . . . . . . . . . . . . . . . . . . . . 117 4.2.2 MiniaturisedNG-μHEMPT. . . . . . . . . . . . . . . . . 128 4.3 NG-μHEMPTDevelopmentSummary . . . . . . . . . . . . . . . 141 5 ConclusionandOutlook 147 Bibliography 157 Appendix 167 List of Figures 1.1 LaserInterferometerSpaceAntenna(LISA)constellation . . . . . 2 1.2 SketchoftheLISAOrbit . . . . . . . . . . . . . . . . . . . . . . . 3 1.3 Summaryofthethrustnoiserequirements . . . . . . . . . . . . . 5 1.4 ImpressionoftheDarwinconfiguration . . . . . . . . . . . . . . 6 2.1 ExBdriftillustration . . . . . . . . . . . . . . . . . . . . . . . . 20 2.2 Visualisationofamagneticbottle . . . . . . . . . . . . . . . . . . 21 2.3 FEEPprinciple . . . . . . . . . . . . . . . . . . . . . . . . . . . . 23 2.4 Simplified view of a two gridded Radio Frequency Ion Thruster (RIT)system . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 25 2.5 SchematicoftheHEMPTconcept . . . . . . . . . . . . . . . . . . 26 2.6 HEMPTplasmapotential . . . . . . . . . . . . . . . . . . . . . . 28 2.7 Pendulumbalancestepresponse . . . . . . . . . . . . . . . . . . 32 2.8 Bodeplotofanarbitrarypendulumbalance . . . . . . . . . . . . 33 2.9 MechanicalBalanceConfiguration . . . . . . . . . . . . . . . . . 35 2.10 Faradaycupschematic . . . . . . . . . . . . . . . . . . . . . . . . 37 2.11 ExampleofFaradaycupmeasurement . . . . . . . . . . . . . . . 38 2.12 ExampleofaRPAmeasurement . . . . . . . . . . . . . . . . . . . 39 3.1 Insideviewofthemicro-Newtonthrustertestfacility . . . . . . . 43 3.2 Blockdiagramofelectricthrustertestfacilityconnections . . . . . 44 3.3 Illustrationofthevacuumfacility . . . . . . . . . . . . . . . . . . 47 3.4 Flowchartofthevacuumsetup . . . . . . . . . . . . . . . . . . . 49 3.5 Measurednoisespectraoftwodifferentcryocoolers . . . . . . . . 50 3.6 Crosssectionalsnapshotofthecustomcryopumpsystem . . . . 51 3.7 Flowchartoftheplasmadiagnosticsetup. . . . . . . . . . . . . . 54 3.8 IllustrationofthedevelopedFaradaycupunit . . . . . . . . . . . 55 3.9 Drawingoftheplasmadiagnosticassembly. . . . . . . . . . . . . 56 3.10 PictureofthedevelopedRetardingPotentialAnalyser(RPA) . . . 57 3.11 SketchoftheRPA . . . . . . . . . . . . . . . . . . . . . . . . . . 59 3.12 ResultoftheFaradaycupcalibration . . . . . . . . . . . . . . . . 61 3.13 Sketchofthependulumbalanceprinciple. . . . . . . . . . . . . . 63 3.14 Illustrationofthethrustbalancesetup . . . . . . . . . . . . . . . 65 X ListofFigures 3.15 PendulumBearingillustration . . . . . . . . . . . . . . . . . . . . 67 3.16 Illustrationofasinglependulumsubassembly . . . . . . . . . . . 68 3.17 Heterodynefrequencygenerationsetup. . . . . . . . . . . . . . . 70 3.18 Laserinterferometersketch. . . . . . . . . . . . . . . . . . . . . . 72 3.19 Illustrationofasinglependulumsubassembly . . . . . . . . . . . 73 3.20 Diagramoftheelectricalsignalflow . . . . . . . . . . . . . . . . 74 3.21 IllustrationoftheDifferentialWavefrontSensing(DWS) . . . . . 75 3.22 Blockdiagramofthemicro-Newtonthrustbalanceassembly . . . 76 3.23 Standardisedmeasurementrunflowchart . . . . . . . . . . . . . 78 3.24 ESCassemblyillustration . . . . . . . . . . . . . . . . . . . . . . 80 3.25 SketchofanElectroStaticComb(ESC) . . . . . . . . . . . . . . . 81 3.26 Figureofapendulumcalibrationrun . . . . . . . . . . . . . . . . 86 3.27 Resultofthependulumcalibration . . . . . . . . . . . . . . . . . 87 3.28 Longtermcalibrationresult . . . . . . . . . . . . . . . . . . . . . 88 3.29 Thrustbalanceperformancesummary . . . . . . . . . . . . . . . 89 3.30 Illustrationofthefrequencysweepused . . . . . . . . . . . . . . 91 3.31 Transferfunctionofthethrustbalance . . . . . . . . . . . . . . . 92 3.32 Postprocessingexample . . . . . . . . . . . . . . . . . . . . . . . 93 3.33 PicturesoftheRITμX . . . . . . . . . . . . . . . . . . . . . . . . 94 3.34 RITμXplumecharacterisationresult . . . . . . . . . . . . . . . . 95 3.35 Transferfunctionofthebalanceconfigurationused . . . . . . . . 96 3.36 Neutralgasthrustmeasurement . . . . . . . . . . . . . . . . . . . 97 3.37 DirectthrustmeasurementoftheRITμX . . . . . . . . . . . . . . 98 3.38 RITμX1μNstepping . . . . . . . . . . . . . . . . . . . . . . . . . 99 3.39 RITμX0:1μNstepping. . . . . . . . . . . . . . . . . . . . . . . . 100 3.40 ThrustnoiseperformanceofthetestedRITμX . . . . . . . . . . . 102 4.1 CrosssectionofEBB20 . . . . . . . . . . . . . . . . . . . . . . . 105 4.2 Summaryofthethrusterperformancesachieveduntil2013 . . . . 106 4.3 EBB20plumeshape . . . . . . . . . . . . . . . . . . . . . . . . . 107 4.4 EBB20magneticfieldtopology . . . . . . . . . . . . . . . . . . . 109 4.5 CrosssectionoftheEBB20MkII . . . . . . . . . . . . . . . . . . 111 4.6 Fluxdensitycomparison . . . . . . . . . . . . . . . . . . . . . . . 112 4.7 MagnetsComparison . . . . . . . . . . . . . . . . . . . . . . . . 113 4.8 NGmagneticfieldgeometry . . . . . . . . . . . . . . . . . . . . . 115 4.9 3Delectrontracinginsidethethruster . . . . . . . . . . . . . . . 116 4.10 DevelopedThrustermodelsillustration . . . . . . . . . . . . . . . 117 4.11 FullsizeNG-μHEMPTillustration . . . . . . . . . . . . . . . . . 118 4.12 PicturesoffiringfullsizeNG-μHEMPT . . . . . . . . . . . . . . 119 4.13 FullsizeNG-μHEMPToperationpointssummary . . . . . . . . . 120 ListofFigures XI 4.14 Thrusterignitionchart . . . . . . . . . . . . . . . . . . . . . . . . 121 4.15 FullsizeNG-μHEMPTthrustmeasurement . . . . . . . . . . . . 122 4.16 FullsizeNG-μHEMPTplumecharacterisationresult . . . . . . . 124 4.17 FullsizeNG-μHEMPTRPAmeasurement . . . . . . . . . . . . . 125 4.18 FullsizeNG-μHEMPTaccelerationefficiency . . . . . . . . . . . 126 4.19 IllustrationofminiNG-μHEMPT . . . . . . . . . . . . . . . . . . 129 4.20 Thrusterdischargechambercomparison . . . . . . . . . . . . . . 130 4.21 PicturesoffiringfullsizeNG-μHEMPT . . . . . . . . . . . . . . 131 4.22 MiniaturisedNG-μHEMPToperationpointssummary . . . . . . 132 4.23 miniHEMPTignition . . . . . . . . . . . . . . . . . . . . . . . . 134 4.24 MiniNG-μHEMPTthrustmeasurement . . . . . . . . . . . . . . 135 4.25 MiniNG-μHEMPTplumecharacterisation . . . . . . . . . . . . 136 4.26 MiniNG-μHEMPTaccelerationefficiency . . . . . . . . . . . . . 138 4.27 miniaturisedNG-μHEMPTthrustnoisemeasurement . . . . . . 140 4.28 SummaryoftheNG-μHEMPToperationspace . . . . . . . . . . 142 5.1 Summaryofthemeasuredthrustnoiseperformances . . . . . . . 150 5.2 IllustrationoftheThrustBalanceMkIV . . . . . . . . . . . . . . 154 5.3 IllustrationofthenewPlasmaDiagnosticAssembly . . . . . . . . 155 1 CombConfiguration . . . . . . . . . . . . . . . . . . . . . . . . . 167 2 ESCdisplacementversusrelativeerror . . . . . . . . . . . . . . . 168 3 ESCdisplacementversusrelativeerror . . . . . . . . . . . . . . . 169 4 ESCdisplacementversusrelativeerror . . . . . . . . . . . . . . . 170

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