Adaptive Structures and mechatronic components for vibration and shape control of satellite payloads (Englisch)
- Neue Suche nach: Baier, H.
- Neue Suche nach: Reindl, M.
- Neue Suche nach: European Space Agency
- Neue Suche nach: Fundacion INASMET
- Neue Suche nach: Baier, H.
- Neue Suche nach: Reindl, M.
- Neue Suche nach: European Space Agency
- Neue Suche nach: Fundacion INASMET
In:
Space mechanisms and tribology
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391-396
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2003
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ISBN:
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ISSN:
- Aufsatz (Konferenz) / Print
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Titel:Adaptive Structures and mechatronic components for vibration and shape control of satellite payloads
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Beteiligte:
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Kongress:European symposium; 10th, Space mechanisms and tribology ; 2003 ; San Sebastian, Spain
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Erschienen in:Space mechanisms and tribology ; 391-396
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Verlag:
- Neue Suche nach: ESA
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Erscheinungsdatum:01.01.2003
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Format / Umfang:6 pages
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ISBN:
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ISSN:
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Medientyp:Aufsatz (Konferenz)
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Format:Print
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Sprache:Englisch
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Schlagwörter:
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Datenquelle:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Inhaltsverzeichnis Konferenzband
Die Inhaltsverzeichnisse werden automatisch erzeugt und basieren auf den im Index des TIB-Portals verfügbaren Einzelnachweisen der enthaltenen Beiträge. Die Anzeige der Inhaltsverzeichnisse kann daher unvollständig oder lückenhaft sein.
- 3
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X-38 Landing gear qualification testingUrgoiti, E. / European Space Agency / Fundacion INASMET et al. | 2003
- 13
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Failure Analysis of International Space Station Control Moment GyroBurt, R. / Loffi, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 27
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Control Moment Gyro CMG 15-45S: a compact CMG product for agile satellites in the one ton classDefendini, A. / Faucheux, P. / Guay, P. / Bangert, K. / Heimel, H. / Privat, M. / Seiler, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 33
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Rotating electrical joints with continuous metallic connectionsMausli, P. A. / Feusier, G. / Gass, V. / European Space Agency / Fundacion INASMET et al. | 2003
- 41
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Influence of coatings and alloying on cold welding due to impact and frettingMerstallinger, A. / Semerad, E. / Dunn, B. D. / European Space Agency / Fundacion INASMET et al. | 2003
- 49
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The effects of vibration in air and in ultrahigh vacuum on solid lubricated bearingsTanaka, Y. / Obara, S. / Sasaki, A. / Imagawa, K. / Maniwa, K. / European Space Agency / Fundacion INASMET et al. | 2003
- 57
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The GERB De-Scan Mechanism - Lubricant Solution Development and In-orbit PerformancecSawyer, E. / Lewis, S. D. / European Space Agency / Fundacion INASMET et al. | 2003
- 65
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New Nanotechnology Solid Lubricants for Superior Dry LubricationFleischer, N. / Genut, M. / Rapoport, L. / Tenne, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 67
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The Vacuum Tribology Model (VTM) of TriboLABGarmendia, I. / Landaberea, A. / Anglada, E. / Fernandez-Sanz, R. / Santiago, R. / Herrada, F. / Encinas, J. M. / European Space Agency / Fundacion INASMET et al. | 2003
- 73
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Micro-Imager Dust Cover, Micro-Imager Contact Sensor, and Mossbauer Spectrometer Contact Sensor Mechanisms for the Mars Exploration RoversDougherty, S. P. / European Space Agency / Fundacion INASMET et al. | 2003
- 81
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Contraves optical terminal-coarse pointing assembly (CPA)Mussett, D. J. / Humphries, M. E. / Henzelin, F. / Szekely, G. / European Space Agency / Fundacion INASMET et al. | 2003
- 89
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Coarse Pointing and Fine Pointing Mechanism (CPA and FPA) for an Optical Communication LinkBarho, R. / Schmid, M. / European Space Agency / Fundacion INASMET et al. | 2003
- 97
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Design and Production of the Metop Satellite IASI Corner Cube MechanismsSpanoudakis, P. / Schwab, P. / Johnson, P. / European Space Agency / Fundacion INASMET et al. | 2003
- 107
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Low Shock Release Unit - easy resettable and 100% reusableMuller, J. / Zauner, C. / European Space Agency / Fundacion INASMET et al. | 2003
- 113
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Very low shock pyromechanismsSoulier, G. / Gaechter, J. P. / Puech, J. M. / European Space Agency / Fundacion INASMET et al. | 2003
- 121
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Pneumatic locking device for magnetic bearing reaction wheelPrivat, M. / Da Costa, A. / European Space Agency / Fundacion INASMET et al. | 2003
- 129
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Clamp Band Assembly for the Beagle 2 LanderHaslehurst, A. / European Space Agency / Fundacion INASMET et al. | 2003
- 139
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A new deployment concept for a space based SAR antennaVega, J. / Quiroz, H. / Kulichevsky, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 145
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Development Summary and Test Results of a 3 meter Unfurlable CFRP Skin Antenna ReflectorSchmid, M. / Barho, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 153
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Studies for Space-Based Deployable Sun ShieldsNurre, J. P. / European Space Agency / Fundacion INASMET et al. | 2003
- 163
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E3000 High Power SADM developmentBamford, S. / McMahon, P. / European Space Agency / Fundacion INASMET et al. | 2003
- 169
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Improved Characteristics of Slip Ring Assemblies Making use of Gold on Gold Metallic ContactsFeusier, G. / Mausli, P.-A. / Gass, V. / European Space Agency / Fundacion INASMET et al. | 2003
- 177
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A Mirror Control Mechanism for Space TelescopeCadiergues, L. / Bourdit, C. / Trouchet, D. / Larcher, V. / Sugranes, P. / Le Letty, R. / Barrillot, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 183
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Dual-axis single-mirror mechanism for beam steering and stabilisation in optical inter satellite linksCoppoolse, W. / Kreienbuehl, M. / Moerschell, J. / Dommann, A. / Bertsch, D. / European Space Agency / Fundacion INASMET et al. | 2003
- 191
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Large Deployable Antenna Reflector Trimming Mechanism LDA-RTMDomingo, M. / Vazquez, J. / European Space Agency / Fundacion INASMET et al. | 2003
- 201
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Mechanical Slit Mask Mechanism for the James Webb Space Telescope SpectrometerHenein, S. / Spanoudakis, P. / Schwab, P. / Giriens, L. / Lisowski, L. / Onillon, E. / Myklebust, L. / European Space Agency / Fundacion INASMET et al. | 2003
- 209
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Bipolar Electromagnetic Actuators and Approaches for their DesignRoschke, T. / Fraulob, S. / Bodrich, T. / Seiler, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 217
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Development of a cryogenic force actuatorNalbandian, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 223
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Surface-Micromachined and High-Aspect Ratio Electrostatic Actuators for Aeronatutic and Space Applications: Design and Lifetime ConsiderationsVescovo, P. / Joseph, E. / Bourbon, G. / Le Moal, P. / Minotti, P. / Hibert, C. / Pont, G. / European Space Agency / Fundacion INASMET et al. | 2003
- 231
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The Development of the SMOS-MIRAS Deployment SystemPlaza, M. A. / Martinez, L. / Cespedosa, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 239
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The ROSETTA Lander Anchoring SystemThiel, M. / Stocker, J. E. / Rohe, C. / Komle, N. I. / Kargl, G. / Hillenmaier, O. / Lell, P. / European Space Agency / Fundacion INASMET et al. | 2003
- 247
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Rosetta Deployable BoomsAndion, J. A. / Lopez, R. / Ybarra, G. / European Space Agency / Fundacion INASMET et al. | 2003
- 255
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Concurrent Actuator Development for the Mars Exploration Rover Instrument Deployment DeviceFleischner, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 265
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Evaporative Losses of Vacuum-compatible Oils Through Labyrinth SealsAnderson, M. J. / Freeman, S. / Roberts, E. W. / European Space Agency / Fundacion INASMET et al. | 2003
- 271
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Towards The Use of Commercial-Off-the-Shelf Motors in SpaceLewis, S. D. / Roberts, E. W. / Anderson, M. / European Space Agency / Fundacion INASMET et al. | 2003
- 279
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The Development of a Low Power Solar Array Drive MechanismWood, B. / Sutter, G. / Hamze, N. / European Space Agency / Fundacion INASMET et al. | 2003
- 285
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Flexure Pivot for Aerospace MechanismsHenein, S. / Spanoudakis, P. / Droz, S. / Myklebust, L. / Onillon, E. / European Space Agency / Fundacion INASMET et al. | 2003
- 289
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Mechanical Design and Test of Rosetta Platform LouvresOsle, M. D. / del Olmo, J. J. R. / European Space Agency / Fundacion INASMET et al. | 2003
- 293
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Design and testing of a spur gear system for cryogenic valve applicationsNomerange, P. / Bomal, J.-C. / Promper, C. / European Space Agency / Fundacion INASMET et al. | 2003
- 297
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Roller Screw Lifetime under Oscillatory Motion: From Dry to Liquid LubricationFalkner, M. / Nitschko, T. / Supper, L. / Traxler, G. / Zemann, J. V. / Roberts, E. W. / European Space Agency / Fundacion INASMET et al. | 2003
- 303
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Design Validation of a Cryogenic Joint for the Spatial Framework of HerschelPereira, C. / European Space Agency / Fundacion INASMET et al. | 2003
- 307
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Effectiveness of transfer film lubrication for ceramic pairs in sliding contact at 800^oC in vacuumSuzuki, M. / Aoki, Y. / European Space Agency / Fundacion INASMET et al. | 2003
- 311
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Wear-life of the molybdenum disulfide sputtered film under hyperthermal atomic oxygen bombardment: in-situ wear-life evaluationsTagawa, M. / Muromoto, M. / Hachiue, S. / Yokota, K. / Ohmae, N. / Matsumoto, K. / Suzuki, M. / European Space Agency / Fundacion INASMET et al. | 2003
- 315
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Hydrostatic lubrication in turbopumps of rocket enginesBassani, R. / Chiulli, E. / Piccigallo, B. / Staffilano, U. / European Space Agency / Fundacion INASMET et al. | 2003
- 319
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Ultra-High Vacuum friction experiments to simulate material transfer and wear of the Platinum-Rhodium proof-mass used in the GRADIO accelerometerFontaine, J. / Le Mogne, T. / Vargiolu, R. / Bodoville, G. / European Space Agency / Fundacion INASMET et al. | 2003
- 323
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Vacuum Tribological Behaviour of Self Lubricant Quasicrystalline Composite Coatingsde Blas, F. J. G. / Roman, A. / De Miguel, C. / Muelas, R. / Aguero, A. / European Space Agency / Fundacion INASMET et al. | 2003
- 329
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The effect of storage conditions on the Tribological properties of solid lubricantsIwaki, M. / Obara, S. / Imagawa, K. / European Space Agency / Fundacion INASMET et al. | 2003
- 333
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Vacuum tribology testing of alloyed MoS~2 films at VTM Model of TriboLABOnate, J. I. / Brizuela, M. / Bausa, M. / Garcia, A. / Braceras, I. / European Space Agency / Fundacion INASMET et al. | 2003
- 337
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Comparative Physical and Tribological Properties of Three Pennzane® Fluids, SHF X-1000, SHF X-2000 and SHF X-3000Venier, C. G. / Jones, W. R. / Jansen, M. J. / Marchetti, M. / European Space Agency / Fundacion INASMET et al. | 2003
- 341
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Two Cryogenic Mechanisms for Earth Based Infrared AstronomySchepis, J. P. / McClendon, M. W. / Webb, M. M. / Zewari, S. W. / Hylan, J. E. / Barthelmy, M. P. / MacKenty, J. / European Space Agency / Fundacion INASMET et al. | 2003
- 347
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Precision Optical Select Mechanisms for the GLAS and SOLSE2 InstrumentsBudinoff, J. G. / European Space Agency / Fundacion INASMET et al. | 2003
- 353
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A Space Qualified Mechanical Speed Regulator for deployable Devices that provides speed control without electrical powering or commandingNunez, A. / Perez, C. / Maldonado, A. / Plaza, M. A. / Cespedosa, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 357
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Application of Torque Margin Ratios for Eddy Current DampersStarin, S. / Rodriguez, T. / European Space Agency / Fundacion INASMET et al. | 2003
- 361
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Thermal Distortion Testing of a 90 degree Deployment HingeLininger, L. / European Space Agency / Fundacion INASMET et al. | 2003
- 365
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In orbit bonding (IOB) of long deployable StructuresSchmidt, T. / Seifart, K. / Eder, J. / Burger, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 371
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Design and Demonstration of Bolt Retractor Separation System for X-38 Deorbit Propulsion StageAhmed, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 379
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The Lifeline: Beagle2 Umbilical ConnectorRogers, A. J. / Standing, J. / European Space Agency / Fundacion INASMET et al. | 2003
- 387
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Caging Mechanisms for the Mars Exploration Rover Instrument Deployment DeviceBilling, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 391
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Adaptive Structures and mechatronic components for vibration and shape control of satellite payloadsBaier, H. / Reindl, M. / European Space Agency / Fundacion INASMET et al. | 2003
- 397
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Design and Test of Normally Centred Piezo Mechanisms and their Control ElectronicBarrilot, F. / Fabbro, H. / Le Letty, R. / Guay, P. / European Space Agency / Fundacion INASMET et al. | 2003
- 401
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Soft Stepping and Disturbance Compensation through Rotary Acceleration Signal ProcessingStarin, S. / Rodriguez, T. / European Space Agency / Fundacion INASMET et al. | 2003
- 405
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Electric Motor Designs for Attenuating Torque Disturbance in Sensitive Space MechanismsMarks, D. B. / Fink, R. A. / European Space Agency / Fundacion INASMET et al. | 2003
- 409
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Solar Paddle Actuator for Small Satellites Using Shape Memory Alloy II -Quantitative ExperimentsIwata, T. / Murakami, H. / Komoda, Y. / Ogawa, A. / European Space Agency / Fundacion INASMET et al. | 2003
- 413
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High-Speed Stepper Motor for MechanismOudet, J. F. / Pagnon, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 423
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Equipment damper original design and qualification resultsDemerville, T. / Guay, P. / European Space Agency / Fundacion INASMET et al. | 2003
- 431
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Electromechanical Design of a Drive Mechanism for the Rotation of the Spectrometer Wheel inside MEDET ExperimentCozzani, A. / Sarti, B. / Casarosa, G. / Ratti, F. / Appolloni, M. / European Space Agency / Fundacion INASMET et al. | 2003