The Vacuum Tribology Model (VTM) of TriboLAB (English)
- New search for: Garmendia, I.
- New search for: Landaberea, A.
- New search for: Anglada, E.
- New search for: Fernandez-Sanz, R.
- New search for: Santiago, R.
- New search for: Herrada, F.
- New search for: Encinas, J. M.
- New search for: European Space Agency
- New search for: Fundacion INASMET
- New search for: Garmendia, I.
- New search for: Landaberea, A.
- New search for: Anglada, E.
- New search for: Fernandez-Sanz, R.
- New search for: Santiago, R.
- New search for: Herrada, F.
- New search for: Encinas, J. M.
- New search for: European Space Agency
- New search for: Fundacion INASMET
In:
Space mechanisms and tribology
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67-72
;
2003
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ISBN:
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ISSN:
- Conference paper / Print
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Title:The Vacuum Tribology Model (VTM) of TriboLAB
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Contributors:Garmendia, I. ( author ) / Landaberea, A. ( author ) / Anglada, E. ( author ) / Fernandez-Sanz, R. ( author ) / Santiago, R. ( author ) / Herrada, F. ( author ) / Encinas, J. M. ( author ) / European Space Agency / Fundacion INASMET
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Conference:European symposium; 10th, Space mechanisms and tribology ; 2003 ; San Sebastian, Spain
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Published in:Space mechanisms and tribology ; 67-72
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Publisher:
- New search for: ESA
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Publication date:2003-01-01
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Size:6 pages
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ISBN:
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ISSN:
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Type of media:Conference paper
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Type of material:Print
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Language:English
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Keywords:
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Source:
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Table of contents conference proceedings
The tables of contents are generated automatically and are based on the data records of the individual contributions available in the index of the TIB portal. The display of the Tables of Contents may therefore be incomplete.
- 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
-
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
-
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
-
Precision Optical Select Mechanisms for the GLAS and SOLSE2 InstrumentsBudinoff, J. G. / European Space Agency / Fundacion INASMET et al. | 2003
- 353
-
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
-
Application of Torque Margin Ratios for Eddy Current DampersStarin, S. / Rodriguez, T. / European Space Agency / Fundacion INASMET et al. | 2003
- 361
-
Thermal Distortion Testing of a 90 degree Deployment HingeLininger, L. / European Space Agency / Fundacion INASMET et al. | 2003
- 365
-
In orbit bonding (IOB) of long deployable StructuresSchmidt, T. / Seifart, K. / Eder, J. / Burger, F. / European Space Agency / Fundacion INASMET et al. | 2003
- 371
-
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
-
Caging Mechanisms for the Mars Exploration Rover Instrument Deployment DeviceBilling, R. / European Space Agency / Fundacion INASMET et al. | 2003
- 391
-
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
-
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
-
Soft Stepping and Disturbance Compensation through Rotary Acceleration Signal ProcessingStarin, S. / Rodriguez, T. / European Space Agency / Fundacion INASMET et al. | 2003
- 405
-
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
-
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