Search Results:
# |
Title |
Authors |
Year: Location |
Link |
Views (since Oct-15) |
1 |
Euclid M2 Mirror Mechanism
| A. Artiagoitia, C. Compostizo, L Rivera | 2017:Hatfield |
|
279 |
2 |
Engineering Test Results of NELS Hold Down And Release System
| J. Augustijn, E. Bongers | 2017:Hatfield |
|
127 |
3 |
Gas Breakdown Mitigation in Satellite Slip-Rings
| F. Avino, D. Bommottet, B. Gafnet, A.A. Howling, P. Martens, I. Furno | 2017:Hatfield |
|
81 |
4 |
Jitter Characterization in Space Mechanisms
| L. Ayari | 2017:Hatfield |
|
104 |
5 |
Qualification of Euclid-Near Infrared Spectro-Photometer Cryomechanism
| J.C. Barriere, O. Corpace, A. Arhancet, D. Bachet, M. Berthé, M. Carty, B. Duboue, L. Dumaye, J. Fontignie, L. Gaillard, D.D. Huyhn, F. Le.Berrurier, Y. Le Noa, J. Martignac, M. Prieur, J.B. Mondier | 2017:Hatfield |
|
90 |
6 |
A Newly Discovered Branch of the Fault Tree Explaining Systemic Reaction Wheel Failures And Anomalies
| W. Bialke, E. Hansell | 2017:Hatfield |
|
146 |
7 |
Optical Ground Support Equipment for the Sentinel-4 Scanner Subsystem
| M. Bircher, D. Blum, Dr. U. Nguyen, B. Zahnd | 2017:Hatfield |
|
59 |
8 |
GOCI II Pointing Mechanism Development
| D. Blattes, F. Di Gesu, P. Coste | 2017:Hatfield |
|
115 |
9 |
New Understanding of Hubble Space Telescope Gyro Current Increase Led to a Method to Save a Failing Gyro
| K. Blumenstock | 2017:Hatfield |
|
62 |
10 |
Delayed Releases on Orbit - One Solved, One not Solved
| E. Boesiger, D. Gibbons | 2017:Hatfield |
|
81 |
11 |
Health Monitoring for Spacecraft Reaction Wheels
| D. Bojiloff, T. Häfner, R. Seiler | 2017:Hatfield |
|
83 |
12 |
LP-PWI Deployable Boom for the JUICE Mission – Innovative Features and Breadboard Model Development
| M. Borys, L. Wisniewski, J. Grygorczuk, T. Kucinski, E Ryszawa, K Bochra, M. Duda, J. Demming, T. Barcinski, R. LeLetty, J. Bergman, J. Wahlund, L Bylander | 2017:Hatfield |
|
102 |
13 |
Space Grease Tribological Behaviour for Reformulation: Numerical and Experimental Investigations
| M. Busquet, M. Renouf, D. Leveque, Y. Berthier, N. Bouscharain, J. Sicre | 2017:Hatfield |
|
85 |
14 |
Development of Advanced Lubricants for Space Mechanisms Based on Ionic Liquids
| M. Buttery, M. Hampson, A. Kent, C. Allegranza | 2017:Hatfield |
|
101 |
15 |
Adhesion Measurements in MoS2 Dry Lubricated Contacts to Inform Predictive Tribological Numerical Models: Comparison between Laboratory-Tested Samples and Ball Bearings from the NIRISS Mechanism
| G. Colas, S. Pajovic, A. Saulot, M. Renouf , Peter Cameron, A. Beaton, A. Gibson, T. Filleter | 2017:Hatfield |
|
79 |
16 |
Linear Actuator System for the Nasa Docking System
| B. Dick, C. Oesch, T. Rupp | 2017:Hatfield |
|
127 |
17 |
The Design, Development, Qualification and Delivery of the Solar Array Drive Assembly (SADA) for the Bepicolombo Mercury Transfer Module (MTM)
| J. Ekre, J. Mürer, M. Miler | 2017:Hatfield |
|
118 |
18 |
Optimagdrive: High Performance Magnetic Gears Development for Space Applications
| J. Esnoz-Larraya, I. Valiente-Blanco. C. Cristache, J. Sanchez-Garcia-Casarrubios, F. Rodriguez-Celis, E. Diez-Jimenez, J. Perez-Diaz | 2017:Hatfield |
|
82 |
19 |
Development and Testing of a High Temperature Shape Memory Actuator Using CN-250X for Hold Down and Release Mechanisms (HRM)
| F. Fouche, A. Hautcoeur, D. Chassoulier, A. Blanc, J. Sicre | 2017:Hatfield |
|
80 |
20 |
Investigation into the Dynamic Particle Generation of Lubricating Greases Used in Space Mechanisms
| J. Galary | 2017:Hatfield |
|
55 |
21 |
Design and Implementation of the Lightweight Advanced Robotic Arm Demonstrator (LARAD)
| M. Garland, E. Allouis., M. Rucinski, A. Coates, R. Marc, D. Lachat, A. Donchev, W. Tubby, J. Hampton, Á. Kisdi, M. Woods, S. Flitcroft, L. Tyler | 2017:Hatfield |
|
73 |
22 |
Encoder In-Orbit Calibration of the MTG Scanner
| A. Gonzalez-Elias, C. Tato-Ribera, S. Reguero Cachafeiro, L. Bouyeron | 2017:Hatfield |
|
71 |
23 |
Magneto-Resistive Angular Sensors for Space Applications: Results of Breadboard and EQM Testing and Lessons Learned
| R. Hahn, T. Schmidt, R. Slatter, B. Olberts, F. Romera | 2017:Hatfield |
|
51 |
24 |
Development of a Dual Released Lanyard Connector for Space Applications
| B. Hill | 2017:Hatfield |
|
34 |
25 |
Dual Stage Isolation - A Passive, Bi-Linear Application for Launch Load Attenuation and On-Orbit Jitter Mitigation
| J. Howat, P. Wilke, M. Mimovich, B. Allen, C. Borst, Y. Takei, S. Yasuda, K. Ishimura | 2017:Hatfield |
|
42 |
26 |
S3/OLCI and S4/UVN Calibration Mechanisms
| J. Jacobs, B. Marquet, J-Y. Plesseria | 2017:Hatfield |
|
27 |
27 |
Torque Enhancement of Dry Lubricated Harmonic® Drive Gears
| M. Jansson, Dr. H. Koenen, R.Noauer, G. Dallhammer, G. Mozdzen, A. Merstallinger | 2017:Hatfield |
|
84 |
28 |
Refocusing Mechanism for MeteoSat 3rd Generation
| P. Janu, C. Neugebauer, H. Plank, B. Strube | 2017:Hatfield |
|
70 |
29 |
Design and Test of a Scan Mechanism for Microwave Imaging Instruments
| I. Köker, C. Hehr, G. Parzianello | 2017:Hatfield |
|
91 |
30 |
High-Bandwidth & Compact Fine Steering Mirror Development for Laser Communications
| S. Kuiper, W. Crowcombe, J. Human, B. Dekker, E. Nieuwkoop, A. Meskers, G. Witvoet, L. Kramer, M. Lemmen, H. Lagemaat, W. van der Hoogt, M. van Koppen | 2017:Hatfield |
|
79 |
31 |
Development, Qualification & Manufacturing of Antenna Pointing Mechanism Rotary Actuators
| J-N. Lajoie, R. Horth, B. Lemelin-Auger, P. Gregorio | 2017:Hatfield |
|
108 |
32 |
Design and Analysis of a Novel Flexible Compliant Joint for Space Mechanisms
| E. Lamacchia, R. Edeson, M. Humphries | 2017:Hatfield |
|
130 |
33 |
The EUCLID VIS Read-Out Shutter Unit: A Low Disturbance Mechanism at Cryogenic Temperature
| C. Larcheveque, L. Genolet, E. Bozzo, S. Paltani, D. Manzoni, M. Castelli, J-P. Heurteau, C. Thomas, J. Constant, R. Michaud, A. Marrei, N. Martini, T. Verhegge | 2017:Hatfield |
|
47 |
34 |
Space Cooler Developments at Thales Cryogenics to Flight Tribological Failure Phenomena
| H. Leenders, G. de Jonge, P. Bollens | 2017:Hatfield |
|
45 |
35 |
Lean Production and Industrialisation of Space Mechanisms
| J. Lurie | 2017:Hatfield |
|
58 |
36 |
A Novel Hold Down & Release Mechanism Using Hook & Loop Technology for Small Deployable Arrays
| A. Malavart, M. Ferris, N. Philips | 2017:Hatfield |
|
101 |
37 |
Long Life Technology Combining Hybrid Ceramic Bearing and Passive Oil Feed System
| K. Maniwa, T. Nogi, S. Obara, K. Kitamura, K. Yamakawa, A. Koyama | 2017:Hatfield |
|
62 |
38 |
Test & Inspection Campaign of Surrey Satellite Technology Ltd First Geostationary Wheel
| S. McLaren | 2017:Hatfield |
|
43 |
39 |
In-Orbit Maintenance of the Rosetta Reaction Wheels (RWAs)
| P. McMahon, R. Seiler, A. Accomazzo, S. Lodiot, P. Van Put, R. Porta | 2017:Hatfield |
|
83 |
40 |
BEAGLE 2 – A Retrospective Look at the Beagle 2 Mechanisms Following Evidence of Successful Deployment
| P. McMahon, R. Slade, J. Clemmet | 2017:Hatfield |
|
71 |
41 |
Comparison of Multipoint Payload Separation Devices for Large Constellations. Discussion of Test Results for Non-Pyrotechnic Multipoint Release Mechanisms used for Payload Release
| A. Mejia, J. Sudick, G. Kaczynsky | 2017:Hatfield |
|
50 |
42 |
New Self Lubricating Polymer Matrix Composites for Journal and Ball Bearing Applications in Space (SLPMC2)
| A. Merstallinger, Z. Simon, G. Nuss, C.E. Paul, M. Palladino, M. Buttery | 2017:Hatfield |
|
70 |
43 |
Pointing Performance Simulation and Correlation of the Sentinel-4 Scanner Subsystem
| S. Michaud, F. Vedovati, J. Catalan, B. Zahnd, M. Herrscher, M. Omiciuolo, S. Patti | 2017:Hatfield |
|
65 |
44 |
Solar Orbiter Instrument Boom Subsystem
| X. Olaskoaga, J.A. Andion | 2017:Hatfield |
|
65 |
45 |
Parabolic Flight Test Campaign of a Breadboard of a Sampling Tool Mechanism for Low Gravity Bodies
| C. Ortega Juaristi, M.A. Carrera Astigarraga, E. Ocerin Martínez, J. Romstedt | 2017:Hatfield |
|
38 |
46 |
Analysis and Monitoring of Cage Dynamics in Ball Bearings for Space Applications
| M. Palladino, S. Giuseppe Neglia, M. Wygachiewicz | 2017:Hatfield |
|
60 |
47 |
Backlash-Free Gas-Tight High Precision Sample Handling Mechanisms – Lessons Learned from Qualification Testing & Design and Lessons Learned of the Core Sample Handling Mechanism (CSHS) on the ExoMars 2020 Rover
| R. Paul, T. Tattusch, D. Redlich, S. Ott, D. Dobrea, L. Richter, M. Thiel , A. Alegre Cubillo, H. Weisz, F. Musso, S. Durrant | 2017:Hatfield |
|
93 |
48 |
Design, Development and Testing of the Motorised Umbilical Separation Device
| O. Poyntz-Wright, W. Holmes, P. Doyle, G. Munro | 2017:Hatfield |
|
66 |
49 |
Sealing Cap for METIS Instrument in Solar Orbiter FDM Subsystem
| B. Provedo, G. Jaio, J. Vinals | 2017:Hatfield |
|
42 |
50 |
High Temperature Electromagnetic Actuator and Sampling Drill for Venus Exploration
| F. Rehnmark, E. Cloninger, C. Hyman, J. Bailey, N. Traeden, K. Zacny, K. Kriechbaum, J. Melko, B. Wilcox,, J. Hall, K. Sherrill | 2017:Hatfield |
|
49 |
51 |
Bi-Stable Shape Memory Alloy Shutter Mechanism Verification by Test
| S. Rieger, R. Barho | 2017:Hatfield |
|
48 |
52 |
MetOP Scan Mechanism (SCM) Development
| L. Rivera, C. Compostizo, G. Gonzalez, A. Altonaga, A. Artiagoitia | 2017:Hatfield |
|
76 |
53 |
Alignment of an Ultra-stable Articulated Deployment System for Antennas
| M. Robroek, M. Kroon, G. Borst, M. Grimminck | 2017:Hatfield |
|
64 |
54 |
Additively Manufactured and Topologically Optimised Compliant Mechanisms: Technological Assessment Approach, Latest Achievements and Current Work in Progress
| H. Saudan, L. Kiener, G. Perruchoud, K. Vaideeswaran, M. Mehdi Dadras | 2017:Hatfield |
|
70 |
55 |
Stainless Steel XD15NW Characterization for the use of Ball Bearings in the Space Environment
| F. Seguin-Henry, L. Cadiergues, A. Tesch, L. Gaillard, S. Dufrenoy, C. Lebreton, M. Maha, D. Buso, P. Durand | 2017:Hatfield |
|
53 |
56 |
Full Aperture Diffuser Assembly, Fully Redundant and High Reliable Optic Mechanism for EnMAP Mission
| S. Senese, M. Thiel, B. Konig, M. Sornig, S. Fischer, A. Bergander, S. Brunner, S. Muller, T. Schmidt, K. Zajac | 2017:Hatfield |
|
48 |
57 |
Supercam Autofocus Mechanism: COTS Equipment Design and Qualification Process for Space use of Ground Equipments
| M. Sodki | 2017:Hatfield |
|
50 |
58 |
DFKI-X: A Novel, Compact and Highly Integrated Robotics Joint for Space Applications
| R. Sonsalla, H. Hanff, P. Schberl, T. Stark, N. Mulsow | 2017:Hatfield |
|
69 |
59 |
Concept Assessment for a 2-Collinear-DoF Strut Prototype with Embedded Electromagnetic Shunt Dampers
| A. Stabile, G. Aglietti, G. Richardson, G. Smet | 2017:Hatfield |
|
29 |
60 |
Design and Development Implications of High Inertia Earth-Science Mechanism Actuator
| S. Starin, E. Harrington | 2017:Hatfield |
|
45 |
61 |
Development of a Mechanism for Space from a Newcomer’s Perspective
| R. Stewart, R. Barton, H. England, J. Glover, K. Hullah, I. Laidler | 2017:Hatfield |
|
94 |
62 |
Development Challenges of a Focus Mechanism Design for ExoMars Mission Submitted to the Harsh Martian Environment and Utilizing Off-the-Shelf Equipment
| A. Verhaeghe, G. Perruchoud, P. Schwab, M. Gumy | 2017:Hatfield |
|
73 |
63 |
Self-Lubricating Polymer Composites: using Numerical Tribology to Hightlight their Design Criterion
| M. Villavicencio, M. Renouf, A. Saulot, Y. Michel, Y. Maheo, G. Colas, T. Filleter, Y. Berthier | 2017:Hatfield |
|
63 |
64 |
First Real-Life Results of Novel Micro Vibration Measurement Facility
| S. Wismer, R. Messing, M. Wagner | 2017:Hatfield |
|
53 |
65 |
Design Features of Novel High Energy Impulsive Drive of Underactuated Mobile Robot for Planetary Exploration
| L. Wisniewski, J. Grygorczuk, D. Mege , J. Gurgurewicz | 2017:Hatfield |
|
101 |