Program
Final program at a glance
| Monday 22 | Tuesday 23 | Wednesday 24 | Thursday 25 | Friday 26 | |||||
|---|---|---|---|---|---|---|---|---|---|
| 8:30 | REGISTRATION and welcome coffee |
8:30 | S3: EXTREME ENVIRONMENTS |
8:30 | S6: GROUND TESTING (2) |
8:30 | S9: STANDARDS, REGULATIONS |
8:30 | S12: CONTAMINATION (3) |
| 10:10 | 10:10 | COFFEE BREAK | 10:10 | COFFEE BREAK | 10:30 | COFFEE BREAK | 10:10 | COFFEE BREAK | |
| 10:15 | OPENING SESSION | 10:30 |
Poster introductions |
10:30 |
Poster introductions |
10:50 |
Poster introductions |
10:30 | S13: FLIGHT EXPERIMENTS |
| 12:30 | LUNCH | 12:00 | LUNCH | 12:20 | LUNCH | 12:50 | LUNCH | 12:20 | LUNCH |
| 14:00 | S1: CONTAMINATION (1) |
13:30 | S5: CONTAMINATION (2) |
14:00 |
S8: New M&P (1) |
14:20 |
S11: New M&P |
||
| 15:40 | COFFEE BREAK | 15:50 | COFFEE BREAK | 16:00 | COFFEE BREAK | 16:20 | COFFEE BREAK | ||
| 16:00 | S2: SYNERGIES - CHARGING (1) Poster introductions |
16:10 | POSTER SESSION 1 | 16:20 | CONTAMINATION ROUND TABLE and POSTER SESSION 2 in // |
16:40 | POSTER SESSION 3 | ||
| 17:50 | Free evening | 18:30 | Welcome cocktail (at City hall) |
19:30 | Conference Dinner |
18:30 | Wine tasting session & Barbecue party |
Final technical program
|
MONDAY, JUNE 22 |
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From 8:30 |
REGISTRATION and Welcome Coffee |
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10:15 – 12:30 |
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10:15 – 10:30 |
Introduction - Welcome |
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10:30 – 11:10 |
On Overview of ESA's ATV missions to the ISS |
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11:10 – 11:50 |
Overview of Rosetta Mission and feedbacks |
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11:50 – 12:30 |
EOR: how severe can the radiation environment be? |
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12:30 – 14:00 |
LUNCH |
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14:00 – 16:00 |
Chairpersons: D. Faye, C. Soares |
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14:00 – 14:20 |
Assessment of materials with outgassing properties out of specifications |
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14:20 – 14:40 |
In-situ ice formation investigation |
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14:40 – 15:00 |
New development for particle deposition monitoring during space instrument integration in cleanroom |
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15:00 – 15:20 |
Investigation of the electron emission proprieties of Ag: from technical Ag surface to ion-cleaned Ag surface. |
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15:20 – 15:40 |
Cleanrooms for sensitive equipment and manufacturing processes regarding molecular organic contamination (MOC): |
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15:40 – 16:00 |
COFFEE BREAK |
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16:00 – 17:20 |
Session 2: SYNERGIES - CHARGING (1) Chairpersons: T. Paulmier, V. Perrin |
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16:00 – 16:20 |
Thermal performance degradation of spacecraft radiator by outgassing of adhesives in space environment |
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16:20 – 16:40 |
Improvements in Modeling Thruster Plume Erosion Damage to Spacecraft Surfaces |
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16:40 – 17:00 |
Material characterization and assessment for the JUICE mission |
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17:00 – 17:20 |
Influence of thermal treatment on electrical and physical properties of coated ceramics for spacecraft application |
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17:20 – 17:50 |
Short poster introductions: contamination , synergies |
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TUESDAY, JUNE 23 |
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8:30 – 10:10 |
Session 3: EXTREME ENVIRONMENTS Chairpersons: D. Nikanpour, M. Nikulainen |
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8:30 – 8:50 |
An overview of the latest materials engineering challenges for the preparation of ESA’s Mercury mission |
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8:50 – 9:10 |
Thermal radiative properties at very high temperatures of materials (pBN and refractory metals) for the Solar Probe Plus mission |
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9:10 – 9:30 |
Ceramics black surface treatment for extreme temperature applications |
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9:30 – 9:50 |
Synergy between temperature and high UV acceleration on mate |
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9:50 – 10:10 |
Behavior of high pressure vessels under an hypervelocity impact |
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10:10 – 10:30 |
COFFEE BREAK |
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10:30 – 12:00 |
Chairpersons: C. Semprimoschnig |
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10:30 – 10:50 |
Particle flux effects on physico-chemical polymer degradations |
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10:50 – 11:10 |
Characterisation of surface properties of laser retro-reflector retrieved from the International Space Station |
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11:10 – 11:30 |
Comparative testing and evaluation of vulnerable external infrastructure materials and components for lunar applications |
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11:30 – 12:00 |
Short poster introductions: ground testing |
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12:00 – 13:30 |
LUNCH |
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13:30 – 15:50 |
Chairpersons: M. van Eesbeek |
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13:30 – 13:50 |
Evaluation of the contamination impact on various spacecraft instruments |
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13:50 – 14:10 |
Recent advances in numerical simulation for outgassing at Airbus Defence and Space |
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14:10 – 14:30 |
Numerical calculations of optical properties of silicone-contamination films |
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14:30 – 14:50 |
UV fixation of molecular contamination: numerical implementation and validation of a physical model |
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14:50 – 15:10 |
Analytical results on the optical influence of UV- and AO-irradiated silicone contaminants |
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15:10 – 15:30 |
Understanding the effect of material selection and testing on the long-term degradation of optical payloads |
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15:30 – 15:50 |
Collaborative activities between JAXA and ESA/ESTEC in materials and contamination fields |
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15:50 – 16:10 |
COFFEE BREAK |
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16:10 |
GROUND TESTING
Strategies for improvement of radiation resistance of white ceramics coatings: experimental results and degradation mechanisms
V. Rejsek, S. Duzellier, S. Lewandowski, T. Paulmier, C. Pons - ONERA
C. Tonon, S. Dagras, C. Perrin - Airbus Defence and Space
C. Casademont, F. Ansart, L. Arurault, P. Lenormand - CIRIMAT
E. Amorim - ESA/ESTEC
Development of new irradiation facilities for material testing
J. Eck, D. Lavielle, M. Thibaut - TRAD
ESTEC's STAR-II facility
A. Polsak, B. Bras, H. Blaauw, C. Semprimoschnig - ESA/ESTEC
Lifetime prediction of scotchweld EC 2216 B/A epoxy adhesive for telecommunications applications using time temperature superposition technique
V. Cesar-Auguste, J. Williamson, C. Semprimoschnig, J.M. Perdigues Armengol - ESA-ESTEC
Induction periods in the kinetics of mass losses of polymeric materials during their destruction by VUV radiation and fast atomic oxygen
V. Skurat, V.L. Talrose - Institute for Energy Problems of Chemical Physics, Russian Academy of Sciences
First results of in-situ Raman spectroscopy measurements in the STAR-II facility at ESTEC-ESA
B. Bras, Y. Butenko, C. Semprimoschnig – ESA-ESTEC
Study on the mechanical property and degradation mechanism of polyimide film in space environments
Z. Shen - Beijing Institute of Spacecraft Environment Engineering
Mechanical testing and characterization of full size thin shell CFRP booms for the DLR solar sail demonstrator Gossamer-1
M. E. Zander - DLR – IAF
M. Sinapius - IAF
C. Hühne - DLR
On ground smart test rig for the verification and evaluation of metallic and ceramic materials testing in space propulsion relevant environment
S. Beyer, S. Schmidt-Wimmer, L. Wermuth - Airbus Defence and Space
New developments in space environment simulation equipment: update
J. Kleiman, S. Horodetsky, V. Issoupov, V. Verba - Integrity Testing Laboratory Inc.
Studies on degradation effects of indium tin oxide coated aluminized polyimide thin films under UV and proton radiation with the Complex Irradiation Facility
M. Dembska - DLR
Degradation of Spacecraft Thermal Control Materials under MEO Radiation Environment
Y. Ding, Z. Shen, X. Nie, Y. Zhnag - Beijing Institute of Spacecraft Environment Engineering
Large structures mechanical and electrical test at cyrogenic temeperatures
A. Carpio Rovira, A. Chapron - Applus Laboratories
Study on degradation mechanisms of ZnO-pigmented thermal control white paints in different space environments
Z. Shen, Y. Ding - Beijing Institute of Spacecraft Environment Engineering
The impact of Boron Nitride Filler on the Performance of Silicone Adhesives Under Cryogenic Conditions
J. Williamson, Y. Goebel, C. Semprimoschnig - ESA
Space materials and flight hardware compatibility with sterilization process
D.B. Margheritis, E.A. Nistico - Thales Alenia Space Italia S.p.a.
Space materials and flight hardware constraints arisen from biological contamination requirements
D.B. Margheritis, E.A. Nistico - Thales Alenia Space Italia S.p.a.
Simulation of the environmental conditions for plant growth on mars
Dmitry Horodetsky and Jacob I. Kleiman - Integrity Testing Laboratory Inc.,
CONTAMINATION
Contamination risks related to additive manufacturing
D. Faye - CNES
K. Kiryukhina - FIALAB
F. Clément - CNES
Evolved gas estimation based on mass and surface area of organic materials
N. Baba - JAMSS
Y. Kimoto - JAXA
Assessment to determine the efficiency of the bake out conducted using parameters obtained from dynamic outgassing test
O. Ergincan, P. de Heij, R. Rampini - ESTEC
Optical materials analyses following laser induced damage in the Uvfrequency domain
Y. Butenko, A. Tighe, L. Mondin, C. Heese, A. Ciapponi, T. Ivanov, D. Wernham - ESA-ESTEC
Outgassing properties of space-bound materials
V. Issoupov, S. Horodetsky, J. Kleiman - Integrity Testing Laboratory Inc.
Air toxicity lessons learned and system impact from ATV 1-5
T. Rohr, C. Semprimoschnig, M. Stienstra, A. Bolkhovitinov - ESA
Photochemically enhanced contamination - synergetic effects between UV and outgassing of organic materials
N. Dias, L. Levan, R. Rampini - ESA / ESTEC
Improved long term outgassing predictions for materials with two distinct outgassing regimes
P. de Heij and R. Rampini- ESA / ESTEC
SYNERGIES AND CHARGING
Electrostatic discharges in spacecraft solar array protective coatings under electron radiation
R. Khasanshin - OAO "Kompozit"
L. Novikov - Lomonosow Moscow State Univ.y, Skobeltsyn Inst. of Nuclear Physics
Dielectric properties of white ceramic coatings
V. Cesar-Auguste, E. Amorim, C. Semprimoschnig - ESA-ESTEC
Analysis of mass loss of a polymeric composite under combined action of electron, proton and electromagnetic radiations
R. Khasanshin, A. Galygin - OAO "Kompozit"
Basic aspects of the assessment of material degradation in long-term missions in the Moon environment and outer space: the radiation-chemical approach
V. Feldman, A. Milinchuk - Lomonosov Moscow State University
Electrical property of ITO/kapton/Al anti-static thermal control coating in space radiation environments
X. Qiu, Y. Zhou, S. Bai - Nanchang Institute of Technology
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WEDNESDAY JUNE 24 |
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8:30 – 10:10 |
Chairpersons: S. Duzellier, M. Tagawa |
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8:30 – 8:50 |
An in-situ study on the thermal and UV degradation of space-grade silicones |
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8:50 – 9:10 |
Black & white thermal control coatings |
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9:10 – 9:30 |
Space environmental simulation on bulk alumina |
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9:30 – 9:50 |
Space environmental qualification of novel candidate materials for multi-layer insulation |
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9:50 – 10:10 |
Research on thermal control material impact effect by micron space debris |
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10:10 – 10:30 |
COFFEE BREAK |
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10:30 – 12:30 |
Session 7: SYNERGIES – CHARGING (2) Chairpersons: C. Puig, J.-F. Roussel |
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10:30 – 10:50 |
Spacecraft charging sensitivity to material properties |
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10:50 – 11:10 |
Effect of space environment on the electric properties of space-used materials |
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11:10 – 11:30 |
Influence of high-energy electron irradiation on the electrical properties of a space-used silicone elastomer |
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11:30 – 11:50 |
Study of secondary arc occurrence on aged “grouted” solar cell coupons |
| 11:50 - 12:10 |
Ion Beam Treatment of GEO Solar Array's flexible cable Conductors For Surface Charge Dissipation In Long-term Missions |
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12:10 – 12:30 |
Short poster introductions: new M&P |
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12:30 – 14:00 |
LUNCH |
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14:00 – 16:00 |
Chairpersons: C. Durin, I. Gouzman |
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14:00 – 14:20 |
CNT-polyimide nanocomposites for space applications |
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14:20 – 14:40 |
Fast-curing process for MAP thermal control coatings |
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14:40 – 15:00 |
Design and measurement of radiowave transmissive thermal control mirror |
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15:00 – 15:20 |
Stabilization to UV of polysiloxanes in geostationary environment |
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15:20 – 15:40 |
Development of nano-hybrid transparent polymer films |
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15:40 – 16:00 |
Short poster introductions: new M&P |
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16:00 – 16:20 |
COFFEE BREAK |
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16:20 |
NEW M&P
Materials characterisation of ALTA white paint coatings for small Geo mission
C. Mooney, J. Williamson, C. Semprimoschnig - ESA
The feasibility study of thermo-chromic paints for space usage as thermal control materials
M. Iwata, H. Ishihara - Kyushu Institute of Technology
A. Hasegawa - PILOT Corporation
Y. Shibahashi - The PILOT Ink Co. Ltd.
Development of space-qualified photocurable silsesquioxane-coated polyimide films
Y. Kimoto - JAXA
T. Fujita, N. Furuta, A. Kitamura, H. Suzuki - Toagosei Co., Ltd.
J. Ishizawa - JAXA
A black thermal control surface for the Solar Orbiter
B. Twomey - Enbio
K. Doherty - University College Dublin
S. McGlynn, J. Carton - Enbio
A. Norman - ESA
T. McCaul - Airbus
K. Stanton - University College Dublin
Enhancement of conductive lubricant films with CNT in space environment
K. Matsumoto, Y. Ohkawa - JAXA
M. Kawamura - Kawamura Research Laboratories, Inc.
Qualification of low and high emissivity coatings for performance enhancement of Sentinel 4
M. Pitzing, M. Graupner - Jena-Optronik
K. Shabtai, D. Katsir - Acktar Ltd.
Novel high specific stiffness materials for space applications
G. Mozdzen, M. Scheerer - Aerospace & Advanced Composites GmbH
A. Norman - ESA-ESTEC
E. Neubauer - RHP-Technology GmbH
H.G. Wulz - RTBV GmbH
A. Merstallinger, V. Liedtke - Aerospace & Advanced Composites GmbH
A structural and thermal evaluation of a CFRP material using K13C2U high thermal conductivity pitch fibre
T. Mccaul, K. Hassell - Airbus Defence and Space Ltd.
Organic semiconducting single crystals for a novel generation of large area, low-weight, room temperature radiation detectors
B. Fraboni, A. Ciavatti, L. Basirico – Dpt. of Physics and Astronomy – Univ. of Bologna
A. Fraleoni-Morgera – Dpt. of Engineering and Architecture – Univ. of Trieste
Space FML, a new family of space materials - Properties and performances of GLARE 1
J.W. Gunnink, J. Homan, P. Brand, J. Frudiger - GTM Advanced Structures
A. Tesch, T. Ghidini - ESA-ESTEC
Innovative silicone adhesives for process improvements
N. Zambon, J. Nguyen, V. Malave - NuSil Technology
Validation of a high temperature shape memory alloy for space applications
M. Collado, N. Nava, C. Rivera - Arquimea Ingeniería, SL
I. López-Ferreño, J. San Juan - Dpto. Física de la Materia Condensada, Univ. del País Vasco
Nanocrystalline glass-ceramic scintillators
D. de Faoite, O. Roberts, L. Hanlon, A. Ulyanov, S. McBreen, K. Stanton - UCD School of Mechanical and Materials Engineering, Univ. College Dublin
Design of microstructure and functional material properties by using rapid hot pressing/rapid sinter pressing
E. Neubauer, M. Kitzmantel, G. Kladler - RHP-Technology GmbH
Spray aerogel for launch vehicle cryogenic tanks
F. Conceição, M. Ochoa, R. Patricio - Active Aerogels
C. Semprimoschnig - ESA-ESTEC
Supplementary power harvesting for spacecrafts on flight using carbonaceous compound considering space environment
D.W. Kim - Seoul National University
J.P. Kim - Pusan National University
D.C. Shin - Koje Colledge
T.G. Kim - Pusan National University
Y.H. Kim - Seoul National University
Advanced aluminium based material for cryo-reservoir applications
V. Liedtke, M. Scheerer, G. Mozdzen, N. Stelzer - Aerospace & Advanced Composites GmbH
G. Atxaga, C. Jimenez - TECNALIA
A. Norman - ESA/ESTEC
B. Arregi - TECNALIA
Proton radiation damage on flexible, low-voltage organic thin-film transistors
B. Fraboni, A. Basile, L. Basirico, T. Cramer – Dpt. of Physics and Astronomy – Univ. of Bologna
P. Cosseddu, A. Bonfiglio – Dpt. of Electrical and Electronic Engineering – Univ. of Cagliari
S. Gerardin, M. Bagatin, A. Paccagnella – Dpt. of Information Engineering, Univ. of Padova
Thermally induced dynamics of solar panels with variable stiffness composite reinforced with curvilinear fibers
S.M. Hamza-Cherif - Dpt. of Mechanical Eng., Faculty of Technology, Univ. of Tlemcen
High mobility oxide semiconductors for light-weight, large-area electronics in radiation harsh environments
T. Cramer, A. Sacchetti - Università di Bologna
M.T. Lobato, A. Rovisco, J. Martins, P. Barquinha, E. Fortunato, R. Martins - Universidade Nova de Lisboa
B. Fraboni - Università di Bologna
Demonstration and challenges for joining technology based on direct bonding usable for construction of (large) structures in space
H. Fischer, E. Gelinck - TNO
C. Semprimoschnig - ESA/ESTEC
M. van Munster, J. van der Heijden - XYCARB
|
THURSDAY JUNE 25 |
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8:30 – 10:10 |
Session 9: STANDARDS, REGULATIONS Chairpersons: N. Baba, T. Rohr |
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8:30 – 8:50 |
Chinese standard test method for spacecraft thermal control coatings |
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8:50 – 9:10 |
Development policy and introduction of ISO16378 “Measurements of thermo-optical properties” |
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9:10 – 9:30 |
Environmental impact risk analysis, induced by spacecraft elements surviving an atmospheric re-entry |
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9:30 – 9:50 |
A method to customise qualification of substitutes in case of materials or processes obsolescence |
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9:50 – 10:10 |
Impact of REACH legislation on European space programmes |
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10:10 – 10:30 |
MATREX - Material Recording Experience: CNES materials database for space applications |
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10:30 – 10:50 |
COFFEE BREAK |
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10:50 – 12:50 |
Session 10: AO – LEO – REENTRY Chairpersons: E. Grossman, T. Minton |
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10:50 – 11:10 |
Pyrolysis of Phenolic Impregnated Carbon Ablator (PICA) |
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11:10 – 11:30 |
Hybrid ablative/ceramic thermal protection system: mission, materials selection, interface development |
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11:30 – 11:50 |
Oxidation of carbon at high temperatures representative of a re-entry environment |
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11:50 – 12:10 |
Effect of high-energy inert gas collisions on the atomic oxygen-induced polymer erosion |
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12:10 – 12:30 |
Simulation of atomic oxygen behavior using the NC-DSMC method in the Combined Space Effects Test Facility |
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12:30 – 12:50 |
Short poster introductions: AO-LEO-Reentry, standards , flight exper. |
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12:50 – 14:20 |
LUNCH |
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14:20 – 16:20 |
Chairpersons: J. Kleiman, S. Remaury |
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14:20 – 14:40 |
Liquid phase deposition of space durable antistatic tin oxide coating on polyimide |
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14:40 – 15:00 |
A high-temperature conductive white thermal control surface for the Solar Orbiter |
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15:00 – 15:20 |
White inorganic plasma electrolytic oxidation coating for spacecrafts |
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15:20 – 15:40 |
Development of silicone adhesives with thermal and electrical properties |
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15:40 – 16:00 |
Particulate Cleanliness and Cleaning Validation for Space Applications |
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16:00 – 16:20 |
Short poster introductions: extreme environments |
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16:20 – 16:40 |
COFFEE BREAK |
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16:40 |
EXTREME ENVIRONMENTS
A new satellite system-level m/od impact risk assessment tool
C. Théroude, G. Chanteperdrix - Airbus Defence and Space
A. Merle - Atos
Behavior of high pressure vessels under an hypervelocity impact
P.L. Hereil, J. Mespoulet, F. Plassard - THIOT INGENIERIE
Challenges in designing dust particle sources for simulated planetary environmental testing
J. Kleiman, S. Horodetsky, V. Issoupov - Integrity Testing Laboratory Inc.
High temperature material assessment and approval
F. Panin - ESA
A. Leupolz - Airbus Defence and Space GmbH
Acktar magic black coating for the challenging environmental conditions of METIS
L. Montemurro, F. Zanetti - CGS
A. Simone, T. Schillaci - TAS-I
M. Castronuovo - ASI
D. Katsir, K. Shabtai - Acktar Ltd.
Plasma sprayed UHTC coatings for rocket throat carbon based materials
R. Marocco - AVIO
M. Tului, I. Moretti - Centro Sviluppo Materiali
Thermo-structural modelling of a plasma discharge tube for the variable specific impulse magnetoplasma rocket
D. de Faoite, D. Browne - UCD School of Mechanical and Materials Eng., Univ. College Dublin
J.I. Del Valle Gamboa - Ad Astra Rocket Company
K. Stanton - UCD School of Mechanical and Materials Eng., Univ. College Dublin
AO - LEO - REENTRY
Resistack: a new detector for atomic oxygen
S. Duzellier, S. Soonckindt, J.P. Chardon - ONERA
E. Laurent - CNES
Collision-induced oxidation of Si atoms embedded in carbon-based materials
M. Tagawa, D. Watanabe, Y. Furuyama - Kobe University
K. Kanda - The University of Hyogo
A. Yoshigoe, Y. Teraoka - Japan Atomic Energy Agency
K. Matsumoto - JAXA
Laser-detonation beam facilities for sub-LEO material erosion studies
K. Yokota, K. Ide, Y. Yamasaki, A. Hatsuda, M. Tagawa - Kobe University
Investigation of atomic oxygen and hypervelocity impact on polymer-based nanocomposites
L. Novikov, E. Voronina, V. Chernik, I. Ermolaev - Lomonosov Moscow State Univ
K. Vernigorov, M. Yablokova, K. Yakovlev - Lomonosov Moscow State University
ATOX erosion of polymers: some results and comparison of in-orbit data and on-ground data.
E. Laurent, J.M. Desmarres - CNES
Application of the results obtained in the LEO environment for prediction of the material behavior in future missions exploring Moon and outer space: a critical view.
A. Milinchuk, V. Feldman - Lomonosov Moscow State University
High absorptance coatings for GHGSAT nanosatellite
V. Latendresse, J. Lavoie, R. V. Kruzelecky, W. Jamroz - MPB Communications
J. McKeever - GHGSat Inc.
V. Isbrucker - Isbrucker Consulting Inc.
D. Katsir, K. Shabtain – Acktar Ltd.
STANDARDS
Innovative thermal management concepts and material solutions for future space vehicles
J. Barcena, C. Jimenez - Tecnalia
B. Esser, A. Gülhan, M. Kuhn, I. Petkov, V. Hannemann - DLR
A. Okan, S. Ontac - Tübitak
J. Merrifield - Fluid Gravity Engineering
S. Gianella - Erbicol SA
A. Ortona, M. Barbato, L. Ferarri - ICIMSI-SUPSI
V. Liedtke- Advanced Aerospace Composites
D. Francesconi, D. Santella, M. Portaluppi - Thales Alenia Space
T. Hideyuki - JAXA
FLIGHT EXPERIMENTS
Device for measuring the micro-meteoroid environment in near-Earth space
A. Telegin, N. Semkin - SSAU
L. Novikov - MSU SINP
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FRIDAY JUNE 26 |
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8:30 – 10:10 |
Chairpersons: Y. Goueffon, R. Rampini |
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8:30 – 8:50 |
In-situ optical characterization of outgassed compounds |
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8:50 – 9:10 |
Development of new apparatus to measure the optical properties of deposited molecular contaminants |
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9:10 – 9:30 |
Evaluation of QCM thermogravimetric analysis (QTGA) data for re-emission modeling |
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9:30 – 9:50 |
Simulation of outgassing test by vacuum TGA |
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9:50 – 10:10 |
In situ real time quantitative and qualitative monitoring of molecular contamination by coupling TGA and RGA: |
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10:10 – 10:30 |
COFFEE BREAK |
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10:30 – 12:30 |
Session 13: FLIGHT EXPERIMENTS Chairpersons: R. Briet, Y. Kimoto |
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10:30 – 10:50 |
New concept of the THERME experiment for thermal coatings ageing measurement in LEO and GEO |
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10:50 – 11:10 |
IST (in-flight experiment with space materials using THERME): in-orbit experimental result over 30 months |
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11:10 – 11:30 |
Aging of thermal coatings on LEO sun-synchronous orbits: in-flight measurements and modelling |
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11:30 – 11:50 |
Micromechanical testing of Teflon® Fluorinated Ethylene Propylene (FEP) retrieved from Hubble Space Telescope (HST) |
|
11:50 – 12:10 |
Space debris experiment SODAD on SAC-D: analysis of in flight data |
|
12:10 – 12:20 |
Conclusions and closure |
|
12:20 – 13:45 |
LUNCH |