Name: European Space Thermal Engineering Workshop 2019
Start: 2019-10-08T08:30:00+02:00
End: 2019-10-10T20:00:00+02:00
Location: ESA/ESTEC

European Space Thermal Engineering Workshop 2019

from Tuesday 8 October 2019 (08:30) to Thursday 10 October 2019 (20:00)

Monday 7 October 2019
Tuesday 8 October 2019

08:45 Registration
Registration
08:45 - 09:45
Room: Newton
09:45 Opening - Harrie Rooijackers (ATG-Europe)
Opening
- Harrie Rooijackers (ATG-Europe)
09:45 - 09:55
Room: Newton
09:55 ESA Missions and Thermal Technology Development Outlook - Stéphane Lapensee (ESA)
ESA Missions and Thermal Technology Development Outlook
- Stéphane Lapensee (ESA)
09:55 - 10:35
Room: Newton
10:35 Coffee Break
Coffee Break
10:35 - 11:00
11:00
11:00 - 13:00
Room: Newton
Contributions

11:00 MetOp-SG SCA Instrument Thermal Design and Verification - José María Garcia Garrido (Airbus Defence and Space S.a.U. Spain) Ulrich Rauscher (Airbus Defence and Space GmbH)

11:30 Thermal design and thermal verification tests of the Solar Orbiter Heat Shield - Claudio Damasio (ESA/ESTEC)

12:00 Thermal Design, Analysis and Validation Plan of the Thermal Architecture for the SMILE Satellite Payload Module - Lorena Del Amo Martin (Airbus)

12:30 The ATHENA Spacecraft - Thermal Design aspects - Moritz Branco (ESA)
13:00 Lunch
Lunch
13:00 - 14:00
14:00
14:00 - 16:00
Room: Newton
Contributions

14:00 Application and Testing of Self-Limiting Heaters for Satellite Thermal Control - Ulrich Rauscher (Airbus Defence and Space GmbH)

14:30 ADMATIS radiators and MLI: from development and qualification to flight - János SZŐKE (ADMATIS) Romain PEYROU-LAUGA (ESA)

15:00 Thermal Control Louvers application using Rosetta heritage - ISABEL SOTO (SENER Aeroespacial)

15:30 Two phase - Mechanically Pumped Loop (MPL) development - Alain CHAIX (Thales Alenia Space)
16:00 Coffee Break
Coffee Break
16:00 - 16:20
16:20
16:20 - 18:10
Room: Newton
Contributions

16:20 Methods to Improve Thermal Test Efficiency (MITTE) - Matthieu Rodriguez (Airbus DS)

16:50 Simulations of formation flying maneuvers of two spacecraft in ESATAN-TMS based on the development of a MATLAB/Simulink tool for defining the required inputs. - Pedro José Herráiz Alijas (SENER Aeroespacial) Natalia de Burgos (SENER Aeroespacial)

17:20 Flight correlation and characterisation of Sentinel-2A/B satellite thermal behavior - Martin Altenburg (Airbus)

17:45 Flight correlation and characterisation of Sentinel-2A/B MSI instrument thermal behavior - ARNAUD LEMOINE (AIRBUS)
18:10 Cocktail
Cocktail
18:10 - 19:30
Wednesday 9 October 2019
09:00
09:00 - 10:30
Room: Newton 1
Contributions

09:00 On-orbit Experiment of Oscillating Heat Pipe and Loop Heat Pipe - Atsushi Okamoto (JAXA)

09:30 Development of a Novel Positive Displacement Pump for Mechanically Pumped Loops - Charlton Castro (AVS Added Value Solutions)

10:00 Minimising Temperature Gradients Within an Optical Support Plate Using Active Thermal Control - Edward Nelson (Argotec)
09:00 - 10:30
Room: Newton 2
Contributions

09:00 Parametrisation of a Thermal Model with ESATAN Thermal Modelling Suite - Krzysztof Domanski (ITP Aero)

09:30 Systema-Thermica - Mathieu Lepilliez (Airbus Defence & Space)

10:00 Post-processing of Thermal Model Data with ESATAN Thermal Modelling Suite - James McIntosh (ITP Aero)
10:30 Coffee Break
Coffee Break
10:30 - 11:00
11:00
11:00 - 13:00
Room: Newton 2
Contributions

11:00 Toward The Integration of Aero-Thermodynamics and Space Debris Re-entry Capabilities within ESATAN-TMS - Alessandro Falchi (AVIO)

11:30 Development and verification of a linear conductor generator with different triangle calculation methods - Jan Philipp Moeller (FH Aachen - University of applied Sciences)

12:00 TROPICS: An interface between OCDT and ThermiCalc for accelerated thermal design - Tobias Flecht (PTScientists GmbH) Marcel Scherrmann (PTScientists GmbH)

12:30 MetOp SG MWI On Ground Calibration Targets: thermal analysis, design and development - Davide Rizzo (OHB Italia S.p.A.)
11:00 - 13:00
Room: Newton 1
Contributions

11:00 A synthesis of 3D MLI efficiency test in ESTEC Thermal Lab - Romain PEYROU-LAUGA (ESA)

11:30 HGAMA SOLAR SIMULATION TEST - Ander Pereda (SENER AEROESPACIAL)

12:00 Contact conductance of copper based brush thermal connections - Katja Janzer (ESA)

12:30 SAOCOM 1A TVAC and a low-power/hi-sensitivity thermal case study - Lucas Cubau (INVAP S.E.)
13:00 Lunch
Lunch
13:00 - 14:00
14:00
14:00 - 16:00
Room: Newton 2
Contributions

14:00 A Modular Approach to Thermal Modelling of CubeSats in ESATAN-TMS - Arne te Nijenhuis (NLR - Royal Netherlands Aerospace Centre)

14:30 Modular Parallel Micro Pump for Adaptive Thermal Control of CubeSats - Ramon van den Berg (NLR)

15:00 Radiative Surface Properties of a Trihedral Array for Lunar Thermal Control Applications - Colin Butler (University of Limerick)

15:30 The Application of a Thermal Mathematical Model during Lander Operations on the surfaces of Small Bodies - Michael Maibaum (German Aerospace Center)
14:00 - 14:30
Room: Newton 1
Contributions

14:00 Sentinel-1 thermally activated Separation Bracket - Arne Sauer (Airbus Defence and Space GmbH)
14:30
14:30 - 16:00
Room: Newton 1
Contributions

14:30 Flexible External Insulation (FEI) at ArianeGroup Bremen Development - Qualification and Application - Nihan Özerson-Yücel (ArianeGroup)

15:00 Development of Variable Emissivity Coating for Thermal Control - Jean-Paul Dudon (Thales Alenia Space)
16:00 Coffee Break
Coffee Break
16:00 - 16:30
16:30
16:30 - 18:00
Room: Newton 1
Contributions

16:30 Compact and lightweight two-phase pumped cooling system with 3D printed aluminium components - Henk Jan van Gerner (NLR)

17:00 Medium LHP state of the art - Typhaine Coquard (airbus defence and space)

17:30 A Separable Loop Heat Pipe for Cooling a Pressurised Cargo Module - Edward Nelson (Argotec)
16:30 - 18:00
Room: Newton 2
Contributions

16:30 Challenges implementing a stratospheric balloon ascent phase in ESATAN-TMS - David González-Bárcena (Universidad Politécnica de Madrid (IDR/UPM)) Javier Piqueras (Universidad Politécnica de Madrid)

17:00 Machine learning algorithms to develop predictive thermal tools for spacecraft simulations - Christian Semler (Maya HTT)

17:30 First steps of numerical simulation using Artificial Intelligence - Vincent Vadez (Dorea) Pierre Alliez (INRIA Sophia Antipolis)
18:00 Dinner
Dinner
18:00 - 21:00
Thursday 10 October 2019
09:00
09:00 - 10:00
Room: Newton
Contributions

09:00 JUICE (Jupiter Icy Moon Explorer) Instruments thermal control and interface - Romain Peyrou-Lauga (ESA)

09:30 Solution flexibility of HiPeR flexible radiators - Niels van der Pas (Airbus Defence and Space Netherlands)
10:00
10:00 - 11:00
Room: Newton
Contributions

10:00 Thermo-elastic test as part of ESA activity: Improvement of methodologies for thermo-elastic predictions and verification - Benoit Laine (ESA)

10:30 Correlation of a Thermal Model for Thermo-Elastic Distortion Predictions - Kimberly Rutherford (ESA)
11:00 Coffee Break
Coffee Break
11:00 - 11:30
11:30
11:30 - 13:00
Room: Newton
Contributions

11:30 Guidelines for accurate thermo-elastic analysis - Alexander van Oostrum (ATG Europe)

12:00 SINAS Made Simple - James Etchells (ESA) Simon Appel (ATG Europe for ESA)

12:30 SINAS: Benefits and points of attention - Alexander van Oostrum (ATG Europe)
13:00 Closure - Harrie Rooijackers (ATG-Europe)
Closure
- Harrie Rooijackers (ATG-Europe)
13:00 - 13:05
Room: Newton
13:05 Lunch
Lunch
13:05 - 14:00

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