European Space Thermal Engineering Workshop 2019

Speaker List

• Pierre Alliez (INRIA Sophia Antipolis)
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    First steps of numerical simulation using Artificial Intelligence

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

• Simon Appel (ATG Europe for ESA)
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    SINAS Made Simple

• Moritz Branco (ESA)
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    The ATHENA Spacecraft - Thermal Design aspects

• Colin Butler (University of Limerick)
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    Radiative Surface Properties of a Trihedral Array for Lunar Thermal Control Applications

• Charlton Castro (AVS Added Value Solutions)
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    Development of a Novel Positive Displacement Pump for Mechanically Pumped Loops

• Alain CHAIX (Thales Alenia Space)
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    Two phase - Mechanically Pumped Loop (MPL) development

• typhaine coquard (airbus defence and space)
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    Medium LHP state of the art

• Lucas Cubau (INVAP S.E.)
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    SAOCOM 1A TVAC and a low-power/hi-sensitivity thermal case study

• claudio damasio (ESA/ESTEC)
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    Thermal design and thermal verification tests of the Solar Orbiter Heat Shield

• Natalia de Burgos (SENER Aeroespacial)
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    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.

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

• Krzysztof Domanski (ITP Aero)
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    Parametrisation of a Thermal Model with ESATAN Thermal Modelling Suite

• jean-paul Dudon (THALES)
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    Development of Variable Emissivity Coating for Thermal Control

• James Etchells (ESA)
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    SINAS Made Simple

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

• Tobias Flecht (PTScientists GmbH)
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    TROPICS: An interface between OCDT and ThermiCalc for accelerated thermal design

• José María Garcia Garrido (Airbus Defence and Space S.a.U. Spain)
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    MetOp-SG SCA Instrument Thermal Design and Verification

• David González-Bárcena (Universidad Politécnica de Madrid (IDR/UPM))
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    Challenges implementing a stratospheric balloon ascent phase in ESATAN-TMS

• Pedro José Herráiz Alijas (SENER Ingeniería y Sistemas)
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    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.

• Katja Janzer (ESA)
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    Contact conductance of copper based brush thermal connections

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

• Stéphane Lapensee (ESA)
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    ESA Missions and Thermal Technology Development Outlook

• ARNAUD LEMOINE (AIRBUS)
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    Flight correlation and characterisation of Sentinel-2A/B MSI instrument thermal behavior

• Mathieu Lepilliez (Airbus Defence & Space)
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    Systema-Thermica

• Michael Maibaum (German Aerospace Center DLR)
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    The Application of a Thermal Mathematical Model during Lander Operations on the surfaces of Small Bodies

• James McIntosh (ITP Aero)
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    Post-processing of Thermal Model Data with ESATAN Thermal Modelling Suite

• Jan Philipp Moeller
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    Development and verification of a linear conductor generator with different triangle calculation methods

• Edward Nelson (Argotec)
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    A Separable Loop Heat Pipe for Cooling a Pressurised Cargo Module

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    Minimising Temperature Gradients Within an Optical Support Plate Using Active Thermal Control

• Atsushi Okamoto (JAXA)
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    On-orbit Experiment of Oscillating Heat Pipe and Loop Heat Pipe

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

• Ander Pereda Sinovas (SENER AEROESPACIAL)
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    HGAMA SOLAR SIMULATION TEST

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

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    ADMATIS radiators and MLI: from development and qualification to flight

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    JUICE (Jupiter Icy Moon Explorer) Instruments thermal control and interface

• Javier Piqueras Carreño
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    Challenges implementing a stratospheric balloon ascent phase in ESATAN-TMS

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

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    MetOp-SG SCA Instrument Thermal Design and Verification

• Davide Rizzo (OHB-Italia S.p.A.)
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    MetOp SG MWI On Ground Calibration Targets: thermal analysis, design and development

• Matthieu Rodriguez (Airbus DS)
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    Methods to Improve Thermal Test Efficiency (MITTE)

• Harrie Rooijackers (ATG-Europe)
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    Closure

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    Opening

• Kimberly Rutherford (ESA)
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    Correlation of a Thermal Model for Thermo-Elastic Distortion Predictions

• Arne Sauer
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    Sentinel-1 thermally activated Separation Bracket

• Marcel Scherrmann (PTScientists GmbH)
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    TROPICS: An interface between OCDT and ThermiCalc for accelerated thermal design

• Christian Semler (Christian)
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    Machine learning algorithms to develop predictive thermal tools for spacecraft simulations

• ISABEL SOTO
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    Thermal Control Louvers application using Rosetta heritage

• János SZŐKE (ADMATIS)
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    ADMATIS radiators and MLI: from development and qualification to flight

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

• Vincent Vadez (DOREA)
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    First steps of numerical simulation using Artificial Intelligence

• Ramon van den Berg (NLR)
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    Modular Parallel Micro Pump for Adaptive Thermal Control of CubeSats

• Niels van der Pas (Airbus Defence and Space Netherlands)
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    Solution flexibility of HiPeR flexible radiators

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

• Alexander van Oostrum (ATG Europe)
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    Guidelines for accurate thermo-elastic analysis

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    SINAS: Benefits and points of attention