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Download Programme (Pdf) | ECSSMET GERMANY 2021 PROGRAMME 23RD– 25TH MARCH 2021 | ECSSMET GERMANY 2021 DAY ONE 23RD MARCH 2021 | ECSSMET GERMANY 2021 23RD MARCH 2021 09:00 – 10:00 | OPENING Opening Speech by Chair of the DLR Exec u tive Board Walther Pelzer Opening Speeches by the Conference Chairmen Christian Hühne (DLR), Torben Henriksen (ESA), Pierre-Yves Tourneau (CNES) 10:00 – 10:15 | BREAK FOR NETWORKING AT VIRTUAL COFFEE TABLES AND VISITING THE VIRTUAL EXHIBITION AND POSTER SESSION 10:15 – 10:45 | KEYNOTE 1 ON ARIANE 6 Isabelle Rongier 10:45 – 11:15 | KEYNOTE 2 ON SPACE DEBRIS Luisa Innocenti 11:15 – 11:45 | KEYNOTE 3 ON FUTURE SPACE MISSIONS Gwenaëlle Aridon 11:45 – 12:00 | BREAK FOR NETWORKING AT VIRTUAL COFFEE TABLES AND VISITING THE VIRTUAL EXHIBITION AND POSTER SESSION 12:00 – 13:00 | PODIUM DISCUSSION ON FUTURE CHALLENGES IN EUROPEAN SPACE ACTIVITIES Luisa Innocenti (ESA), Isabelle Rongier (ArianeGroup), Gwenaëlle Aridon (Airbus Defence & Space) Moderated by Tiziana Cardone (ESA) 13:00 – 13:45 | BREAK FOR NETWORKING AT VIRTUAL COFFEE TABLES AND VISITING THE VIRTUAL EXHIBITION AND POSTER SESSION | ECSSMET GERMANY 2021 BLOCK 1 | 13:45 – 16:15 | 23RD MARCH 2021 SESSION 1 SESSION 2 SESSION 3 SESSION 4 Thermo-Elastic Prediction ALM - Design Process Buckling of Structures Structural Architectures and Design Chair: Benoit Laine, Christian Puillet Chair: Stefano Beretta, Bianca Maria Colosimo Chair: Christian Hühne, Andreas Kommer Chair: Marina Wolff, Olaf Mierheim Modelling Guidelines for Thermo-Elastic Analyses Development of Design Methods for AM including CAD Experimental Investigation of the Buckling Process of a Mechanical justication of spacecraft components Design, Optimisation, FEM Analysis and Manufacturing Cylindrical Composite Shell under Static Axial Loading starting from interfaces - An end-to-end approach to Alexander van Oostrum – ATG Europe B.V. features establish, evaluate, track and exchange interface loads Co-Authors: A. van Oostrum, A. Peman Falk Odermann – DLR Frédéric Duboeuf and Charles Chary – Siemens and Sonaca Robert Meitzner – ArianeGroup Co-Authors: E. Lemaire, A. Remouchamps, T. Van Eekelen, C. Chary, M. François, A. Vargalui, 13:45 – 14:15 G. Rodrigues Quantifying Uncertainties in Thermo-Elastic Implementation of Additive Manufacturing for Sensitivity to measurement parameters of the TAS-I experience in using Altair SimSolid solution for Predictions spacecraft design vibration correlation technique to predict shell pressurized modules pre-design phase buckling loads - A numerical study Simon Appel and Alberto Peman – ATG-Europe / ESA Marco Mulser – OHB System AG Stefano Destefanis – Thales Alenia Space Co-Authors: J. Wijker, A. van Oostrum Co-Authors: M. Samoil, C. Greve, P. Geißler, P. Vermeer, M. Lippert, C Katzenschwanz, Theodor Baciu – DLR Co-Authors: M. Bellini, G. Guglielminetti, G. Turinetti M. Meisnar, L. Pambaguian Co-Authors: F. Franzoni, R. Degenhardt, M. A. Arbelo 14:15 – 15:45 Improvement of methodologies for thermo-elastic Development of ALM Technology for Space Structures Benchmarking of vibration correlation technique for Design, Analysis, Manufacturing and Qualification of predictions and verification An Opto-mechanical case study prediction of buckling load of cylindrical shells the Sentinel-4 Optical Instrument Module Structure Luca Perachino – Thales Alenia Space Bruno Barroqueiro – Active Space Technologies Kaspars Kalnins – Riga Technical University Markus Geiss – OHB System AG Co-Authors: S. Behar-Lafenetre, J. D‘Amico, M. Vaughan, S. Sablerolle, B. Laine Co-Authors: T. Ernst, M. Sauerbrey, C. Tschepe, H. Loew, M. Podehl 14:45 – 15:15 Themo-elastic test campain in the frame of ESA activity Development of Design Methods for AM including CAD New formulation of buckling and post buckling for Design and Manufacturing of JUICE J-Mag Calibration „I-Meter“ Design / FEM Analysis / Manufacturing Features Composite panels with holes in Manufacturing Alignment System JACS Aerostructures Philippe Baussart – Thales Alenia Space Armin Widhammer – OHB System AG Fabian Preller – INVENT GmbH Co-Authors: S. Sablerolle Co-Authors: M. Meschenmoser, T. Sedlmaier, S. Senese, C. Katzenschwanz, M. Eick, R. Schwarz, Leonardo Liuzzi Co-Authors: T. Sdunnus, I. Rodrigues, J. Esteves S. Gruber, G. Rodrigues, S. Caeiro Co-Authors: P. Caracciolo 15:15 – 15:45 Methodologies and uncertainties for the thermo-elastic Methodology for hybrid part design using additive Nondimensional buckling equations for launch vehicle When is an aluminum structure preferable over a verification of space instruments manufacturing and technological pairs for fast structures design sandwich structure? prototyping Stefano Lucarelli – Airbus Defence and Space Ines Uriol Balbin – Delft University of Technology Els Lemmens – QinetiQ Space Co-Authors: M. Pellizzari Robin Kromer – Arts et Métiers ParisTech Co-Authors: C. Bisagni Co-Authors: E. Gruhier, N. Perry, E. Lacoste 15:45 – 16:15 16:15 – 16:30 | BREAK FOR NETWORKING AT VIRTUAL COFFEE TABLES AND VISITING THE VIRTUAL EXHIBITION AND POSTER SESSION | ECSSMET GERMANY 2021 BLOCK 2 | 16:30 – 19:00 | 23RD MARCH 2021 SESSION 5 SESSION 6 SESSION 7 SESSION 8 Thermo-Elastics - Disturbance in Optical Instruments ALM - Certification, Requirments and Constraints Launchers Multifunctional Structures and Structural Health Chair: Simon Appel, Stéphanie Behar-Lafenetre Chair: Christian Hühne, Tommaso Ghidini Chair: Marie Jaquesson, Joaquín Martin Monitoring Chair: Daniel Stefaniak, Daniel Kaufman Impact of the friction on the thermoelastic behavior of A Summary of NASA’s Efforts for the Development of A Trade of Study for the Structure of the Callisto Structure-borne Ultrasonic Multi-Hop Sensor Network the SuperCam instrument and Certification and Qualification of Additively Vehicle Equipment Bay for Temperature Monitoring of Satellites (SUMSENS) Manufactured Hardware Damien Hoarau – MECANO ID Olaf Mierheim – DLR Krisztian Vajna – INVENT GmbH Co-Authors: S. Orsingher, M. Heim Richard Russell – NASA Co-Authors: L. Heinrich, T. Glaser, N. Lidon, F. Marteau, Y. Guerin, K. Pfaab, C. Serieys, C. Hühne Co-Authors: K. Vajna, M. Koch, M. Brandt, S. Lingelbach 16:30 – 17:00 End-To-End STOP analysis on PLATO TOU Thermoplastics and additive manufacturing: Maturation of selected and promising CFRP- Optical Fiber Sensor for Atmospheric Reentry from ground to out-of-earth application technologies for a representative future launcher Experiments James Etchells and Simon Blake – ATG-Europe / ESA upper stage demonstration Co-Authors: S. Appel, M. Rieder, T. Bandy, V. Cessa, D.Piazza Ugo Lafont – ESA - ESTEC Emile Haddad – MPB Communications Inc. Co-Authors: M. Costa, R. Rampini Marina Wolff – MT Aerospace AG Co-Authors: K. Tagziria, H. Chen, F. Klinberg, A. Guelhan, B. Aissa, D. Barba, I. McKenzie 17:00 – 17:30 PLATO Spacecraft: Thermo-Elastic Distortion Requirement on AM part - Dynamic performance Laser surface preparation before adhesive bonding Development of Modular Multifunctional Structure Verification Concept and Demonstrator Tests on launcher structures – an overview of current Panel Thomas Le Caillec – CITD Engineering and Technologies developments Jan Junker – OHB System AG Co-Authors: L. Hernandez Alvarez, M. Garcia-Cosio Carmena, M. E. Castaño, S. Laborde, Christoph Tschepe – INVENT GmbH D. Escolar, I. Ngan Michel Leroy – ArianeGroup Co-Authors: F. Ruess, P. Marzai, S. Das Co-Authors: A. Mercier, E. Chauray, E. Del Olmo, M. Peron 17:30 – 18:00 FLEX FLORIS Instrument Optical Module Structure Effects of resistivity and emissivity of laser melted Analysis of mounting flux generated by flatness Design and Manufacturing of a Multifunctional Highly (IOMS) metals on the performance of the Super High defect at the interface between two launcher Integrated Satellite Panel Structure Temperature Additive Manufactured Resistojet (STAR) structures Borja Provedo – Sener Aeroespacial Zhuzhell Montano Rejas – DLR Co-Authors: C. Borque, F. Del Campo Christopher Ogunlesi – University of Southampton Kévin Mathis – CNES Co-Authors: R. Keimer, S. Geier, M. Lange, O. Mierheim, J. Petersen, A. Pototzky, J. Wolff Co-Authors: F. Romei, M. Robinson, A. Hamilton, M. Kim Co-Authors: T. Tafadjira, N. Amsing 18:00 – 18:30 BLAST: Black Laser Surface Treatment Quality of AM polymer parts produced using a printer Interstages Structure Development with Out Of without build volume constraints in space environment Autoclave Process for Future Launch Vehicles Marko Piskacev – Azimut Space GmbH Anna Daurskikh – Azimut Space GmbH Victor Diaz – Airbus Defence and Space Co-Authors: A. Sgambati, A. Baptista, L. Facciolati, E. Lallemand, A. Makaya, U. Lafont Co-Authors: J. Vilanova, F. Lavelle, J. Bru 18:30 – 19:00 | ECSSMET GERMANY 2021 DAY TWO 24TH MARCH 2021 | ECSSMET GERMANY 2021 BLOCK 1 | 08:30 – 10:30 | 24TH MARCH 2021 SESSION 9 SESSION 10 SESSION 11 SESSION 12 In-Space Manufacturing Acoustics - Testing Structural Dynamics - Deployable Structures - Solar Arrays and Deployable Chair: Olaf Mierheim, Advenit Makaya Chair: David Boban, Dario Di Maio Payload Isolation and Damping 1 Subsystems Chair: Andy Kiley, Eric Standarovski Chair: Martin Hillebrandt , Thomas Sinn In-Orbit Manufacturing and Assembly: Direct field acoustic test of European space hardware Payload comfort during Ariane 5 launches Deployable barrel for a cubesat’s optical payload a new game changer for Airbus at system level of assembly Aurélien Hot – CNES Akash Yalagach – University of Auckland Gwenaelle Aridon – Airbus Defence and Space Mariano Alvarez Blanco – Siemens Industry Software
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