Technical Sessions

You may first check the List of Abstracts to know in which session you are scheduled.

Room 5 - view floor plan

Time Title Presenter Company
15:30 Scale Resolving Simulations of Vortex Boundary Layer Interactions for a Generic Strake Vortex Nils RATHJE TU Braunschweig
15:50 Influence of the Leading Edge Radius on Vortex Development at Hybrid Delta Wing Configurations Dominik SEDLACK TU Munich
16:10 Transonic Buffet Onset Sensitivity to Gust Disturbances Nicholas GIANNELIS University of Newcastle
16:30 Dynamic Stall Models for Post Flutter Analysis of an Aeroelastic Wing Section Yann BLAIRON Ecole de l’air et de l’Espace
16:50 Optimized Active Flow Separation Control in the Slat Cut Region Using Low Duty Cycle Pulsed Jets Faycal BAHRI University of Nottingham
17:10 Fast Frequency Based Unsteady Solver for Heaving and Pitching Subsonic and Supersonic Airfoils Hemant JOSHI University of Hertfordshire
17:30 Effects of the Reduced Frequency on the Aerodynamic Characteristics of a Pitching NACA 0012 Airfoil Under Moderate Reynolds Number Teng ZHOU Chinese Academy of Sciences

Room 1 - view floor plan

Time Title Presented by Company
15:30 Multifidelity aerodynamic analyses of a hybrid laminar flow control and variable camber coupled wing Mauricio JENTYS Technical University of Munich
15:50 High-fidelity RANS simulations of subsonic and supersonic performance of an Experimental HTB aircraft at 0º, 5º and 10º angles of attack Santiago HERNANDEZ University of Coruña
16:10 Unsteady simulations of an aircraft with installed engine and rotating fan Fulvio SARTOR ONERA
16:30 Wing Rock Prediction in Free-to-Roll Motion Using CFD Simulations Mohamed SEREEZ Coventry University
16:50 Numerical Study on the Ducted Scramjet Combustor Sang Gon LEE Konkuk Univ.
17:10 Aeropropulsive Assessment of the Scramjet Hypersonic Experimental Vehicle Pietro RONCIONI CIRA
17:30 Numerical Study of Magnus effect and damping roll derivative for the M823 bomb configuration José JIMENEZ-VARONA INTA

Room 2 - view floor plan

Time Title Presented by Company
15:30 A Multidisciplinary Modeling System for Designing Fuselage Structures: Extending the Multidisciplinary Modeler Bas van MANEN Fokker Aerostructures
15:50 A multidisciplinary modeling system for aircraft structural components Tobie van den BERG Fokker Aerostructures B.V. - GKN Aerospace
16:10 Dynamic workflow generation applied to aircraft moveable architecture optimization  Jente SONNEVELD TU Delft
16:30 Design automation strategies for stress analysis in critical aerospace components during conceptual design phases Alejandro PRADAS GOMEZ Chalmers University of Technology
16:50 Multidisciplinary design space exploration: An electric fan thruster component design use case Petter ANDERSSON GKN Global Technology Center, Sweden

Room 6 - view floor plan

Time Title Presented by Company
15:30 High Angle of Attack Control Design for Missile Agile Turn Based on Reinforcement Learning Youngjun LEE Seoul National University
15:50 A method to generate a constrained terrain following trajectory using circular path Hyunju LEE Korea Aerospace University
16:10 Nonlinear Dynamic Inversion Autopilot Design for Thrust Vector and Aerodynamic Controlled Aerial Vehicles Rabiya BIYIKLI Roketsan Missiles Inc.
16:30 Deep reinforcement learning based integrated guidance and control for a longitudinal missile system Jeongsu AHN 충북대학교(Chungbuk Nat'l Univ)
16:50 Augmented Pursuit Guidance for Flight Trajectory Shaping Jong-Chan PARK KAIST
17:10 Improving the Interception Performance of Classical Guidance Methods by using Vision Based Multiple Model Estimation Algorithms Yagiz KURT ASELSAN Research Center
17:30 Mid-Course Trajectory Optimization of VFDR Missiles via Pseudospectral Sequential Convex Programming Boseok KIM KAIST

Room 11 - view floor plan

Time Title Presented by Company
15:30 Fault-Tolerant Control of Fixed-Wing VTOL Aircraft with Actuator Failures Based on Incremental Nonlinear Dynamic Inversion Hanna LEE Seoul National University
15:50 Adaptive Flight Control for Aerodynamic Interactions in Multicopter eVTOL Concept Metehan YAYLA Middle East Technical University
16:10 Safe Attitude Controller Design for Multicopter via High-order Control Barrier Function Jinrae KIM Seoul National University
16:30 Performance Comparison of Deep Reinforcement Learning-Based Quadcopter Guidance Algorithms Sevket Utku AYDINLI Middle East Technical University
16:50 Control Design for VTOL Aircraft of Lift+Cruise Configuration using Mode-Switching Algorithm Jiwon LEE Seoul National University
17:10 Modeling and position control of electromechanical actuators for the tiltrotor conversion system of eVTOL aircraft Lining YANG School of Mechanical Engineering and Automation, Beihang Univ.
17:30 Tilt Angle Control Planning for eVTOL using Trim Analysis Jeongseok HYUN Konkuk University

Chairs: Shia Hui Peng & Thomas Arnoult

Room 12 - view floor plan

Time Title Presented by Company
15:30 Implications of extended hybrid laminar flow control suction panels on structural wing design Lennart LOBITZ TU. Braunschweig
15:50 Closed-loop control of an open-cavity flow with magnetically actuated microvalves Thomas ARNOULT Centrale Lille Institut
16:10 Investigation of the skin-friction drag reduction capabilities of wall- normal created plasma jets in wall-bounded turbulent flow Atilla ALTINTAS Chalmers University of Technology
16:30 Investigating the Effectiveness of Vortex Generators in Aviation through High-Fidelity CFD Analysis Mihai Vladut HOTHAZIE National Institute for Aerospace Research "Elie Carafoli"
16:50 In Search for Passive Fluid Control Devices for the Reduction of Viscous Drag of Turbulent Boundary Layers Markus RÜTTEN DLR - German Aerospace Center
17:10 Riblet surface effect on laminar to turbulent transition by Direct Numerical Simulation Kento KANEKO The University of Tokyo
17:30 Bubble suppression on a high lift wing section using synthetic jet Amsha SATHYABABU Indian institute of science

Room 10 - view floor plan

Time Title Presented by Company
15:30 Development and Qualification of the Avionic Support Structure of the Ariane 6 Upper Liquid Propulsion Module Mark Guethler ArianeGroup GmbH
15:50 Compliant high support stiffness rocket gimbal for Thrust Vector Control on liquid engine Guillaume Hueber EPFL
16:10 Vertue, a green orbital module to meet the growing demand for in-orbit operations Carlo Bianco Finis Terrae SRL
16:30 Optimising ConOps of Water Electrolysis Propulsion systems using Deep Q-Learning Sascha Dengler Technical University Munich, Chair of Space Propulsion and Mobility
16:50 Heat transfer characterisation of a 3D-printed Water  Electrolysis Propulsion spacecraft thruster Sascha Dengler Technical University Munich, Chair of Space Propulsion and Mobility
17:10 6kN green fuel throttleable development engine – Design and Manufacturing Jan Sturla Hegre Nammo Raufoss AS

Chairs: N. Girard & B. Schade

Room 12 - view floor plan

Time Title Presenter Company
15:30 Towards A New Class Of Engine For Future Heavy LIft Launch Vehicles Amaya ESPINOSA CNES Direction du Transport Spatial
15:50 LUNA NOVA – Advanced Green Propulsion Systems Christian HESSEL ArianeGroup
16:10 PROMETHEUS®: Precursor of new low-cost rocket Engine Family Pamela SIMONTACCHI ArianeGroup
16:30 RELIANCE - Design, Manufacturing and Testing of the Breadboard Engine Gianluca LIGGIERI Nammo Raufoss AS
16:50 Research and Development of the Small LOX/Methane Propulsion System for an Experimental Reusable Winged Rocket WIRES#015 Tatsuya HASHIZUME JAXA
17:10 KARI’s Additive Rocket Engine Initiative for Low-Cost and Sustainable Access to Space Lim BYOUNGJIK Korea Aerospace Research Institute
17:30 Development of Liquid Oxygen/Liquid Methane Pressurization Systems for Launch Vehicles Cheulwoong KIM Korea Aerospace Research Institute

Room 6 - view floor plan

Time Title Presenter Company
15:30 Activities in space electric propulsion at the French Space Agency – CNES Ulysse WELLER CNES
15:50 Time-Resolved 3D Characterization of the Plume of  a Low-Power Ablative Pulsed Plasma Thruster  Scherezade BARQUERO Universidad Carlos III de Madrid
16:10 First ignition of a magnetic arch EPT cluster composed of two ECR plasma sources Célian BOYE UNIVERSIDAD CARLOS III DE MADRID
16:30 Faraday Cup design for Electrodeless Plasma Thrusters Marco Riccardo INCHINGOLO Universidad Carlos III de Madrid
16:50 Flight results of the miniature 1J pulsed plasma thruster PETRUS Felix SCHÄFER Institute of Space Systems, Univerity Stuttgart
17:30 Preliminary Investigation of A High Efficiency Liquid Micro Pulsed Plasma Thruster (L-PPT) Marcin CHUCHLA Liftero Sp. z o. o.

Chairs: F. Maggi & K.W. Naumann

Room 3 - view floor plan

Time Title Presenter Company
15:30 Agglomeration in solid propellants loaded with inert particles – Study of propellant formulation influence using Shadowgraphy Image Processing Thomas DECKER ONERA
15:50 Heterogeneous Combustion of AP / HTPB / RDX with Detailed Kinetics  Pierre BERNIGAUD ONERA 
16:10 Simulation of heterogeneous Solid Rocket Motors with the Level-Set Method Michael MOROFF Fraunhofer
16:30 Analysis of performance dispersion in pyrotechnic igniters employing BKNO3 pellets Barbara BETTI Avio spa
16:50 Effect of molted or machined surfaces on small scale SRM igntition Olivier ORLANDI ArianeGroup
17:10 The basic design of laser initiated detonator and investigation results of the ignition characteristics Yoshiki MATSUURA IHI Aerospace
17:30 Ignition promotion and combustion inhibition of the CL-20 using graphene oxide Jiaxin SU Nanjing University of Science and Technology

Room 12 - view floor plan

Time Title Presented by Company
15:30 ReFEx: Reusability Flight Experiment – A Demonstration Experiment for Technologies for Aerodynamically Controlled RLV Stages Peter RICKMERS German Aerospace Center (DLR)
15:50 ReFEx: Reusability Flight Experiment-Planning a MORABA Campaign in South Australia Alexander SCHMIDT German Aerospace Center (DLR)
16:10 ReFEx: Reusability Flight Experiment - Trajectory Design Leonid BUSSLER German Aerospace Center (DLR)
16:30 ReFEx: Reusability Flight Experiment – Flight Safety Analysis Jose Luis                     REDONDO GUTIERREZ German Aerospace Center (DLR)
16:50 ReFEx: Reusability Flight Experiment – Architecture and Algorithmic Design of the GNC Subsystem Jose Luis                      REDONDO GUTIERREZ German Aerospace Center (DLR)
17:10 ReFEx: Reusability Flight Experiment - Design of an Exoatmospheric Control System Johannes ROBENS German Aerospace Center (DLR)
17:30 ReFEx: Reusability Flight Experiment - Development of a cold-gas RCS using off-the-shelf components Jonas HOFFMEISTER German Aerospace Center (DLR)

Room 12 - view floor plan

Time Title Presented by Company
15:30 Functionally Graded Materials designed for thrusters : resistance in combustion environment and under laser thermal flux Lisa AUDOUARD ONERA
15:50 Analysis of an arc heated air plasma generator for material screening applications Mathilde RIDARD ArianeGroup
16:10 Numerical Investigation of the Effects of Structural Property Variability on the Material Response of a Fibrous Ablator Sean McDANIEL University of Kentucky
16:30 Comparison of experimental Fatigue Life Study for two Inner Liner Materials for Liquid Rocket Engines Pascal KRINGE DLR
16:50 Hybrid Rocket Engines Design for Materials Characterization Gabriele MANGIONI AVIO
17:10 Understanding coke deposition on carbon fibers Francisco                          TORRES-HERRADOR Von Karman Institute
17:30 Oxidation behavior of an UHTCMC with a structure of Cf / HfB2 – HfC – SiC under oxyacetylene torch and plasma torch. Thomas BOURDEAU LCTS - CNRS

Room 5 - view floor plan

Time Title Presenter Company
9:00 Multi-Objective Aerodynamic Optimization of Supercritical Airfoils with Variational Autencoders Runze LI Tsinghua University
9:20 Numerical Optimization of Single-/Multi-Element Aerofoils Using Gradient-Based Methods Xinying LIU Zurich University of Applied Sciences
9:40 Split-Canard Optimization for Improvement of Canard Aerodynamic Performance Batuhan NASUHBEYOGLU Roketsan Missile, Inc
10:00 Airfoil Aerodynamic Optimization for Mars Exploration Aircraft Giuseppe PEZZELLA University of Campania
10:20 Application of a Deep Neural Network for Cp Prediction on Multiple Wing Geometries in a Transonic Regime Alejandro GORGUES Universidad de Alcala de Henares
10:40 Prediction of Aerodynamic Coefficients for Multi-Swept Delta Wings via a Hybrid Neural Network Moritz ZIEHER TU Munich
11:00 An Adjoint-Based Approach for Finding Smooth Surface Waviness Tolerances for Natural Laminar Flow Design Mohammad MONIRPIRI KTH Royal Institute of Technology

Room 1 - view floor plan

Time Title Presented by Company
09:00 Optimizing the thermocapillary-driven melting of phase change materials in microgravity Andriy                         BORSHCHAK KACHALOV E-USOC, UPM
09:20 Hybrid Digital Twin for Satellite Attitude Control System Based on FMI Co-Simulation Technology Yang XIE Chinese Academy of Military Sciences
09:40 Study of the ineteraction between a droplet and an acoustic waves Ronan PLIQUE Onera
10:00 Satellite Temperature Field Digital Twin Building Based on Partition Method Xingwen PENG National University of Defence Technology
10:20 A high-order accurate framework for thermal fluid-structure interaction Vincenzo GULIZZI Università degli Studi di Palermo
10:40 Transonic flow oscillations in cavity/store problems Nicholas F GIANNELIS THE UNIVERSITY OF NEWCASTLE
11:00 Numerical rebuilding of a free-flying ring interfering with a two-dimensional shock wave Luigi CUTRONE CIRA

Room 2 - view floor plan

Time Title Presented by Company
9:00 Knowledge-based Integration of Aircraft System Simulation within Aircraft Conceptual System Design Ingo Staack Linköping University
9:20 DEFAINE - Design Exploration Framework based on AI for froNt-loaded Engineering: Achievements and Open Challenges Max Baan ParaPy
9:40 An MBSE approach to support Knowledge Based Engineering application development G. La Rocca Technische Universiteit Delft
10:00 Q&A - Round Table    

Room 11 - view floor plan

Time Title Presented by Company
09:00 Effects of Flexibility on Reorientation of Multibody Spacecraft Using Internal Torques Behrad VATANKHAHGHADIM Politecnico di Milano
09:20 The nanosatellite-class attitude control facility at ESA-ESTEC Andrea CURATOLO Alma Mater Studiorum Università di Bologna
09:40 RelGNCPy: A simulation toolkit for relative Guidance,  Navigation and Control in Satellite Formations Michał BLAZEJCZYK AGH University of Science and Technology
10:00 Single-Frame Attitude Determination from Low Resolution Earth Imaging  Daniel CHOUKROUN Ben-Gurion University of the Negev
10:20 Robust Attitude Control Using Electrospray Thrusters Gianni PECORA Politecnico di Torino
10:40 Disturbance Compensation Strategies for Satellite Combined Attitude and Sun Tracking System Renuganth VARANTHARAJOO Universiti Putra Malaysia
11:00 Optimal Time Terrestrial Mapping Scheduling for Spaceborne Push-broom Imagers Heekun ROH Korea Advanced Institute of Science and Technology (KAIST)

Room 12 - view floor plan

Time Title Presented by Company
09:00 OCTRA as Ultrasonically Absorptive Thermal Protection Material for Hypersonic Transition Suppression analyzed on a 7° cone Viola WARTEMANN DLR
09:20 Experimental and Simulative Evaluation of a Reinforcement Leaning Based Cold Gas Thrust Chamber Pressure Controller Till HÖRGER DLR - German Aerospace Center
09:40 Mechanical design of a deployable morphing aeroshell for 12U CubeSat atmospheric reentry Ignazio DIMINO CIRA, The Italian Aerospace Research Centre
10:00 Verification of the Electrical Thrust Control Valve in the Small LOX/Methane Engine Firing Tests Yutaro OTA IHI corporation
10:20 Development of a dual-position oxidizer main valve Moongeun HONG Korea Aerospace Research Institute

Room 4 - view floor plan

Time Title Presented by Company
09:00 Consideration of Technology Scalability in the Design of Electric Propulsion System Architectures    Benedikt AIGNER  
09:20 Architectural Trade-offs for a Hybrid-Electric Regional Aircraft Philip BALACK German Aerospace Center DLR e.V.
09:40   Advanced Hybrid-Electric Propulsion Systems  and Integrations in Airliner Malte Christopher SCHWARZE Advanced Aircraft Design
10:00 Evaluation of hybrid electric powertrain topologies and their integration in future aircraft concepts for general aviation Thorben HAMMER German Aerospace Center (DLR)
10:20 High-level Sizing Method for Hybrid Electric Distributed Propulsion Aircraft Baptiste LEGRAND Avions Mauboussin
10:40 Feasibility studies for a medium size regional aircraft with battery powered propulsion system Jonas LUDOWICY German Aerospace Center (DLR)

Room 10 - view floor plan

Time Title Presented by Company
09:00 Enabling a European In-Space Transportation ecosystem Yann Tincelin European Space Agency - ESA
09:20 Mechanical Ground Systems within the SAMMA Project - Review and way forward Carola Glasgow MT Aerospace AG
09:40 Cryogenic Upper Stage Development for Future Korean  Small-Lift Launch Vehicles KEEJOO LEE KARI
10:00 Agile component of infrastructure in New Space companies Tobiasz Mayer Sieć Badawcza Łukasiewicz – Instytut Lotnictwa
10:20 Applying Machine Learning to Routine Satellite Ground Segment Operations by Means of Automated Anomaly Detection Leonard Schlag DLR
10:40 Use the AI tools for Space systems delivery Jamel METMATI RHEA

Chairs: S. Schleichtriem & J. Hardi

Room 12 - view floor plan

Time Title Presenter Company
9:00 PROMETHEUS® tests on T1 Bench in Vernon Antoine REMY ArianeGroup
9:20 Results of Hot-fire Testing of 30kN LOX/Methane Full-expander Cycle Engine Kazuki SAKAKI Japan Aerospace Exploration Agency
9:40 Hydrogen generation from aluminum composites hydrolysis  for space propulsion Luciano GALFETTI Politecnico di Milano DAER Dep
10:00 Satellite Water Propulsion: 3D Printed Ceramic Thruster & Space Debris Mitigation Concept Jérôme HILDEBRANDT Institute of Space Systems, University of Stuttgart
10:20 Demonstration plan of fault diagnosis in propulsion system during HTV-X experiment mission for future technologies Kaname KAWATSU JAXA
10:40 Investigation of a two-phase vortex flow in a tank with liquid residues  for its discharge under low-gravity conditions Valeriy TRUSHLYAKOV Оmsk Technical University

Chairs: A. Simone & U. Weller

Room 6 - view floor plan

Time Title Presenter Company
9:00 ECRA Thruster latest development at ONERA Victor DESANGLES ONERA
9:20 An Experimental Setup for the Performance Analysis of Low-Power Hollow Cathodes at High Applied Magnetic Field Strengths Jakob BALKENHOHL The University of Auckland
9:40 Design and testing of a heaterless hollow cathode for a low- current electric thruster Mathew DENYS Victoria University of Wellington
10:00 High thrust, low power, green propellant electro-thermal resistojet thruster Kamil PIECHA Liftero
10:20 Design, fabrication and characterization of electrically controlled solid microthruster Wei ZHANG Nanjing University of Science and Technology
10:40 Optimization of Wave-Plasma Interaction in RF Powered Propulsion Technology based on Ultra-Compact Helicon Reactor Theodora ANDREESCU COMOTI

Chairs: L. Galfetti & E. Orbekk

Room 3 - view floor plan

Time Title Presenter Company
9:00 Effect of flame radiation on aluminum particle combustion Stany GALLIER ArianeGroup
9:20 Study of aluminum droplet ignition in a solid propellant flame Dmitry DAVIDENKO ONERA
9:40 Evolution of aluminum droplets in solid-propellant combustion by image analysis using deep learning Magdeleine AIRIAU ONERA
10:00 Experimental estimation of the amount of residual slag remaining inside orbital insertion stage solid rocket motor Yoshiki MATSUURA IHI Aerospace
10:20 Simplified Numerical Modeling of Film Cooling and Mixture Ratio Bias in Liquid Rocket Thrust Chambers Gianluca COCIRLA Sapienza University of Rome
10:40 Study of SRM Nozzle Divergent Performance Improvement Under Fixed Geometrical Constraints Daniele BIANCHI Department of Mechanical and Aerospace Engineering, Sapienza University of Rome
11:00 Multiphase and Multidimensional Effects on Solid Rocket Nozzle Performance Gianluca COCIRLA Sapienza University of Rome

Room 12 - view floor plan

Time Title Presented by Company
9:00 MINI-APTERROS: A GNC demonstrator for Vertical Landing and Thrust Vector Control systems Hadrien AFSA MCA Ingénierie
9:20 OVERVIEW OF CALLISTO VEHICLE DEVELOPMENT STATUS Jean DESMARIAUX CNES
9:40 Further Progress in Aerodynamic Studies for CALLISTO -  Reusable VTVL Launcher First Stage Demonstrator Joseph KLEVANSKI DLR
10:00 CALLISTO – on repurposing an expendable reaction control system (RCS) for a reusable demonstrator  Simon FURNES NAMMO
10:20 CALLISTO - Flight Worthiness Process: how to prepare the tripartite go to flight decision? Arnaud BIARD CNES
10:40 Themis Demonstration Programme  Nathalie DELATTRE ArianeGroup

Room 12 - view floor plan

Time Title Presented by Company
09:00 Vibration test of upper stage engine for KSLV-II Jinhyuk KIM Korea Aerospace Research Institute
09:20 Wear and heat of aircraft materials in case of emergency landing situations Eric DELETOMBE ONERA
09:40 Development of low-shock separation systems for payload fairings Christoph KARL Beyond Gravity
10:00 In situ characterization of aeronautical fasteners subjected to lightning using MHz X-ray visualization A. JARNAC ONERA
10:20 Design, Fabrication and Performance of Planar Solid Propellant Micro-thruster Based on SU-8 Photoresist Jianbing XU Nanjing University of Science and Technology
10:40 Energy harvesting from a rotary sandwich structure with magnetorheological core under aerodynamic pressure Taha SOLEYMANI Aviation
11:00 Diagnosis and Prognosis of Structural Damage Growth with Parameter Sharing in Fleet Maintenance Digital Twins Leiting DONG Beihang University

Room 6 - view floor plan

Time Title Presented by Company Country
09:00 Four Months to Orbit: Fast-Tracking CubeSat Development for Reliability Through In-Orbit-Demonstrations Michael LINDER EPFL Switzerland
09:20 Lightweight, Cost-effective, and Multi-functional Bio-based Composite Laminate Design for Satellite Applications Daniele TORRISI Tu Delft Italy
09:40 Primer Vector theory based optimal guidance for orbital transfers in cis-lunar environment Gabriele GEMIGNANI University of Pisa Italy
10:00 Thermodynamic Analysis of Martian Habitats Evandros THEODOSIOU Department of Mechanical Enginnering, Imperial College London United Kingdom
10:20 Asclepios Mission III: THIRD ITERATION OF THE STUDENT-LED ANALOG MISSION SIMULATING A HUMAN EXPEDITION TO THE LUNAR SOUTH POLE Evandros THEODOSIOU Asclepios Mission III Switzerland
10:40 Overview of the Twardowsky Hybrid Sounding Rocket Avionics Design Bartosz KOSCIANEK ISAE-SUPAERO France
11:00 A new step towards modular, versatile and cost-effective avionics for PERSEUS small reusable launcher Mickaël GOMES CT Ingenierie France

Chairs: D. Reckzeh & E. Otero Sola

Room 6 - view floor plan

Time Title Presented by Company
09:00 Scalability assessment of hybrid-electric technology application to various aircraft classes – an overview of opportunities and challenges Maurice F.M. HOOGREEF Delft University of Technology
09:20 Scaling of Aircraft Incorporating the Semi Aeroelastic Hinged Wings  Jonathan COOPER University of Bristol
09:40 Flight Dynamics of Aircraft Incorporating the Semi Aeroelastic Hinge Huaiyuan GU University of Bristol 
10:00 Advancements in the development of a novel wing design method in conceptual aircraft design Tim EFFING RWTH Aachen University
10:20 Hybrid Laminar Flow Control ready for Series Application Bram van de KAMP DLR
10:40 Investigating potentials of active flow control via retrofit of commercial aircraft Valerio MOSCA Institute of Aircraft Design and Lightweight Structures TU Braunschweig
11:00 Two-phase pumped cooling system for power electronics; analyses and experimental results Henk Jan van GERNER NLR

Room 5 - view floor plan

Time Title Presenter Company
16:30 Summary Data from the Seventh CFD Drag Prediction Workshop Raj NANGIA University of Bristol
16:50 Aerodynamic Analysis of Tandem Tilt Wing eVTOL Aircraft in Cruise Phase Atsushi SHINOZUKA University of Tokyo
17:10 Wind Tunnel Experiments of an eVTOL Wing-Propeller Configuration Catharina MOREIRA TU Munich
17:30 Quick Preliminary Aerodynamic Estimation for a Distributed Propulsion Aircraft with Propellers in Front of the Wing David PLANAS ISAE-Supaero & ONERA
17:50 Installation Effect on Hover Propeller Performance Ohad GUR Israel Aerospace Industries
18:10 Stall Development Control of a Blended Wing-Body UAV Using a Bioinspired Leading Edge Design Raffaello MARIANI KTH Royal Institute of Technology
18:30 Experimental Analysis of the Flowfield Over an Aeroelastic Wind Tunnel Model for Tail Buffeting Analysis Julius STEGMUELLER TU Munich

Room 1 - view floor plan

Time Title Presented by Company
16:30  DNS of flow inside pipes with large relative roughness height Mariangela De MAIO Università di Roma Sapienza
16:50 Modeling of polyatomic gas flows within a kinetic Fokker-Planck approach using a direct modeling method Aaron NAGEL German Aerospace Center (DLR)
17:10 DNS of turbulent ribbed channel flow with heat transfer and comparison with current RANS capabilities Tiziano SANTESE TUM
17:30 Shell models of turbulence in aero-optics Albina TROPINA Texas A&M University
17:50 Assessment of RANS methods for low-Reynolds number compressible flows Francesco Antonio D'ANIELLO Italian Aerospace Research Centre
18:10 VoF-to-DPM 3D Model for non-reacting gas liquid two-phase flow  Mariano Di MATTEO Université Libre de Bruxelles
18:30 A New Framework for Data-assisted Turbulence Modeling Chenyu WU Tsinghua University

Room 6 - view floor plan

Time Title Presented by Company
16:30 Coupling of particle and continuum methods for the simulation of radiative and particle laden flows Stefan FECHTER German Aerospace Center
16:50 Aerodynamic simulation of the near-field of an aircraft using different mesh adaptation strategies Younes BOUHAFID ONERA
17:10 Deep learning-based model for predicting the unsteady fluid-structure interaction of flapping wings Wrik MALLIK University of Glasgow
17:30 Exponential Differencing BGK Method for Multiscale Flow Simulation Félix GARMIRIAN Institute of Space Systems - University of Stuttgart
17:50 Robust CAD Methodology for CFD optimizations Patrick WEGENER German Aerospace Center (DLR)
18:10 Assessment of neural network-based predictions of chemical production rates in CFD solvers Sebastian KARL DLR
18:30 A local unstructured re-meshing technique for handling multi-body separation in 2D flows. Alessia ASSONTIS University of Rome La Sapienza

Room 11 - view floor plan

Time Title Presented by Company
16:30 Sensor fault detection and isolation for electro-mechanical actuators in a reusable launch vehicle TVC system Stefano FARI German Aerospace Center (DLR)
16:50 Electromechanical TVC using direct engine deflection measurement feedback for reusable stages Philippe SAUNOIS ArianeGroup
17:10 GNC Improvements between Vega and Vega-C Angelo TOMASSINI Avio spa
17:30 Modelling and Stability Analysis of Sloshing on Liquid-Propelled Reusable Launch Vehicles José Alfredo MACES-HERNANDEZ German Aerospace Center (DLR)
17:50 Sensitivity analysis of GNC strategies to propulsion system parameters for multi-orbits deliveries Alberto SARRITZU Politecnico di Milano
18:10 Robustness analysis for closed-loop model reference adaptive attitude control for a satellite launcher Julia GUIMARAES INPE
18:30 Multi-phase Robust Optimization of a Hybrid Guidance Architecture for Launch Vehicles Akan SELIM ROKETSAN Inc.

Room 4 - view floor plan

Time Title Presented by Company
16:30 Characterisation of thermal management specific heat rejection for electric propulsion architectures Antje LINK  
16:50 First Order Thermal Analysis Methodology for Hybrid-Electric Propelled Aircraft in Early Design Stages Jaap van MUIJDEN NLR
17:10 Load Flow Analysis of Hybrid AC-DC Power Systems for the Application in Electrified Aircraft Propulsion Victor BAHRS German Aerospace Center (DLR)
17:30 Dynamic combustion characteristics of electrically controlled solid propellant with transient voltage Zhiwen WANG Nanjing University of Science &Technology

Room 10 - view floor plan

Time Title Presented by Company
16:30 Miniature Fast Steering Mirrors (FSM) for Space Optical Communication in NanoSats and CubeSats Gérald Aigouy  CEDRAT TECHNOLOGIES
16:50 GNSS relative navigation for operations in cislunar space Marco SABATINI Scuola di Ingegneria Aerospaziale, Sapienza Università di Roma
17:10 Achievements and Development Status of the H2O2 based Roll and Attitude Control System for VEGA launchers Gabriele Guerra Nammo AS
17:30 A feasibility study of a future European Single-Stage-To-Orbit (SSTO) spaceplane Julien SENON IPSA
17:50 Design of the Scramjet Hypersonic Experimental Vehicle Sara Di Benedetto CIRA
18:10 Low-Cost Uncrewed Lunar Landers: Mission Design and Preliminary Feasibility Assessment Conall de Paor ISAE-Supaero

Chairs: N. Girard & S. Soller

Room 12 - view floor plan

Time Title Presenter Company
16:30 Research and test activities on sustainable space propulsion systems at TU Darmstadt Henrike JAKOB Technische Universität Darmstadt
16:50 Development of the hollow detonative chamber for the RDE applications Piotr WOLANSKI Lukasiewicz-Institute of Aviation
17:10 Steady 1D Viscous Non-adiabatic Flow Model for the Determination of Inner Geometry and Power Density Profile of Nuclear Fuel Element Elia PUCCINELLI University of Pisa
17:30 Experimental validation of the electric sail concept Stéphane MAZOUFFRE CNRS
17:50 Investigation of a Cathode-Vapor-Feed Electrolyser for a Water Electrolysis Propulsion System Sören HEIZMANN Technical University of Munich
18:10 Heat Transfer Assessment in a Vaporizing Liquid Microthruster undergoing Dual Heating Control Donato FONTANAROSA Dept. Mechanical Engineering - KU Leuven
18:30 Assessment of characteristic length-scale measurements in H2 detonation from simultaneous planar laser-induced fluorescence of hydroxyl radical and nitric oxide Samir Boset ROJAS CHAVEZ King Abdullah University of Science and Technology

Room 6 - view floor plan

Time Title Presenter Company
16:30 Electric field simulation of FEEP thruster for cubesat application Jeongsik SHIN University
16:50 Measurements of xenon ions velocity in Cylindrical Hall Thruster with Laser-Induced Fluorescence spectroscopy Tatiana PERROTIN Universidad Carlos III de Madrid
17:10 Advancements of a VLEO satellite system study utilizing an RF Helicon-based Plasma Thruster Georg HERDRICH Institute of Space Systems (IRS), University of Stuttgart
17:30 Resistive MHD simulations of a self-field Magneto Plasma Dynamic thruster over the 5 to 40 kA current range Yevhen TKACHENKO Sorbonne University / LERMA
17:50 Development of a neutraliser for air-breathing electric propulsion in very-low Earth orbit  Mansur TISAEV University of Surrey
18:30 Earth atmosphere remnants as an electric propulsion propellant Chloe BERENGUER DEDALOS Ltd

Chairs: M. Kobald & C. Schmierer

Room 3 - view floor plan

Time Title Presenter Company
16:30 Boosting Green Propellants: The Sustainable Armored Grain for Hybrid Rocket Propulsion Riccardo BISIN Politecnico di Milano
16:50 Effect of Injection System and Fuel Grain Length on a 1000 N Thrust-Class HRE Daniele CARDILLO CIRA (Centro Italiano Ricerche Aerospaziali)
17:10 Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket Marco FABIANI Sapienza University of Rome
17:30 Particle-based modeling of the unsteady flow in a high-test peroxide catalytic chamber Nora M. BIEWAGEN German Aerospace Center (DLR)
17:50 Transition of Pressure Oscillations in Hybrid Rocket Combustion using Paraffin Wax Fuel Wonjeong HYUN Konkuk University
18:30 Combustion Instabilities Induced by Multi-Stepped Hybrid Rocket Fuel Grains Artur Elias                                   de MORAIS BERTOLDI University of Brasília
18:50 A new combustion phenomenon: penetrative combustion of 3D printed fuel grain for hybrid rocket engine Xiaodong YU Nanjing University of Science and Technology

Chairs: A. Biard & M. Sippel

Room 12 - view floor plan

Time Title Presented by Company
16:30 Trajectory optimization of semi-reusable launchers Arnaud RUIZ ArianeGroup
16:50 Analysis of Novel Concepts for the Return of Upper Rocket Stages Sophie FÖRSTE Institute of Space Systems (IRS)
17:10 Circularity and Sustainability in Aerospace: The Case of Spacecraft Materials  Margot CLAUSS Luleå University of Technology
17:30 Configuration studies, design, and development of landing legs  for VTVL reusable launch vehicles Anett KRAMMER Almatech
17:50 A liquid reusable strap-on booster system discussion for future European launch vehicles Moritz ELLERBECK MT Aerospace AG
18:10 Progress Summary of H2020-project FALCon Martin SIPPEL DLR-SART

Room 2 - view floor plan

Time Title Presented by Company
16:40 Presentation and objective of Euro2Moon association (10mn)    
16:50 A prospective market & business perspective on Lunar ISRU for propellant applications Matteo AINARDI Arthur D Little
17:10 An Economically Viable Lunar ISRU Process for Oxygen and Metal Production and Related Benefits for Terrestrial Applications Pierre Alexis JOURMEL Airbus Defense and Space
17:30 A large-scale laboratory demonstrator for the production of oxygen from lunar regolith: Challenges and opportunities Dennis HARRIES ESRIC
17:50 Silicon photovoltaics, a low cost technology to power lunar
installations		 Romain CARIOU CEA
18:10 Regenerative Fuel Cell System technologies development Cédric DUPONT Air Liquide
18:30 EUROHAB: A Secondary Habitat concept for the South Pole of the Moon Nisheet SINGH SPARTAN SPACE

Room 12 - view floor plan

Time Title Presented by Company
16:30 SPH Technique for enhancing prediction of crash behavior of plain weave fabric composites coupons Redouane LOMBARKIA U. Laval
16:50 Thermal effects in optomechanical systems for space applications  Fatouma MAAMAR Satellites development center, Algerian Space Agency,
17:10 A global-local defect/damage initiation and propagation model for launcher composite structures pre-sizing Alexy TAILLEUR CNES, ICA
17:30 Robust X-ray Phase Contrast Imaging applied to lightning-induced damaged CFRP Laureen GUITARD CEA Saclay/ONERA Palaiseau
17:50 Recent Progress in Wrapped Tow Reinforced (WrapToR) Composite Truss Structures Benjamin King              SUTTON WOODS University of Bristol
18:10 Demise performance of Composite Overwrapped Pressure Vessels in reentry conditions Joseph El RASSI Von Karman Institute

Room 6 - view floor plan

Time Title Presented by Company
16:30 Small launcher system conceptual design efficiency improvement research status Rubén                              GONZALEZ-GONZALEZ Instituto Universitario de Microgravedad Ignacio Da Riva, Universidad Politécnica de Madrid
16:50 Structural design of PERSEUS bi-liquid demonstrator: ASTREOS-1 Ronan GEFFRAULT CT ingénierie
17:10 Cold gas roll control for a 30kg experimental rocket Florian COURTEVILLE SUPAREO SPACE SECTION
17:40 Design of the regenerative cooling system for a 4kN LOX/Ethanol student-built liquid rocket engine Raphael AUBRY ISAE Supaéro
18:00 Design and testing of the combustion chamber of a H2O2/ABS student-developed hybrid rocket engine Daniel CANTOS ISAE-SUPAERO / Supaero Space Section
18:20 PERSEUS and Minerva: Firing tests Arthur                                  BERLET DECHAUFFOUR ArianeGroup 

Chairs: A. Strohmayer & E. Stumpf

Room 6 - view floor plan

Time Title Presented by Company
16:30 E-VTOL Concept Design with a New Underwing ‘FanFoil’ Ducted Fan Concept to Improve Aerodynamic Efficiency Victor MALDONADO Texas Tech University
16:50 Integrating Environmental Life Cycle Assessments in the Design Optimization of Electric UAVs Félix POLLET ISAE-SUPAERO
17:10 Conceptual design optimization of Hybrid-Electric Regional Aircraft using SPPH architecture Laurent BOVET ELISA Aerospace

Chairs: J. Mansouri & J-P. Kneib

Room 12 - view floor plan

Time Title Presented by Company
16:30 LEONEEDS - A Space Debris Recycling Space Station Joshua BENARROCH Institut Polytechnique des Sciences Avancées
16:50 INSIDeR : Innovative Net & Space Inflatable structures for active Debris Removal Eliot DE MAGNEVAL CT INGENIERIE
17:10 Development of a novel capture system Emmanuel ONILLON Centre Suisse D'electronique et de Microtechnique
17:30 Non-Cooperative Target Pose Estimation Based on Dynamic Region-Aware Convolution Neural Network Zhaoxiang ZHANG The university of tokyo
17:50 Deployment dynamics for rotating space tether systems Valeriy TRUSHLYAKOV Omsk Technical University
18:10 Just-in-time Collision Avoidance (JCA) using nanosatellite swarms (nanotugs) Giorgia DI DIO, Maura COLUCCI, Marco TOMMASI, Yoann BEN HAMOU IPSA (engineering school)
18:30 Space-based passive orbital maneuver detection algorithm via a new characterization Bichun GONG Nanjing University of Aeronautics & Astronautics

Room 5 - view floor plan

Time Title Presenter Company
9:00 Dynamic Instability of a Thin Shell Type Aeroshell Capsule with Pitching Motion in Transonic Wind Tunnel Hideto TAKASAWA Hokkaido University
9:20 Longitudinal and Lateral Stability Characteristics of Cone Based Waveriders Agnivo GHOSH Indian Institute of Science
9:40 Mid-Fidelity Investigation of Aerodynamic Interactions on Stability and Control of eVTOL Distributed Propulsion Murat SENIPEK Turkish Aerospace
10:00 The Impact of Unsteady Inflow Conditions on the Instabiity and Transition of Separated Flows in Low Pressure Turbines Himpu MARBONA Universidad Politecnica de Madrid
10:20 Numerical and Experimental Investigation of the Shock Wave Boundary Layer Interaction of Laminar/Transitional Flow Past a Sharp Fin Tobias ECKER German Aerospace Center (DLR)
10:40 Investigation of Fluid Structure Interaction on a Flexible Cantilevered Plate Due to Shock Impingement Kartika AHUJA Indian Institute of Science
11:00 Coherent Solutions to Roll Damping Derivatives Evaluation for a Generic Rockete Model Ionut BUNESCU National Institute for Aerospace Research

Room 4 - view floor plan

Time Title Presented by Company
09:00 An update of the CNES stratospheric balloon activities Vincent DUBOURG CNES
09:20 Reconstruction of georeferenced observations using images by autonomous payloads in sounding balloon flights Carlo BETTANINI Università di Padova
09:40 Stratospheric Flight of a Balloon-Borne Solar Cell Testing Facility Salvo MARCUCCIO Università di Pisa
10:00 A small long endurance LTA with H2 as lift gas and FC propulsion system Patrick HENDRICK Université Libre de Bruxelles
10:20 Design and development of the ATEMO atmosphere monitoring device Federico TOSON Università di Padova

Room 1 - view floor plan

Time Title Presented by Company
09:00 Radio Communication Blackout Mitigation: Ray Tracing Analysis and Signal Characterization including Experimental Validation for Non-magnetized Plasmas Johannes Sebastian LAUR University of Luxembourg
09:20 A Study on Plasma Formation on Hypersonic Vehicles using Computational Fluid Dynamics Salvatore ESPOSITO Politecnico di Torino
09:40 Numerical Rebuilding of Plasma Wind Tunnel Experiments for Investigation of Magnetohydrodynamic Flow Interactions within the EU Project MEESST Alessa SPERBER Institute of Space Systems
10:00 Multiphase MHD model for electric explosions: Application to lightning protection systems Fabien THOLIN ONERA
10:20 PIC schemes for multi-scale plasma simulations Tobias OTT Institute of Space Systems
10:40 Modelisation of plasma discharge for aerospace  applications : Streamer to arc transition Eve PACHOUD ONERA
11:00 Bayesian calibration of a finite-rate nitridation model from molecular beam and plasma wind tunnel experiments Michele CAPRIATI von Karman Institute

Room 6 - view floor plan

Time Title Presented by Company
09:00 Simulation of Safety Relevant Aspects of LH2 Systems Birgit GOBEREIT DLR
09:20 Fundamentals Of Aircraft Hydrogen Tank Design With System Simulation Michael SIELEMANN Modelon Deutschland GmbH
09:40 Analysis and simulation of a cryogenic hydrogen aircraft fuel tank George LAMPEAS University of Patras
10:00 Modelling of the cathode air supply for a pressurized hydrogen fuel cell system in airborne applications Daniel FRANK University of Ulm
10:20 Round table discussion: what does it take to change to alternative propulsion systems?    

Room 11 - view floor plan

Time Title Presented by Company
09:00 Onboard Trajectory Optimization for Radius to Fix Turns   Daniel M. GIERSZEWSKI Technische Universität München
09:20 Embedding Pontryagin’s Principle in Neural Networks for Optimal Asteroid Landing Sergio CUEVAS del VALLE Universidad Rey Juan Carlos
09:40 Variable-Performance Electrospray Maneuvers Optimization Giuseppe Di PASQUALE IENAI SPACE
10:00 Multi-Objective Controller Optimization and Robustness Analysis by the Example of Electro-Mechanical Flight Surface Actuation Kolja MICHEL German Aerospace Center (DLR)
10:20 A Dual-Based Linear Programming formulation of Optimal Control: Fuel-Optimal Rendezvous Guidance and Boresight Pointing Applications Sergio CUEVAS del VALLE Universidad Rey Juan Carlos
10:40 Entry Vehicle Trajectory Optimization using Convex Programming and Post-correction technique jung CHEOL-GOO KAIST
11:00 An Indirect Estimation Approach of Underactuated Evader Strategy for Orbital Pursuit-evasion Game Jiang  SHAO China Academy of Space Technology

Chairs: M. Martin-Benito & P. Lapenna

Room 12 - view floor plan

Time Title Presenter Company
9:00 Large Eddy Simulations of injectors near-field and heat transfer in rocket combustion chambers Pasquale Eduardo LAPENNA Sapienza University of Rome
9:20 Analysis of Detailed-Chemistry Schemes for the Numerical Simulation of Supercritical LOx/CH4 Flames Tim HORCHLER German Aerospace Center (DLR)
9:40 Experimental Analysis of a Capacitively Cooled, Low-Pressure GCH4/GOX Combustion Chamber Rahand DALDHAD University
10:00 Estimation of Hard Start Mechanism by Visualization Test of Hypergolic Bipropellant Thruster Kohji TOMINAGA Japan Aerospace Exploration Agency (JAXA)
10:20 Assessment of phase-separation phenomena in LREs cryogenic flows Davide CAVALIERI Sapienza Università di Roma
10:40 Reduced Order Modeling for the prediction of combustion instabilities in liquid rocket engines: coaxial injection response and acoustic damping modeling Thomas SCHMITT Laboratoire EM2C
11:00 Sensitivity study on a low order model for the analysis of transverse combustion instability Alessandro MONTANARI Sapienza University of Rome

Room 6 - view floor plan

Time Title Presenter Company
9:00 Power converter with high gain, high performance for space thrusters based on electrospray technology Francisco José                 BLAZQUEZ PLAZA Universidad Carlos III de Madrid
9:20 Ionic liquids performance for externally wetted electrospray propulsion system David VILLEGAS-PRADOS ienai SPACE
9:40 Numerical modelling of supersonic magnetic nozzles Jakub GLOWACKI Victoria University of Wellington
10:00 Effects of magnetic nozzle configuration on ion beam generation for RF electrode-less plasma thrusters Antonella CALDARELLI The University of Auckland
10:20 The Hēki Mission: Testing Superconducting Magnet Technology for Space Propulsion on the International Space Station Randy POLLOCK Robinson Research Institute
11:00 Integration and Testing of a High Temperature Superconductor Magnet with a Central Cathode Electrostatic Thruster Chris R. ACHESON Robinson Research Institute

Chairs: F. Maggi & H. Ciezki

Room 3 - view floor plan

Time Title Presenter Company
9:00 Sea launch experiment of LT fuel hybrid sounding rocket C1 Yutaka WADA Chiba Institute of Technology
9:20 Experimental investigation of paraffin-based fuel doped with MgB2 and MWCNTs in a 1-kN hybrid rocket engine Artur Elias                                   de MORAIS BERTOLDI University of Brasília
9:40 Optical investigation of paraffin-based fuel combustion in a  hybrid rocket slab burner Riccardo GELAIN Université libre de Bruxelles
10:00 Preliminary testing and analysis of the end-burning swirling flow hybrid rocket engine using torch igniter Tomasz PALACZ AGH UST
10:20 Mass Transfer due to Liquid Layer Flow for Paraffin-Based Fuels in Hybrid Rocket Engines Jungpyo LEE University of Brasilia
11:00 Diode Laser Ignition Characteristics of ABS and Oxygen hybrid rocket motor Hanqing XIA Beijing Institute of Technology

Chairs: J. Van Den Eynde & K. Mathis

Room 12 - view floor plan

Time Title Presented by Company
9:00 European Flexible Heat Shields: Advanced TPS Design and Tests for Future In-Orbit Demonstration - 2 Giuseppe GOVERNALE Politecnico di Torino
9:20 Flight Experiment of Transpiration Cooled Sharp Edge Fins on the Sounding Rocket HIFLIER1 Jonas PEICHL German Aerospace Center (DLR)
9:40 DLR project TRANSIENT: Testing reusable cryogenic insulation and thermal protection systems  Jascha WILKEN German Aerospace Center (DLR)
10:00 BFS an atmospheric reentry kit to bring NANOSAT Payloads « Back From Space »,  Stephane HEINRICH eNOVA Aerospace
10:20 Cold-Gas Experiments on Advanced Nozzles in Subsonic Counter-Flows Giuseppe SCARLATELLA Technische Universität Dresden
10:40 Anomaly detection with LSTM Autoencoder and SVDD for Reusable Rockets Andrea VENNITTI Technische Universität Dresden

Room 2 - view floor plan

Time Title Presented by Company
9:00 System Analysis of Water Electrolysis Propulsion for different Spacecraft Mission Scenarios Sören HEIZMANN Technical University of Munich (TUM)
9:20 Using the CO2DGM model to characterize and to diagnose electric thrusters meant for propulsion near Mars or Venus Konstantinos KATSONIS DEDALOS Ltd
9:40 Design of translunar injection trajectories using phasing loops in a TPBVP Fu-Yuen HSIAO1 Department of Aerospace Engineering
10:00 RELIANCE, an electric pump-fed main engine for ESA’s lunar lander Adrien BOIRON Nammo Raufoss
10:20 Surfaces for space exploration Malgorzata HOLYNSKA ESA/ESTEC
10:40 Fault-tolerant Orbit and attitude control of Solar sail with a rapid inspection and repair strategy of faulty RCDs Hongyi XIE National University of Defence Technology

Room 12 - view floor plan

Time Title Presented by Company
09:00 Sandwich hybrid structural component for tilt rotor aircraft Giuseppe MANTEGNA University of Enna Kore
09:20 Mechanical Properties of Additively Manufactured Titanium Alloy Sandwich Structures for Thermal Protection Philipp NIEKE The University of Auckland
09:40 Exploring the Benefits and Limitations of Wire-based Direct Energy Deposition of Magnesium Alloys  Stefan GNEIGER AIT Austrian Institute of Technology, LKR Light Metals Technologies Ranshofen
10:00 Analysis of Process Parameters Effects on Final Properties of Additively Manufactured Components for Space Applications Davide ZUIN Politecnico di Milano
10:20 Exploring the potential of GATOR Morphing Skins through high-fidelity FEA: A study of the unique design parameters Rafael Martin HEEB University of Bristol
10:40 Low cycle fatigue and creep properties of a new L-PBF additive manufacturing copper-maraging steel metal matrix composite for liquid rocket engine thrust chambers Matteo CRACHI Politecnico di Torino

Room 6 - view floor plan

Time Title Presented by Company
09:00 Numerical optimization of airfoils for wings with integrated tubular high-pressure hydrogen tanks Florian DEXL Technische Universität Dresden
09:20 Overall Parametric Design and Integration of On-Board Systems for a Hydrogen-Powered Concept Aircraft Thimo BIELSKY Hamburg University of Technology
09:40 Setting up a framework for the high-fidelity simulations of contrails from future hydrogen-fueled aircraft Tânia FERREIRA Stanford University
10:00 Heat exchanger integration into an aero-engine bypass duct Raul BAJIMAYA Cranfield University
10:20 Kinetic Energy Recovery from a landing aircraft: Evaluating Onboard Energy Storage Solutions Robert CAMILLIERI University of Malta
10:40 Investigating the power and energy flows for a Kinetic Energy Recovery from a landing aircraft Robert CAMILLIERI University of Malta
11:00 Investigating the influence of turbofan engine design on climate for a short-to-medium-range flight network Harjot Singh SALUJA Delft University of Technology

Chairs: S. Missionnier & C. Colombo

Room 12 - view floor plan

Time Title Presented by Company
9:00 On the recovery of CH4 on the launch pad: cryogenic challenges towards an environmentally responsible access to space Davide DURI CEA
9:20 Sensitivity analysis of collision avoidance manoeuvre with low thrust propulsion Camilla COLOMBO Politecnico di Milano
9:40 Hypervelocity impact simulations between space objects with various shapes and lattice core sandwich panels Mi JANG Chungnam National University
10:00 Thermite-for-Demise (T4D): Preliminary assessment on the effects of a thermite charge in plasma wind tunnel experiments Alessandro FINAZZI Politecnico di Milano
10:20 ESD sensitivity analysis of thermites for satellite demise Filippo MAGGI Politecnico di Milano
10:40 Characterization of space objects’ attitude motion using Lomb-Scargle Periodogram Giorgio ISOLETTA University of Naples "Federico II"
11:00 Assessment of the CZ-6A RB and the H-2A DEB fragmentation events Sergio BONACCORSI Politecnico di Milano

Room 10 - view floor plan

Time Title Presented by Company
09:00 Conceptual Design of a New Test Setup to Simulate Aircraft tyre Spin-up Dynamics Rasoul SHABANI Urmia University
09:20 Wing loads models for a tiltrotor from flight data acquired during tests Robert MAAS Royal NLR
09:40 High speed flight experimental test capability development in the UAE Joao Felipe                          de ARAUJO MARTOS Technology Innovation Institute - TII
10:00 Safety review of lithium ion battery for space environment through modeling and simulation Minho LEE Chungnam National University
10:20 FIRST ACOUSTIC RESULTS OF UPPER STAGE TESTS AT P5.2  Gerhard KRÜHSEL German Aerospace Center
10:40 Testing of components for a future European heavy  launcher Alexandru-Claudiu        CĂNCESCU COMOTI
11:00 Green Propulsion Demonstrator “The LÄNDer” Florian MERZ German Aerospace Center (DLR)

Room 5 - view floor plan

Time Title Presenter Company
16:30 Free Flight Testing of Proximal Cubes in Cold Hypersonic Flow Daniel KOVACS von Karman Institute for Fluid Dynamics
16:50 Hybrid Flow Control on Hypersonic Flow Shock Wave Boundary Layer Interactions: Combinations of Micro-Ramp and Jet Blowing Mohd Rashdan SAAD National Defense Institute of Malaysia
17:10 High Enthalpy Characterization Using Tunable Diode Laser Absorption Spectroscopy Ciro SALVI German Aerospace Center (DLR)
17:30 From First Principles Physics to Massively Parallel Simulations: A High Fidelity Plasma Tunnel Model for Hypersonic Flow Conditions Marco PANESI University of Illinois Urbana-Champaign
17:50 Comparison of Different Fidelity Approaches for the Coupled Aerothermal Heating of Hypersonic Reentry Vehicle Fynn BARZ German Aerospace Center (DLR)
18:10 Heat Flux Measurement During Short Run Time Shock Tube Experiments Serguei PONIAEV Ioffe Institute
18:30 Simulation of Rarefied Gas Flow in a Channel Applying Artificial Neuron Network Iskander KHALIDOV St Petersburg Naval Polytechnic University
18:50 Rough Surface Calculation in Rarefied Gas Flow Applying the Solution of Inverse Problem Olga AKSENOVA St Petersburg Naval Polytechnic University

Chairs: Salvo Marcuccio & Federico Toson

Room 4 - view floor plan

Time Title Presented by Company
16:30 Design and deployment methods for a Martian exploration airship Philippe MACHERET EPFL
16:50 On the Optimal Preliminary Design of High-Altitude Airships: Automated Procedure and the Effect of Constraints Carlo RIBOLDI Politecnico di Milano
17:10 Technical and Regulatory Hurdles for the use of Hydrogen in Lighter-Than-Air carriers Patrick HENDRICK Université Libre de Bruxelles
17:30 Thrust-Based Flight Stabilization and Guidance for Autonomous Airships Carlo RIBOLDI Politecnico di Milano
17:50 Review of strategies for Stratospheric Airships Low-altitude Return Phase: Challenges and Risk Mitigation Strategy Patrick HENDRICK Université Libre de Bruxelles

Room 1 - view floor plan

Time Title Presented by Company
16:30 JWST Mission Post-Flight Analysis: Evolution of Fairing Environmental Conditions Frederik JACOBS European Space Agency
16:50 Multi-physics Atmospheric Entry Simulations in Pursuit of Magnetic Shielding Techniques  Thomas GREENSLADE University of Southampton
17:10 A cloud-based multi-fidelity solution for debris re-entry prediction Agnes CHAN Re CAE
17:30 Development of a photon Monte Carlo radiative heat transfer solver for CFD applications Georgii OBLAPENKO German Aerospace Center (DLR)
17:50 A Holistic CFD and DSMC Transport Database for Multiphysics Re-entry and Ablation Modeling Mitchell GOSMA University of Illinois at Urbana-Champaign
18:10 Preliminary analysis of a CFD code implementing H2/He State-to-State kinetics for Gas and Ice Giants entry conditions    Francesco BONELLI Politecnico di Bari
18:30 Finite element formulation for the analysis of hypersonic flows in thermal non-equilibrium with two- and three-temperature model Artem KOROBENKO University of Calgary

Room 6 - view floor plan

Time Title Presented by Company
15:30 Environmental and Economic Assessment of Alternative Fuels and Power Trains on Aircraft Level Andreas STROHMAYER University of Stuttgart
15:50 Environmental performance of Sustainable Aviation Fuels with high electricity input Pablo SILVA ORTIZ TU Munich
16:10 Techno-economic Analysis of Sustainable Aviation Fuels: e-fuels Leandro MAGALHÃES ISEC Lisbon Institute for Education and Sciences,
16:30 Sustainable Aviation Fuels in the European Union: a critical analysis of the ReFuelEU Aviation Initiative Stamatios VASSILOPOULOS International Institute of Air and Space Law, Leiden University
16:50 Round table discussion: what does it take to have measurable impact from alternative fuels?    

Room 11 - view floor plan

Time Title Presented by Company
16:30 Concepts for Independent Monitoring of Flight Control Laws Dominik HÜBENER Technische Universität Berlin
16:50 Optimal control of a combat aircraft with thrust vectoring  during take off Juan MANZANERO Airbus Defence and Space
17:10 Lidar-based Gust Load Alleviation - Results Obtained on a Generic Long Range Aircraft Configuration Christian WALLACE DLR (German Aerospace Center)
17:30 Flight dynamics analysis and trajectory optimization of some gliding phases Sebastien KOLB Centre de Recherche de l'Ecole de l'Air
17:50 Classification of Flight Control Law Requirements in the Context of Model-Based Software Development and Verification Alexander ARNOLD Technische Universität Berlin
18:10 Flight test verification of Hardware in the Loop simulations of the PZL-130 Orlik aircraft stabilization system that uses trim tabs in the lateral channel Albert ZAJDEL Łukasiewicz Research Network - Institute of Aviation
18:30 Model-Based Development of a Library with Standard Functions for Safety-Critical Flight Control Laws Dmitry CHERNETSOV Technische Universität Berlin

Chairs: D. Greuel & M. Bellenoue

Room 12 - view floor plan

Time Title Presenter Company
16:30 Flash-boiling effect on spray formed by two impinging jets Łukasz Jan KAPUSTA Warsaw University of Technology
16:50 DESIGN LOOP PROCESS FOR INJECTOR DOME OF LIQUID ROCKET ENGINE Alessio GIZZI AVIO S.p.A
17:10 Injection characterization of multi-injector rocket combustion chambers Arianna REMIDDI Sapienza University of Rome
17:30 Outflow measurements on porous injector elements Markus SELZER German Aerospace Center
17:50 Data-driven multi-fidelity surrogate models for Rocket Engines injector design Jose Felix                             ZAPATA USANDIVARAS ISAE-SUPAERO/CERFACS
18:10 One-dimensional Modeling of Ignition Timing for Hypergolic Bipropellant Thrusters Yu DAIMON Japan Aeropace Exploration Agency

Chairs: H. Cziezki & K.W. Naumann

Room 6 - view floor plan

Time Title Presenter Company
16:30 Vacuum Test Campaign of a Hydrogen Peroxide Propulsion System for CubeSats Angelo PASINI University of Pisa
16:50 Pt/Al2O3 catalyst for 98 w% hydrogen peroxide decomposition:  influence of spherical catalyst diameter on performance and longevity Camille COTTENOT PPrime
17:10 Implementation of Microencapsulated Fuels in Combination with Hydrogen Peroxide for Creation of New Monopropellants  Robin SCHOLL German Aerospace Center (DLR)
17:30 Activation Energy Determination of High-Test Peroxide Decomposition in Inconel 718 Crucibles Julian SCHOLL German Aerospace Center (DLR)
17:50 A 2023 overview of French in-space chemical propulsion activities supported by CNES Simone ALFANO CNES
18:10 From Lampoldshausen to Orbit: DLR Spin-off GreenDelta and the Development status of Green Propellant Thrusters based on H2O2 and N2O Lukas WERLING German Aerospace Center (DLR)

Room 3 - view floor plan

Time Title Presenter Company
16:30 Design Study of a 30kN LOX/LCH4 Aerospike Rocket Engine for Lunar Lander Application Ralf STARK German Aerospace Center
16:50 ACTiVE – Experimental investigation of the pressure distribution of linear aerospike nozzles with aerodynamic thrust vectoring Jan SLEDER-KATZMANN Technische Universität Dresden
17:10 Cooling system analysis of a clustered module aerospike for upper-stage applications Alessio SERENO Sapienza University of Rome
17:30 The Impact of Guide Tubes on Flow Separation in Rocket Nozzles Ralf STARK German Aerospace Center

Chairs: G. Ordonneau & J. Van Den Eynde

Room 12 - view floor plan

Time Title Presented by Company
16:30 Aerothermal analysis of the RETALT2 SSTO vehicle Mariasole LAURETI DLR - Institute of Aerodynamics and Flow Technology
16:50 Aerodynamic and aerothermal comparison between the CAL1C and CAL1D geometries for the CALLISTO vehicle Moritz ERTL DLR
17:10 ReFEx: Reusability Flight Experiment - Aerothermodynamics Divek SURUJHLAL German Aerospace Center (DLR)
17:30 Numerical Investigation of the Effects of Post-Combustion due to Fuel Outflow in Bleed Engine Cycles of a Retro Propulsion-Assisted Launch Vehicle Yannik FELDNER German Aerospace Center (DLR)
17:50 Preparatory CFD Studies for Subsonic Analyses of a Reusable First Stage Launcher during Landing within the RETPRO Project Tamas BYKERK DLR
18:10 A standard model for the investigation of aerodynamic and aerothermal loads on a re-usable launch vehicle Tamas BYKERK DLR

Room 2 - view floor plan

Time Title Presented by Company
16:30 Results of Air Revitalization System study by adsorbent Cédric DUPONT Air Liquide
16:50 Lunar pilot plant payload design toward in situ demonstration of oxygen extraction by carbothermal reduction Alice DOTTORI Politecnico di Milano
17:10 Regolith-based Lunar Habitats - an Engineering Approach to Radiation Shielding Yulia AKISHEVA ISAE
17:30 Plasmas for in-situ resource utilization on Mars: fuels, lifesupport and agriculture Tiago SILVA Universidade de Lisboa
17:50 Characterisation of the Dust Cloud During Landing on Lunar and Martian Surfaces Claudia JIMENEZ CUESTA University of Glasgow,

Room 12 - view floor plan

Time Title Presented by Company
16:30 Characterization of self-healing polymers under simulated space environment Laura PERNIGONI Politecnico di Milano
16:50 Aeroelastic tailoring of a composite cantilever stiffened-plate  Bara'ah FRAIHAT Khalifa University of Science and Technology
17:10 Towards toolless manufacturing of aerospace CFRP components via thermoplastic AFP Lars BRANDT German Aerospace Center (DLR)
17:30 Novel Scalable Infusion Approach, Utilizing Automated Preforming and Smart Mold with Microvibrations for Manufacture of Integral Aerospace Structures Zvicka DEUTSCH IAI
17:50 Tribological characteristics of CrN/DLC friction pair on cylinder block/valve plate interface in electrohydrostatic actuator pumps for aerospace Yucheng LI School of Mechanical Engineering and Automation, Beihang Univ.
18:10 Rapid & low-energy curing and 3D printing of thermoset composites using frontal polymerization Philippe GEUBELLE University of Illinois at Urbana-Champaign
18:30 Fabrication and Testing of Elastomeric Composite skin for 1D Morphing Wing Application DILSHAD AHMAD khalifa university

Room 6 - view floor plan

Time Title Presented by Company
16:30 Design and performance analysis of box-wing hybrid-electric aircraft: a viable solution for a sustainable regional aviation Karim ABU SALEM University of Pisa
16:50 Experimental and numerical investigations on large fuselage configurations  Guillaume ARNOULT ONERA
17:10 Developing Certifiable Liquid Hydrogen “Gondola” Airliner, Design Innovations & Challenges Raj NANGIA                    Jonathan COOPER nangia
17:30 Agent-based modelling of cargo airlift to evaluate system of systems architectures and operations Nikolaos KALLIATAKIS German Aerospace Center (DLR)
17:50 Towards Highly Integrated Engine Architectures for Next Generation SMR Aircraft: A Blended Wing Body Perspective Brendan COYLE ISAE-SUPAERO
18:10 Multidisciplinary Design Optimisation of Wing-In-Ground Effect Aircraft For Regional Coastal Transport Rejish JESUDASAN KTH Royal Institute of Technology
18:30 Establishing the DLR-F25 as a research baseline aircraft for the short-medium range market in 2035 Sebastian WÖHLER DLR

Room 12 - view floor plan

Time Title Presented by Company
16:30 From short to too-short arcs: admissible states region theory for ground-based observations Laura PIROVANO ISAE-SUPAERO
16:50 Exploring large astronomical data archives for the characterization of space debris Elisabeth RACHITH EPFL
17:10 Managing Space as  Global Commons Daniel PATTON  
17:30 History, Concepts and Challenges of suggesting an 18th UN Sustainable Development Goal related to Space Andreas LOSCH University of Bern
17:50 Can Regulatory Actions Guide or Dictate Sustainability in Space? Bernd M WEISS Luleå University of Technology
18:10 Sustainable Space Hub at EPFL: a review of ongoing research projects Stephan HELLMICH Ecole Polytechnique Fédérale de Lausanne
18:30 Sustainability Aspects of Rapid Prototyping and Frequent IODs with CubeSats Angelina FROLOVA EPFL

Room 10 - view floor plan

Time Title Presented by Company
16:30 Advanced RNP Helicopter Procedure and Instrument Flight Procedure Design Heinz WIPF AIRNAV CONSULTING GmbH
16:50 Evaluation of MEMS sensors and PSP for resolving low amplitude, instationary pressure oscillations on moving bodies Niklas WENDEL German Aerospace Center (DLR) e.V.
17:10 Experimental measurements of radio signal attenuation and Faraday rotation due to electron number density in a plasma flow Diana LUIS VKI
17:30 FLOw boiling REgimes iN microgravity Conditions Experiment (FLORENCE): REXUS-27 sounding rocket campaign Pinar ENEREN KU Leuven
17:50 Analysis of perturbative effects of a momentum flux probe in a plasma plume Séverin ASTRUC ONERA
18:10 Thermomechanical calibration of FBG sensors for aerospace applications Alessandro AIMASSO Politecnico di Torino

Room 5 - view floor plan

Time Title Presenter Company
9:00 The Common Inlet Configuration: An Advanced Boundary Layer Ingestion Engine Integration Concept Michel MEHEUT ONERA
9:20 Aerodynamic Performance of a Small Flying Wing UAV Using Passive Bio-inspired Microfibers Victor MALDONADO Texax Tech University
9:40 Investigation of Heavy Ekranoplanes Construction Concepts Alexander NEBYLOV St Petersburg State University
10:00 Design and Testing of a Reefed Disk-Gap-Band Parachute of Huygens Heritage for Sounding Rocket Recovery Mohamed SUJAHUDEEN Delft Aerospace Rocket Engineering
10:20 Flow Characteristics of a Flat Plate Airfoil Resembling Spinning Samara Using PIV G YOGESHWARAN Indian Institute of Science
10:40 The Use of Computational Fluid Dynamics Methods to Improve Aerodynamic Properties of a Newly Designed Twin-Jet Engine Aerial Target Lukasz KISZKOWIAK Military University of Technology
11:00 Modeling Periodic Evolution of Aero-Optical Caused by Supersonic Mixing Layer Yubo LI Nanjing University of Aeronautics and Astronautics

Room 1 - view floor plan

Time Title Presented by Company
9:00 Numerical simulation of phase change induced by pressure variations in cryogenic tanks Annafederica URBANOrbano ISAE SUPAERO
9:20 Direct numerical simulation of sloshing and phase change in LH2 tanks Leandro Germes MARTINEZ CNRS UMR 6614 – CORIA
9:40 CFD Analysis of the Lateral Sloshing Phenomenon inside an Aerospace LCH4 Cryogenic Tank Matteo CIMINI Sapienza University of Rome
10:00 Setup of a numerical methodology for the study of active-pressurization of cryogenic tanks Francesca ROSSETTI Sapienza university of Rome
10:20 On the capillary rise of cryogenic liquids in microgravity: numerical analysis and experiments Domenico FIORINI von Karman Institute
10:40 Investigation of Various Baffle Design Effects on Center of Gravity Deviation in a Training Aircraft Wing Fuel Tank using CFD and 1D Simulations Kerem KARAHAN Turkish Aerospace

Room 11 - view floor plan

Time Title Presented by Company
9:00 A finite state machine approach to nano-satellite SW design: the HERMES case study Margherita PICCININ Politecnico di Milano
9:20 Development of a Modular Half-Duplex Frequency-Agile X-Band Transceiver for CubeSats and Robotic Spacecraft Robin BONNY EPFL
9:40 6-DOF orbit-attitude stabilization around an asteroid by using performance based intermittent event-triggered control Hongyi XIE Politecnico di Milano
10:00 An arbitrary order H∞ interval filter for spacecraft navigation units Irryhl MOHAMMEDI IMS Laboratory - Université de Bordeaux
10:20 Filtering techniques assessment towards pose estimation enhancement for image-based proximity navigation with uncooperative space objects Gaia Letizia CIVARDI Politecnico di milano
10:40 Deep reinforcement learning for spacecraft attitude tracking manoeuvres Jan LOETTGEN University of Glasgow
11:00 Artificial Intelligence in Planetary Exploration: Enabling Autonomous Decision-Making for Spacecraft Anton IVANOV Technology Innovation Institute

Chairs: Marc Bourgeois & Antonio Esposito

Room 6 - view floor plan

Time Title Presented by Company
9:00 Study and Development of a Real-Time Pilot Performance  Monitoring System Based on Physiological Signals Gabriele LUZZANI Politecnico di Torino
9:20 Pilot’s Awareness Sensor System (PASS) Kaltham ALROWAHI Abu Dhabi Polytechnic Al Ain
9:40 Preliminary study of tracking vs boundary avoidance task effects on rotorcraft pilot involuntary response Qiuyang XIA Politecnico di Milano
10:00 A haptic device embedded in rotorcraft seats for target acquistition and tracking tasks Francesco Walter PRIZIO Politecnico di Milano
10:20 Integrating the LNAS energy-optimized trajectory guidance cues into the Airbus A320 primary cockpit displays Marie GOETZ DLR - German Aerospace Center

Room 12 - view floor plan

Time Title Presenter Company
9:00 Investigation of Different Porous Injection Technologies in a LOX/CH4 Rocket Combustor with Optical Access at Sub-, Trans- and Supercritical Conditions Ivens Daniel HoOFFMANN German Aerospace Center (DLR)
9:20 Experimental Investigation of a LOX/Methane Liquid Centered Swirl Coaxial Injector During Ignition, Startup and Subcritical Operation Alexander BEE German Aerospace Center (DLR)
9:40 Cold flow analysis of spray angle and droplet size distribution  of a pintle injector for green hypergolic propellants Philipp TEUFFEL German Aerospace Center (DLR)
10:00 Spray Behavior of Bi-swirl Injector in a LOx/LNG Small Rocket Engine Yun Hyeong KANG Pukyong National University
10:20 Work in progress: design, manufacturing and test of a H2O2-Ethanol Pintle injector on PERGOLA bench Miguel   MARTIN-BENITO CNES
10:40 Throttling hot-firing tests of methane engine thrust chamber with uni-element shear coaxial injector Cheolwoong KANG Chungbuk National University

Chairs: L. Werling & G. Jacob

Room 6 - view floor plan

Time Title Presenter Company
9:00 Development of the Liquid Green Propellants at the Łukasiewicz-Institute of Aviation Paweł STEZYCKI Institute of Aviation
9:20 Hypergolic Propellants with Hydrogen Peroxide: Carbon-Based Nanomaterials as Additives in Ionic Liquid Fuels Sophie C. RICKER DLR (German Aerospace Center)
9:40 Hypergolic ignition of amine-based fuels with hydrogen  peroxide Stefania CARLOTTI Politecnico di Milano
10:00 INVESTIGATION OF INJECTION STRATEGIES FOR A 400N STAGED HYDROGEN PEROXIDE BIPROPELLANT ENGINE Livia ORDONNEZ-VALLES Hochschule Bremen
11:00 Safe Monopropellant for Small Satellite Propulsion Systems Shinji IGARASHI IHI Aerospace Co., LTD.

Chairs: J. Steelant & C. Kirchberger

Room 3 - view floor plan

Time Title Presenter Company
9:00 Numerical investigation of the impact of injectors location on fuel mixing in the HIFiRE 2 Scramjet combustor Antonella INGENITO Sapienza University of Rome
9:20 Numerical simulation of the effect of different divergent angle of pylon Prasanth P NAIR Indian Institute of Technology Gandhinagar
9:40 Interactive optimization of fluidic injection for single expansion ramp nozzle based on a modified autoencoder Yunjia YANG Tsinghua University
10:00 Experimental and Numerical Study of Supersonic Flow in Scramjet Combustor in Expansion Tube Semra GUMRUK TOKGOZ Tubitak SAGE
10:20 Experimental study of thermal cracking characteristics of hydrocarbon aviation fuels through endothermic reactions Sung-rok HWANG Pukyong National University

Room 12 - view floor plan

Time Title Presented by Company
9:00 Disruptive and efficient rear fuselage for dual use high speed Rotary Wing platforms  Juan Manuel Jiménez GARCIA  Airbus Helicopters España SAU
9:20 Advancements in Upper Stage Technologies and Design within ESA’s Future Launchers Preparatory Programme (FLPP) Andreas FLOCK ESA
9:40 Preliminary Design of a CubeSat Demonstrator for an Origami-inspired Deployable Structure Joshika SACHITHANANDAN Delft University of Technology
10:00 Gravel Deflector Aircraft Integration José Manuel Chorro MARTINEZ AIRBUS
10:20 Load alleviation through simultaneous optimization of wingbox layout and size Hammad RAHMAN Delft University of Technology
10:40 Helicopter main rotor blade structure parametric optimization using graphic programming language Jakub KOCJAN Military University of Technology Warsaw
11:00 PROGRESS OF THE P160C SOLID ROCKET MOTOR DEVELOPMENT, FUTURE COMMON PROPULSIVE SRM FOR ARIANE 6 BLOCK2 AND VEGA-C/VEGA-E EUROPEAN LAUNCHERS Etienne BANDELIER Europropulsion

Room 10 - view floor plan

Time Title Presented by Company
9:00 Experimental validation of aircraft fuselage sections by testing at the stiffened panel level George LAMPEAS UNIV. PATRAS
9:20 Eco-efficient manufacturing of horizontal tail plane (HTP) structures for next-generation aircrafts – the role of surface pretreatment for adhesive joints Uwe LOMMATZSCH Fraunhofer
9:40 Investigations on forging of low-density Mg-Li alloys Nikolaus PAPENBERG AIT Austrian Institute of Technology, LKR Light Metals Technologies Ranshofen
10:00 Latest advances in characterization of metallic materials for aerospace industry at European Synchrotron Radiation Facility (ESRF) Andrea Francesco CIUFFINI  ESRF
10:20 Constitutive modeling of AA2024 aluminium alloy under dynamic loading Gunasilan MANAR National Defence University Malaysia
10:40 Roadmap Towards a Qualified Aluminium Green Propellant Diaphragm Tank Timothy JØRAHOLMEN1 Nammo

Chairs: E. Otero Sola & M. Bourgois

Room 6 - view floor plan

Time Title Presented by Company
9:00 Alignment of national and European R&I aviation funding programmes Gustavo ALONSO Universidad Politecnica de Madrid
9:20 Aircraft Fuel Efficiency Improvements: The Pathway to Evidence-Based Forecasts Michael WEINOLD PSI
9:40 Sonic boom of commercial hypersonic aircraft  Martina LOFQVIST https://destinus.ch/
10:00 Robust climate optimal flight planning toward identifying “win-win” solutions: concept of equivalent CO2 emissions Abolfazl SIMORGH Universidad Carlos III de Madrid
10:20 A Reinforcement Learning Approach to Conflict Resolution of Climate Optimal Trajectories Fateme BANESHI Department of Aerospace Engineering, Universidad Carlos III de Madrid
10:40 Modelling and simulation of new regulatory measures in prospective scenarios for air transport Antoine SALGAS ISAE-SUPAERO
11:00 Single and Multi-Agent Reinforcement Learning Approach to Optimise Aircraft Ground Trajectories in Airports Maxime SZYMANSKI École de technologie supérieure 

Chairs: C. Colombo & E. David

Room 12 - view floor plan

Time Title Presented by Company
9:00 Tracking the health of the space debris environment with THEMIS Camilla COLOMBO Politecnico di Milano
9:20 Promoting responsible space practices: A primer on the Space Sustainability Rating Adrien SAADA eSpace (EPFL Space Center)
9:40 Feasibility study of a single-score Life-Cycle Assessment for Space missions: preliminary results. Marnix VERKAMMEN Delft University of Technology
10:00 Using Life Cycle Assessment results as key parameters during Launch Vehicle Design and Optimisation Thomas BELLIER ISAE Supaero
10:20 Rapid Life Cycle Assessment Software for Future Space Transportation Vehicles’ Design Mathieu UDRIOT Ecole Polytechnique Fédérale de Lausanne
10:40 Comparison Study on the Environmental Impact of Different Launcher Architectures Jan-Steffen FISCHER University of Stuttgart, Institute of Space Systems

Room 12 - view floor plan

Time Title Presented by Company
9:00 A MBSE-based framework for aircraft systems design and evaluation Hajer SAADA Collins Aerospace
9:20 A Conceptual Design Methodology for Hybrid Aircraft using Multiple Disciplinary Optimization Shuanghou DENG Nanjing University of Aeronautics and Astronautics
9:40 An MBSE Architectural Framework for the Agile Design and Optimization of Complex System Francesco TORRIGIANI DLR
10:00 A data driven approach to predict life cycle cost of commercial aircraft Xiaojia ZHAO Nanjing University of Aeronautics and Astronautics
10:20 Model-based comparative evaluation of stability performance of hydraulic servo actuators and electro mechanical actuators for flight controls Mingwei SUN School of Mechanical Engineering and Automation, Beihang University
10:50 Automated filtering of on-board system architectures through certification specification requirements Carlos CABALEIRO German Aerospace Center (DLR) & Politecnico di Torino
11:10 Cabin Air Quality in Commercial Aircrafts with an Adaptive Environmental Control System Strategy Paolo GRASSO Collins Aerospace

Room 2 - view floor plan

Time Title Presented by Company
9:00 Verification of Turbopump in the Small Thrust LOX/Methane Engine Firing Tests Keisuke BANDO IHI Corporation
9:20 Pumps and Turbopumps Test by Similitude Dan. IFRIM Romanian R&D Institute for Gas Turbines
9:40 Exploring the potential of electropump feed systems for extending high thrust and deep throttle performance for CH4/LOX rocket engines Simona DANESCU COMOTI - Romanian Research & Development Institute for Gas Turbines
10:00 Research Activities on Numerical and Experimental Studies of Cavitation Instabilities in the Rocket Engine Turbopump Keita YAMAMOTO JAXA
10:20 Identification of degradation profiles for turbopump bearings in reusable liquid propellant rocket engines Federica GALLI IRSEEM-CNES
10:40 Performance estimation of supersonic impulse turbine at transient conditions Robson H. S. HAHN DLR - German Aerospace Center

Chairs: M. Gargiulo & N. Ahmed

Room 4 - view floor plan

Time Title Presenter Company
9:00 Navigation in Non-Static Environments with Autonomous Drones: A Kalman Filter Reinforcement Learning Approach Francesco MARINO Politecnico di Troino
9:20 Collaborative Localization Assisted RFI Detection Using Low-Cost COTS GNSS Receivers Naveed AHMED Norwegian University of Science and Technology
9:40 Analysis of Soil Contamination Effects on Maize Plant using
UAV-Mounted Multispectral Camera		 Massimiliano GARGIULO Italian Aerospace Research Centre
10:00 Mission Planning of Manned-Unmanned Aircraft Teaming based on Reinforcement Learning: Suppression of Enemy Air Defenses(SEAD) Mission Jae-Woo LEE Konkuk University
10:20 A holistic platform utilizing SDR for aiding automated airport and waterdrome inspections that utilize drones. Nikolaos ASTYRAKAKIS Hellenic Mediterranean University
10:40 Repeatable and scalable Image Acquisition from Drone
equipped with Multispectral and Thermal Sensor for proximal
sensing processing of Nature Based Solutions		 Francesco TUFABO Italian Aerospace Research Centre
11:00 Precision Meteorological Prediction Employing A Data-Driven, Adaptive, Real-Time (DART) Approach Sujit SINHA University of Kentucky

Room 5 - view floor plan

Time Title Presenter Company
16:00 Surrogate Model-Based Acoustic Optimization of Jet Nozzle Exit Geometries using Large Eddy Simulation Guangda YANG Northwestern Polytechnical University
16:20 Study of Geometry Effects on Aerodynamics and Aeroacoustics of Various Scale Rotors Witold KLIMCZYK Institute of Aviation
16:40 Investigating the Noise Reduction Techniques for Rotor Drones Harika GURRAM TU Delft
17:00 Aerodynamic and Aeroacoustic Effects of Bio-inspired Rotors to a Multi-Rotorcraft: A Numerical Study Robbie WILKINS University of the West of England
17:20 Method for Analysis of Propeller Performance for off-the-shelf Propellers Using Reverse CAD and Aerodynamic Algorithm Craig MASCARENHAS Harvard University Cambridge UK
17:40 Cavity noise reduction with sweeping actuators Abderrahmane BELKALLOCH University of Blida
18:00 Reduced-Scale Generic Future Fighter Aerodynamic Model Using Neuro-Fuzzy Hybridized with Differential Evolution Vitor SANT'ANA Linköping University

Room 1 - view floor plan

Time Title Presented by Company
16:00 Numerical Analysis on the Film-cooling Effect with Varying Coolant Flow-rate in GCH4-LOx Liquid Rocket Engines Hong Yeong PARK Pukyong National University
16:20 Simulation of plume impingement on flat plates via the hybrid Fokker-Planck – DSMC approach Leo BASOV German Aerospace Center (DLR)
16:40 Computational Study for Axisymmetric Nozzle at Transonic and Supersonic Flow Regime Berker ÖZKARADUMAN Turkish Aerospace
17:00 Numerical simulation of flight effect on the afterburning plume exhausting from a solid rocket motor Adrien LANGENAIS ONERA
17:20 Hybrid NS-DSMC simulation of a full scale solid rocket motor reactive exhaust at high altitude Antoine CLOUT ONERA
17:40 Effect of nozzle seal rupture on internal motor dynamics Laurent FRANCOIS ONERA
18:00 A numerical study of resonance ignition for space propulsion systems T. JEREMY                                 P. KARPOWSKI STFS, TU Darmstadt

Room 11 - view floor plan

Time Title Presented by Company
16:00 All-in-one integrated UAV avionics architecture with AI capabilities and 5G connectivity Kirill SHILOV Sky-Drones Technologies Ltd
16:20 Testing of an Autonomous Rocket Engine Control Approach on a Cold Gas Vertical Take-Off Vertical Landing Platform: Preliminary Results and Outlook Felix EBERT Technical University of Munich
16:40 Aerodynamic Parameter Estimation for Fixed-wing UAV Using Iterated Extended Kalman Filter Junhyun LIM ChungNam National University
17:00 Region of Attraction Estimation Using Multiple Shape Functions in Sum-of-Squares Optimization for Aerospace System Bhaskar BISWAS Cranfield University, U.K.
17:20 Nonlinear model predictive guidance for tilt-rotor UAV performing terrain-following flight for mine detection Sangmin LEE Seoul National University
17:40 Total Energy Control for the Automatic Landing of UAS with Large Aspect Ratio and Low Wing Loading Bryan LAABS TU Berlin
18:00 A Tailless Flapping Wing MAV’s Attitude Stabilization using observer-based sliding mode control Inrae KIM Chungnam National Univ.

Chairs: Andrea Alaimo & Sara Bagassi

Room 6 - view floor plan

Time Title Presented by Company
16:00 ACORDE: A new method to assess onboard radiation risks related to human factors Hernán ASOREY Comisión Nacional de Energía Atómica 
16:20 Enabling Single-Pilot Operations technological and operative scenarios: a state-of-the-art review with possible cues Nicola PUCA Politecnico di Torino
16:40 Virtual pilot: a review of the human pilot's mathematical modeling techniques Francesca RONCOLINI Politecnico di Milano
17:00 Investigation of seated passengers vibration using a full-flight simulator Antonio ESPOSITO Università degli Studi di Enna "Kore"
17:20 Extended Reality Safety Nets for Attention Guidance in Airport Control Towers Sara BAGASSI University of Bologna

Chairs: J. Deeken & A. Urbano

Room 12 - view floor plan

Time Title Presenter Company
16:00 Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation Riccardo BISIN Politecnico di Milano
16:20 DESIGN LOOP PROCESS FOR COOLING JACKET OF LIQUID ROCKET ENGINE Michele Urbano MARTINI AVIO S.p.A
16:40 Numerical Framework for the Investigation of a Transpiration Cooled LOx/LH2 Rocket Engine Combustion Chamber Jonas PEICHL Deutsches Zentrum für Luft-und Raumfahrt
17:00 Investigation of Heat Transfer and Nucleate Boiling of Ethanol in Additively Manufactured Cooling Channels Sebastian SOLLER ArianeGroup
17:20 Improving cooling channel heat transfer via femtosecond laser texturing Frederik MERTENS KU Leuven
17:40 Characteristics of a superheated wall cooling through pulsed injection of a liquid jet Noritaka SAKO Kyoto University

Chairs: H. Cziezki & L. Galfetti

Room 6 - view floor plan

Time Title Presenter Company
16:00 Nitromethane as a Green Propellant: First Results of a Combustion Test Campaign Maxim KURILOV DLR Deutsches Zentrum für Luft- und Raumfahrt
16:20 Fluid Hammer Phenomena in a Nitromethane-based Green Propellant in Hot Gas Test Runs Sebastian KLEIN German Aerospace Center
16:40 Influence of La And Si Promoters on the Anaerobic Heterogeneous Catalytic Decomposition of Ammonium Dinitramide (ADN) via Alumina Supported Iridium Active Sites Kerem Emre ERCAN Roketsan Missile Inc.
17:00 Nitrous Oxide Modelling: from Single Phase Incompressible to FML Mass Flow Rate Model Simone La LUNA Politecnico di Milano
17:20 Cold-Flow Testing of various injector designs for a novel hypergolic and green propellant combination developed at DLR Lampoldshausen Alberto SARRITZU University of Pisa
17:40 Satellite Water Propulsion: Electrolyzer Development & FMEA Alexandros VIKAS Istitute of Space Systems

Room 3 - view floor plan

Time Title Presenter Company
16:00 Organic Rankine Cycle Waste Heat Recovery for Turboshaft Engines of Turboelectric Aircraft Dabo KREMPUS Delft University of Technology
16:20 Simulation of Plasma Injector Module for Plasma Assisted Combustion in scramjet Ancelin ROCAMORA ONERA
16:40 Performance Assessment of a 1D Steady Modeled Thermally Choked Dual-Mode Ramjet Jean-Etienne DURAND ONERA
17:00 Low-frequency shock oscillations in supersonic planar nozzles Abdellah HADJADJ INSA Rouen
17:20 Unsteady Thermal Throat Position under Acoustic Forcing Frédéric OLIVON ONERA

Room 12 - view floor plan

Time Title Presented by Company
16:00 A 3D aeroelastic beam modelling approach for time domain non-uniform lifting structures flutter analysis Carmelo Rosario VINDIGNI Kore University of Enna
16:20 Effect of aeroelasticity on the acoustic imprint of TOP contoured nozzles in overexpanded conditions Martina FORMIDABILE Delft University of Technology
16:40 Comparison of Tiltrotor Whirl Flutter Analyses with Gimballed and Hingeless Hub Models Ui-Jin HWANG Chungnam National University
17:00 Stability and flying qualities analysis of flexible aircraft by coupling the Vortex Lattice method and the discontinuous Galerkin method Fernando MONTANO Università degli Studi di Palermo
17:20 Analysis of the structural behavior of wings with nonlinear components for passive load reduction Daniel HAHN Institute of Aircraft Design and Lightweight Structures, TU BRaunschweig
17:40 Load alleviation using polymorphing wings: The effect of the morphing rate.  Zawar HAIDER Khalifa University
18:00 Smart Blade Dynamic Stall Suppression Reza MOOSAVI University of Hertfordshire

Room 10 - view floor plan

Time Title Presented by Company
16:00 Convergence of Machine Learning and Finite Element methods, the smart superelements Jean-Daniel LECUYER Hexagon Manufacturing Intelligence
16:20 Thermal transfer effects on postbuckling behaviors of common bulkhead structures Chang-Min LEE Chungnam National University
16:40 Derivation of Buckling Knockdown Factors for Hemispherical Shells with Foam Core Chang-Hoon SIM Chungnam National University
17:00 Wing Structure Optimization of a Truss-Braced Wing Regional Jet Aircraft with Strength, Stiffness, and Stability Requirements Saeed HOSSEINI Amirkabir University of Technology
17:20 Derivation and Verification of a Flexible Hexapod Model for Multi-Body Space Observatories Alison PONCHE University Carlos III of Madrid
17:40 Predictions of wing structural responses by physical-based machine learning framework Yujie GUO Nanjing University of Aeronautics and Astronautics
10:40 High-fidelity multidimensional models for stress and dynamic analyses of advanced helicopter blades Rodolfo AZZARA Politecnico di Torino

Chairs: J. van den Eynde & Marc Bourgois

Room 12 - view floor plan

Time Title Presented by Company
16:00 Multi-Objective Multidisciplinary Design Optimization of Regional Truss-Braced Wing Jet Aircraft Saeed HOSSEINI Amirkabir University of Technology
16:20 Next steps in aerostructural design of ultra-high aspect ratio wings Yiyuan MA Technische Universität Braunschweig
16:40 Multi-fidelity Multidisciplinary Analysis Methodology for Preliminary Design of Ultra-high Aspect Ratio Strut Braced Wing Aircraft Shon MORI ONERA
17:00 Thermoplastic Induction Welding for Sustainable Aircraft: an Industrial Perspective Laura MAININI Collins Aerospace

Chairs: C. Colombo & E. David

Room 12 - view floor plan

Time Title Presented by Company
16:00 Application of LLP in Satellite Supply Chain Abrahim BAHARI  
16:20 Optimized multi-satellite manoeuvring strategy for responsive Earth observation Nicola CIMMINO University of Naples Federico II
16:40 A Concurrent Methodology for Optimizing Constellation Deployment and Launcher Selection. Brandon ESCAMILLA Universidad Carlos III de Madrid
17:00 MOTUS - motorized dispenser for the nanosatellite constellation deployment Tomasz PALACZ AGH UST
17:20 Propellant Management Challenges Related to the Operation of the Depot on Orbit Mikaeel SHAIKH,            Biswajeet PRADHAN Universitaet Bremen
17:40 Suborbital Taxi Transfer Manan JOSHI MIT ADT University

Room 6 - view floor plan

Time Title Presented by Company
16:00 Ariane 6 Cryogenic Upper Liquid Propulsive Module Multi-Boost Mission Development, A System Inter Disciplinary Challenge François PEYRAUD ARIANE GROUP
16:20 Analysis of sonic boom propagation and population disturbance of hypersonic vehicle trajectories Steffen CALLSEN German Aerospace Center (DLR)
16:40 Space System Certification for Human Spaceflight-Historical Practices and New Approaches for Safety Tim A. BULK SAS International
17:00 Comparative review of Multidisciplinary Design Analysis and Optimization architectures for the preliminary design of a liquid rocket engine Lucas BARATON ISAE SUPAERO
17:20 Design Optimisation of Hybrid Propellant Launch Vehicles Mitchell GALETTLY University of Sydney
17:40 Semi-supervised temperature field information fusion method based on taylor modal decomposition for spacecraft application Li XINCHENG National University of Defense Technology
18:00 From the ground to DREAM ON: ground support equipment to new PERSEUS bi-liquid demonstrator Fabien CHAMPALOU CT INGENIERIE

Room 2 - view floor plan

Time Title Presented by Company
16:00 A performance modelling approach to open fan propeller module Nicolas TANTOT Safran SA
16:20 Stability analysis of simplified labyrinth seals model to geometric and flow hypotheses Giorgia FOSCHI Ecole Centrale de Lyon
16:40 Investigation of tip flow structures of a transonic axial compressor stage based on the harmonic balance method  Koray SEVINC TUSAŞ Engine Industries Inc.
17:00 Machine Learning Applied to Turbine Inlet Manifold Instrumentation Sarah GELBING ArianeGroup GmbH
17:20 Keeping turbofans cool: Aerodynamic upgrade of bypass    surface heat exchangers (EU Project SACOC) Jorge                GARCIA-TISCAR Polytechnic University of Valencia
17:40 Piezo actor based HCF testing of LRE turbine blades Jörg RICCIUS DLR Lampoldshausen

Chairs: L-M. Garcia-Cuevas & A. Kopyt

Room 4 - view floor plan

Time Title Presenter Company
16:00 Design of unmanned air vehicles with distributed electric propulsion: range improvement and noise emission Luis-Miguel GARCIA-CUEVAS Universitat Politècnica de València
16:20 Possible Design Configurations for Martian VTOL Aerobots Vishal YOUHANNA Cranfield University
16:40 Design of an Unmanned Return Module for the Conditions of Stratospheric Phenomena Measurements Pavol PECHO University of Zilina
17:00 Flight efficiency of multirotor, new definitions and function sensitivity in-flight tests Wojciech GRENDYSA Warsaw University of Technology
17:20 A Versatile Dynamic Rotor and Propeller Model for eVTOL Simulation Applications Ceren Cansu ESMEK Turkish Aerospace
17:40 Augmented Reality in UAV Simulator for Advanced Training Antoni KOPYT Warsaw University of Technology

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