Chairs: nc
15:05 Numerical Simulation of Petrea Volubilis Falling Seed
MENDEZ Carlos (Universidad Politécnica de Madrid, Universidad Nacional de Asunción)
Lien
15:30 Nudging-Based Steady State Estimation of Turbulent Flows Around an Airfoil Near Stalling Conditions
MARQUET Olivier (DAAA, ONERA The French Aerospace Lab, Meudon, F-92190, France)
15:55 Towards the Prediction of Wall Pressure Fluctuations for Space Launchers using ZDES-based Convolutional Neural Networks
LECLER Simon (DAAA, ONERA, Université Paris Saclay)
16:20 Towards a Numerical Multi-Fidelity Strategy for Unsteady Aerodynamics Studies of Reusable Launch Vehicles: Application to Arianne Next
WEISS Pierre-Elie (ONERA)
16:45 Effect of ‘Ramped Vane’ Vortex Generators on a Flare-Induced Shock-Boundary Layer Interaction Flowfield
T Nilavarasan (Defence Institute of Advanced Technology)
17:10 Energy Transfer in Turbulence Using Lattice Boltzmann Method Based on Large Eddy Simulation
ALOUI Fethi (Université Polytechnique Hauts-de-France, LAMIH UMR CNRS 8201, INSA Hauts-de-France)
Chairs: nc
15:05 Restrike Model for an MHD Solver: Application to Plasma-Assisted Supersonic Combustion in a Scramjet
BOURLET Aymeric (ONERA – Centre de Palaiseau)
15:30 Simulation of Plasmas for Electric Propulsion Using the Energy-Conserving Semi-Implicit PIC Scheme
PARODI Pietro (KU Leuven and von Karman Institute for Fluid Dynamics, Belgium)
15:55 Heat Flux Characterization of an Under-Expanded Supersonic Plasma Jet Over a Catalytic Probe
CAPRIATI Michele (von Karman Institute for Fluid Dynamics – VKI))
16:20 Assessment of Electron Transpiration Cooling Phenomena in Inductively-Cooled Plasma Facility
LAFAURIE Victor (von Karman Institute for Fluid Dynamics – VKI))
16:45 Development of a Multi-Component Diffusion Fluid Solver for a Two-Temperature Argon Plasma Sheath
GANGEMI Giuseppe Matteo (von Karman Institute for Fluid Dynamics – VKI))
17:10 Effect of Electron Number Densities on the Radio Signal Attenuation in an Inductively Coupled Plasma Facility
LUIS Diana (von Karman Institute for Fluid Dynamics – VKI))
Chairs: ANSELMO Luciano & MARTINEZ MORALES Juan Esteban
15:05 Analysis of conjunctions between two satellites with no communication
LUCKEN Romain (Share My Space)
15:30 Analysis and Assessment of Collision for Large Constellations Satellites
ABDEL-AZIZ Yehia (National Research Institute of Astronomy and Geophysics – NRIAG))
15:55 Utilization of CubeSat nanosatellites as reference objects for evaluating the ballistic coefficients of low-altitude satellites
BELOKONOV Igor (Samara National Research University)
16:20 Machine Learning techiques applied to space objects uncontrolled re-entry predictions
PANICO Alessandro (Politecnico di Milano)
16:45 CNES tools and methods for de-orbit and re-entry trajectories evaluation
GOESTER Jean-François (CNES)
17:10 Thermite-for-Demise (T4D): Concept Definition for Exothermic Reaction-Aided Spacecraft Demise during Re-entry
FINAZZI Alessandro (Politecnico di Milano)
17:35 BFS « Back From Space » , an atmospheric reentry kit for Newspace application
PIERONNE Christian (ESTACA)
Chairs: nc
15:05 Incremental Nonlinear Dynamic Inversion Control with Gaussian Process Regression For Aircraft Carrier Landing
LAMSU Kim (Korea Advanced Institute of Science and Technology)
15:30 A point of view on machine learning for GNC for space applications: towards non linear control
GANET-SCHOELLER (Martine ArianeGroup)
15:55 Global linear parameter varying (LPV) model development for fighter aircraft
MILLIDERE Murat (Middle East Technical University)
16:20 Anti Sloshing Control Law Design For Launchers Using A Model-Free Approach
COCAUL Périclès (DTIS, ONERA, Université Paris Saclay, F-91123 Palaiseau, France)
16:45 Hybrid Genetic Algorithm Solution to Structured H Infinity Control Problem and Application to Lateral – Directional Dynamics of Highly Maneuverable Aircraft
OZKAN Salih Volkan (Aerospace Engineering Department, Middle East Technical University, Ankara, 06800, Turkey)
17:10 Reference Governor Based Solution for Satellite Attitude Control with Sloshing and Actuation Constraints
CASSARO Mario (ONERA – The French Aerospace Lab – Centre de Toulouse)
17:35 Flight Control System Constraints on The Yaw Instability Level of Fighter Aircraft Design
ÖZNURLU Can (Middle East Technical University)
Chair: BACH Christian
15:05 Pre-conceptual staging trade-offs of reusable launch vehicles
GUILLERMO JOAQUIN (Dominguez Calabuig DLR)
15:30 Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact
SARRITZU Alberto (Universita di Pisa)
15:55 Health Monitoring for RLVs: Architecture Selection and Discussion
VENNITTI Andrea (TU Dresden)
16:20 Reliability estimation methodology for Liquid Rocket Engines
AYALA FERNANDEZ Lucía (TU Braunschweig)
16:45 Sensibility study for different nozzle configuration on the heat load and aerodynamic behaviour for the THEMIS demonstrator
LANTELME Melissa (ONERA)
17:10 On The Integration of Aerospike Nozzles In Rotating Detonation Engines
BACH Christian (TU Dresden)
17:35 Round Table Discussion
BACH Christian (TU Dresden)
Chairs: DOS SANTOS HAHN Robson & GIRARD Nathalie
15:05 TARES2020: Technologies for Future Liquid Propellant Engines at ArianeGroup
SOLLER Sebastian (Ariane Group Ottobrunn)
15:30 Configuration Design Studies of a LOX-LCH4 Booster Engine and Stage for a Futuristic Indian Launcher
MOHAN Kiran (Liquid Propulsion Systems Centre (LPSC), ISRO)
15:55 Configuration Studies on An Electric Pump Fed Upper Stage Rocket Engine
MOHAN Kiran (Liquid Propulsion Systems Centre (LPSC), ISRO)
16:20 Prospective of Self-Pressurized Technology for In Space Satellite Mission
LA LUNA Simone (Politecnico di Milano)
Chairs: Nathalie GIRARD & Michel BERDOYES
15:05 LES and ROM of the acoustic damping in a nonreactive pressurized test rig including coupled cavities and multiple jets
MARCHAL David (Laboratoire EM2C, CNRS, CentraleSupélec, Université Paris-Saclay)
15:30 Low-order modeling of combustion instability using a hybrid real/ideal gas mixture model
D’ALESSANDRO Simone (Sapienza Università di Roma)
15:55 Disturbance energy transport, a tool to analyze backward-facing step combustion instabilities
KLEIN Jean-Michel (ONERA)
16:20 Preliminary study of the high-frequency instability of an aerospike rocket engine
ROSSI Federico (Pangea aerospace)
Chairs: NAUMANN Karl-Wieland & PARAVAN Christian
15:05 Thermophoresis as a possible mechanism for aluminum oxide lobe formation
GALLIER Stany (ArianeGroup)
15:30 Evolution of aluminum droplets in solid propellant combustion by image analysis using deep learning
AIRIAU Magdeleine (ONERA/DMPE)
15:55 Effect of Coated Nano-Aluminum Powders on the Agglomeration in Solid Propellant
YAVOR Yinon (Afeka College of Engineering)
16:20 Combustion of Green AN-Al-Water Propellants
YAVOR Yinon (Afeka College of Engineering)
16:45 Study of the effect of particles on the two-phase flow field and radiation in aluminized rocket engine plumes
DE GIORGI Maria grazia (University of Salento Department of Engineering Innovation)
17:10 Numerical simulation of the boron particle agglomeration in combustion of boron-containing solid propellants
RASHKOVSKIY Sergey
17:35 A Revised Model of Ammonium Perchlorate Combustion with Detailed Kinetics
BERNIGAUD Pierre (ONERA – The French Aerospace Lab)
Chairs: nc
15:05 Glide back recovery of a winged reusable launch vehicle with wind estimate
EDORH Prince (CNES)
15:30 Semi-free oscillation method for dynamic stability characterization on re-usable launcher first-stage
PARIS Sebastien (von Karman Institute for Fluid Dynamics)
15:55 Optimal reconfigurable allocation of a multi-engine cluster for a reusable launch vehicle
MURATA Renato (ONERA)
16:20 Control strategies comparison and performance evaluation for a reusable VTVL platform based on a rocket engine
AFILIPOAE Tudorel-Petronel (National Institute for Aerospace Research ‘Elie Carafoli’)
16:45 Impact of control gain design on Remaining Useful Life for a Liquid Propellant Reusable Engine
THUILLIER Julien (CNES)
17:10 Hypersonic Retrograde Propulsion Experiments – A Basis for Validation of CFD within RETPRO
KIRCHHECK Daniel (DLR)
17:35 Reconstruction of Wind Tunnel Tests using CFD for a Reusable First Stage during Rocket Retro-propulsion
BYKERK Tamas or KARL Sebastian (DLR)
Chairs: nc
15:05 Product Assurance Overview of Additive Manufactured Components for Space Applications
ZUIN Davide (Politecnico di Milano)
15:30 Space Flight Hardware fabricated by Additive Manufacturing to JUICE Mission
PERIÑAN BUTRON Antonio (CATEC)
15:55 Additive manufacturing capabilities for heat switch technology: Key challenges & knowledge gaps
MASEK Jakub (Brno University of Technology, Faculty of Mechanical Engineering)
16:20 Additive manufacturing process development for realization of Preburner Pump Impeller of LOX hydrocarbon based rocket engine using AlSi10Mg material
VERMA Rajeev (Indian Space Research Organisation)
Chairs: nc
15:05 An Overview of the EURASTROS Study
GÜLHAN Ali (German Aerospace Center – DLR e.V.)
15:30 System design of EURASTROS reference configurations and mission
PLEBUCH Alex (ArianeGroup)
15:55 Cost Estimation and Development Approach of the EURASTROS Concept
BRAUKHANE Andy (DLR – German Aerospace Center)
16:20 EURASTROS capsule design and re-entry analysis
MARQUARDT Pascal (DLR
16:45 EURASTROS ascent trajectory and abort analysis
BERGMANN Kevin (German Aerospace Center (DLR), Institute of Space Systems)
Chair: RÜTTEN Markus
15:05 Aerodynamic and structural study of active flow and morphing deformation high lift system, integrated in the leading edge of transport aircraft wing
CAMARA AGUIAR Nelson (Altran Technologies SA)
15:30 Application of Flow Control in the Wing-Pylon Region for Lift Enhancement
JABBAL Mark (University of Nottingham)
15:55 Effects of Zero Net Mass Flux devices on a Next-Generation Tiltrotor airplane in subsonic regime by numerical simulation at high Reynolds number
MAROUF Abderahmane (ICUBE / University of Strasbourg)
16:20 Experimental Investigation on fractal/multiscale trippings for passive control of turbulent flow separation
SEPETAUSKAS Vinicius (LMFL / Centrale Lille)
16:45 Experimental assessment of the active flow control over the flight deck of a frigate
DERHILLE Elvina (Onera – DAAA/ELV)
17:10 An experimental study of trailing vortex dynamics in cruise and high-lift wing configurations.
CRUZ MARQUEZ Rolando (LMFL / Onera)
Chairs: nc
09:00 Aerodynamic Calculation of Rough Surface in Rarefied Gas Flow Applying the Solution of Inverse Problem
AKSENOVA Olga (St.Petersburg Naval Polytechnic University)
09:25 Simulation of Rarefied Gas Flow Applying Artificial Neuron Network
AKSENOVA Olga (St.Petersburg Naval Polytechnic University)
09:50 HyperCODA – Extension of Flow Solver CODA Towards Rocket Flows
FECHTER Stefan (DLR – German Aerospace Center, Institute of Aerodynamics and Flow Technology)
10:15 Evaluation of Aerodynamic Characteristics in Oscillatory Coning Motion Using CFD Methods
SEREEZ Mohamed Coventry University)
10:40 Creating an External Store Separation Analysis Infrastructure Using the Grid Method with the Help of Open Source Software
DEMIR Görkem (Turkish Aerospace Industries)
11:05 A Dynamic Mode Decomposition Approach for Data Assimilation in the Presence of Parameter Uncertainties
VERVYNCK Arthur (DAAA, ONERA, Université Paris Saclay, F-92190 Meudon, France)
Chairs: ABDEL-AZIZ Yehia & LUCKEN Romain
09:00 Starting procedure for space-based laser trackers to autonomously reach distant reflecting targets by means of very narrow beams
GAMBI Jose M. (U. Carlos III de Madrid)
09:25 Shadow Imaging of Geostationary Satellites: silhouette reconstruction from accurate polychro-matic modelling of diffraction and atmospheric disturbances
LABRIJI Hanae (DTIS, ONERA, Université Paris Saclay)
09:50 SNOS: automatic optimal observations scheduling for sensor networks
FARACO Niccolò (Politecnico di Milano)
10:15 A software suite for orbit determination in Space Surveillance and Tracking applications
MONTARULI Marco Felice (Politecnico di Milano)
10:40 Shape Memory Composite Structures for Space Debris Removal
SANTO Loredana (University of Rome Tor Vergata)
11:05 Design of a vehicle for active debris removal: PERSEPHONE (Performing Space Environment Protection from Hazardous Objects by Net Elimination)
MEISSE Elise (Institut Polytechnique des Sciences Avancées – IPSA)
11:30 Debris removal in GEO by Ion Beam: Challenges and Prospects
ASLANOV Vladimir (Samara National Research University)
Chairs: MISSONNIER Sophie – (TCHOUKIEN David)
May the Force be with You
TCHOUKIEN David (CNES)
Minerva, igniting the future
CHOPINET Jean-Noël (Ariane Group)
Using Motopumps to increase rocket engine performances
BOUISSON Emrys (IPSA/Innovative Propulsion Laboratory)
Using an adaptive nozzle to improve rocket engine performances
SENON Julien (IPSA/Innovative Propulsion Laboratory)
The 5th element: Modular ground support equipment to new PERSEUS bi-liquid launcher
CHAMPALOU Fabien (CT Ingénierie)
Extended Q&A (through digital board)
Chairs: MARTELLI Emanuele & SOLLER Sebastian
09:00 Linear dynamical model of overexpanded supersonic jet resonances
JAUNET Vincent (Institut PPRIME — ISAE-ENSMA)
09:25 High Altitude Rocket Reactive Jet Flow Simulations with a Hybrid NS-DSMC Methodology
CHARTON Virgile (ONERA – Centre de Palaiseau)
09:50 Parametric study of transition fluidic control in a dual-bell nozzle
FERRERO Andrea (Politecnico di Torino)
10:15 Advanced nozzle concept trade-off and selection criteria based on launcher mission constraints
WEBER Felix (Sapienza Università di Roma)
10:40 Impacts of Solidity and Radius Ratio on Centrifugal Turbines
LIU Yu Min (Aero-Thermo-Mechanics Dept., Université Libre de Bruxelles / EPF École d’ingénieurs)
11:05 Experimental study on the effect of cryogenic two-phase flow inlet conditions on the suction capacity of a high speed centrifugal pump equipped with an inducer: first results on saturated pure liquid
DURI Davide (ArianeGroup Vernon)
11:30 Design Practices on Supersonic Turbines for Liquid Propellant Rocket Engine in the Frame of CNES/DLR Cooperation
DOS SANTOS HAHN Robson Henrique (DLR – German Aerospace Center, Institute of Space Propulsion)
Chairs: HARDI Justin & DUCRUIX Sébastien
09:00 REST HF-7 and HF-9 Test Case: Lessons learned for comparing simulation results with test data of a representative LOX/H2 thrust chamber with high-frequency combustion instabilities
ARMBRUSTER Wolfgang (DLR – German Aerospace Center, Institute of Space Propulsion)
09:25 REST HF-9 Test Case: Numerical reproduction of OH* radiation measurements of unsteady supercritical LOx/H2 combustion
TONTI Federica (DLR – German Aerospace Center, Institute of Space Propulsion)
09:50 REST HF-9 test case: Large-Eddy Simulation of DLR’s BKD configuration
SCHMITT Thomas (Laboratoire EM2C, CNRS, CentraleSupelec, Université Paris-Saclay)
10:15 REST HF-10 test case: URANS Simulations of Excited Methane Flames under Real Gas Conditions
KAESS Roland (Ariane Group Ottobrunn)
10:40 REST HF-10 Test Case: Numerical Simulation of a Single Coaxial LOX-CH4 Injector with Forced Mass Flow Oscillations Using the DLR TAU-Code
HORCHLER Tim (German Aerospace Center (DLR), Institute of Aerodynamics and Flow Technology)
11:05 REST HF-10 test case: Large-Eddy Simulations using the AVBP solver
MARCHAL David (Laboratoire EM2C, CNRS, Centrale Supelec, Université Paris-Saclay)
Chairs: PARAVAN Christian & RASHKOVSKIY Sergey (Backup: ORLANDI Oliver)
09:00 Solid Rocket Motor Internal Ballistics Simulation Using Eulerian Multiphase Models
FAVINI Bernardo (Sapienza University of Rome)
09:25 High-fidelity one-dimensional model of solid propellant combustion: formulation, numerical strategy, coupling with a CFD software for simulating ignition transients in complete solid rocket motors
FRANCOIS Laurent (ONERA/DMPE)
09:50 Non-linear one-dimensional combustion response model integration in a CFD software, test case and simplified rocket motor applications
CARRICART Maialen (ONERA/DMPE)
10:15 Quantitative experimental characterization of solid-propellant surface temperature before ignition for future model validation
DEVILLERS Robin (ONERA/DMPE)
10:40 SRM ignition studies at lab-scale
ORLANDI Olivier (ArianeGroup)
Chairs: nc
09:00 Study on future European winged reusable launchers
CALLSEN Steffen (DLR)
09:25 Update on the THEMIS low cost and reusable rocket stage demonstration
VILA Jerome (ArianeWorks)
09:50 Evaluation of Parametric Cost Estimation in the Preliminary Design Phase of Reusable Launch Vehicles
STAPPERT Sven (DLR)
10:15 Design of fly-back reusable launch vehicle architecture using air-breathing propulsion
BALESDENT Mathieu (ONERA)
10:40 Uncertainty-based approach to assess optimal design margins for future aerospace systems
BALESDENT Mathieu (ONERA)
11:05 Standard Reuse System for Small Launch Vehicles MAROQUENE
FROISSART François (Sirius Space)
11:30 GARRUD: Autonomous re-Entry system technology demonstrator for sounding rockets
MHATRE Pranjal (Bharati vidyapeeth college of engineering, Navi Mumbai)
Chairs: nc
09:00 Metalization of polymer based composite by cold spray
DELLORO Francesco (Mines-Paris-Tech)
09:25 Analysis of the fire reaction of fiber reinforced polymer matrix composites exposed to a flame
COPPALLE Alexis (CORIA INSA Rouen)
09:50 Study of carbon nanotube/cyanate ester composite materials dedicated to cryogenic storage vessels
BOUILLONNEC Jonathan (CNES)
10:15 New generation of sustainable and safe antimicrobial surfaces for Space indoor applications
DUDAY David (LIST, Luxembourg Institute of Science and Technology)
10:40 3D printing of multifunctional polymer for space application
LAFONT Ugo (European Space Agency)
Chairs: nc
09:00 Solid Rocket Motors and Gas Dynamic Systems for Orbital Propulsion
RINGEISEN Axel (Bayern-Chemie GmbH)
09:25 A Dynamic Mass flow rate Tool for the PPS®5000 Hall Thruster Unit
KOPPEL Christophe (KopooS Consulting Ind.)
09:50 Anomaly Detection Method of Spacecraft Propulsion Using Multiplexed Fiber Bragg Gratings
TOMINAGA Kohji (Japan Aerospace Exploration Agency)
10:15 Lunanova kick stage study: An overview of the system propulsion tradeoffs
ORDONEZ VALLES Livia (Hochschule of Bremen/Technische Universität Dresden)
10:40 Theion Crystal Battery: a gamechanger for the space industry
EHMES Ulrich (Theion)
11:05 A Model-Based Approach to Flight and Ground Software for Constellations
MENDHAM Peter (Bright Ascension Ltd)
11:30 Airships for Satellite Data Acquisition and Disaster Management
PARTHIBAN P. (Indian Space Research Organisation)
Chair: PERNOD Philippe
09:00 On the fabrication of durable dielectric-barrier discharge plasma actuators
HEHNER Marc T. (Institute of Fluid Mechanics (ISTM), Karlsruhe Institute of Technology – KIT)
09:25 Leading Edge Vortex Induced Effects on Electrical Characteristics of a DBD Plasma Actuator
KISSING Johannes (Institute of Fluid Mechanics and Aerodynamics (SLA), TU Darmstadt)
09:50 Numerical Reconstruction of Plasma Wind Tunnel Experiments Featuring Magnetohydrodynamic Effects
DONALDSON Nathan (University of Southampton)
10:15 Interactions in micro-jets forced by dielectric barrier discharge
FRIDLENDER Tom (Institut PPRIME – UPR 3346 – Université de Poitiers)
10:40 Plasma-assisted heat dynamics in supersonic channel flow.
ZNAMENSKAYA Irina (Lomonosov Moscow State University)
Chairs: nc
15:35 Numerical Investigation on the Aerodynamic Design of Quadrotor Blades Operating in the Martian Atmosphere
CARREÑO RUIZ Manuel (Department of Mechanical and Aereospace Engineering, Politecnico di Torino)
16:00 Experimental Aerodynamic Investigation of a Krueger Flap Device Using Particle Image Velocimetry
TANGUY Geoffrey (Univ. Lille, CNRS, ONERA, Arts et Metiers Paris Tech, Centrale Lille, Laboratory of Fluid Mechanics of Lille Kampé de Fériet F-59000, France)
16:25 Flow Separation and Wake of a Transport Aircraft Configuration at Beginning Stall
EHRLE Maximilian (Institute of Aerodynamics and Gas Dynamics, University of Stuttgart, Germany)
16:50 Novel Morphing High Lift Devices for Laminar Wing Design of Turboprop Aircraft – Large Scale Wind Tunnel and CFD Assessment
WALLIN Stefan (FLOW Turbulence Lab, Dept. Engineering Mechanics, KTH, SE-100 44 Stockholm, Sweden)
17:15 Research of Engineering Solutions for a Vertical Take-Off and Landing Transport Platform
VITALY Gubskiy (TsAGI)
Chairs: nc
15:35 Experimental Investigations of a Wavy Surface Effect on Couete-Taylor-Poiseuille Flow
ALOUI Fethi (Université Polytechnique Hauts-de-France, LAMIH UMR CNRS 8201, INSA Hauts-de-France
16:00 Comparison of the Couette Flow for Air and Helium
LEBIGA Vadim (Khristianovich Institute of Theoretical and Applied Mechanics SB RAS
16:25 Numerical Simulation of the Mach Wave and the Supersonic Boundary Layer Interaction on a Flat Plate with a Sharp Leading Edge
EGOROV Ivan
16:50 A Study of the Laminar-Turbulent Transition on Swept Wings with chi = 72 deg
SEMIONOV Nikolai (Khristianovich Institute of Theoretical and Applied Mechanics
17:15 Receptivity of Supersonic Boundary Layer to Free Stream Entropy and Acoustic Perturbations
PALCHEKOVSKAYA Natalia (Moscow Institite of Physics and Technology
17:40 Receptivity of Supersonic Boundary Layer to Three-Dimensional Acoustic Perturbations
EGOROV Ivan (Moscow Institute of Physics and Technology
18:05 Secondary Instability of Hypersonic and High Enthalpy Boundary Layers with High Temperature Effects
CHEN Xianliang (School of Aerospace Engineering, Tsinghua University
Chairs: KNEIB Jean-Paul & PAEK Sung Wook
15:35 Research initiative sustainable space logistics: an overview on the work performed at EPFL from 2019 to 2021 in space logistics modelling and optimisation
UDRIOT Mathieu (EPFL Space Center -Switzerland)
16:00 A Sustainable and Affordable Access to Space
MAROQUENE FROISSART François (Sirius Space Services – France)
16:25 Verification of the Technology Combination Analysis Tool (TCAT) for space logistics modeling in the Earth-Moon system
PAEK Sung Wook (City University of London – United Kingdom)
16:50 Multidisciplinary analysis of launch vehicles including environmental impact
TORMENA Enrico (ISAE Supaero – France)
17:15 RAMS as a Crucial Contributor Towards Space Sustainability
RADU Silvana (European Space Agency – Netherlands)
17:40 Space grade Biomethane production for Themis reusable stage demonstrator
KURELA Michal (CNES – France)
18:05 An Automatic Domain Splitting Initial Orbit Determination Technique for Short-arc Optical Measurements
CIPOLLONE Riccardo (Politecnico di Milano – Italy)
Chairs: nc
15:35 Trajectory optimization for the computation of safe emergency trajectories
ONGALE-OBEYI Maëva (Thales AVS France SAS-ENAC)
16:00 Missionisable on-board flight safety based on real-time autonomous decision-making for microlauncher services
MARTIN Nil (GTD Sistemas de Informacion SA – Spain)
16:25 Robust FDIR approach for future hybrid navigation system for VEGA-C
RAMIREZ NAVIDAD Sergio (SENER Aeroespacial – Spain)
16:50 Analysis of some nonlinear features in the flight dynamics of a jet airplane
KOLB Sébastien (Centre de Recherche de l’Ecole de l’air (CREA) – France)
17:15 Advanced Guidance Approach for Multi-Body/Multi-Actuator Spacecraft Repointing under Attitude Constraints
PONCHE Alison (UC3M – Spain)
17:40 Switching the Controller During an Approach to The Runway For the Twin-engine Aircraft Under Both Engine Failure
ERGÖCMEN Burak (Suleyman Demirel University – Turkey)
[POSTER] Longitudinal/Lateral Coupled Dynamic Analysis of a Slow Lateral Motion
BASUYAU Henri (ELISA Aerospace – France)
Chair: BACH Christian
15:05 Pre-conceptual staging trade-offs of reusable launch vehicles
GUILLERMO JOAQUIN (Dominguez Calabuig DLR)
15:30 Eco-design of future reusable launchers: insight into their life-cycle and atmospheric impact
SARRITZU Alberto (Universita di Pisa)
15:55 Health Monitoring for RLVs: Architecture Selection and Discussion
VENNITTI Andrea (TU Dresden)
16:20 Reliability estimation methodology for Liquid Rocket Engines
AYALA FERNANDEZ Lucía (TU Braunschweig)
16:45 Sensibility study for different nozzle configuration on the heat load and aerodynamic behaviour for the THEMIS demonstrator
LANTELME Melissa (ONERA)
17:10 On The Integration of Aerospike Nozzles In Rotating Detonation Engines
BACH Christian (TU Dresden)
17:35 Round Table Discussion
BACH Christian (TU Dresden)
Chairs: DOS SANTOS HAHN Robson & GIRARD Nathalie
15:05 TARES2020: Technologies for Future Liquid Propellant Engines at ArianeGroup
SOLLER Sebastian (Ariane Group Ottobrunn)
15:30 Configuration Design Studies of a LOX-LCH4 Booster Engine and Stage for a Futuristic Indian Launcher
MOHAN Kiran (Liquid Propulsion Systems Centre (LPSC), ISRO)
15:55 Configuration Studies on An Electric Pump Fed Upper Stage Rocket Engine
MOHAN Kiran (Liquid Propulsion Systems Centre (LPSC), ISRO)
16:20 Prospective of Self-Pressurized Technology for In Space Satellite Mission
LA LUNA Simone (Politecnico di Milano)
Chairs: Nathalie GIRARD & Michel BERDOYES
15:05 LES and ROM of the acoustic damping in a nonreactive pressurized test rig including coupled cavities and multiple jets
MARCHAL David (Laboratoire EM2C, CNRS, CentraleSupélec, Université Paris-Saclay)
15:30 Low-order modeling of combustion instability using a hybrid real/ideal gas mixture model
D’ALESSANDRO Simone (Sapienza Università di Roma)
15:55 Disturbance energy transport, a tool to analyze backward-facing step combustion instabilities
KLEIN Jean-Michel (ONERA)
16:20 Preliminary study of the high-frequency instability of an aerospike rocket engine
ROSSI Federico (Pangea aerospace)
Chairs: NAUMANN Karl-Wieland & PARAVAN Christian
15:05 Thermophoresis as a possible mechanism for aluminum oxide lobe formation
GALLIER Stany (ArianeGroup)
15:30 Evolution of aluminum droplets in solid propellant combustion by image analysis using deep learning
AIRIAU Magdeleine (ONERA/DMPE)
15:55 Effect of Coated Nano-Aluminum Powders on the Agglomeration in Solid Propellant
YAVOR Yinon (Afeka College of Engineering)
16:20 Combustion of Green AN-Al-Water Propellants
YAVOR Yinon (Afeka College of Engineering)
16:45 Study of the effect of particles on the two-phase flow field and radiation in aluminized rocket engine plumes
DE GIORGI Maria grazia (University of Salento Department of Engineering Innovation)
17:10 Numerical simulation of the boron particle agglomeration in combustion of boron-containing solid propellants
RASHKOVSKIY Sergey
17:35 A Revised Model of Ammonium Perchlorate Combustion with Detailed Kinetics
BERNIGAUD Pierre (ONERA – The French Aerospace Lab)
Chairs: nc
15:05 Glide back recovery of a winged reusable launch vehicle with wind estimate
EDORH Prince (CNES)
15:30 Semi-free oscillation method for dynamic stability characterization on re-usable launcher first-stage
PARIS Sebastien (von Karman Institute for Fluid Dynamics)
15:55 Optimal reconfigurable allocation of a multi-engine cluster for a reusable launch vehicle
MURATA Renato (ONERA)
16:20 Control strategies comparison and performance evaluation for a reusable VTVL platform based on a rocket engine
AFILIPOAE Tudorel-Petronel (National Institute for Aerospace Research ‘Elie Carafoli’)
16:45 Impact of control gain design on Remaining Useful Life for a Liquid Propellant Reusable Engine
THUILLIER Julien (CNES)
17:10 Hypersonic Retrograde Propulsion Experiments – A Basis for Validation of CFD within RETPRO
KIRCHHECK Daniel (DLR)
17:35 Reconstruction of Wind Tunnel Tests using CFD for a Reusable First Stage during Rocket Retro-propulsion
BYKERK Tamas or KARL Sebastian (DLR)
Chairs: nc
15:05 Product Assurance Overview of Additive Manufactured Components for Space Applications
ZUIN Davide (Politecnico di Milano)
15:30 Space Flight Hardware fabricated by Additive Manufacturing to JUICE Mission
PERIÑAN BUTRON Antonio (CATEC)
15:55 Additive manufacturing capabilities for heat switch technology: Key challenges & knowledge gaps
MASEK Jakub (Brno University of Technology, Faculty of Mechanical Engineering)
16:20 Additive manufacturing process development for realization of Preburner Pump Impeller of LOX hydrocarbon based rocket engine using AlSi10Mg material
VERMA Rajeev (Indian Space Research Organisation)
Chairs: nc
15:05 An Overview of the EURASTROS Study
GÜLHAN Ali (German Aerospace Center – DLR e.V.)
15:30 System design of EURASTROS reference configurations and mission
PLEBUCH Alex (ArianeGroup)
15:55 Cost Estimation and Development Approach of the EURASTROS Concept
BRAUKHANE Andy (DLR – German Aerospace Center)
16:20 EURASTROS capsule design and re-entry analysis
MARQUARDT Pascal (DLR
16:45 EURASTROS ascent trajectory and abort analysis
BERGMANN Kevin (German Aerospace Center (DLR), Institute of Space Systems)
Chair: RÜTTEN Markus
15:05 Aerodynamic and structural study of active flow and morphing deformation high lift system, integrated in the leading edge of transport aircraft wing
CAMARA AGUIAR Nelson (Altran Technologies SA)
15:30 Application of Flow Control in the Wing-Pylon Region for Lift Enhancement
JABBAL Mark (University of Nottingham)
15:55 Effects of Zero Net Mass Flux devices on a Next-Generation Tiltrotor airplane in subsonic regime by numerical simulation at high Reynolds number
MAROUF Abderahmane (ICUBE / University of Strasbourg)
16:20 Experimental Investigation on fractal/multiscale trippings for passive control of turbulent flow separation
SEPETAUSKAS Vinicius (LMFL / Centrale Lille)
16:45 Experimental assessment of the active flow control over the flight deck of a frigate
DERHILLE Elvina (Onera – DAAA/ELV)
17:10 An experimental study of trailing vortex dynamics in cruise and high-lift wing configurations.
CRUZ MARQUEZ Rolando (LMFL / Onera)