8th European Symposium on Aerothermodynamics for Space Vehicles Final Programme Monday 2nd of March 2015 12:30 - 14:30
Registration
Opening Ceremony
14:30 - 14:35
Welcome
14:35 - 14:55
(ESA, C. Stavrinidis)
14:55 - 15:15
(IPFN / IST, Prof. Bruno Soares Goncalves)
15:15 - 15:35
(VKI, Prof. J. P. Contzen)
15:35 - 15:55
(ESA, J. Longo)
15:55 - 16:15
Coffee break
Plenary Session In Flight Experimentation 16:15 - 16:35
Business Case Analysis of a Multi-Functional In-Flight Experimental System Euroconsult, M. Puteaux
Round Table Commercial Access to Space Providers 16:35 - 16:55
AIRBUS Defence & Space, A. Schuette
16:55 - 17:15
XCOR Space Expeditions, H. van Hulten
17:15 - 17:35
Swiss Space Systems S3, P. Jaussi
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Monday 2 March 2015
Round Table Commercial Sub-system Providers 17:35 - 17:55
Swedish Space Corporation SSC, G. Florin
17:55 - 18:15
QB50, J-M Muylaert
18:15 - 18:35
ESA schemes for the realization of the In-Flight Demonstration, U. Becker
18:35-19:35
Symposium highlight I The IXV Project (G. Tumino)
19:35 - 21:00
Symposium Welcome Cocktail
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Monday 2 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles Tuesday 3rd of March 2015 08:30 - 09:00
Registration & Speaker Debriefing
09:00 - 09:30
Plenary Lecture (Auditorium) ESA-Technologies in support to design for demise (L. Innocenti) Room 01.1
Auditorium
Room 02.1
Room 01.2
Long Range Transatmospheric Systems I
Entry, Descent and Landing I
Design for Demise I
Physical Modelling I
Chairs:M. Sippel & R. Molina
Chairs:J. Underwood & G. Florin
Chairs:M. Balat-Pichelin & M. Spel
Chairs:A. Bultel & D. Giordano
09:35 - 09:55
The SpaceLiner Hypersonic System “ Aerothermodynamic Requirements and Design Process | Sippel, M. | DLR SART, Germany
09:30 - 09:50
Supersonic Parachute Aerodynamic Testing and Fluid Structure Interaction Simulation 09:30 - 09:50 | Underwood, J. | Vorticity Ltd, United Kingdom
Design Recommendations for the Demise of Metallic Tanks During Atmospheric reentry | Vérant, J.-L. | ONERA, France
09:55 - 10:15
Conceptual Design of the SpaceLiner Thermal Protection System | Schwanekamp, T. | DLR, Germany
09:50 - 10:10
Sounding Rockets and Stratospheric Balloons, Unique Test platforms for Reentry Systems at Esrange | Florin, G. | Swedish Space Corporation, Sweden
09:50 - 10:10
Study of the Atmospheric Entry of Metallic Space Debris – Oxidation and Emissivity 09:50 - 10:10 Evaluation to Contribute to Design for Demise | Balat-Pichelin, M. | PROMESCNRS, France
State-Resolved Modeling of NonEquilibrium Processes in Nitrogen Flows | Lopez, B. | IPFN-IST, Portugal
10:15 - 10:35
Hypersonic Morphing for a Cabin Escape System: Results of First Design Loop | Haya, R. | DEIMOS Space S.L.U., Spain
10:10 - 10:30
Supersonic Parachute Testing Using a MAXUS Sounding Rocket Piggy-Back Payload | Underwood, J. | Vorticity Ltd, United Kingdom
10:10 - 10:30
Characterisation of Material Demisability through Plasma Wind Tunnel Experiments | 10:10 - 10:30 Pagan, A. | University of Stuttgart, Germany
Review of Global Rate Coefficients of Partially Non-equilibrium Argon with Electron Impact Ionization for Space Vehicle Application | Upadhyay, P. | University of Stuttgart, Germany
10:35 - 10:55
Aerothermodynamics analysis of the Spaceliner Cabin Escape System modified via a morphing system | Laroche, E. | ONERA, France
10:30 - 10:50
Subsonic Parachutes for Future Mars Missions | Underwood, J. | Vorticity Ltd, United Kingdom
10:30 - 10:50
Determination of Total and Spectral Emissivities of Space-relevant Materials | Massuti-Ballester, B. | University of Stuttgart, Germany
Influence of the Modeling of the Excited States Behavior on the Radiation Emitted by a Nitrogen Plasma Produced within a Shock Tube | Annaloro, J. | CNES, France
09:30 - 09:50
10:30 - 10:50
Status of Shock Layer Radiation Validation Studies | Brandis, A. | ERC Inc at NASA Ames, United States
Coffee break
10:55 - 11:10
Gas Surface Interation I
Propulsion Modelling I
Measurements Techniques I
Numerical Modelling I
Chairs:W. Owens & L. Marraffa
Chairs:J. Martinez-Schramm & J. Steelant
Chairs:A. Pagan & N. Murray
Chairs:R. Schwane & T. Schwartzentruber
11:10 - 11:30
Oxidation at High Temperature in Air Plasma for the TPS of IXV – Passive/active Transition and Temperature 11:10 - 11:30 Jump | Balat-Pichelin, M. | PROMESCNRS, France
LAPCAT II Intake Starting Tests | McGilvray, M. | University of Oxford, United Kingdom
11:10 - 11:30
Laser-based Surface Recession Measurements of Ablating Heat Shield Materials in High-Enthalpy Flows | Pagan, A. | University of Stuttgart, Germany
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Tuesday 3 March 2015
11:10 - 11:30
Validation of a Parallel 3D Direct Simulation Monte Carlo Solver for Atmospheric Entry Applications | Nizenkov, P. | University of Stuttgart, Germany
8th European Symposium on Aerothermodynamics for Space Vehicles
11:30 - 11:50
Experimental Investigations of Characteristics of the Air Intake with Internal Compression | Talyzin, V. | TsAGI, Russia
11:50 - 12:10
Deformation and Cracking in CFRP Ablator During Arc Wind Tunnel Heating | Ogawa, R. | Tokyo University of Science , Japan
11:50 - 12:10
Experimental Comparative Synthesis on the Scramjet Powered Waverider Vehicle in 11:50 - 12:10 HEG and F4 within the LAPCAT II Project | Martinez Schramm, J. | DLR, Germany
First Results on Ablation Radiation Coupling through Optical Emission Spectroscopy from the Vacuum Ultraviolet 11:50 - 12:10 to the Visible | Hermann, T. | University of Stuttgart, Germany
Modeling of Surface Recombination in the DSMC Method | Bondar, Y. | ITAM, NSU, Russia
12:10 - 12:30
Final CFD Design of SCIROCCO Arc-jet Test Conditions for IXV TPS Interfaces | Trifoni, E. | CIRA, Italy
12:10 - 12:30
Tests of the LAPCAT II Small Scale Flight Experiment Model in th Onera F4 Wind Tunnel | Viguier, P. | ONERA, France
12:10 - 12:30
Analysis of Fibrous Felts for Flexible Ablators Using Synchrotron Hard X-ray Micro-tomography | Panerai, F. | NASA Ames Research Center, United States
12:10 - 12:30
VV Exchange Modeling in the DSMC Method | Bondar, Y. | ITAM SB RAS, Russia
12:30 - 12:50
Electric Sensor for Monitoring Ablation Processes in Thermal Protection Systems of Spacecraft and Probes | Mendes, A. | Active Space Technologies SA, Portugal
12:30 - 12:50
Direct Molecular Simulation: Dissociation of Nitrogen from First Principles | Schwartzentruber, T. | University of Minnesota, United States
11:30 - 11:50
Experimental Characterization of Cork Based Thermal Protection Material P50 | Sakraker, I. | VKI, Belgium
12:30 - 12:50
12:30 - 12: 50
11:30 - 11:50
Characterisation of a Hybrid Heat Shield for Hyperbolic Atmospheric Entries | Massuti-Ballester, B. | University of Stuttgart, Germany
12:50 - 14:20
Lunch
14:20 - 14:50
Plenary Lecture (Auditorium) ESA-Technologies in support to launchers (J. Breteau)
11:30 - 11:50
Implementation of State-to-state Rovibrational Bin Model for Molecular Nitrogen in DSMC | Torres, E. | VKI, Belgium
Technologies for Re-entry Vehicles I
Boundary Layer Flows I
Design for Demise II
Physical Modelling II
Chairs:B. Reimann & F. Massobrio
Chairs:D. Neeb & K. Hannemann
Chairs:M. Spel & R. Molina
Chairs:B. Esser & P. Omaly
14:55 - 15:15
Numerical Simulation of the Free Pitch Oscillation for a Reentry Vehicle in 14:55 - 15:15 Transonic Wind Tunnel Flow. | Reimann, B. | DLR, Germany
Experimental Flow Characterization and Heat Flux Augmentation Analysis of a Hypersonic Turbulent Boundary Layer Along a Rough Surface | Neeb, D. | DLR, Germany
14:50 - 15:15
First Spacecraft Demise Workshop: Test Case Description and Results | Spel, M. | R.Tech, France
14:55 - 15:15
Validation of Aerothermal Chemistry Models for Re-entry Applications: Theoretical and Computational Synthesis | Joiner, N. | Fluid Gravity Engineering, United Kingdom
15:15 - 15:35
Experimental study of the Dynamic Stability of the IXV Configuration | Gawehn, T. | DLR, Germany
High-temperature Gase Effects on the Highenthalpy Flow on the Wind-ward Side 15:15 - 15:35 Boundary-layer of a Generic Capsule Geometry | Stemmer, C. | Technische Universitat Munchen, Germany
Navier-Stokes Computations for Hollow Cylinders and Cubes Relevant for Satellite Debris | Couchman, B. | Fluid Gravity Engineering, United Kingdom
15:15 - 15:35
Experimental Determination of Recombination Coefficients at High Pressures | Esser, B. | DLR, Germany
15:15 - 15:35
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Tuesday 3 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
15:35 - 15:55
Assembly and Integration of Instrumented Nose and Windward CMC TPS for IXV 15:35 - 15:55 Program | Brach Prever, E. | Thales Alenia Space - Italia, Italy
Numerical Investigation of RoughnessInduced Transition at Mach 6 in the European ATLLAS-2 Programme | Van den 15:35 - 15:55 Eynde, J. | University of Southampton, United Kingdom
Simplified Aerothermal Models for Destructive Entry Analysis | Merrifield, J. | 15:35 - 15:55 Fluid Gravity Engineering, United Kingdom
Elementary Stage Rate Coefficients Of The Heterogeneous Catalytic Recombination In Dissociated Air On β-Cristobalite And αAl2O3 | Kovalev, V. | Lomonosov Moscow State University, Russia
15:55 - 16:15
Intermediate Experimental Vehicle, Esa Program - IXV ATDB Tool And Aerothermodynamic Characterization From the Design to the Flight | Mareschi, V. | Thales Alenia Space - Italia, Italy
15:55 - 16:15
Direct Numerical Simulation of Hypersonic Flows over Compression Ramps and Study of Appearing Görtler Vortices | 15:55 - 16:15 Klioutchnikov, I. | RWTH Aachen University, Shock Wave Laboratory, Germany
Attitude Dependant Thermal Flux Estimation for Geometric Primitives Towards the Improvement of Destructive Re-entry Simulations | Donaldson, N. | University of Oxford, United Kingdom
15:55 - 16:15
Atomic Oxygen and Carbon Monoxide Recombination Coefficient on Ceramics at High Temperature for Martian Entry Simulation | Balat-Pichelin, M. | PROMESCNRS, France
16:15 - 16:35
Flight Predictions for the IXV Mission | Haya Ramos, R. | DEIMOS Space S.L.U., Spain
16:15 - 16:35
Flow Control of a High-speed Boundary Layer by Localized Wall Heating or Cooling 16:15 - 16:35 | Egorov, I. | TsAGI, Russia
A Heat Balance Integral Method for Destructive Re-entry Codes | Beck, J. | Belstead Research Limited, United Kingdom
16:15 - 16:35
Calculation of Collision Integrals for Ablation Species | Bellemans, A. | VKI, Belgium
16:35 - 16:55
Assessment of Aero-thermodynamic Characteristics of the USV3 Vehicle | 16:35 - 16:55 Catalano, P. | C.I.R.A. - Italian Aerospace Research Center, Italy
16:35 - 16:55
16:35 - 16:55
A Technology Transfer Opportunity: from Ablative Heat Shield Design to Biomass Pyrolysis Reactor Design | Magin, T. | VKI, Belgium
Coffee Break
16:55 - 17:10
Gas Surface Interation II
Ground Based Facilities I
Measurement Techniques II
Numerical Modelling II
Chairs:B. Massuti-Ballester & J. M. Bouilly
Chairs:O. Chazot & L. Walpot
Chairs:A. Lemal & A. Mohamed
Chairs:J-M Vaassen & M. Fertig
17:10 - 17:30
Light Weight Ablator Response Model Development & Challenges | Mansour, N. | NASA, United States
17:30 - 17:50
A New Global Approach to Evaluate the Surface Catalytic Efficiency of TPS Materials Based on arc Jet Experiments and Numerical Predictions | Trifoni, E. | CIRA, Italy
17:10 - 17:30
ESTHER: A New Generation Two-Stage, Combustion Driven Shock-Tube for Planetary Entries Studies | Lino da Silva, M. | Instituto Superior Tecnico, Portugal
17:10 - 17:30
Spectroscopic Measurement of Plasma Flow Generated by 10kW and Φ75mm ICP 17:10 - 17:30 Heater | Miyatani, S. | University of Tokyo, Japan
Implementation of h/p Adaptivity on Hybrid Meshes for the Simulation of Chemically Reactive re-entry Flows. | Papoutsakis, A. | FORTH, Greece
17:30 - 17:50
Enhancement of the VKI Plasmatron Facility Capabilities for Testing High Heat17:30 - 17:50 Flux re-entry Conditions | Chazot, O. | VKI, Belgium
Prediction of non Equilibrium Peak Radiation Behind Shock Waves in Earth 17:30 - 17:50 Reentry | Lemal, A. | Ecole Centrale Paris, France
Implementation of Multitemperature Models in the Low Diffusion Particle Method for the Simulation of Internal Energy Nonequilibrium Effects in Continuum Flow Regions | Mirza, A. | University of Stuttgart, Germany
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Tuesday 3 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
17:50 - 18:10
Heat Transfer in Underexpanded Chemically non-equilibrium Carbon Dioxide Jets: an Experiment at Inductive Plasma 17:50 - 18:10 Torch and Extrapolation to Martian Atmosphere Entry Conditions. | Kolesnikov, A. | Lomonosov Moscow State University, Russia
Limits of Simulating Gas Giant Entry at True Flight Velocity in an Expansion Tube | 17:50 - 18:10 James, C. | The University of Queensland, Australia
18:10 - 18:30
Gas-Surface Interaction. Experimental Determination of PM1000 and CVD-C/SiC Catalytic Properties | Massuti-Ballester, B. | University of Stuttgart, Germany
Characterization of Ground Testing Condition in High Enthalpy and Plasma Wind Tunnels for Aerospace Missions | del Val Benítez, A. | VKI, Belgium
18:10 - 18:30
Flow Characterization and MHD Tests in High Enthalpy Argon Flow| Steffens, L. | DLR, Germany
18:10 - 18:30
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Tuesday 3 March 2015
17:50 - 18:10
18:10 - 18:30
Strongly Coupled Approach To Solve Fluid Structure Interaction Problems Using Industrial Solvers | Vaassen, J. | OpenEngineering S.A., Belgium
8th European Symposium on Aerothermodynamics for Space Vehicles Wednesday 4th of March 2015 08:00-08:30
Registration & Speaker Debriefing
08:30-09:00
Plenary Lecture (Auditorium) NASA Entry Descent and Landing Program (M. Wright) Room 02.1
Room 01.2
Room 01.1
Auditorium
Gas Surface Interation III
Entry, Descent and Landing II
Flow Phenomena on Propulsion Systems I
Numerical Modelling III
Chairs:P. Leyland & Ph. Reynier
Chairs:E. Clopeau & V. Mareschi
Chairs:L. Konozsy & Ph. Behruzi
Chairs:G. Colonna & P. Gnemmi
Temperature Measurements of Acetone Flashing Jet by Laser Induced Fluorescence 09:05-09:25 | Simonini, A.| VKI, Belgium
Self-consistent Collisional-radiative Model for Shock Tube in Jupiter Atmosphere | Colonna, G. | CNR-Istituto di Metodologie Inorganiche e dei Plasmi, Italy
09:25-09:45
Experimental Investigation of Dynamic Characteristics for MarcoPolo-R ERC in Low 09:25-09:45 Subsonic Flow Using the Free Flight Technique | Preci, A. | DLR, Germany
Experimental and Numerical Investigation of Acoustic Liquid Manipulation for Trapping and Positioning Cryogenic Propellants | Konozsy, L. | Cranfield University, United Kingdom
09:25-09:45
An Adaptive Hybrid Statistical Narrow Band Model for Coupled Radiative Transfer in Atomspheric Entry Flows | Scoggins, J. | VKI, Belgium
Off-Stagnation Tests of ESA IXV TPS Interfaces in Plasmatron | Ceglia, G. | CIRA, Italy
09:45-10:05
Marco Polo-R ERC Dynamic Stability Characterization. | Berner, C. | ISL, France
09:45-10:05
Experimental and Numerical Study of the Flow Characteristics in a Cryogenic Valve 09:45-10:05 with Liquid Nitrogen and Water | Peveroni, L. | VKI, Belgium
Noise Reduction Scheme for Probabilistic Radiation Modelling in DSMC | Petkow, D. | Gradel sárl, Luxembourg
On an Analytical Model of Thermal Coupling of a Viscous Fluid and an Elastic Wall with Ablation | Campos, L. | (IST), Universidade de Lisboa, Portugal
10:05-10:25
MarcoPolo-R ERC Dynamic Stability Characterization : Computational Campaign | Charbonnier, D. | CFS Engineering, Switzerland
10:05-10:25
Boiling Crisis Dynamics: Low Gravity Experiments and Modeling | Nikolayev, V. | SPEC, Atomic Energy Commission at Saclay, France
Influence of the Modeling of the Excited States Behavior on the Radiation Emitted by a Nitrogen Plasma Produced within a Shock Tube | Annaloro, J. | CNES, France
09:05-09:25
The ESA ARC Project : Ablation Radiation Coupling for hypervelocity re-entry with low density type ablators | Leyland, P. | EPFL, Switzerland
09:05-09:25
MarcoPolo-R ERC Dynamic Stability Characterisation : Study Logic | Clopeau, E. | Airbus Defence and Space, France
09:25-09:45
Heat Convention Through Flat Plate | Taploo, A. | SRM University, India
09:45-10:05
10:05-10:25
09:05-09:25
10:05-10:25
Coffee break
10:25-10:40
Flight Experiment I
Numerical Modelling IV
Measurement Techniques III
Physical Modelling III
Chairs:G. Rufolo & Th. Eggers
Chairs:M. Fertig & H. Wong
Chairs:G. Herdrich & A. Passaro
Chairs: G. Candler & G. Colonna
10:40-11:00
The Intermediate eXperimental Vehicle In Flight Experimentation. From the Design to 10:40-11:00 the Flight. | Rufolo, G. | CIRA, Italy
Aerothermoelastic Structural Topology Optimisation for a Hypersonic Transport Aircraft Wing | Verstraete, D. | The University of Sydney, Australia
10:40-11:00
STARDUST SLIT in-flight data: Improvement of Analysis | Herdrich, G. | University of Stuttgart, Germany
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
10:40-11:00
Quasi-Classical Trajectory Analysis of the N2 + N2 Dissociation Reaction | Candler, G. | University of Minnesota, United States
8th European Symposium on Aerothermodynamics for Space Vehicles
Development of an Infrared Break Up ReEntry Sensor | Greger, R. | RUAG Space, Switzerland
11:00-11:20
Plasma Assisted CO2 Dissociation Models for Environment, Energy and Aerospace Applications. | Colonna, G. | CNR-Istituto di Metodologie Inorganiche e dei Plasmi, Italy
Flying Catalysis in Lifting Atmospheric Entry | VILADEGUT, A. | VKI, Belgium
11:20-11:40
Comparison of Quantum Mechanical and Empirical Potential Energy Surfaces for N2 Dissociation | Jaffe, R. | NASA Ames Research Center, United States
11:40-12:00
Frequency Comb High Speed Broadband Spectroscopic Sensor To Probe Aerodynamic Flows | Mohamed, A. | ONERA, France
11:40-12:00
Non-equilibrium Modeling of Inductively Coupled RF Plasmas | Panesi, M. | University of Illinois at Urbana Champaign, United States
12:00-12:20
Modular Power Bus for Space Vehicles (MPBus) | Pérez, B. | Najera Aerospace, 12:00-12:20 Spain
11:00-11:20
Aerothermal Environment Assessment of the Hexafly-INT Experimental Flight Test Vehicle (EFTV) | Carandente, V. | CIRA, Italy
11:00-11:20
Rapid Aero-Thermodynamic Analysis for Hypersonic Air Vehicles | Wuilbercq, R. | University of Strathclyde, United Kingdom
11:20-11:40
Wind Tunnel Experiments on the SHEFEXII Configuration in the Frame of the Post Flight Analyses | Thiele, T. | DLR, Germany
11:20-11:40
Investigation of Heatflux Modification by Magnetohydrodynamic Interaction 11:20-11:40 Employing the DLR CFD Code TAU | Fertig, M. | DLR, Germany
11:40-12:00
Huygens Flight Performance Analyses | Underwood, J. | Vorticity Ltd, United Kingdom
11:40-12:00
12:00-12:20
Assessment of Hypersonic Aerodynamic Performance of the EFTV-ESM Configuration in the Framework of Hexafly- 12:00-12:20 INT Research Programme | Carandente, V. | CIRA, Italy
11:00-11:20
12:20-13:50
Lunch
13:50-14:20
Plenary Lecture (Auditorium) Phys4Entry Project (D. Bruno)
A Reduced-order Modeling Approach to Enable Kinetic Simulations of Nonequilibrium Hypersonic Flows | Panesi, M. | University of Illinois at Urbana Champaign, United States
Gas Surface Interation IV
Ground Based Facilities II
Propulsion Modelling II
Physical Modelling IV
Chairs:D. D’Ambrosio & H. Weihs
Chairs:L. Marraffa & J. Brazier
Chairs:A. Schettino & M. Sippel
Chairs:M. Panesi & L. da Silva
14:25-14:45
Finite Rate Surface Catalysis Modelling of PM1000 and SiC Employing the DLR CFD Solver TAU | Fertig, M. | DLR, Germany
14:45-15:05
Rebuilding Thermal Response and Ablation Radiation Coupling for Superorbital Return 14:45-15:05 | Mora-Monteros, J. | EPFL, Switzerland
14:25-14:45
A Multi-domain ALE Algorithm for Simulating Flows inside Free-piston Driven 14:25-14:45 Test Facilities | Bensassi, K. | VKI, Belgium
Development and Validation of Numerical Solvers for the Analysis of High-pressure Combustion in Liquid Rocket Engines | Schettino, A. | CIRA, Italy
14:25-14:45
Diffusion Monte Carlo Models of Confined Hydrogen Species |Micca Longo, G. | CNRIMIP, Italy
Numerical Simulation of a Tandem Nozzle Flow for a High Enthalpy Impulse Wind Tunnel | Qian, Z. | AVIC Aerodynamics Research Institute, China
Hybrid Paraffin-Based Technology Demostrator in the Framework of the Italian Hyprob Program: Status of Design and Development Activities | DI CLEMENTE, M. | CIRA, Italy
14:45-15:05
Development of Detailed Chemistry Models for Boundary Layer Catalytic Recombination | Bellas, G. | VKI, Belgium
14:45-15:05
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
15:05-15:25
On the Analysis of Radiative Heat Transfer Influence Inside the Piston-Driven Shock 15:05-15:25 Tunnel HELM | Garcia Garrido, J. | University of the Federal Armed Forces Munich, Germany
Large-eddy Simulations of Solid-Rocket Motors Reactive Plumes | Poubeau, A. | CERFACS, France
15:05-15:25
15:25-15:45
A Fully Implicit Material Response Code with Ablation and Pyrolysis for Simulation of Thermal Protection Systems | D'Ambrosio, D. | Politecnico di Torino, Italy
15:25-15:45
Standard Probe Testing in European High Enthalpy Facilities | Merrifield, J. | Fluid Gravity Engineering, United Kingdom
15:25-15:45
A Zooming Approach to Investigate Heat Transfer in Liquid Rocket Engines with ESPSS Propulsion Simulation Tool | Leonardi, M. | La Sapienza, Italy
15:25-15:45
15:45-16:05
A Finite Element Approach for the Design of Innovative Ablative Materials for Space Applications | Scigliano, R.. | CIRA, Italy
15:45-16:05
An overview of HyFIE Technical Research Project: cross testing in main European hypersonic wind-tunnels on EXPERT body. | Brazier, J. | ONERA, France
15:45-16:05
15:05-15:25
Carbon Gasification in PICA Ablators | Grana-Otero, J. | University of Kentucky, United States
Modeling Rarefied Molecular Oxygen Flows by CT-DSMC | Frezzotti, A. | Politecnico di Milano, Italy
15:45-16:05
Coffee Break
16:05-16:20
Technologies for Re-entry Vehicles II
Ground Based Facilities III
Measurement Techniques IV
Numerical Modelling V
Chairs:B. Esser & L. Walpot
Chairs:M. da Silva & J. Brazier
Chairs:F. Schrijer & G. Herdrich
Chairs:G. Pont & J. Peiro
16:20-16:40
Experimental Verification of Thermal Management Concepts for Space Vehicles | 16:20-16:40 Esser, B. | DLR, Germany
The Oxford High Density Tunnel | Doherty, 16:20-16:40 L. | University of Oxford, United Kingdom
Experimental Results on ShockWave/Boundary-Layer Interaction Induced 16:20-16:40 by a Movable Wedge | Daub, D. | DLR, Germany
Hypersonic Aero-Thermo-Dynamic Heating Prediction With Unstructured Residual Distribution Methods | Garicano Mena, J. | VKI, Belgium
16:40-17:00
Aeroelastic Instabilities of FGM Panels under Thermo-Mechanical Loads | Zappino, 16:40-17:00 E. | Politecnico di Torino, Italy
The Oxford Stalker Tunnel | McGilvray, M. | University of Oxford, United Kingdom
16:40-17:00
Development and Application of Temperature Sensitive Paints in the High Enthalpy Shock Tunnel Göttingen, HEG | Martinez Schramm, J. | DLR, Germany
16:40-17:00
Hypersonic Aero-Thermo-Dynamic Heating Prediction With High-Order Discontinous Galerkin Spectral Methods | Garicano Mena, J. | VKI, Belgium
17:00-17:20
Derogation of Aeroshell Aerodynamic Performance due to Recession of Lightweight Ablator along a Reentry Trajectory | Fujita, K. | JAXA, Japan
Experimental Study to Increase the Shock Speed in a Free Piston Double Diaphragm Shock Tube | Ishida , H. | Waseda University, Japan
17:00-17:20
Locally resolved boundary layer radiation during ablation testing | Helber, B. | VKI, 17:00-17:20 Belgium
Characteristics of Aerodynamic Heating on a Sharp Cone in Hypersonic Flow | Wang, Q. | Institute of Mechanics, CAS, China
17:20-17:40
Flow over the Axisymmetrical Body in Hypersonic Flow of Perfect Gas | Egorov, I. 17:20-17:40 | Central Aerohydrodynamic Institute (TsAGI), Russia
17:20-17:40
Application of Particle Image Velocimetry for Aero(thermo)dynamics | Schrijer, F. | 17:20-17:40 Delft University of Technology, Netherlands
CFD Modeling of the Ariane 6 Space Launcher from Ground to Space | Pont, G. | Airbus Defence and Space, France
17:00-17:20
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
17:40-18:00
Simplified Aerothermodynamic Methodolgy 17:40-18:00 for Reentry Analyses at S3| Vuitel, B. | Swiss Space Systems, Switzerland
17:40-18:00
Experimental Investigation of Heat Flux Fluctuations on the Rear Cover of a Planetary Probe Entry-Configuration | Neeb, D. | DLR, Germany
18:00-18:15
Introduction ESA (G. Saccoccia)
18:15-18:30
Symposium highlight II The ESTHER facility (M. da Silva)
18:45-23:30
Visiting ESTHER facility Symposium Dinner
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
17:40-18:00
Application of SMILE++ Computational Tool to High-enthalpy Ionized Flows | Bondar, Y. | ITAM SB RAS, Russia
8th European Symposium on Aerothermodynamics for Space Vehicles Thursday 5th of March 2015 08:30 - 09:00
Registration & Speaker Debriefing
09:00 - 09:30
Plenary Lecture (Auditorium) The SHEFEX II Project (H. Weihs) Room 02.1
Room 01.2
Room 01.1
Auditorium
Long Range Transatmospheric Systems II
Ground Based Facilities IV
Measurement Techniques V
Physical Modelling V
Chairs:R. Haya Ramos & S. Portigliotti
Chairs:D. Saile & Chr. Mundt
Chairs:J. Martinez Schramm & A. Schettino
Chairs:D. Giordano & Th. Magin
09:30 - 09:50
Numerical Integral Method for kinetic equations in gases and plasmas | Donoso Vargas, J. | Numerical Integral Method for kinetic equations in gases and plasmas, Spain
Application of Free Flight Force Measurements using Complex Models in a Large Scale Shock Tunnel | Martinez Schramm, J. | DLR, Germany
09:50 - 10:10
Validation Of Aerothermal Chemistry Models For Re-entry Applications: Synthesis Of Experimental Achievements | Reynier, P. | Ingénierie et Systèmes Avancés, France
10:10 - 10:30
Three-component Free-flight Force Measurement in Shock Tunnel HIEST | Tanno, H. | JAXA, Japan
10:10 - 10:30
Title TBC E. Kustova et al.
10:30 - 10:50
Force Measurement Using A Pulse-type Strain-gaged Balance in Hypersonic Shock Tunnel | Wang, Y. | Institute of Mechanics, CAS, China
10:30 - 10:50
Influence of the Modeling of the Excited States Behavior on the Radiation Emitted by a Nitrogen Plasma Produced within a Shock Tube | Annaloro, J. | CNES, France
09:35 - 09:55
Aerodynamics and Flying Qualities Requirements for a Long-range 09:30 - 09:50 Transportation System | Haya Ramos, R. | DEIMOS Space S.L.U., Spain
Design of a Hot Plume Interaction Facility at DLR Cologne | Saile, D. | DLR, Germany
09:55 - 10:15
The Thermal and Structural Paradox for Hypersonic Cruisers | Steelant, J. | ESAESTEC, Netherlands
09:50 - 10:10
Experiments on a Hot Plume Base Flow Interaction at Mach 2 | Blinde, P.L. | Delft 09:50 - 10:10 University of Technology, Netherlands
10:15 - 10:35
Hypersonic Passenger Transport Vehicles: Major Achievements Realized within the LAPCAT-II Project | Steelant, J. | ESAESTEC, Netherlands
10:10 - 10:30
Design of a GH2/GOX Combustion Chamber for the Hot Plume Interaction Experiments at DLR Cologne | Saile, D. | DLR, Germany
10:35 - 10:55
Low Speed Handling Qualities of a Notional 10:30 - 10:50 Waverider Design | Verstraete, D. | The University of Sydney, Australia
Force Measurements by Means of Optical Tracking in the High Enthalpy Shock Tunnel Göttingen, HEG | Martinez Schramm, J. | DLR, Germany
09:30 - 09:50
Coffee break
10:55 - 11:10
Gas Surface Interation V
Entry, Descent and Landing III
Design for Demise III
Numerical Modelling VI
Chairs:Th. Reimer & H. Boehrk
Chairs:F. Punzo & L. Ferracina
Chairs:J. Annaloro & S. Radulovic
Chairs:R. Schwane & T. Langener
11:10 - 11:30
A Fast Pod-Based Aerotherma Design Environment Tool | Catalano, P. | CIRA, Italy
11:10 - 11:30
European Sounding Rocket Experiment on Hypersonic Deployable Re-entry Demonstrator | Marraffa, L. | ESA, The Netherlands
11:10 - 11:30
Elaboration of a New Spacecraft-oriented Tool: PAMPERO | Annaloro, J. | CNES, France
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Thursday 5 March 2015
11:10 - 11:30
Molecular Simulation of Oxygen Reactions with Realistic Silica and Carbon Surfaces at High Temperature | Schwartzentruber, T. | University of Minnesota, United States
8th European Symposium on Aerothermodynamics for Space Vehicles
11:30 - 11:50
Case Studies for Uncertainty Quantification of High-fidelity Spacecraft Oriented Break11:30 - 11:50 up Tools | Fritsche, B. | HTG GmbH, Germany
Fully Implicit Integrated Approach For The Numerical Simulation of Aerothermal Flows Through and Around Ablative Thermal Protection Systems | Schrooyen, P. | University Catholique de Louvain, Belgium
11:50 - 12:10
Design of a Transpiration Cooled Sharp Leading Edge for SHEFEX III | Dittert, C. | 11:50 - 12:10 DLR, Germany
Research and Development on Reentry System using Inflatable Aeroshell for Small 11:50 - 12:10 Satellite | Yamada, K. | JAXA, Japan
Application of the SAM Destructive re-entry Code to the Spacecraft Demise 11:50 - 12:10 Thermodynamics and Integration Test Cases | Beck, J. | Belstead Research Limited, United Kingdom
Preliminary numerical and experimental analysis of the spallation phenomenon | Martin, A. | University of Kentucky, United States
12:10 - 12:30
The SHEFEX-II Thermal Protection System 12:10 - 12:30 | Böhrk, H. | DLR, Germany
Exomars-2016 Entry Descent And Landing Operational Approach And Sensitivity Analysis | Guilanyà Jané, R. | GMV, Germany
12:30 - 12:50
Analytical Determination of the Thermal Loads on the Re-entry Vehicle SHEFEX III | Kolbe, A. | DLR, Germany
11:30 - 11:50
Numerical Investigation of the Thermal Benefit of Using a High Thermal Conductivity CMC for the Leading Edge of Hypersonic Vehicles | Reimer, T. | DLR, Germany
Inflatable and Foldable Aerothermodynamics Decelerators As Part Of Aero Sekur EDL Technologies | Messidoro, A. | Aero Sekur, Italy
11:30 - 11:50
12:30 - 12: 50
12:10 - 12:30
12:10 - 12:30
12:30 - 12:50
12:30 - 12:50
12:50 - 14:20
Lunch
14:20 - 14:50
Plenary Lecture (Auditorium) TEXUS 48 Flight Experiment for PMD Maturation (Ph. Behruzi) Flight Experiment II
Design for Demise IV
Flow Phenomena on Propulsion Systems II
Numerical Modelling VII
Chairs:F. Sourgen & J-M Muylaert
Chairs:B. Piazolles & B. Fritsche
Chairs:C. Dinescu & R. Vetrano
Chairs:H. Wong & D. Drikakis
14:55 - 15:15
MUSIC/FAST, a Pre-Design and Pre-Mission Analysis Tool for the Earth Atmospheric Re14:55 - 15:15 entry of Spacecraft, Capsules and deorbited Satellites | Sourgen, F. | ONERA, France
Monte-Carlo Analysis of Object Reentry in Earth's Atmosphere Based on Results of Taguchi Method | Plazolles, B. | R.Tech, France
14:50 - 15:15
A Verification and Validation Approach for Eulerian Modelling of Sloshing Flows | Dinescu, C. | NUMECA International , Belgium
15:15 - 15:35
Aerothermodynamic Re-entry Analysis of the CubeSat-sized Entry Vehicle MIRKA2 | Pagan, A. | University of Stuttgart, Germany
DEBRIS Tool and its Use in Mission Analysis Activities | Haya, R. | DEIMOS Space S.L.U., Spain
15:15 - 15:35
Liquid Propellant Sloshing: A study about the use of Open Source CFD Software | 15:15 - 15:35 Rebelo, T. | CEIIA - Center for Innovation and Creative Engineering, Portugal
15:15 - 15:35
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Thursday 5 March 2015
14:55 - 15:15
An Open-Source Hypersonic Aerodynamic and Aerothermodynamic Modeling Tool. | Mehta, P. | University of Strathclyde, United Kingdom
Simulations of Rarefied and Continuum Hypersonic Flow Over Reentry Objects | Scanlon, T. | University of Strathclyde, United Kingdom
8th European Symposium on Aerothermodynamics for Space Vehicles
15:35 - 15:55
CubeSat Aerothermodynamics and end-of15:35 - 15:55 life Computations | Vashchenkov, P. | Novosibirsk State University, Russia
a Preliminary Investigation of Child Object Demise for Uncontrolled Re-entry | Wada, S. | JAXA, Japan
15:55 - 16:15
QARMAN: An Atmospheric Entry Experiment on CubeSat Platform | Sakraker, I. | VKI, Belgium
15:55 - 16:15
ATV5 Shallow Reentry Mission: Challenges 15:55 - 16:15 and Achievements | De Pasquale, E. | ESA, France
16:15 - 16:35
16:15 - 16:35
16:15 - 16:35
15:35 - 15:55
Numerical Investigation of Flow Phenomena in a Planar ExpansionDeflection Nozzle | Wagner, B. | DLR, Germany
15:35 - 15:55
GPU-based DSMC as a Powerful Tool for Investigation of High-altitude Aerothermodynamics of Reentry Vehicles | Kashkovsky, A. | Novosibirsk State University, Russia
Droplet Sizing and Infrared Temperature Measurements in Superheated Sprays | Lamanna, G. | University of Stuttgart, Germany
15:55 - 16:15
Modeling Compressible Reacting Flows Using GP-GPU | Colonna, G. | CNR-Istituto di Metodologie Inorganiche e dei Plasmi, Italy
Multiphase Fluid Hammer with Noncryogenic and Cryogenic Fluids | Vetrano, R. | VKI, Belgium
16:15 - 16:35
Coffee Break
16:35 - 16:50
Gas Surface Interation VI
Boundary Layer Flows II
Measurement Techniques VI
Physical Modelling VI
Chairs:L. Ferracina & F. Punzo
Chairs:A. Passaro& T. Langener
Chairs:N. Murray & A. Mohamed
Chairs:P. Noeding & H. Wong
16:50 - 17:10
On the Flight Extrapolation of StagnationPoint Ablative Material Plasma Wind Tunnel 16:50 - 17:10 Tests | Turchi, A. | VKI, Belgium
Experimental Characterization of Roughness-Induced Transition on a Flat Plate at Mach 6 in the European ATLLAS-2 Programme | Passaro, A. | Alta S.p.A, Italy
16:50 - 17:10
High Heat Flux Measurements and Boundary Layer Investigation in VKI Plasmatron | Chazot, O. | VKI, Belgium
16:50 - 17:10
Numerical Modeling of Non-Newtonian Polarizable and Magnetizable Fluid Flow | Tzirakis, K. | IACM, FORTH, Greece
17:10 - 17:30
Coupling Internal Radiation to Material Response of Thermal Protection Systems | 17:10 - 17:30 Haussener, S. | Ecole Polytechnique Federale de Lausanne, Switzerland
Numerical Studies of 3D Instabilities Propagating in Supersonic CompressionCorner Flow | Novikov, A. | Central Aerohydrodynamic Institute (TsAGI), Russia
17:10 - 17:30
Catalytic Heating Effect on Metals and Quartz for Exomars Entry Conditions | Kolesnikov, A. | A.Ishlinskiy Institute for Problems in Mechanics of RAS, Russia
17:10 - 17:30
Critical Factor Analysis of Aerodynamic Force Predictions in Hypervelocity Nonequilibrium Flow Using HB2 Model | Li, K. | Institute of Mechanics, CAS, China
17:30 - 17:50
17:30 - 17:50
Radio Pulsar Receiver Systems for Space Navigation| Brito, D. | INESC-ID, Instituto 17:30 - 17:50 Superior Técnico, Universidade de Lisboa, Portugal
Comparative CFD Analyses of Shock Tube Experiments in CO2 Flow under Mars Entry Conditions | Noeding, P. | Airbus Defence and Space, Germany
18:10-19:10
Shock-wave/boundary layer Interaction on sharp and blunted flat plates | 17:30 - 17:50 Palchekovskaya, N. | Central aerohydrodynamic institute (TsAGI), Russia
Award Ceremony
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Thursday 5 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles Friday 6th of March 2015
09:00 - 18:00
VKI dedicated LS Physics of Sloshing (Room 01.1)
09:00 - 18:00
4th ESPSS Workshop (Room 02.1)
09:00 - 18:00
1st Spacecraft Demise Workshop (Room 02.2)
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Friday 6 March 2015
