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8th European Symposium on Aerothermodynamics for Space Vehicles
version 11.02.2015
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, G. Saccoccia)
15:55 - 16:15
(ESA, J. Longo)
16:15 - 16:35
Coffee break
Plenary Session
In Flight Experimentation
16:35 - 16:55
Business Case Analysis of a Multi-Functional In-Flight Experimental System
Euroconsult, M. Puteaux
Round Table
Commercial Access to Space Providers
16:55 - 17:15
AIRBUS Defence & Space, A. Schuette
17:15 - 17:35
XCOR Space Expeditions, H. van Hulten
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Monday 2 March 2015
17:35 - 17:55
Swiss Space Systems S3, P. Jaussi
Round Table
Commercial Sub-system Providers
17:55 - 18:15
Suborbital Research Association, Dr. V. Pletser
18:15 - 18:35
Swedish Space Corporation SSC, G. Florin
18:35 - 18:55
QB50, J-M Muylaert
19:00 - 20:00
Symposium highlight I
The IXV Project (G. Tumino)
20:00 - 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:S. Lingard & 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
| Lingard, S. | 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 | Lingard, S. | 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 | Lingard, S. | 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
Coffe 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
Aero-Thermal Evaluation of Silicon Carbide
Flexible TPS using a 30kW ICP Torch |
11:30 - 11:50
Owens, W. | University of Vermont, United
States
Experimental Investigations of
Characteristics of the Air Intake with
Internal Compression | Talyzin, V. |
TsAGI, Russia
11:50 - 12:10
Experimental Characterization of Cork
Based Thermal Protection Material P50 |
Sakraker, I. | VKI, Belgium
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 | Molchanova, A. | ITAM,
NSU, Russia
12:10 - 12:30
Deformation and Cracking in CFRP Ablator
During Arc Wind Tunnel Heating | Ogawa,
R. | Tokyo University of Science , Japan
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
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 & Exhibition
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
17:30 - 17:50
Light Weight Ablator Response Model
Development & Challenges | Mansour, N.
| NASA, United States
Heat Convention Through Flat Plate |
Taploo, A. | SRM University, India
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
18:10 - 18:30
Gas-Surface Interaction. Experimental
Determination of PM1000 and CVD-C/SiC
Catalytic Properties | Massuti-Ballester, B.
| University of Stuttgart, Germany
18:10 - 18:30
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
Radio Pulsar Receiver Systems for Space
Navigation| Brito, D. | INESC-ID, Instituto
17:50 - 18:10
Superior Técnico, Universidade de Lisboa,
Portugal
18:10 - 18:30
18:10 - 18:30
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Tuesday 3 March 2015
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
08:30 - 09:00
Registration & Speaker Debriefing
09:00 - 09:30
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 & C. Chiarelli
Chairs:L. Konozsy & Ph. Behruzi
Chairs:G. Colonna & P. Gnemmi
09:35 - 09:55
The ESA ARC Project : Ablation Radiation
Coupling for hypervelocity re-entry with
low density type ablators | Leyland, P. |
EPFL, Switzerland
09:30 - 09:50
MarcoPolo-R ERC Dynamic Stability
Characterisation : Study Logic | Clopeau,
E. | Airbus Defence and Space, France
09:30 - 09:50
Multiphase Fluid Hammer with Noncryogenic and Cryogenic Fluids | Vetrano,
R. | VKI, Belgium
09:30 - 09:50
Self-consistent Collisional-radiative Model
for Shock Tube in Jupiter Atmosphere |
Colonna, G. | CNR-Istituto di Metodologie
Inorganiche e dei Plasmi, Italy
09:55 - 10:15
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
09:50 - 10:10
Experimental Investigation of Dynamic
Characteristics for MarcoPolo-R ERC in Low
09:50 - 10:10
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
09:50 - 10:10
An Adaptive Hybrid Statistical Narrow Band
Model for Coupled Radiative Transfer in
Atomspheric Entry Flows | Scoggins, J. |
VKI, Belgium
10:15 - 10:35
Off-Stagnation Tests of ESA IXV TPS
Interfaces in Plasmatron | Trifoni, E. |
CIRA, Italy
10:10 - 10:30
Marco Polo-R ERC Dynamic Stability
Characterization. | Berner, C. | ISL,
France
10:10 - 10:30
Experimental and Numerical Study of the
Flow Characteristics in a Cryogenic Valve
10:10 - 10:30
with Liquid Nitrogen and Water | Peveroni,
L. | VKI, Belgium
Noise Reduction Scheme for Probabilistic
Radiation Modelling in DSMC | Petkow, D. |
Gradel sárl, Luxembourg
10:35 - 10:55
Final CFD Design of SCIROCCO Arc-jet
Test Conditions for IXV TPS Interfaces |
Trifoni, E. | CIRA, Italy
10:30 - 10:50
MarcoPolo-R ERC Dynamic Stability
Characterization : Computational
Campaign | Charbonnier, D. | CFS
Engineering, Switzerland
10:30 - 10:50
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
10:30 - 10:50
Coffe break
10:55 - 11:10
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
11:10 - 11:30
The Intermediate eXperimental Vehicle In
Flight Experimentation. From the Design to 11:10 - 11:30
the Flight. | Rufolo, G. | CIRA, Italy
Aerothermoelastic Structural Topology
Optimisation for a Hypersonic Transport
Aircraft Wing | Verstraete, D. | The
University of Sydney, Australia
11:10 - 11:30
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
11:10 - 11:30
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
11:30 - 11:50
Plasma Assisted CO2 Dissociation Models
for Environment, Energy and Aerospace
Applications. | Colonna, G. | CNR-Istituto
di Metodologie Inorganiche e dei Plasmi,
Italy
CATE: CATalytic Experiment on the
Intermediate eXperimental Vehicle |
VILADEGUT, A. | VKI, Belgium
11:50 - 12:10
Comparison of Quantum Mechanical and
Empirical Potential Energy Surfaces for N2
Dissociation | Jaffe, R. | NASA Ames
Research Center, United States
12:10 - 12:30
Frequency Comb High Speed Broadband
Spectroscopic Sensor To Probe
Aerodynamic Flows | Mohamed, A. |
ONERA, France
12:10 - 12:30
Diffusion Monte Carlo Models of Confined
Hydrogen Species |Micca Longo, G. | CNRIMIP, Italy
12:30 - 12:50
Modular Power Bus for Space Vehicles
(MPBus) | Pérez, B. | Najera Aerospace, 12:30 - 12:50
Spain
11:30 - 11:50
Aerothermal Environment Assessment of
the Hexafly-INT Experimental Flight Test
Vehicle (EFTV) | Carandente, V. | CIRA,
Italy
11:30 - 11:50
Rapid Aero-Thermodynamic Analysis for
Hypersonic Air Vehicles | Wuilbercq, R. |
University of Strathclyde, United Kingdom
11:50 - 12:10
Wind Tunnel Experiments on the SHEFEXII Configuration in the Frame of the Post
Flight Analyses | Thiele, T. | DLR,
Germany
11:50 - 12:10
Investigation of Heatflux Modification by
Magnetohydrodynamic Interaction
11:50 - 12:10
Employing the DLR CFD Code TAU | Fertig,
M. | DLR, Germany
12:10 - 12:30
Huygens Flight Performance Analyses |
12:10 - 12:30
Lingard, S. | Vorticity Ltd, United Kingdom
12:30 - 12:50
Assessment of Hypersonic Aerodynamic
Performance of the EFTV-ESM
Configuration in the Framework of Hexafly- 12:30 - 12: 50
INT Research Programme | Carandente, V.
| CIRA, Italy
11:30 - 11:50
12:50 - 14:20
Lunch & Exhibition
14:20 - 14:50
Plenary Lecture (Auditorium)
Phys4Entry Project (D. Bruno)
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
14:55 - 15:15
Finite Rate Surface Catalysis Modelling of
PM1000 and SiC Employing the DLR CFD
Solver TAU | Fertig, M. | DLR, Germany
15:15 - 15:35
Rebuilding Thermal Response and Ablation
Radiation Coupling for Superorbital Return 15:15 - 15:35
| Mora-Monteros, J. | EPFL, Switzerland
14:55 - 15:15
A Multi-domain ALE Algorithm for
Simulating Flows inside Free-piston Driven
14:50 - 15:15
Test Facilities | Bensassi, K. | VKI,
Belgium
Numerical Simulation of a Tandem Nozzle
Flow for a High Enthalpy Impulse Wind
Tunnel | Qian, Z. | AVIC Aerodynamics
Research Institute, China
15:15 - 15:35
Development and Validation of Numerical
Solvers for the Analysis of High-pressure
Combustion in Liquid Rocket Engines |
Schettino, A. | CIRA, Italy
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
14:55 - 15:15
Non-equilibrium Modeling of Inductively
Coupled RF Plasmas | Panesi, M. |
University of Illinois at Urbana Champaign,
United States
15:15 - 15:35
A Reduced-order Modeling Approach to
Enable Kinetic Simulations of Nonequilibrium Hypersonic Flows | Panesi, M.
| University of Illinois at Urbana
Champaign, United States
8th European Symposium on Aerothermodynamics for Space Vehicles
15:35 - 15:55
On the Analysis of Radiative Heat Transfer
Influence Inside the Piston-Driven Shock
15:35 - 15:55
Tunnel HELM | Garcia Garrido, J. |
University of the Federal Armed Forces
Munich, Germany
Hybrid Paraffin-Based Technology
Demostrator in the Framework of the
Italian Hyprob Program: Status of Design
and Development Activities | DI
CLEMENTE, M. | CIRA, Italy
15:35 - 15:55
Development of Detailed Chemistry Models
for Boundary Layer Catalytic
Recombination | Bellas, G. | VKI, Belgium
15:55 - 16:15
A Fully Implicit Material Response Code
with Ablation and Pyrolysis for Simulation
of Thermal Protection Systems |
D'Ambrosio, D. | Politecnico di Torino,
Italy
15:55 - 16:15
Standard Probe Testing in European High
Enthalpy Facilities | Merrifield, J. | Fluid
Gravity Engineering, United Kingdom
15:55 - 16:15
Large-eddy Simulations of Solid-Rocket
Motors Reactive Plumes | Poubeau, A. |
CERFACS, France
15:55 - 16:15
Modeling Rarefied Molecular Oxygen Flows
by CT-DSMC | Frezzotti, A. | Politecnico di
Milano, Italy
16:15 - 16:35
A Finite Element Approach for the Design
of Innovative Ablative Materials for Space
Applications | Scigliano, R.. | CIRA, Italy
16:15 - 16:35
An overview of HyFIE Technical Research
Project: cross testing in main European
hypersonic wind-tunnels on EXPERT body.
| Brazier, J. | ONERA, France
16:15 - 16:35
A Zooming Approach to Investigate Heat
Transfer in Liquid Rocket Engines with
ESPSS Propulsion Simulation Tool |
Leonardi, M. | La Sapienza, Italy
16:15 - 16:35
15:35 - 15:55
Carbon Gasification in PICA Ablators |
Grana-Otero, J. | University of Kentucky,
United States
Coffee Break
16:35 - 16:50
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
16:50 - 17:10
Experimental Verification of Thermal
Management Concepts for Space Vehicles | 16:50 - 17:10
Esser, B. | DLR, Germany
The Oxford High Density Tunnel | Doherty,
16:50 - 17:10
L. | University of Oxford, United Kingdom
Experimental Results on ShockWave/Boundary-Layer Interaction Induced
16:50 - 17:10
by a Movable Wedge | Daub, D. | DLR,
Germany
Hypersonic Aero-Thermo-Dynamic Heating
Prediction With High-Order Discontinous
Galerkin Spectral Methods | Garicano
Mena, J. | VKI, Belgium
17:10 - 17:30
Aeroelastic Instabilities of FGM Panels
under Thermo-Mechanical Loads | Zappino, 17:10 - 17:30
E. | Politecnico di Torino, Italy
The Oxford Stalker Tunnel | McGilvray, M.
| University of Oxford, United Kingdom
17:10 - 17:30
Development and Application of
Temperature Sensitive Paints in the High
Enthalpy Shock Tunnel Göttingen, HEG |
Martinez Schramm, J. | DLR, Germany
17:10 - 17:30
Hypersonic Aero-Thermo-Dynamic Heating
Prediction With Unstructured Residual
Distribution Methods | Garicano Mena, J. |
VKI, Belgium
17:30 - 17:50
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
17:30 - 17:50
Locally resolved boundary layer radiation
during ablation testing | Helber, B. | VKI, 17:30 - 17:50
Belgium
Characteristics of Aerodynamic Heating on
a Sharp Cone in Hypersonic Flow | Wang,
Q. | Institute of Mechanics, CAS, China
17:50 - 18:10
Flow over the Axisymmetrical Body in
Hypersonic Flow of Perfect Gas | Egorov, I.
17:50 - 18:10
| Central Aerohydrodynamic Institute
(TsAGI), Russia
17:50 - 18:10
Application of Particle Image Velocimetry
for Aero(thermo)dynamics | Schrijer, F. | 17:50 - 18:10
Delft University of Technology, Netherlands
CFD Modeling of the Ariane 6 Space
Launcher from Ground to Space | Pont, G.
| Airbus Defence and Space, France
17:30 - 17:50
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
18:10 - 18:30
18:10 - 18:30
18:10 - 18:30
Experimental Investigation of Heat Flux
Fluctuations on the Rear Cover of a
Planetary Probe Entry-Configuration |
Neeb, D. | DLR, Germany
18:30 - 19:30
Symposium highlight II
The ESTEHER facility (M. da Silva)
19:30 - 23:30
Visiting ESTHER facility
Symposium Dinner
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Wednesday 4 March 2015
18:10 - 18:30
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
Coffe 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 | Cinquegrana, D. |
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 & Exhibition
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
Aeroshape Design of the Demise
Observation Capsule DOC | Gardi, R. |
CIRA, Italy
15:15 - 15:35
MUSIC/FAST, a Pre-Design and Pre-Mission
Analysis Tool for the Earth Atmospheric Re15:15 - 15:35
entry of Spacecraft, Capsules and deorbited Satellites | Sourgen, F. | ONERA,
France
14:55 - 15:15
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
14:55 - 15:15
Spontaneous Rayleigh-Brillouin Scattering
Profiles for Air Using the Direct Simulation
Monte Carlo Method | Scanlon, T. |
University of Strathclyde, United Kingdom
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
An Open-Source Hypersonic Aerodynamic
and Aerothermodynamic Modeling Tool. |
Mehta, P. | University of Strathclyde,
United Kingdom
8th European Symposium on Aerothermodynamics for Space Vehicles - Programme Thursday 5 March 2015
8th European Symposium on Aerothermodynamics for Space Vehicles
15:35 - 15:55
Aerothermodynamic Re-entry Analysis of
the CubeSat-sized Entry Vehicle MIRKA2 |
Pagan, A. | University of Stuttgart,
Germany
15:55 - 16:15
CubeSat Aerothermodynamics and end-of15:55 - 16:15
life Computations | Vashchenkov, P. |
Novosibirsk State University, Russia
16:15 - 16:35
QARMAN: An Atmospheric Entry
Experiment on CubeSat Platform |
Sakraker, I. | VKI, Belgium
15:35 - 15:55
a Preliminary Investigation of Child Object
Demise for Uncontrolled Re-entry | Wada,
S. | JAXA, Japan
15:35 - 15:55
ATV5 Shallow Reentry Mission: Challenges
15:55 - 16:15
and Achievements | De Pasquale, E. |
ESA, France
16:15 - 16:35
16:15 - 16:35
Temperature Measurements of Acetone
Flashing Jet by Laser Induced Fluorescence 15:35 - 15:55
| Vetrano, M. | VKI, Belgium
Simulations of Rarefied and Continuum
Hypersonic Flow Over Reentry Objects |
Scanlon, T. | University of Strathclyde,
United Kingdom
Numerical Investigation of Flow
Phenomena in a Planar ExpansionDeflection Nozzle | Wagner, B. | DLR,
Germany
15:55 - 16:15
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
16:15 - 16:35
Modeling Compressible Reacting Flows
Using GP-GPU | Colonna, G. | CNR-Istituto
di Metodologie Inorganiche e dei Plasmi,
Italy
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
Characterization of Ground Testing
Condition in High Enthalpy and Plasma
Wind Tunnels for Aerospace Missions | del
Val Benítez, A. | VKI, Belgium
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
Coupling Internal Radiation to Material
Response of Thermal Protection Systems |
17:30 - 17:50
Haussener, S. | Ecole Polytechnique
Federale de Lausanne, Switzerland
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
17:10 - 17:30
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