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6th European Workshop on Thermal Protection Systems and
Hot Structures
Last update: 24 Maart 2009
Please click here to download the TPS-HS Abstract Book (pdf).
Wednesday, 1 April 2009 - DLR Grosser Hörsaal |
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08:30 |
Registration |
09:15-11:00 |
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- Welcome (IRS-ESA)
- Return, TPS and Hot structure technologies at DLR, L. Fröbel, DLR
- The IXV Programme - ESA’s Atmospheric Re-Entry Technology Demonstrator, G. Tumino, ESA
- EXPERT - A European Aerothermodynamics In-Flight Testbed, J. Gavira, ESA
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11:00-11:30 |
Coffee break |
11:30-13:00 |
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- Thermal Protection System (TPS) and Hot Structures Activity within the FLPP Core Technology Project, G. Ramusat, ESA
- Experimental and Numerical Entry Simulation at IRS, G. Herdrich, Institut fuer Raumfahrtsysteme (IRS)
- Plasma Power Handling in the ITER Fusion Device, G. Federici, Fusion for Energy
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13:00-14:15 |
Lunch break |
14:15-15:45 |
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14:15-15:45 |
- The Intermediate eXperimental Vehicle (IXV): the European Flight Opportunity for TPS&HS Technologies, A. Denaro, NGL Prime S.p.A
- TPS & HS Subsystem Activities for IXV PDR Preparation, M.T. Signorelli, Thales Alenia Space
- Thermo-Mechanical Design of the IXV Nose Assembly, R. Knoche, ASTRIUM Space Transportation
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- Thermal Non-Equilibrium in the Boundary Layer of a Flat Plate in RF Air Plasma, P. Boubert, CORIA
- ASA - A System Devoted to Hypersonic-Related Technologies, F. Fosssati, Thales Alenia Space, Italy
- On-going Capabilities and Developments of Re-Entry Plasma Ground Tests in EADS-Astrium, B. van Ootegem, ASTRIUM
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15:45-16:15 |
Coffee break |
16:15-18:15 |
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14:15-15:45 |
- Thermal Protection Systems Portfolio of ASTRIUM GmbH - Recent Developments, W.P.P. Fischer, ASTRIUM Space Transportation
- CMC Thermal Protection System Pre-Development for Re-Entry Demonstrator Vehicles, T. Pichon, SNECMA Propulsion Solide
- Investigations of Passive to Active Oxidation on C/SiC Hot Structures, F. Infed, MT Aerospace
- TPS Joining Technologies, J. Marcos, Fundacion INASMET
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- Development and Verification of an Instrumented Aerothermal Thermal Protection System Heat Shield Plug for Flight on the Mars Science Laboratory, E. Martinez, NASA
- Advanced Heat Flux Measurement during Re-entry Flight using The Non-Integer System Identification (NISI) Procedure, S. Lohle, University of Stuttgart
- DEDALO: Thermo-Mechanical Monitoring by Fiber Optic Devices on UHTC Structures, V. Latini, S.A.B. Aerospace
- Airborne Re-Entry Observation Experiment SLIT: UV Spectroscopy During Stardust and ATV Re-entry, S. Lohle, IRS
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18:30-20:00 |
Welcome drink (sponsored by DLR) |
09:00-10:30 |
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- The Sharp Edge Flight Experiment SHEFEX II, a Status Report, H. Weihs, DLR
- Design and Thermo-Mechanical Analysis of the Aerodynamic Control Surfaces on SHEFEX-II, H. Elsäßer, Institute of Structues and Design
- SHEFEX II Flight Instrumentation, T. Thiele, DLR
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- Thermal Conductivity Measurements under Non-Standard Conditions, S. Vidi, Bavarian Centre for Aerospace Reseacrh
- High Temperature Thermal Conductivity Measurement Apparatus, M. Selzer, DLR
- The Use of Flash Methods to Determine Thermal Conductivity, W. Hohenauer, Austrian Institute of Technology
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10:30-11:00 |
Coffee break |
11:00-13:00 |
IRS Room 1Session 6A: The EXPERT Vehicle - Part 1Chair: A. Thirkettle, A. Gulhan |
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- TPS Design Methodology for the EXPERT capsule, J. Thoemel, ESA
- TPS Design, Development and Verification Approach for EXPERT Program, E. Brach Prever, Thales Alenia Space, Italy
- Thermal-Structural Performances of the EXPERT Thermal Protection System, J. Fatemi, Dutch Space
- Thermo-Mechanical Design of The Expert Nose and Testing of The Load Introductions, T. Reimer, DLR
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- Development of a European Ablative Material for Heatshields of Sample Return Missions, H. Ritter, ESA
- Enhanced Ablative TPS Study for High-Energy Entry Missions, F. Fossati, Thales Alenia Space Italy
- Mechanical and Ablative Properties of Silica-Phenolic Composites for Thermal Protection Systems, M.L. Gregori, Inst. Of Aeronautics and Space
- Estimating Properties of Materials Interacted with High-Enthalpy Gas Flow by Inverse Problems Technique, A.V. Nenarokomov, Moscow Aviation Institute
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13:00-14:15 |
Lunch break |
14:15-16:15 |
IRS Room 1Session 7A: The EXPERT Vehicle - Part 2Chair: F. Ratti, E. Brach-Prever (TBC) |
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- Status of the IRS EXPERT Instrumentations PYREX, PHLUX and RESPECT, G. Herdrich, University of Stuttgart
- EXPERT Open Flap Assembly and its Instrumentation, A. Gulhan, DLR
- Thermal Measurement Techniques for Movable Control Surfaces in Re-entry Vehicles, C. Pereira, RUAG Aerospace
- Qualification of a ceramic fin for flight on European Experimental re-entering capsule EXPERT, A. Del Vecchio, CIRA
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- Ablation Response of Fibrous Materials with Different Matrices: Modeling, Comparison, and Application, J. Lachaud, NASA Ames Research Center
- Design and Numerical Modelling of Charring Ablators for Re-Entry Applications, T. van Eekelen, SAMTECH SA
- Navier-Stokes Simulations with Graphite Surface Ablation for Atmospheric Entry, D. Bianchi, La Sapienza University, Rome
- Numerical Rebuilding of Ablative Test Cases Using KCMA, P. Reynier, ISA
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17:30-22:00 |
Visit Schloss Ludwigsburg and Workshop dinner |
09:00-10:30 |
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- ASTRIUM's TPS Experiments on SHEFEX II - Design & Analyses, W.P.P. Fischer, ASTRIUM
- Design and Layout of the Combined Sensor System COMPARE for SHEFEX II, A. Preci, Univ. of Stuttgart
- Heat Balance of the Transpiration-Cooled Heat Shield Experiment AKTiV on SHEFEX II, H. Boehrk, DLR
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- Upgrade of three Laboratory Test Setups to measure Material Properties and Antenna Models at High Temperatures occurring during Re-entry Vehicle Flights, P. Kabacis, Wroclaw University of Technology
- Computed Tomography for Non-Destructive Inspection of TPS Components, T. Ullmann, DLR
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10:30-11:00 |
Coffee break |
11:00-13:00 |
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- Film Cooling Investigation of a Double Wedge Model in Hypersonic Flow, K.A. Heufer, RWTH
- UHTC Thermal Sprayed Coating as a TPS for Re-Entry Vehicles, M. Tului, Centro Sviluppo Materiali
- Analysis and Design of UHTC Hot Structures for Ground and Flight Tests, M. De Stefano Fumo, University of Naples
- Modeling Elastic and Thermal Properties of 2.5D Carbon Fiber C/SiC Hybrid Matrix Composites by Homogenization Method, L. Pardini, CTA, IAE
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- Computational Aeroheating Analyses of a Capsule in Martian Atmosphere, G. Pezzella, CIRA
- Thermal Protection System of the ExoMars Entry Probe, J-M. Bouilly, EADS ASTRIUM Space Transportation
- Dust Particle Erosion during Mars Entry, K. Keller, HPS
- Particle Erosion Tests on an Ablative Material in Martian Atmosphere, B. Esser, DLR
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13:20-14:00 |
Visits of Institutes at DLR & IRS |
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