Sunday 29th September 2019 17:00 => 20:00 REGISTRATION

19:00 => 21:00 WELCOME COCKTAIL Monday 30th September 2019 8:30 REGISTRATION

9:00 WELCOME COFFEE ROOM PLENARY SESSION – Torre Cintola / Sala Cupola CONFERENCE OPENING 10:00 (G. Ortega, ESA) KEYNOTE SPEECH: As "FAR" as Italy can go... 10:30 (G. Saccoccia, ASI)

KEYNOTE SPEECH: Leonardo: the Flight and the Moon: Why the Apulian Science Academy is celebrating Leonardo 11:00 (Prof. L. Borzacchini and Prof. E. Scandale, University of Bari)

KEYNOTE SPEECH: Critical data analysis of an hypersonic speed departure: the Space Shuttle Columbia last flight 11:30 (General Roberto Vittori, Italian Goverment)

12:00 LUNCH

KEYNOTE SPEECH: The Space Rider Development Programme 14:00 (J. Longo, ESA)

PLENARY ROUND TABLE: Enabling Sub-orbital Flight: Perspectives, Challenges, and Opportunities 14:30 G.Saccoccia (ASI), M. Sippel (DLR), A. Cassell (NASA), F. Cupertino (University of Bari), T. Hideyuki (JAXA), G. Ortega (ESA) 15:30 COFFEE BREAK Session 1.1 - Expendable Session 1.3 - Supersonic and Session 1.2 - Re-usable Space Space Transportation Systems Hypersonic Flight Missions and Session 1.4 - Decelerators Transportation Systems and Exploration Vehicles Vehicles

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

Helmut Ciezki (DLR), Tanno Hideyuki (JAXA) Pierluigi Pirrelli (SITAEL) Jorgen Bru (ESA) Don Ellerby (NASA) Nicole Viola (Politechnic of Torino) Steve Lindgard (Vorticity) Chairpersons Alejandro M. San Martin (JPL) Mariano Sanchez (Deimos) Jean-Francois Perelgritz (Airbus DS) Philippe Tran (ArianeGroup)

Adaptive Deployable Entry Development and Testing of the Particle Size In Solid Rocket Analysis of VTVL and VTHL Placement Technology Parachute Recovery System for Motor Plume: New Experimental Reusable Launch Vehicle (Adept)Sounding Rocket Flight the Reusable PLD Space Miura 1 16:00 Method Configurations Test Suborbital Rocket (Filippo Maggi, Politecnico Di Milano) (Leonid Bussler, DLR) (Alan Cassell, NASA Ames Research (Charles Lowry, Airborne Systems Center) North America) Design and Qualification Testing Preliminary Safety Assessment of Space Rider Critical Reusability of Two European Parachute High Altitude Drop Tests of the Candidate Stratofly Vehicle Challenges Mortars for the Esa Exomars 2020 Exomars Rsp Parachute System Configurations 16:20 (Angelo Denaro, Thales Alenia Mission (John Underwood, Vorticity Ltd) (Khooshboo Dani, University of Space S.p.a.) (Rudi Matthijssen, APP Southern California) ArianeGroup) Feasibility of Development of Noise and Vibration Simulation Numerical Simulation of the Mechanically Deployable Aero- Green Throttleable Liquid and Measurement In High Speed HYSHOT Li Combustor for Decelerators for Mars Entry Propulsion for Exploration and Vehicles 16:40 Hypersonic Propulsion (Lisa Peacocke, Imperial College Space Transportation (Nicholas Eaton, Space Acoustics (Pietro De Palma, Politecnico di Bari) London) (Adam Okninski, Institute of Aviation) GmbH) Stratofly Project Approaches for Innovative Evolution and Evaluation of the Structural Schemes and Flight Vehicle Design of A Manned Aurora – A New Pioneering RLV DARE Large Envelope Advanced Modelization of Hypersonic Mars Entry System Concept Parachute System 17:00 Aircraft and Space Vehicles (Csaba Jéger, ESA) (Wolfgang Fischer, POLARIS) (Lars Pepermans, Delft Aerospace (Jacobo Diaz, Universidade da Rocket Engineering) Coruña)

The FLPP-LPSR (Liquid Propulsion Stage Recovery) CFD / FSI Simulaton of Parachute 17:20 Project: Description and Results Inflation (Francisco Garcia, Payload (John Underwood, Vorticity Ltd) Aerospace S.L.) 17:40 END OF DAY 1

WELCOME COCKTAIL sponsored by SITAEL (P. Pirelli, SITAEL) 19:00 => 21:00 and AWARD to the Best Conference Paper (J. Longo, ESA)

1 Tuesday 1st October 2019 Session 2.2 - Supersonic and Session 2.4 - Testing Facilities, Session 2.1 - Re-usable Space Session 2.3 - Thermal Protection Systems Hypersonic Flight Missions and Verification and Validation Transportation Systems TPS Vehicles Methods ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

Jorgen Bru (ESA) Kazuhisa Fujita (JAXA) Stijn Lemmens (ESA) Thomas Reimer (DLR) Chairpersons Gerrie Mullen (Reaction Engines) Rodrigo Haya Ramos (SENER) Alessandro Gabrielli (ASI) Jean-Marc Bouilly (ArianeGroup) Damien Gille (Arianespace) Nicole Viola (Politechnic of Torino) Gérard Ordonneau (ONERA) Heiko Ritter (ESA)

Performance Capability Experiments In T6: A Subsonic and Supersonic Ground Development of A Novel Mass Hypervelocity, Transient and Multi- European Solutions for Heatshields of High Experiments for the Callisto VTVL Flow Measurement Device for Mode Ground Test Facility for High- Energy Entry Probes 9:10 Launcher Demonstrator High Speed Intake Testing Enthalpy Aerothermodynamics (Jean-Marc Bouilly, ArianeGroup Sas) (Johannes Riehmer, DLR) (Luke Doherty, University of Oxford) Research (Peter Collen, University of Oxford)

Characterization of SRM Plumes The Influence of Mach Waves On Experimental Investigation of Overview of Heatshield for Extreme Entry With Alumina Particulate In Laminar-Turbulent Transition for Supersonic Panel Flutter Environment Technology (HEEET) 9:30 Subscale Testing Supersonic Flow (Alessandro D'aguanno, Delft (Don Ellerby, NASA) (Dominik Saile, DLR) (Ivan Egorov, TSAGI) University of Technology)

Modeling and Simulation of Aerospace TPS Material A Sub-Orbital Testbed Vehicle for Supersonic Combustion and Characterizations At CIRA By Ballistic Entries for Saturn, Uranus, and Engine-Assisted Braking On Re- Plasma Assisted Combustion Means of SLI Radioactive Beam Neptune With HEEET TPS 9:50 Entry (Christer Fureby, the Swedish Tracer, IBA and IR-thermography (Dinesh Prabhu, Ama, Inc.) (Renato Salles, Omnidea Lda.) Defense Research Agency - FOI) (Mario De Cesare, CIRA)

From Hypersonic Aircraft To Ascent and Re-Entry Vehicles: Refurbishment and Thermal and Mechanical Analysis European Technology Roadmaps Characterisation of the Oxford Low Preliminary Heatshield Design for A Potential of the Body Flap Assembly of for Future Reusable Space Density Hypersonic Wind Tunnel European Probe To An Outer Planet 10:10 Space Rider Re-Entry Module Transportation Systems (Nathan Donaldson, University of (Heiko Ritter, ESA) (Roberto Scicliano, CIRA) (Roberta Fusaro, Politecnico di Oxford) Torino)

Stratofly Vehicle: A Test Bed for Volume Reconstruction of Optically Ultra-Fast Passenger Transport Integrated Solid Metals Heat Thin Plasma Flows By 3-D Light Study of Functionally Graded Ablative Options Enabled By Reusable Pipes Technology Field Deconvolution Material With Density Gradient 10:30 Launch Vehicles (Roberta Fusaro, Politecnico di (Martin Eberhart, University of (Toshiyuki Suzuki, JAXA) (Martin Sippel, DLR) Torino) Stuttgart / Institute of Space Systems)

Stratofly thermal and Energy Management Concept: Enabling Solid Carbon Produced During Miura-1 Avionics System: An Technology Towards Reusable Titan Entry Simulation By An Arc- Development of A Low-Density Phenolic- 10:50 Affordable and Reliable Approach Access To Space and Reentry Driven Flow Facility Impregnated Fibrous Ablator (Emanuele Di Sotto, GMV) Vehicles (Antonio Esposito, University of (Christian Zuber, DLR) (Roberta Fusaro, Politecnico di Naples Federico II) Torino) 11:10 COFFEE BREAK Session 2.5 - Re-usable Space Session 2.6 - Supersonic and Session 2.8 - Testing Facilities, Transportation Systems and Session 2.7 - Thermal Protection Systems Hypersonic Flight Missions and Verification and Validation Sub-orbital and Small Launch TPS Vehicles Methods Systems

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Jorgen Bru (ESA) Kazuhisa Fujita (JAXA) Thierry Magin (VKI) Thomas Reimer (DLR) Burkard Esser (DLR) Rodrigo Haya Ramos (SENER) Marco Marini (CIRA) Jean-Marc Bouilly (ArianeGroup) Chairpersons Mariano Sanchez Nogales (Deimos Nicole Viola (Politechnic of Torino) Gérard Ordonneau (ONERA) Heiko Ritter (ESA) Space) PLD Space Reusable Small Launchers: Recovery System Main Challenges and Goals of the Planned Wind Tunnel Experiments Cork P50 and TPS3L Ablation Experiments Strategy for Two Rocket H2020 Stratofly Project At DLR Köln for the Reusability for the Demise Observation Capsule Including 11:30 Developments (Roberta Fusaro, Politecnico di Flight Experiment (REFEX) An Adhesive Bonded TPS3L Structure (Francisco Garcia, Payload Torino) (Andreas Flock, DLR) (Bernd Helber, Von Karman Institute) Aerospace S.L.) Total Temperature Measurements Experimental Investigation of Characterization of the thermal Degradation In the Oxford New Suborbital Rocket Fluidic Thrust Vectoring for of Carbon-Phenolic Materials: An High Density Tunnel Demonstrator - Ilr-33 Amber Scramjets Experimental Effort On the ZURAM® Ablator 11:50 (Tobias Hermann, University of (Michal Pakosz, Institute of Aviation) (Christopher Hambidge, University of (Francisco Torres Herrador, Von Karman Oxford) Oxford) Institute)

Assessment of Combustion Small-Launchers Platforms Towards High Resolution Photogrammetric Models for thermodynamic 3D Focused Schlieren Imaging Comparison Surface Analysis of Ablation Processes In Modeling of the Engines for Using A Plenoptic Camera 12:10 (Jasmine Rimani, Politecnico Di High-Enthalpy Air Plasma Flow Hypersonic Propulsion (Philipp Kerth, University of Oxford) Torino) (Felix Grigat, Institute of Space Systems IRS) (Ali Can Ispir, Von Karman Institute)

Optimization Framework Coupled A Novel Approach To Flight-To- Carbon/Phenolic Composites and Phenolic With Ecosimpro Platform for the Ground Scaling In Plasma Impregnated Carbon Ablators based on ex- Propulsion Power Plant of A Facilities: Axisymmetric To Planar 12:30 PAN carbon fibers Hypersonic Aircraf Transformation (Maurizio Natali, University of Perugia) (Ali Can Ispir, Von Karman Institute)t (David Leiser, University of Stuttgart) 12:50 LUNCH ROOM PLENARY SESSION – Torre Cintola / Sala Cupola

PLENARY ROUND TABLE: Micro and Nano-launcher Systems

14:30 T. Kranz (ESA), J. Bru (ESA), A. Gabrielli (ASI), G. Avanzini (Distretto Tecnologica Aerospaziale DTA/UniSalento), M. Bello Mora (Deimos), A. Argemi Samso (PANGEA), J. Vila (ArianeWorks), F. Spaziani Brunella (AVIO ELV), T. Pardal (ONMIDEA), S. Caruel (Arianespace), C. Schmierer (HyImpulse), A. Boiron (NAMMO)

16:00 COFFEE BREAK Session 2.10 - Supersonic and Session 2.12 - Testing Facilities, Session 2.9 - Session 2.11 - Thermal Protection Systems Hypersonic Flight Missions and Verification and Validation Aerothermodynamics TPS Vehicles Methods

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

Burkard Esser (DLR) Kazuhisa Fujita (JAXA) Thierry Magin (VKI) Thomas Reimer (DLR) Chairpersons Marcello Amato (CIRA) Rodrigo Haya Ramos (SENER) Marco Marini (CIRA) Jean-Marc Bouilly (ArianeGroup) Philippe Tran (Arianegroup) Nicole Viola (Politechnic of Torino) Gérard Ordonneau (ONERA) Heiko Ritter (ESA)

2 Development of Non-Oscillatory Hydrogen-Based Thrusters for Finite Element thermal Modelling Surrogate Modeling Assisted Calibration of Lattice Boltzmann Method for Supersonic and Hypersonic for Complex Isotropic Graphite TACOT Material Database Through Bayesian 16:20 Shock Wave Flows Flight: Experimental Specimens Tested In the L3K Arc Inference Using MSL Flight Data (Zuheyr Alsalihi, Von Karman Characterization Heater (Przemyslaw Rostkowski, University Of Illinois Institute) (Filippo Maggi, Politecnico Di Milano) (Matthew Ross, DSTL) At Urbana-champaign)

Vibrational Energy Balance In Stratofly Project Challenges In the Ablative-Material Numerical Test International Experimental Investigation of Jet In Exchange and Non-Reactive Fields of Airframe, Series (AblaNTIS): An Supersonic Cross-Flow By Means Collisions of Nitric Oxide In Aerothermodynamics, High- Experimental/Numerical Effort To Support the of PIV 16:40 Dissociated Air Speed Propulsion and Energy Validation of Material thermal-Response (Ferry Schrijer, Delft University of (Daniil Andrienko, Texas A&M Management Systems Tools Technology) University) (Marco Marini, CIRA) (Alessandro Turchi, Von Karman Institute) Propulsion Test Vehicles Need for Low-Noise High-Speed Multi-Scale Modeling of Low-Density Carbon- 17:00 (Gerrie Mullen, Reaction Engines Facilities In Europe Phenolic Ablators Ltd) (Johan Steelant, ESA) (Michael Barnhardt, NASA) Session 2.14 - Supersonic and Session 2.16- Testing Facilities, Session 2.13 - Session 2.15 - Thermal Protection Systems Hypersonic Flight Missions and Verification and Validation Aerothermodynamics TPS Vehicles Methods

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

Burkard Esser (DLR) Kazuhisa Fujita (JAXA) Thomas Reimer (DLR) Chairpersons Marcello Amato (CIRA) Rodrigo Haya Ramos (SENER) Jean-Marc Bouilly (ArianeGroup) Philippe Tran (Arianegroup) Nicole Viola (Politechnic of Torino) Heiko Ritter (ESA) Detailed Chemistry Simulations of Diffusing Meteor Trails With Preliminary Numerical Microscopic Imaging of Heatshield Oxidation Application To Radio Characterization of Stratofly In 4D 17:20 Observations Vehicle’S Intake (Francesco Panerai, University of Illinois at (Federico Bariselli, von Karman (Pietro Roncioni, CIRA) Urbana-champaign) Institute for Fluid Dynamics) Exploring the Impact of the Initial Technology Development and Stratofly High-Speed Propelled Temperature Field Uncertainty On the Infusion by NASA's Entry Vehicle Preliminary Aero-thermal Response of Ablative Materials Using Model 17:40 Systems Modeling Project Design Selection Techniques (Michael Barnhardt, NASA) (Roberto SCIGLIANO, CIRA) (Giulio Gori, INRIA - CMAP Ecole Polytechnique)

Calculation of Radiative Shock-Boundary Layer Interaction Processes In Plasmas Using the Phenomena In A Hydrogen Coupling Strategies for Modeling TPS Particle-Based Pic-Dsmc Code Transpiration Cooled Supersonic 18:00 (Alexandre Martin, University of Kentucky) Piclas Combustion Ramjet (Scramjet) (Julian Beyer, University of Stuttgart) (Friedolin Strauss, DLR)

ROOM PLENARY SESSION – Torre Cintola / Sala Cupola

KEYNOTE SPEECH: ArianeWorks and the future of European Launchers 18:30 (J. Vila, CNES)

19:00 END OF DAY 2 20:00 Poolside Dinner at the Beach Bar of Torre Cintola 23:30 Wednesday 2nd October 2019 ROOM PLENARY SESSION – Torre Cintola / Sala Cupola KEYNOTE SPEECH: Space Passenger Transportation Systems: Comparison of SpaceLiner and SpaceX' BFR 8:30 (M. Sippel, DLR) Session 3.2 - Supersonic and Session 3.1 - Hypersonic Flight Missions and Session 3.3 - Thermal Protection Session 3.4 - Engineering Session 3.5 - Workshop on Technology Aerothermodynamics Vehicles and (Re)-Entry and Systems TPS Software Tools Roadmaps to target Reusability Aero-Assisted Vehicles ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Adam Okninski (Polish Institute of Fabio Pinna (VKI) Alejandro Miguel San Martin (JPL) David Glass (NASA) Jorgen Bru (ESA) Aviation) Jim Merrifield (Fluid Gravity) Kazuhisa Fujita (JAXA) Jean-Marc Bouilly (ArianeGroup) Victor Fernandez Villace (ESA) Chairpersons Philippe Tran (ArianeGroup) Mariano Sanchez Nogales (Deimos André Fueser (ArianeGroup) Heiko Ritter (ESA) Nicole Viola (POLITO) Stein Lemmens (ESA) Space) Advanced Approaches of Part 1 – Methodologies and Tools to support Experimental and Numerical State To State Vs Multi- Structural Safety Management In Strategic Decision Investigation On Static and From IXV To Space Rider : CMC Temperature Models for Multidisciplinary Optimization of Dynamic Stability of A Blunted thermal Protection System Simulating Hypersonic Flows Hypersonic Aircrafts and Space Technology Roadmap Methodology at a 9:10 Body Configuration – Project Evolutions (Francesco Bonelli, Politecnico Di Vehicles Glance Overview (Jacques Valverde, ArianeGroup) Bari) (Aitor Baldomir, University of A (N. Viola, POLITO) (Thomas Gawehn, DLR) Coruña) Optimal Design of Multilayer Transition Prediction On Reentry- Experimental Study On Static and Trade-off and Models Generation thermal Protection Based On F Trajectory With Pse At Chemical Dynamic Stability of A Blunt Body for Small Launchers TRIS - Technology Roamapping Strategy Tool Materials Morphology 9:30 Equilibrium Configuration (Giuseppe Governale, Politecnico Di (R. Fusaro, POLITO) (Aleksey Nenarokomov, Moscow (Jean-Philippe Brazier, ONERA) (Thomas Gawehn, DLR) Torino) Aviation Institute) Methodology and Tools for Technology Roadmapping: Open Discussion Development of A Vibration- Thermosensitive Coating A reduced discretization approach Dissociation Model for High- Numerical Investigation of Wind Francesco Morsillo SITAEL; Fulvio Spaziani Dedicated To Smart TPS for Very for a re-entry optimal control Enthalpy Air Tunnel Test To Measure Dynamic Brunella AVIO ELV; Jim Merrifield FGE; Marc High Temperature - 850 °C To problem with minimum heating 9:50 (Tom Schwartzentruber, University Stability Vales DASSAULT; Marco Marini CIRA; Mariano 1650°C (Blanca Pablos, Universitaet der of Minnesota) (Bodo Reimann, DLR) Sanchez Nogales DEIMOS; Rodrigo Haya (Lilian Martinez, NDT°physics) Bundeswehr Munich) Ramos SENER; Thilo Kranz ESA STS; Tiago Pardal OMNIDEA

Part 2 – European Technology Roadmap for Aerothermodynamics Hybrid RANS/LES Computations Automatic Derivation of Stability hypersonic transportation Investigation of An RLV Cryogenic Assessment of An Entry Descent of Pitch Damping Derivatives for Equations and their Application Tank Insulation Including A Purge and Landing System for A A Blunt Body Configuration To Hypersonic and High-Enthalpy European Past and Current Projects in 10:10 Gap System Penetrator Mission On Mars (Lars Tysell, Foi, Swedish Defence Shear Flows Hypersonic Transportation (Carolin Rauh, DLR) (Davy Chaillot, Arianegroup) Research Agency) (Fabio Pinna, Von Karman Institute) (V. Fernandez, ESA / R. Fusaro, POLITO)

Direct Numerical Simulations of A Flying Qualities Analysis of Chemical Non-Equilibrium DYNAST Robust Optimal Planning of Research and Development of Hypersonic Flow On A (Dynamic Stability of Capsules Controlled Re-Entry Trajectories Case study 1: Roadmap for the H2020 Plasma Sprayed UHTC Coatings Compression Corner With and Blunt Bodies At Angle of With Atmospheric Uncertainties STRATOFLY Project 10:30 for Hypersonic Applications Roughness Elements Attack) (Manuel Sanjurjo Rivo, Universidad (N. Viola, POLITO) (Mario De Stefano Fumo, CIRA) (Giuseppe Chiapparino, Technical (Davide Bonetti, DEIMOS Space Carlos III de Madrid) University of Munich) S.L.U.)

3 The Future of Hypersonic Flight in Europe: Open discussion Numerical Predictions of Dust- Study of A Collector-Intake Bayindir Saracoglu VKI; Francesco Morsillo Induced Heat Flux Augmentation Numerical Simulation of System for VLEO Air-Breathing High Enthalpy Testing of UHT-CMC SITAEL; Fulvio Spaziani Brunella AVIO ELV; In Hypersonic Blunt-Body Flows Transpiration Cooling with a Two- Platforms Materials for Space Application Helmut Ciezki DLR; Jim Merrifield FGE; Johan 10:50 Using A Discontinuous Galerkin Dimensional Substructure (Damien Le Quang, Von Karman (Burkard Esser, DLR) Steelant ESA; Marc Vales DASSAULT; Marco Multiphase Flow Solver (Imran Naved, University of Oxford) Institute) Marini CIRA; Mariano Sanchez Nogales (Eric Ching, Stanford University) DEIMOS; Philipe Tran ARIANE GROUP; Rodrigo Haya Ramos SENER; Thilo Kranz ESA; Tiago Pardal OMNIDEA 11:10 COFFEE BREAK Session 3.9- Engineering Session 3.6 - Session 3.7 - (Re)-Entry and Session 3.8 - Thermal Protection Session 3.10 - Workshop on Technology Software Tools and Testing Aerothermodynamics Aero-Assisted Vehicles Systems TPS Roadmaps to target Reusability Facilities

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Alessandro Turchi (VKI) Adam Okninski (Polish Institute of Alejandro Miguel San Martin (JPL) David Glass (NASA) Jorgen Bru (ESA) Jim Merrifield (Fluid Gravity) Aviation) Kazuhisa Fujita (JAXA) Jean-Marc Bouilly (ArianeGroup) Victor Fernandez Villace (ESA) Chairpersons Mariano Sanchez Nogales (Deimos Stein Lemmens (ESA) André Fueser (ArianeGroup) Heiko Ritter (ESA) Nicole Viola (POLITO) Space)

Measurements of Radiating Transpiration Cooling At Mach 5 Hypersonic Flow Simulation Part 3 – Facing the Challenges of Reusability Space Rider Mission Engineering Hypervelocity Air Shock-Layers In Employing Porous UHTC Using Lattice Boltzmann Method - (Davide Bonetti, DEIMOS Space 11:30 the T6 Aluminium Shock Tube (Hassan Saad Ifti, University of A Feasibility Assessment Study FLPP Reusable technologies S.L.U.) (Peter Collen, University of Oxford) Oxford) (Thibaut Van Hoof, CENAERO) (J. Bru, ESA)

Challenges and Innovations In the Characterisation of Internal Heat Modeling Hydrogen Ionization In Guidance, Navigation, and Control Transfer Mechanisms In Determination of Dynamic Hypersonic Shock Tube: the Self- Sys-Tem for Entry, Descent and Reusability – From a Propulsion Point of Transpiring Porous Media Using Derivatives of Re-Entry Vehicles Consistent State-To-State Landing of Nasa’S Mars 2020 View 11:50 Optical Diagnostics Using Unsteady Cfd Simulations Approach Mission (H. Ciezki. DLR) (Kharthik Chakravarthy, University of (Jan Vos, CFS Engineering) (Gianpiero Colonna, CNR) (Paul Brugarolas, California Instittute Oxford) of Technology) Studying the Film Effectiveness of Multi-Disciplinary Vehicle Design Thermodynamic and Transport On Orbit and Re-Entry Services Transpiration Cooled Walls Using Based On the Tools ASTOS and Properties of Silicon-Seeded Air THEMIS as a Reusable Launcher Performed By Space Drones Pressure Sensitive Paint ESPSS 12:10 Plasmas (J. Vila, ArianeWorks) (Stefania Cantoni, CIRA) (Marc Ewenz Rocher, University Of (Andreas Wiegand, Astos Solutions (Gianpiero Colonna, CNR) Oxford) GmbH) Evaluation of Destruction Criteria Determining the thermal Response Validation of Wind Tunnel Test An ES-BGK Model for Rarefied During Atmospheric Re-Entry of A Flexible TPS In A High and CFD Techniques for Retro- An updated Database Architecture to Support Polyatomic Perfect Gases With Simulation Enthalpy Environment Propulsion (Retpro) Within the New Launchers Programmes 12:30 Vibrational Relaxation (Bent Fritsche, Htg- Hyperschall (Emma Johnstone, Fluid Gravity FLPP (R. Fusaro, POLITO) (Yann Dauvois, CEA) Technologie Göttingen) Engineering Ltd) (Daniel Kirchheck, DLR) Reusability - Main Technical Challenges: Open Discussion

Alessandro Gabrielli ASI; Francesco Morsillo SITAEL; Fulvio Spaziani Brunella AVIO ELV; Probabilistic Risk Analysis and Performance Evaluation of A Dual- Gerrie Mullen REACTION ENGINES; Helmut Margin Process Mode Scramjet Combustor With Ciezki DLR; Jerome Vila ARIANE WORKS; Jim for A Flexible thermal Protection 12:50 Jet Fuel Merrifield FGE; Manuel Sanjurjo Rivo U. System (Masahiro Takahashi, JAXA) CARLOS III; Marc Vales DASSAULT; Marco (Steven Tobin, NASA) Marini CIRA; Mariano Sanchez Nogales DEIMOS; Philipe Tran ARIANE GROUP; Rodrigo Haya Ramos SENER; Thilo Kranz ESA; Tiago Pardal OMNIDEA; Ulf Palmnäs ADVISOR TO SSC 13:10 LUNCH ROOM PLENARY SESSION – Torre Cintola / Sala Cupola

PLENARY ROUND TABLE: Space Ports and Commercial Space Transportation

D. Nicolini, (ESA), E. Odd Roger (ANDOYASPACE), U.Palmnäs (ESRANGE), Jorge A. Pardo (INTA), F. Morsillo (SITAEL), L Apolloni (CNES), 14:30 M. Sanchez (Deimos), M. A. Bello-Mora (Deimos), S. Hammond (Shetland Space Centre), A. Gabrielli (ASI), A. Cramarossa (ASI), G. Di Antonio (ENAC), A. Zilli (Distretto Tecnologica Aerospaziale DTA)

16:00 COFFEE BREAK Session 3.14 - Testing Facilities, Session 3.11 - Session 3.12 - (Re)-Entry and Session 3.13 - Design for Demise Session 3.15 - Workshop on Technology Verification and Validation Aerothermodynamics Aero-Assisted Vehicles and Clean Space Roadmaps to target Reusability Methods

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Bernd Helbe (VKI) Adam Okninski (Polish Institute of Alejandro Miguel San Martin (JPL) Jorgen Bru (ESA) Stein Lemmens (ESA) Jim Merrifield (Fluid Gravity) Aviation) Kazuhisa Fujita (JAXA) Victor Fernandez Villace (ESA) Chairpersons Antonio Caiazzo (ESA) Mariano Sanchez Nogales (Deimos Stein Lemmens (ESA) André Fueser (ArianeGroup) Nicole Viola (POLITO) Space) Boundary Layer Transition Aerothermal Characterization Predicting Acoustic Loads With Plasma Wind Tunnel Demisability Studies On the Hexafly-Int Data of Comars+ In L2K Martian Skylon Project Direct CFD On GPUs Testing of Spacecraft Equipment 16:20 Hypersonic Glide Vehicle Flow Environment (G. Mullen, REL) (Oliver Gloth, enGits GmbH) (James Beck, Belstead Research) (Alexander Wagner, DLR) (Lars Steffens, DLR) Aerodynamic Characterization of Experimental Study of A Space Debris In the Vki Longshot Hypersonic Glide-Type Vehicle Pre-Commissioning Work for Progress In Probabilistic Hypersonic Tunnel Using A Free- and A Re-Entering Cubesat With Reflected Shock Mode in the Case study 2: Roadmap for a Reusable SSTO Assessment of Destructive Entry 16:40 Flight Measurement Technique the Hypersonic Rarefied Wind Oxford T6 Stalker Tunnel (R. Fusaro, POLITO) (James Beck, Belstead Research) (Guillaume Grossir, Von Karman Tunnel Marhy (Suria Subiah, University of Oxford) Institute) (Romain Joussot, CNRS, ICARE) Reusability - Main Operational Challenges: Open Discussion

Alessandro Gabrielli ASI; Francesco Morsillo SITAEL; Fulvio Spaziani Brunella AVIO ELV; Aerodynamic Testing of the Aerothermodynamic Assessment Test Facility To Investigate Plume- Gerrie Mullen REACTION ENGINES; Helmut Modelling Capsule Stability Skylon Spaceplane of Atmospheric Emissions From Regolith Interactions Ciezki DLR; Jerome Vila ARIANE WORKS; Jim Accounting for Shape Change 17:00 (Andrew Hyslop, University of Re-Entry Demise (Hossein Zare-behtash, University of Merrifield FGE; Manuel Sanjurjo Rivo (Dominik Neeb, DLR) Oxford) (James Beck, Belstead Research) Glasgow) UNIVERSITY CARLOS III; Marc Vales DASSAULT; Marco Marini CIRA; Mariano Sanchez Nogales DEIMOS; Philipe Tran ARIANE GROUP; Rodrigo Haya Ramos SENER; Tiago Pardal OMNIDEA; Ulf Palmnäs ADVISOR TO SSC

Session 3.16 - Session 3.17 - (Re)-Entry and Session 3.18 - Design for Demise Session 3.19 - Session 3.20 - Workshop on Technology Aerothermodynamics Aero-Assisted Vehicles and Clean Space Aerothermodynamics Roadmaps to target Reusability

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

4 Adam Okninski (Polish Institute of Bernd Helbe (VKI) Alejandro Miguel San Martin (JPL) Jorgen Bru (ESA) Aviation) Stein Lemmens (ESA) Jim Merrifield (Fluid Gravity) Kazuhisa Fujita (JAXA) Victor Fernandez Villace (ESA) Chairpersons Matthias Holzwarth (ArianeGroup) Antonio Caiazzo (ESA) Mariano Sanchez Nogales (Deimos André Fueser (ArianeGroup) Nicole Viola (POLITO) Stein Lemmens (ESA) Space)

EHD and MHD Effects In Investigation of Ideal Magnetic Assessment of the Re-Entry Numerical Investigations of Part 4 – Future STEPS Modification of Supersonic and Configurations for Advanced Casualty Risk From Small Charring Material Demisability In Hypersonic Rarefied Flows for Reentry Control 17:20 Launcher Upper Stages Atmospheric Entry Conditions Upcoming Developments Reentry Applications (Matthew Austin, Florida Institute of (James Beck, Belstead Research) (Pierre Schrooyen, CENAERO) (R. Fusaro and N. Viola, POLITO) (Romain Joussot, CNRS, ICARE) Technology)

Monte Carlo Simulation of Non-Catalytic Assessment and Reduced-Order Kinetics and Aerocapture Trajectories for Ground Testing Strategy for Space Blunt Body Stagnation Flow Final Discussion and Conclusions Radiation Small Science Missions At Venus, Debris Demise Replication In A Shock Tube Modeling In Hypersonic Entries 17:40 Mars, and Neptune Orbiter (Andrea Fagnani, Von Karman (Yosheph Yang, Korea Advanced (All, moderated by V. Fernandez, ESA) With US3D Missions Institute) Institute of Science and Technology) (Bruno Lopez, UIUC) (William Strauss, JPL) Fulvio Spaziani Brunella AVIO ELV; Helmut Heat-Shield Shape-Change Ciezki DLR; Jim Merrifield FGE; Manuel How To Build Coarse-Grain Effects On Aerodynamic and Simulation of Unsteady Effects Sanjurjo Rivo UNIVERSITY CARLOS III; Marc Models Consistent From the Vales DASSAULT; Marco Marini CIRA; Mariano Stability Characteristics of Re- On Shock Speed In A Shock Tube Kinetic To Fluid Regimes Sanchez Nogales DEIMOS; Rodrigo Haya 18:00 Entry Capsules (Matthew Satchell, the University of (Thierry Magin, Von Karman Ramos SENER; Tiago Pardal OMNIDEA (Alessandro Turchi, Von Karman Oxford) Institute) Institute) 18:20 END OF DAY 3

Gala Dinner at the "Abazzia di San Lorenzo, Fasano" 19:00 23:30 KEYNOTE SPEECH: Space Bussines Opportunities in the Apulia Region Giuseppe Acierno (President of DTA) and Michele Emiliano (President of Apulia Region)

Thursday 3rd October 2019 ROOM PLENARY SESSION – Torre Cintola / Sala Cupola KEYNOTE SPEECH: Enabling Entry Technologies for Robotic Science and Human Missions in the coming decades 8:30 (Don Ellerby, NASA)

Session 4.2 - (Re)-Entry and Session 4.1 - Session 4.3 - Design for Demise Session 4.4 - Multidisciplinary Aero-Assisted Vehicles and Aerothermodynamics and Clean Space and Multi-physics Vehicle Design Aerothermodynamics

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Don Ellerby (NASA) Marcello Amato (CIRA) Johann Bals (DLR) Stein Lemmens (ESA) Kazuhisa Fujita (JAXA) Thomas Reimer (DLR) Tiago Pardal (Omnidea) Chairpersons Antonio Caiazzo (ESA) Burkard Esser (DLR) Jean-Marc Bouilly (ArianeGroup) Sven Weikert (ASTOS) European Flexible Heat Shields: Multi-Disciplinary and Multi- Diagnostics of Expansion Tube Advanced TPS Design and Tests Metallic Alloy and CFRP Demise Fidelity Evaluation of VYVL and Flows By Laser Absorption for Future In-Orbit Demonstration Ablation Tests In the VKI VTHL Reusable Launch Vehicle 9:10 Spectroscopy (EFESTO) Inductively-Coupled Plasmatron System Dynamics and Control (Makoto Matsui, Shizuoka University) (Davide Bonetti, DEIMOS Space (Bernd Helber, Von Karman Institute) (Lâle Evrim Briese, DLR) S.L.U.) Spatially Resolved Electron Measurement of Dynamic Stability Multiscale Heating Correlations Free-Flight CFD Simulations Density Measurement In Front of of Earth Return Capsules In Low Applied To Destructive Entry Ballistic Range and Flight Tests Shock Layer By Laser Supersonic and Transonic Methodologies 9:30 (Michael Barnhardt, Analytical Interferometer Conditions Using Balloon Tests (Jim Merrifield, Fluid Gravity Mechanics Associates) (Makoto Matsui, Shizuoka University) (John Underwood, Vorticity Ltd) Engineering Ltd) Coupled CFD Material thermal Robust Multi-Objective Response Analysis of A Cube At Supersonic Parachute Testing Study On the Demisability of Optimisation of A Descent Simulated Wind-Tunnel and Flight Using A Maxus Sounding Rocket Optical Payloads Guidance Strategy for A TSTO 9:50 Conditions Piggy-Back Payload (Jim Merrifield, Fluid Gravity Spaceplane (Jim Merrifield, Fluid Gravity (John Underwood, Vorticity Ltd) Engineering Ltd) (Christie Maddock, University of Engineering Ltd) Strathclyde) Mini-IRENE Flight Experiment – Concepts and Considerations for Molecular Beam Studies of Stepwise Qualification Approach Re-Entry Experiments To Inform Modern Techniques and Carbon and Silicon Carbide of A Deployable and Flexible Heat Fragmentation Prediction for Technologies for Space Flight Ablation By Atomic Oxygen 10:10 Shield for An Orbital Re-Entry Destructive Entry Vehicle Engineering (Guillermo (Tom Schwartzentruber, Montana Mission (Jim Merrifield, Fluid Gravity Ortega, ESA) State University) (Paolo Vernillo, CIRA) Engineering Ltd) Application of Particle-Based Continuum Methods To A Demisability of Novel Bio- The Importance of Bow Shock Space Rider - Aerodynamics and Hypersonic Flow With Composite Material Under Adaption In CFD Simulations for Aerothermodynamics from Shock/Shock Interaction Around A Experimentally Simulated 10:30 Hypersonic Flows hypersonic to subsonic flight Double Cone Uncontrolled Re-Entry Conditions (Jan Vos, CFS Engineering) (Olivier Lambert, Dassault-aviation) (Paul Nizenkov, boltzplatz - (Adam Pagan, University of Stuttgart) Numerical Plasma Dynamics) Nonequilibrium Dissociation Effect of Ablation Shape Change Translational Temperature Model for Hypersonic Flow Based An ESA study on Design for In Transonic and Subsonic Measurements of CO2 Flow In On Computational Chemistry Demise certification Aerodynamics for A High Speed 10:50 Expansion Tube (Tom Schwartzentruber, University (Orr Cohen, ESA) Entry Capsule (Satoshi Nomura, JAXA) of Minnesota) (Jorge Sancho, SENER) 11:10 COFFEE BREAK

Session 4.5 - Session 4.6 - Session 4.7 - Session 4.8 - Flight Data Aerothermodynamics Aerothermodynamics Aerothermodyanmics and Testing Exploitation

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno Fabio Pinna (VKI) Manuel Sanjurjo Rivo (University Don Ellerby (NASA) Marcello Amato (CIRA) Jim Merrifield (Fluid Gravity) Carlos III) Kazuhisa Fujita (JAXA) Thomas Reimer (DLR) Chairpersons Mariano Sanchez Nogales (Deimos Tiago Pardal (Omnidea) Burkard Esser (DLR), Jean-Marc Bouilly (ArianeGroup) Space) Sven Weikert (ASTOS) Thermodynamic Analysis of Aerodynamic Database IXV Flight Catalysis Determination Modeling Heatshield Erosion Due Boundary Layer Species During Development for A Future In Inductively Coupled Plasma To Dust Particle Impacts for A Ablation Reusable Space Launch Vehicle, Facility 11:30 Martian Entry Vehicle (Maitreyee Sharma Priyadarshini, the Orbital 500R (Alan Viladegut, Von Karman Institute) (Grant Palmer, Ama, Inc.) University of Illinois, Urbana- (Tristan Stindt, Fluid Gravity Champaign) Engineering) Construction of an Ab-Initio Based State-Resolved Transport for the Analysis of the AEDB Hypersonic Boundary Layer Non-Equilibrium Chemistry Model O+O2 System Based On Ab Initio Performance During the Exomars Instability Measurements at Mach 7 for Air Mixtures Potential Energy Surface Analysis Schiaparelli Descent 11:50 and Flight Total Enthalpy (Marco Panesi, University of Illinois (Kelly Stephani, University of Illinois (Emma Johnstone, Fluid Gravity (S. Wylie, University of Oxford) at Urbana Champaign) At Urbana-champaign) Engineering Ltd)

European Shock-Tube for Hight Radiative Attenuation Through Exploitation of Flight Data From Experimental Radiation Enthalpy Research: Design and Heat Shield Doping: A Multi-Scale Balloon Drop Tests for Earth Measurement From CO2 Flow In Instrumentation, Manufacturing, Approach From Ab Initio To CFD Return Capsules 12:10 Shock Tube and Expansion Tube and Acceptance Testing (Marco Panesi, University of Illinois (Emma Johnstone, Fluid Gravity (Hiroki Takayanagi, JAXA) (M. Lino da Silva, Universidade de at Urbana Champaign) Engineering Ltd) Lisboa)

5 Analysis of the Aerothermal and A Stability Based Transition Force Measurement Comparison Simulation of Exhaust Plumes in Material Performance During the Prediction Criterion for Up To of Blunt Cones In High-Enthalpy Rarefied Atmosphere Exomars Schiaparelli Descent 12:30 Mach 8 Hypersonic Flows Shock Tunnel Heg and Hiest (A. Award, ONERA) (Emma Johnstone, Fluid Gravity (Jean Perraud, ONERA) (Hideyuki Tanno, JAXA) Engineering Ltd) Numerical Computation of the Experimental Characterization of Aerothermodynamic and Preliminary Design of an Origami Exomars Schiaparelli the Hypersonic Flow Around Trajectory Studies On Optimal Foldable De-orbiting Sail for a 3U Communications Blackout Cubes Earth Re-Entry of A Capsule CubeSAT 12:50 Compared With Flight (Thomas Rees, Imperial College (Fabian Teschner, University of the (C. Vendittozzia, Universidade de (Tristan Stindt, Fluid Gravity London) Bundeswehr Munich) Brasilia) Engineering) 13:10 LUNCH ROOM PLENARY SESSION – Torre Cintola / Sala Cupola PLENARY ROUND TABLE: The Upcoming Exploration of the Moon 14:30 A. Casell (NASA), B. Foing (ESA), S. Schlechtriem (DLR), F. Liucci (ESA), P. Bousquet (CNES), J. Merrifield (Fluid Gravity Engineering), J. Van Tooren (Arianegroup) 16:00 COFFEE BREAK

Session 4.9 - Session 4.10- Session 4.11 - Deplyoable Session 4.12 - Flight Data Aerothermodynamics Aerothermodynamics Aeroshells Exploitation

ROOM Torre Cintola/Sala Cupola Levante Primo Piano (L) Primo Piano (S) Saletta meno uno

Manuel Sanjurjo Rivo (University Don Ellerby (NASA) Marcello Amato (CIRA) Carlos III) Thierry Magin (VKI) Kazuhisa Fujita (JAXA) Thomas Reimer (DLR) Adam Okninski (Polish Institute of Chairpersons Marc Vales (Dassault) Burkard Esser (DLR) Jean-Marc Bouilly (ArianeGroup) Aviation) Matthias Holzwarth (ArianeGroup) Modelling and Simulation of European Studies To Advance Direct Molecular Simulation of Overview of the Test-Flights of the Heterogeneous Reactions With Development of Deployable and Dissociating Oxygen In 0D KRUPS Capsule Statistical Particle Methods Inflatable Aerodynamic 16:20 Adiabatic Reactor (Alexandre Martin, University of (Wladimir Reschke, University of Decelerators (Erik Torres, University of Minnesota) Kentucky) Stuttgart) (John Underwood, Vorticity Ltd) Comparison of Chemical Modeling for High-Temperature Flight Data Analysis of the Gas Effects With Direct Numerical CFD Computations of Orbital and Flight Demonstration of Deployable Multicolor Imaging Pyrometry Simulations of Roughness- Super-Orbital Re-Entry Heating Aeroshell Technology Using Nano- Experiment On Esa’S Induced Transition In A Re-Entry 16:40 On Primitive Shapes Satellite Opportunity Intermediate Experimental Vehicle Scenario of A Hemispherical (Jeroen Van Den Eynde, ESA) (Kazuhiko Yamada, JAXA) IXV Capsule (Thomas Roesgen, ETH Zurich) (Friedrich Ulrich, Technical University of Munich) PLENARY SESSION – Torre Cintola / Sala Cupola CONFERENCE CLOSURE 17:00 (G. Ortega, ESA) 18:00 END OF DAY 4

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