Sunday, June 30th
18:00 - 20:00 Welcome Reception	Room: Holiday Inn - Registration Area
Monday, July 1st
09:00 - 10:00 Welcome Coffee	Room: Holiday Inn - Registration Area
10:00 - 12:30 Opening Ceremony	Room: Holiday Inn - Forum 1-3
12:30 - 14:00 Lunch Break I
14:00 - 15:00 PLENARY SESSION	MoAP Room: Holiday Inn - Forum 1-3 Chair: to be confirmed Rapporteur: to be confirmed
Space Transportation Challenges A. Fabrizi , M. Eymard and R. Densing
15:00 - 15:30 Networking Break	Room: Holiday Inn- Meeting Area Foyer
15:30 - 18:50 TECHNICAL SESSIONS
SI.08: Space Debris I - Orbital Debris Mitigation Tools and Technologies	MoA01 Room: Holiday Inn - Forum 1 Chair: Luciano Anselmo CoChair: Valery Trushlyakov Rapporteur: to be confirmed
Orbital Lifetime Estimation using ESA‘s OSCAR tool (*) V. Braun, J. Gelhaus, C. Kebschull, S. Flegel, M. Möckel, J. Radtke, C. Wiedemann, H. Krag and P. Vörsmann Space Debris Mitigation Support : POLPO® Software for a Green Access to the Space (*) S. Sanvido, M. Andrenucci, T. Fossati and M. Volpi Applying of Gas-generating Compositions for Liquid Rockets Effectiveness Improving (*) V. Trushlyakov, D. Lempert and M. Belkova Controlled Deorbiting of an Upper stages from Placing Orbit of SLV with Oxygen-kerosene Main Liquid Propulsion Engine (*) V. Trushlyakov, J. Makarov, J. Shatrov and A. Baranov Removal of Separating Parts using a Liquid Rocket Engine S. Muriana and V.I. Trushlyakov Astrium perspective on space debris mitigation & remediation(*) P. Voigt, D. Alary, C. Cougnet, M. Oswald and J. Utzmann
MS.8: Polymer Matrix Composites and Applications	MoA02 Room: Holiday Inn - Forum 2 Chair: Anatoly Tashkinov Rapporteur: to be confirmed
Design and manufacture of advanced composite structures using Fibre - Patch - Preforming M. Coquel and M. Steyer Laser-assisted winding of thermoplastic based composite for future launchers application M. Krzeminski, B. Defoort, L. Jaguenaud, P. Briant Finite Element Analysis of the Interaction between a Crack and Micro-Inclusions in Aligned Carbon Nanofiber Composites (*) S. Kim, H.T. Ting and A-V. Phan Advanced Composite Materials and Technologies for Large Solid Rocket Motor F. Lillo, V. Vinti, R. Buono, P. Perugini, A. Mataloni and B. D‘Andrea Recent Research and Development of Composite Thin-wall Lenticular Tube and Space Applications W. J. Chen, D. X. Zhang, G. Q. Fang and F. J. Peng Insight into mechano-chemical properties of the interface between cellulose and thermoplastic polymers S. Patriche, R. Dinica, B. Epureanu and M.  Banu Natural fibre composites; Recent developments A.W. van Vuure, L.Q. Tran, C.A. Fuentes, L. Osorio, E. Trujillo, N.V. Hong, D. Perremans, F. Bensadoun, J. Baets and I. Verpoest
PP.15: Euroturbo/Eucass Air Breathing I	MoA03 Room: Holiday Inn - Forum 11 Chair: Gerard Bois CoChair: Yury Tsirkunov Rapporteur: to be confirmed
Aerodynamic performance of two very high lift low pressure turbine airfoils (T106c – T2) at low reynolds and high mach numbers T. Arts Rotors with variable parameters in dynamics for aircraft and power installations R. Turmanidze and A. Peikrishvili Investigation of capabilities synthetic jets application for active control in diffuser ducts with flow separation using hight resolution RANS/ILES - method (*) D.A. Lyubimov and I.V. Potekhina Numerical investigation on effectiveness of axially uniform and non-uniform tip clearance height on the performance of single stage transonic axial flow compressor P. Batabyal, D. B. Alone and S.K. Maharana Velocity measurements behind a compressor cascade equipped with passive vortex generators C. Sahin and T. Arts
PP.29: Combustion Modeling	MoA04 Room: Holiday Inn - Forum 6 Chair: Christian Stemmer CoChair: Mohan Varma Rapporteur: to be confirmed
The Role of Presumed Probability Density Function in the Simulation of Non-premixed Turbulent Combustion A. Coclite, G. Pascazio, P. De Palma and L. Cutrone Multiscale Aviation Kerosene Modeling: from ab initio Quantum Chemistry to the Combustion Chamber Simulations V.L. Kovalev, S.O. Adamson, A.S. Vetchinkin and A.V. Vagner Investigation of different modeling approaches for CFD simulation of high pressure rocket combustors B. Ivancic, H. Riedmann, M.  Frey, O.  Knab, S. Karl and K. Hannemann Numerical Investigation of Spray Combustion and Flow in LOX/H2 Subscale Rocket Combustors H. Riedmann, B. Kniesner, M. Frey and C-D. Munz A Posteriori Computation of OH* Radiation from Numerical Simulations in Rocket Combustion Chambers T. Fiala and T. Sattelmayer Large Eddy Simulation of supersonic non-reactive and reactive flows with an immersed boundary method (*) L. Bouheraoua, G. Ribert, P. Domingo and G. Lartigue Development and Evaluation of Transient Analysis Tool for Rocket Engine A. Ogawara and C. Sezaki Numerical simulations of slame of single co-axial injector V.P. Zhukov and M. Feil
PP.22: Green Propellants I	MoA05 Room: Holiday Inn - Forum 7 Chair: Christophe Koppel CoChair: Yann Batonneau Rapporteur: to be confirmed
A New Nitrate Ester Composite Propellant D. A. Reese, L.J. Groven and S. F. Son Options for Green Monopropellants R.L. Sackheim and R. Masse Experimental Study of a Nitrous Oxide/Ethanol Propulsion System: Technology Demonstration with a BBM S. Tokudome, T. Yagishita, K. Goto, H. Habu, N. Suzuki, F. Fukuyoshi, Y. Daimoh and F. Okuno Green Propulsion: Catalysts for FP7 Project GRASP Y. Batonneau, R. Brahmi, B. Cartoixa, K. Farhat, C. Kappenstein, S. Keav, G. Kharchafi, L. Pirault-Roy, M. Saouabe and C. Scharlemann Cellular ceramic versus pellets as catalyst support for green propulsion applications R. Brahmi, K. Farhat, R. Amrousse, Y. Batonneau, C. Kappenstein and B. Cartoixa Hot-Firing tests using a low temperature derivative of LMP-103S K. Anflo, P. Thormählen and M. Persson Green Rocket Engine Test Site for High Performance Green Propulsion J. Olsson, M. Persson, K. Anflo and T. Hasanof
SI.01: Air & Space MDO	MoA06 Room: Holiday Inn - Forum 9 Chair: Martin Sippel CoChair: Philippe Tatry Rapporteur: to be confirmed
Multi-disciplinary Design Optimization of Hypersonic Vehicles with the Generalized Sensitivity Based Concurrent Subspace Optimization Process L. Yan, W. Huang, J. Li and X-Q. Chen An Integrated Approach for the Multidisciplinary Optimization of Engine Cycles for Rotorcraft I. Goulos, V. Pachidis, F. Hempert, V. Sethi, R. D‘Ippolito and M. D‘Auria Design of two-rotored UAV Cyclocopter C.H. Lee, S.Y. Min, J.W. Lee and S.J. Kim Development of Numerical Simulation Method for Safety Evaluation of Launch Abort during Ascent Phase N. Tani, K. Kawatsu, E. Wada, K. Fujimoto and N. Yamanishi
FD.1: Air Traffic Management/Trajectory Optimisation	MoA07 Room: Novotel Tegernsee Chair: Charles Vallet Rapporteur: to be confirmed
Software Tool for Simulation of Aircraft Trajectories J. Crespo, J. Alonso, A. López and R. Arnaldo Optimization of Mid to Long Range Flights Considering Air-to-Air Refueling for Fuel Savings M. Bittner, C. Hornfeck, F. Fisch, M. Schwarze and F. Holzapfel Onboard Wake Vortex Flight Safety System A. Belotserkovskiy, N. Baranov and M.  Kanevskiy Optimality of standard flight procedures of commercial aircraft A. Franco, A. Valenzuela and D. Rivas UAV In-Flight Awareness: A Tool to Improve Safety(*) A. Mattei, E. Fonseca, N.M. Figueira, O. Trindade and F. Vaz Autonomous Formation Flying in spacecraft (*) S. Thangavel, C. Santhosh Kumar, A. Manigandan and V. Kishore
MS.1: Design and optimisation	MoA08 Room: Novotel Chiemsee Chair: Evgeny Shakhmatov CoChair: Jochen Albus Rapporteur: to be confirmed
Shear Effects in the Homogenisation of Slender Composite Wings J. Dizy, R. Palacios and S. Pinho Analytical and Experimental Study of the Integral Aerodynamic Characteristics of Low-Wind Turbines (*) M.Z. Valiev, V. Pakhov, V. Zherekhov and G. Barakos Weight Reduction of an U.A.V.’s Wing through Topology Optimization N.R. Farias and A.M. Wahrahfting Surrogate models for helicopter loads A. Struzik, E. Burnaev and P. Prikhodko An Abaqus-embedded Optimizer for Composite Components R. Winkler, B. Goller and H. Haller
FD.9: Navigation/FDIR	MoA09 Room: Novotel Königssee Chair: Christian Philippe Rapporteur: to be confirmed
Data fusion with Hydra Star Tracker on Spot6 D. Piot, L. Oddos-Marcel, B. Gelin, A. Thieuw, P. Genty, P. E. Martinez, S. Airey and S. Kowaltschek Autonomous Multirotor UAV Flight Control System based on GPS and INS data fusion K.E. Shilov Modeling of group objects motion V. Abrosimov A Mathematical Formulation of a Novel Adaptive ARE-Based Fault-Tolerant Flight Control System M. Al-Malki and D. Gu Single Camera Absolute Structure from Motion Using H∞ Data Fusion for a Next Generation Planetary Lander L .M. Feetham, N. Aouf, C. Bourdarias and T. Voirin
FP.01: B.L. Transition I	MoA10 Room: Holiday Inn - Forum 14 Chair: Valery Chernoray Rapporteur: to be confirmed
Modelling of local heating/cooling effect on laminar-turbulent transition in supersonic flows with engineering correlations and Reynolds averaged Navier-Stokes equations R.V. Kovalev, V.V. Kudryavtsev and D.A. Churakov Experimental investigation of effect of ultrasonically absorptive coating locations on second mode disturbances in hypersonic boundary layer S. Lukashevich, S. Morozov and A. Shiplyuk On the origin high level pulsations in vicinity of lateral edge of blunted triangular plate in supersonic flow A.D. Kosinov, N.V. Semionov, Y.G. Yermolaev and A.V. Vaganov Experimental study of receptivity of supersonic boundary layer on swept wing N.V. Semionov, A.D. Kosinov and Yu.G. Yermolaev Effect of the local wall cooling/heating on the hypersonic boundary layer stability and transition A. Sidorenko, P. Polivanov, Y. Gromyko, D. Bountin and A. Maslov Influence of external disturbances on nonlinear processes of three-dimensional supersonic boundary layer N.V. Semionov, A.D. Kosinov and Y.G. Yermolaev Research of formation and development of stationary vortices and its secondary instability after the roughness element on the leading edge of the oblique wing S.N. Tolkachev, V.N. Gorev and V.V. Kozlov Laminar-turbulent transition structure on classical and wavy wing at low Reynolds number. I.D. Zverkov, V.V. Kozlov, A.V. Kryukov, A.V. Boiko and S. Hein
FP.08: Flow Control II	MoA11 Room: Holiday Inn - Forum 15 Chair: Alexander Kosinov CoChair: Sebastian Willems Rapporteur: to be confirmed
Flow control of an oblique shock wave reflection by micro-ramps: effects of location and size R.H.M. Giepman, F.F.J. Schrijer and B.W. Van Oudheusden Unstable Behavior of Subsonic Round and Plane Jets in a Transverse Acoustic Field V.V. Kozlov, G.R. Grek, G.V. Kozlov and Y.A. Litvinenko Control of Recirculation Flow Near the Step in Supersonic Stream (*) V.M. Fomin, B.V. Postnikov and K.A. Lomanovich Wave drag reduction due to a self aligning Aerodisk C. Schnepf, O. Wysocki and E. Schülein Numerical simulation of supersonic boundary layer transition tripped by transverse injection E. Orlik, I. Fedioun and N. Lardjane Effect of passive Air Jet Vortex Generator on NACA0012 Performance (*) F. Tejero, P. Doerffer and O. Szulc
FP.11: Flow Control I Plasmas	MoA12 Room: Holiday Inn - Forum 16 Chair: Chloé Génin Rapporteur: to be confirmed
Combined laser-microwave discharge in supersonic flows I.Ch Mashek, V.F. Lashkov, R.S. Khoronzhuk, D.P. Potapenko and V.G. Brovkin Optimization of MHD effect on the ionized flow past the circular cylinder at high values of Hall parameter E.G. Sheikin, C.W. Yang and V.S. Sukhomlinov Control of Oblique Shocks in Supersonic Inlet by Energy Deposition (*) H. Yan Study of the oscillating ion wind induced by DBD for various O2/N2 concentration ratios P.A. Polivanov, O.I. Vishnyakov, A.A. Sidorenko and A.A. Maslov Instability Wave Control in Turbulent Jet by Acoustical and Plasma Actuators V. Kopiev, Yu. Akishev, V. Bityurin, I. Kossyi, I. Belyaev, G. Faranosov, Vl. Kopiev, I. Moralev, N. Ostricov and M. Zaitsev On a possibility of laminar flow control on a swept wing by means of plasma actuators (*) S.L. Chernyshev, A.P. Kuryachii, S.V. Manuilovich, D.A. Rusyanov and V.V. Skvortsov Efficiency of Spark Jet M. Golbabaei-Asl, D. Knight and S.  Wilkinson
PP.01: LRE LOX-CH4/LNG	MoA13 Room: Holiday Inn - Forum 10 Chair: Oskar Haidn CoChair: Takeo Tomita Rapporteur: to be confirmed
Astrium‘s LOXLCH4 Gas Generator Development Programme S. Soller, C. Maeding, B. Kniesner and R. Blasi Near wall recombination effects on the prediction of heat flux in O2/CH4 combustion chambers (*) B. Betti, D. Bianchi, F. Creta, E. Martelli, F. Nasuti and M. Onofri Numerical and Experimental Investigation of the Methane Film Cooling in Subscale Combustion Chamber Y. Daimon, H. Negishi, M. Koshi and D. Suslov CFD Modelling and Simulations of the HYPROB Regenerative LOX/CH4 Thrust Chamber P. Roncioni, D. Cardillo, M. Panelli, D. Ricci, M. Di Clemente and F. Battista Design and Testing of an GOX/GCH4 Igniter for Rocket Engine Thrust Chambers. F. Battista, A. French, M. Ferraiuolo, A. Martucci, P. Roncioni, M. Fragiacomo, V. Salvatore and L. De Rose Synthesis of oxygen-methane combustion activities in In-Space Propulsion (ISP-1) Program G. Ordonneau Characterization of a double swirl injector in a LOX/LCH4 fueled combustor on Mascotte test bench (*) N. Fdida, L. Vingert, G. Ordonneau, A. Ristori, C. Brossard, R. Stützer and J. Sender Injector Characterization for a GOX-GCH4 Single Element Combustion Chamber (*) M.P. Celano, S. Silvestri, G. Schlieben, C. Kirchberger and O.J. Haidn
PP.08: SRM Propellants	MoA14 Room: Novotel Chiemsee Chair: Luigi DeLuca CoChair: Leonard Caveny Rapporteur: to be confirmed
Martin Summerfield and the first USA operational liquid rockets L. H.  Caveny The knowledge base for definition of characteristics of the condensed combustion products V.A. Babuk and A.N. Ivonenko Modeling of Heterogeneous Structure and Properties of Composite Solid Propellants D. Davidenko and Y. Fabignon Combustion mechanism of ammonium perchlorate-ferrocene mixtures V.P. Sinditskii, A.N. Chernyi and D.A. Marchenkov Combustion anomalies in solid rocket propellant M. Fassina and L.T. DeLuca Comparing AP- and AN-Based Propellants with Low Aluminum Content M. Fassina, S. Dossi, L. Galfetti and L.T. DeLuca Development of modified reсoil force gage for studying gasification processes of energetic materials A.S. Mamaev , V.E. Zarko and A.B. Kiskin Combustion of Pyrotechnic composites for micro tube R. Shen, S. Wu, J. Liu, Y. Ye, Y. Hu, P. Zhu and L. Wu
Tuesday, July 2nd
08:30 - 11:50 TECHNICAL SESSIONS
SI.09: Space Debris-II	TuM01 Room: Holiday Inn - Forum 1 Chair: Vladimir Aslanov CoChair: Michele Lavagna Rapporteur: to be confirmed
Debris Selection and Optimal Path Planning for Debris Removal in the SSO: Low-Thrust case J. Olympio and N. Frouvelle ADR concepts from CNES funded study OTV T. Salmon, C. Cougnet, R. Axthelm, L.  Lequette, C. Dupont, B.  Chamot, M. Richard, C. Saunders and A. Pisseloup Astrium ST’s Active Debris Removal Systems I. Retat, B. Bischof, X. Clerc, J. Magné and B. Mädiger Active Removal of Large Massive Objects by Hybrid Propulsion Module (*) L.T. DeLuca, M. Lavagna, F. Maggi, P. Tadini, C. Pardini, L. Anselmo, M. Grassi, A. Francesconi, N. Viola and U. Tancredi Contact-less Active Debris Removal: the Hybrid Propulsion Alternative M. Lavagna, R. Benvenuto, L.T. DeLuca, F. Maggi, P. Tadini and M. Graziano
MS.9: Thermal Protections for Space Vehicles	TuM02 Room: Holiday Inn - Forum 2 Chair: Michel Berdoyes CoChair: Eduard Vasilevskiy Rapporteur: to be confirmed
Ceramic matrix composite thermal protection systems for large-scale demonstration on IXV R. Barreteau and T. Pichon Analysis of Composite Truss-core Sandwich Panels for Thermal Protection Systems P. Manolo and A.M. Humberto IXV Re-entry Demonstrator: Windward and Nose Assemblies CMC Thermal Protection Systems – Analysis and Tests from Development to Qualification F. Girard and C. Juillard Novel Method for the Evaluation of Ultra High Temperature CMCs applied in Orbital and Airbreathing Propulsion. S. Schmidt-Wimmer, S. Beyer, F.  Wigger, K.  Bubenheim and C. Wilhelmi Electrical Conductivity Tomography as Health Monitoring System for Thermal Protection Systems G. Herdrich, A. Preci and W. Fischer Ablation resistance of thermo-ablative composite under liquid alumina particle impacts: influence of the composite structure and composition (*) P. Fuzet, S. Goutier, M. Vardelle, G. Mariaux, P. Aubrun, I. Guenot, E. Mariage, F. Plazanet, N. Cesco and P. Supie
PP.16: Euroturbo/Eucass Air Breathing II	TuM03 Room: Holiday Inn - Forum 3 Chair: Tony Arts CoChair: Allan Grosvenor Rapporteur: to be confirmed
Turbofan engine concept with centrifugal compressor stages A. Glukhovskoy, A. Korshunov and K. Korshunova The Ljungström turbine for aeronautical applications(*) F. Buysschaert, S. Newman, S. Walker, H. Antoine and P. Hendrick Experimental testing of carbon brush seals for aero-engine bearing chambers B. Outirba and P. Hendrick Otho Turbojet engine, a challenge of actual engines C. Pavel and V. Stanciu CFD/Monte Carlo simulation of dusty gas flow in a set "rotor-stator" of airfoil cascades Y. Tsirkunov and D. Romanyuk Very Small Gas Turbine Jet Engines - Current Limits and Potential for Improvement D. Hirndorf, A. Hupfer, W. Erhard and H.-P Kau Testing and analysis of the impact on engine cycle parameters and control system modifications using hydrogen or methane as fuel in an industrial gas turbine (*) H. Funke, J. Keinz, S. Börner, P. Hendrick and R. Elsing SPLINE for blades grids design A. Korshunov, V. Shershnev and K. Korshunova
PP.30: Turbomachinery	TuM04 Room: Holiday Inn - Forum 6 Chair: Luigi DeLuca CoChair: Wolfgang. Kitsche Rapporteur: to be confirmed
Dynamic design method of internal flow systems for rocket turbopumps T. Shimura, S. Kawasaki, M Uchiumi, T. Kimura, M. Hayashi and J. Matsui Fuel Turbopump for LOX-LCH4 Lyra Demo Engine M. Rudnykh, D. Liuzzi, G. Caggiano, A.G. Kravchenko, S.V. Chembartsev, A. De Lillis and E. D‘Aversa On the working process theory of high temperature jet and turbojet engines in experimental achivements light of modern physics M.J. Ivanov, V.K. Mamaev and G.B. Zhestkov P.I.V. Flow Characterization Inside a Large-Scale U-Shaped Smooth and Ribbed Rotating Channel A. Ristori, I. Da Costa, F. Chedevergne, P. Roux and D. Carru
PP.23: Comb Testing (4) + Ignition (4)	TuM05 Room: Holiday Inn - Forum 7 Chair: Vladimir Zarko CoChair: Ralf Stark Rapporteur: to be confirmed
Coupling high-speed Imaging Diagnostics to Study a LOX/GH2 Flame in a High-pressure Rocket Combustor N. Fdida, L. Vingert, G. Ordonneau and S. Petitot Optical Investigation on the Hypergolic MMH/NTO Combustion in Spacecraft Propulsion R. Stützer, S. Bublies, T. Mayer, S. Kraus, W. Clauss and M. Oschwald Design and testing of a new high pressure chamber with optical access (BOHP) G. Martins and C. Verplancke Developing thrust chamber assembly of LOX - LNG expander cycle liquid-propellant rocket engine A. Gurtovoi, V. Kosmacheva, V. Rachuk, D. Scarpino, S. Carapellese, M. Biagioni, A. De Lillis and E. D’Aversa Ignition and flameholding of hydrocarbon fuels in high-speed flow (*) M.A. Goldfeld Investigation of Plasma Bunch for Artificial Ignition of Fuel in Supersonic Flow (*) M.A. Goldfeld, S.S. Katsnelson and G.A. Pozdnyakov Ignition delay times of kerosene(Jet-A)/air mixtures V.P. Zhukov, V.A. Sechenov and A.Yu Starikovskii
SI.02: Optimization of aircraft design and operations	TuM06 Room: Holiday Inn - Forum 9 Chair: Philippe Tatry CoChair: Vyatcheslav Baklanov Rapporteur: to be confirmed
Novel approach to multi-objective aircraft family optimization T. Druot, C.B. Blondel, F. Gubarev, V. Kushnir, S. Morozov, S. Alestra and C. Brand Optimization of continuous airworthiness problems (*) Q. Hassan, M. Najeeb and K. Kustroń Aircraft comfort with distributed propulsion system V.S. Baklanov and A.A. Mirzoyan Designing cleaning devices for laminar wings Y. Steiner, P.  Leyland, P. Wilhelm and S. Bustamante The Pattern and Relationship between Errors and Contribution Factors in Aviation Maintenance M.Y. Bao, S.D. Ding and K. Marais Lagrangian Droplet Impingement Analysis and Validation for a Swept Wing (*) S. Ozgen, E. Tarhan and M. Canibek Advantages of Systems Integration and new Technologies for Systems Testability during Aircraft Manufacturing Phase G. Soriano-Rull and A. Corrales-Dominguez
FD.2: Real Time Avionics and Networks	TuM07 Room: Novotel Tegernsee Chair: Andrea Martelli Rapporteur: to be confirmed
A family of testbenches to support testing of real-time avionics systems V.V. Balashov, M.V. Chistolinov and R.L. Smeliansky Design and modeling of a dataflow avionics system P.B. Panfilov and S.M. Salibekyan Combining static priority and weighted round-robin like packet scheduling in AFDX for incremental certification and mixed criticality support M. Boyer, N. Navet, M. Fumey, J. Migge and L. Havet Certifying Network Calculus in a Proof Assistant E. Mabille, M. Boyer, L. Fejoz and S. Merz CAN bus solutions for Data Handling Space Systems M. Caramia, L. Bolognino and G. Furano Saving the Software Specification by Transforming the old SA/RT Models into UML (*) T. Weyrath, H. Schreyer and J. Sellen DYANA: an integrated development environment for simulation and verification of real-time avionics systems V.A. Antonenko, E.V. Chemeritsky, A.B. Glonina, I.V. Konnov, V.N. Pashkov, V.V. Podymov, K.O. Savenkov, R.L. Smeliansky, P.M. Vdovin and D.Y. Volkanov Adaptative Integration systems using FPGA COTS devices E. Fonseca, A.L.P. Mattei and W.C. Cunha
MS.2: Cryogenic and Rocket Engines	TuM08 Room: Novotel Chiemsee Chair: Genevieve Inglebert CoChair: Eduard Vasilevskiy Rapporteur: to be confirmed
Cryogenic engine realisation _ challenges overcome P.V. Venkitakrishnan Cryogenic propellant technologies validation in microgravity in FLPP/CUST program A. Sirbi Paragina, J. Kauffmann, G. Pilchen, B. Schmitz, P. Behruzi, M. Dreyer and A. Schuette Preparing technologies for enabling European restartable cryogenic upper stages A. Sirbi Paragina, J. Kauffmann, G. Pilchen, T. Renk, M. Guethler, A. Ferrarese, P. Behruzi, C. Roettger and S. Bianchi Application of Extreme Values Analysis for the Definition of Operational Domains of Liquid Rocket Engines (*) B. Férard Generative Manufacturing of Rocket Engine Thrust Chamber Components and Fluid Control Equipment T. Sebald, S. Beyer, K.U. Heins, K. Schmidtke, F. Palm and L. Pambaguian Experimental investigation of blanching effects of typical liquid rocket engine combustion chamber wall materials (*) H. Duval, B. Lefez, T. Da Silva Botelho, G. Inglebert, S. Bégoc, J. Riccius and B. Hannoyer
PP.20: Ram/scramjet Modeling	TuM09 Room: Holiday Inn - Forum 12 Chair: Manuel Frey CoChair: Piotr Wolanski Rapporteur: to be confirmed
Assessment of turbulence models on transverse jet in cross-flow. R. Thundil Karuppa Raj and P. S. Rathore Numerical Simulation of Hypersonic Air Intake Flow in Scramjet Propulsion S. Frauholz, B. U. Reinartz, S. Müller and M. Behr LES Investigation of a Central Strut Injector with Perpendicular Injection for Scramjet Applications. S. Eberhardt and S. Hickel Computations of Complete Flow Fields in an Axisymmetirc Scramjet Using Accurate Anti-Diffusive WENO RANS Solvers J.Y. Yang, C.Y. Yan, J.C. Huang, Y.H. Lai and C.S. Kuo Mathematical research of gas-dynamic processes in pulse ejector F.A. Slobodkina and A.V. Obukhov Numerical Study of Air Vitiation Effects on Scramjet Performance with Different Fueled Combustion Heater J. Xing and W. Li Mixing and combustion characteristics for the transverse injection flow field in supersonic crossflows W. Huang, J. P. Wu, L. Yan, J. Li and Z. G. Wang Theoretic Analysis of Ejector Mode of Rocket Based Combined Cycle Propulsion B. Wang, Q.F. Xie, M.X. Zou and H.Q. Zhang
FP.02: B.L. Transition II	TuM10 Room: Holiday Inn - Forum 14 Chair: Ivanov Misha CoChair: Jean-Denis Parisse Rapporteur: to be confirmed
Receptivity of BL to non-linear FST (*) M. V. Ustinov Investigation of flat plate transitional boundary layer in hypersonic flow by means of naphthalene based PLIF T. Regert, Y. Babou, O. Marxen, M. Avelar Camarinha and O. Chazot Physics of Transitional Shear Flows A.V. Boiko, A.V. Dovgal, G.R. Grek and V.V. Kozlov Experimental study of localized disturbances at straight and swept wing boundary layer. V.V. Kozlov, M.M. Katasonov, P.A. Motyrev and D.S. Sboev Stability of high-speed boundary layer on a sharp cone with localized wall heating or cooling V.G. Soudakov, A.V. Fedorov and I.V. Egorov On the relative receptivity of 2D and 3D supersonic boundary layer to stationary disturbances at Mach 2 A.D. Kosinov, A.V. Panina, N.V. Semionov and Yu.G Yermolaev Prediction of Laminar-Turbulent Transition on an Airfoil at High Level of Free-Stream Turbulence V. Chernoray
FP.09: Heat Transfer	TuM11 Room: Holiday Inn - Forum 15 Chair: Andrei Sidorenko Rapporteur: to be confirmed
Simulation of an Ablative Thermal Protection System for the Hypersonic Ascend of an Electromagnetically Launched Payload Carrier (*) D. Lancelle and O. Bozic Off-Stagnation Point Testing in Plasma Facility A. Viladegut and O. Chazot Evolution of turbulent heat flux across a shock wave R. Quadros, P. Sashittal, A. Ramachandran and K. Sinha Structure of a laminar viscous hypersonic gas flow over the delta wing with blunt leading edges. S. Alexandrov, A. Shalaev and A.V. Vaganov Influence of small spatial perturbations on heat transfer at hypersonic flow N. Palchekovskaya and V. Shvedchenko
FP.16: Wind tunnel and measurement techniques I	TuM12 Room: Holiday Inn - Forum 16 Chair: Luca Boccaletto Rapporteur: to be confirmed
Aerodynamic performance of the high-lift laminar wing at free flight and ETW in-tunnel conditions I. Kursakov, S. Bosnyakov, E. Kazhan, S. Matyash, S. Mikhailov and A. Lysenkov Vacuum ultraviolet radiation studies in a plasma torch facility C.M.  Jacobs, U.A. Sheikh, M.E.  MacDonald and C.O. Laux Jet Simulation Facility using the Ludwieg Tube Principle S. Stephan, R. Radespiel and R. Müller-Eigner Interference of High Lift Systems in Low Speed Wind Tunnels V. Zherekhov , A. Sungatullin and R. Stepanov Noise characterization of short duration and conventional hypersonic wind tunnels Yu. Gromyko, D. Bountin, A. Sidorenko, P. Polivanov, A. Maslov, A. Polivanov and V.V. Kudryavtsev
PP.02: LRE Cooling 1	TuM13 Room: Holiday Inn - Forum 10 Chair: Rolf Radespiel CoChair: Francesco Nasuti Rapporteur: to be confirmed
Experimental investigations on liquid film cooling in a GOX/ kerosene rocket combustion chamber. C. Kirchberger, G. Schlieben and O.J. Haidn Transfer of an analytical transpiration cooling model to the cooling analysis of rocket combustion chambers made of ceramic matrix composites (*) M. Selzer, H. Hald, A. Herbertz, S. Schweikert and J. von Wolfersdorf Radiative Heat Transfer Analysis in Modern Rocket Combustion Chambers F. Goebel, B. Kniesner, M.  Frey, O.  Knab and C. Mundt Evolution of Cooling-Channel Properties for Varying Aspect Ratio M. Pizzarelli, F. Nasuti and M. Onofri Numerical simulation of transpiration cooling through porous media W. Dahmen, V. Gerber, T. Gotzen and S. Müller Transient Fluid-Structure Interaction Analysis of a Cooled Rocket Thrust Chamber Based on Three Coupling Domains(*) D. Kowollik, M. Haupt and P. Horst Simulation of liquid, transcritical and gaseous cooling films C. Höglauer, B. Kniesner, O.  Knab, G. Schlieben and O.J. Haidn Consideration of wall roughness effects in the prediction of heat transfer in rocket combustion chambers B. Kniesner, M.  Frey and O.  Knab
PP.09: SRM Systems	TuM14 Room: Holiday Inn - Forum 11 Chair: Jean Thépenier CoChair: Ruiqi Shen Rapporteur: to be confirmed
Efficient numerical coupling strategy for evaporating polydisperse sprays in unsteady multi-species flows: Application to solid rocket motor simulations (*) A. Sibra, J. Dupays, A. Murrone, F. Laurent and M. Massot Self-Organizing of the Reactionary Zones of the Energetic Materials and Concept of the Smart Solid Micro-Propulsion System (*) A.N. Lukin Analysis of Pressure Blips in Aft-Finocyl Solid Rocket Motor (*) M. Di Giacinto, B. Favini and E. Cavallini Influence of Viscoelastic properties of Solid Propellants on Starting Transient of Solid Rocket Motors K. Krishna Raj, K. Sabarinath, G. Sandeep, M. Karuppasamy Pandian, K. Sathya Prabhakar and V.R. Sanal Kumar Parametric Study of Design Options affecting Solid Rocket Motor Start-up and Onset of Pressure Oscillations M. Di Giacinto, E. Cavallini, B. Favini and J. Steelant Simulation of turbulent two-phase flows in combustion chambers of solid rocket motors K. Volkov, V. Emelyanov and I. Teterina
11:50 - 12:30 PLENARY SESSION	TuAP Room: Holiday Inn - Forum 1 Chair: to be confirmed Rapporteur: to be confirmed
Developments in Aeronautics and Space Materials Y. Barbaux
12:30 - 14:00 Lunch Break II	Room: Restaurant Holiday Inn and Novotel
14:00 - 17:20 TECHNICAL SESSIONS
MAAT Programme	TuA01 Room: Holiday Inn - Forum 1 Chair: Farbod Khoshnoud Rapporteur: to be confirmed
Piezoelectric energy harvesting for airships and investigation of bio-inspired energy harvesters F. Khoshnoud, A. Shahba, O. Riaz, R. Shah, R. Shimura, Y.K. Chen, G. Gaviraghi, G. Pissanidis and B.  Patel Two dimensional numerical Modeling of nanosecond plasma Actuators, a preliminary study of application in propulsion systems M. Abdollahzadeh, J. Páscoa and P.J. Oliveira Aeroelastic vibration control of hybrid airships using regenerative actuators V. Patel, F. Khoshnoud, Y.K. Chen, D.  Montalvao and G.  Pissanidis Space launching base in stratosphere G. Gaviraghi, D. Vucinic, P. Rukshan , F. Khoshnoud and P. Marzocca Solar human powered airships as small airship feeders G.N.P. Sunkara, F. Khoshnoud, Y.K. Chen and G. Gaviraghi Conceptual Design of an Energy Harvesting System for Air Vehicles Landing Gear A. Bidmead, F. Khoshnoud and Y.K. Chen Self-Powered Dynamic Systems F. Khoshnoud, Y.K. Chen, R.K. Calay, C.W. de Silva and H. Owhadi Solar-powered Airships with Biologically Inspired Propulsion J. Hewitt, F. Khoshnoud, D.J. Dell and Y.K. Chen By-pass transition effects in propulsion components of high-altitude airships R. Vizinho, J. Páscoa and M. Silvestre Control of Airships in the framework of Optimal Uncertainty Quantification (for MAAT symposium) F. Khoshnoud, B.A.M.S. Abeysinghe, Y.K. Chen and R.K. Calay
MS.10: Structural Dynamics II	TuA02 Room: Holiday Inn - Forum 2 Chair: Maria Sidoryuk CoChair: Stephane Muller Rapporteur: to be confirmed
Keynote Lecture Complex decreasing of vibroacoustical loadings in aircraft systems E.V Shakhmatov Keynote Lecture The problem of eigen value and the mode of aircraft rotating element motion A.A. Tashkinov and N.A. Shevelev Ditching simulation of Air and Space vehicles using ALE methods A. Robert, J.-B. Mouillet and T. Schwoertzig System Development of Impact Test at Subsonic Level for Simulation of Bird Strike Dynamics on Airplane A. Sakuma, N. Torii, A. Mizushima and H. Shoji A parametric analytic study of Transmission Loss and Noise Reduction factors of an infinite multi-layered cylinder J. Magniez, M.A. Hamdi, J.D. Chazot and B. Troclet Computing the vibrations of polygonal panels under distributed random excitation using the image source method J. Cuenca
PP.17: Hypersonics	TuA03 Room: Holiday Inn - Forum 3 Chair: Alexander Kuranov CoChair: Hong Yan Rapporteur: to be confirmed
Conversion of hydrocarbon fuel in a thermal protection reactors of hypersonic aircraft A.L. Kuranov, A.V. Korabelnikov and A.M. Mikhailov Plasma control of sock wave configuration in M=2 inlet at off-design mode S. Leonov, F. Falempin, M.A. Goldfeld and A. Firsov Research on Hypersonic Inlet Leading Edge Radius Effect on Wall Static Pressure and Heat Flux Z. Wang, H. Bai and K. Zhang Numerical Prediction and Experimental Verification of Shock Oscillation for a Hypersonic Inlet at Low Supersonic Mach Numbers A.Y. Yu, D.W. Yang, J. Wu, H.L. Ni and J.L. Le The Design and Study of Osculating Curved Cone Waverider-based Airbreathing Integrated Hypersonic Vehicle H.E. Yuanyuan, W.U. Yingchuan, Y.U. Anyuan, H. Wei and L. Jialing Numerical Investigation on the Start/Unstart Performance of a Supersonic Inlet S.B. Li, S.B. Luo, W. Huang, Z. G. Wang and L. Yan A Numerical Investigation of Air Intakes for the 14-X Hypersonic Vehicle Scramjet Engine A. F. Moura and M. A.  Rosa Air Intake Design for the Acceleration Propulsion Unit of the LAPCAT MR2 Hypersonic Aircraft (*) C. Meerts and J. Steelant
PP.31: Propellant Management	TuA04 Room: Holiday Inn - Forum 6 Chair: Valery Trushlyakov CoChair: Piotr Wolanski Rapporteur: to be confirmed
Hot run test results of a validation optimized water-ice phase change heat accumulator and comparison to numerical analysis (*) J. Riccius, J. Leiner, J. Castro and J. Rigola Modeling and experimental validation of the heat accumulator in a Low Trust Cryogenic Propulsion (LTCP) system (*) S. Torras, J. Castro, J. Rigola, S. Morales, J. Riccius and J. Leiner Analyses of Cryogenic Propellant Tank Pressurization based upon Experiments and Numerical Simulations (*) C. Ludwig and M. Dreyer Study on the gas retention capability of metallic screens C. Höfflin and J. Gerstmann Electrical Capacitance Tomography system for determination of liquids in tanks rockets and satellites Z. Gut and P. Wolanski Numerical Investigations on Fluid Flow through Metal Screens. F. Middelstädt and J. Gerstmann Flow Resistance of Metallic Screens in Liquid, Gaseous and Cryogenic Flow A. Fischer and J. Gerstmann
PP.24: Nano Ingredients	TuA05 Room: Holiday Inn - Forum 7 Chair: Valery Babuk CoChair: Alexander Gromov Rapporteur: to be confirmed
Modeling of propellant combustion with nano-aluminum particles J. Dupays, Y. Fabignon, J.M. Lamet, E. Radenac and L.  Tessé Coating nano-sized aluminum to improve solid rocket propellant performance A. Reina, T.I. Gorbenko, I. Krawiec, G.  Colombo and L.T. DeLuca Rheological and Mechanical Behavior of Coated Aluminum loaded Nano-composites A. Reina, C. Paravan, M. Morlacchi, A.  Frosi, F. Maggi and L.T. DeLuca Use of nanoparticles in gas generating and energetic materials (review) V.E. Zarko and M.B. Talawar Nano-sized aluminum for solid fuel regression rate enhancement C. Paravan, A. Reina, A.  Frosi and L.T. DeLuca Nano-sized bimetallic aluminum-copper powders in HTPB-based fuels G. Vadalà, C. Paravan, P. Leoni, L.T. DeLuca, A.B. Vorozhtsov, N.G. Rodkevich and M.I. Lerner Controlled oxidation of aluminum nano and micro particles: Modeling and validation J.B. Gouriet, G. Litrico, L.L. Perez, P. Rambaud and P. Proulx On the Statistics of Nanoaluminum Thermal Characterization and its Correlation with the Slow Oxidation/Combustion Parameters (*) A.A. Gromov, C. Paravan, F. Maggi, L.T. DeLuca and U. Teipel
SI.03: Space Mission Models	TuA06 Room: Holiday Inn - Forum 9 Chair: Walter Zinner CoChair: Jung-IL Shu Rapporteur: to be confirmed
The AOCS‘ effects on the Propulsion Subsystem using the ESPSS Satellite Library C. Koppel, M. de Rosa, F. Rodríguez Lucas and J. Steelant A New Mission Design Approach for a Multi-disciplinary Space Rocket System Design J.I. Shu, T.J. Kwon, J.W. Lee, S.H. Kim and J. Chung New information intelligent monitoring technology for complex technical objects under dynamic conditions in real time B.V. Sokolov, M.Yu Okhtilev, V.A. Zelentsov and S.A. Potrasaev Surrogate models for space trajectory problems G. Hericher, D. Yarotski, M. Lebedev, S. Morozov, S. Alestra and C. Brand Challenges and future trends in Uncertainty-Based Multidisciplinary Design Optimization for space transportation system design L Brevault, M Balesdent, N Berend and R LeRiche Re-entry trajectory optimization for a SSTO vehicle in the presence of atmospheric uncertainties (*) F. Pescetelli, E. Minisci and R. Brown Deployment of the tethered satellite system (TSS): numerical modeling and dynamic control. V.A. Leontyev and B.A. Smolnikov
FD.3: Aircrafts/Helicopters Control	TuA07 Room: Novotel Tegernsee Chair: Alexander V. Nebylov Rapporteur: to be confirmed
LPV Control Design to Suppress Wing Rock Motion M.E. Sidoryuk Helicopter flight control design tool integrating handling qualities requirements J.C. Antonioli, A. Taghizad, T. Rakotomamonjy and M. Ouladsine Biodynamic Pilot Modelling for Aero‐Elastic Aircraft L.E. Zaichik, Y.P. Yashin, P.A. Desyatnik and H. Smaili WIG-Craft Flight Control Systems Development A.V. Nebylov Flight Dynamics Simulation & Mission Analysis of Integrated Helicopter-Engine Systems Using a Comprehensive Aeroelastic Rotor Model I. Goulos, V. Pachidis and P. Pilidis Nonlinear analysis of the longitudinal flight dynamics of a transport airplane S. Kolb, L. Hetru and T. M. Faure Automatic flight control system for general aviation M. Al-saegh
MS.3: Advanced Technologies, Smart Systems and Testing	TuA08 Room: Novotel Chiemsee Chair: Claudio Delle Donne Rapporteur: to be confirmed
New product vision for Aerospace by applying of lightweight Al-Li based alloys and Al-Mg-Sc material technologies B. Lenczowski Development design principles of large precision space reflector antennas, containing actuators of smart material E.A. Vasilyeva and A.N. Likhachev Influence of thickness on fatigue crack growth properties of titanium Ti-6Al-4V β annealed and aluminium-lithium 2050 T84 (*) L. Bieker and B. Journet Small-scale burner test for the characterisation of the combustion of aeronautic composite materials S. Dahikar, J.-M. Most and D. Denis Graduated justification methodology by multilevel severe tests A. Urien and J.M. Larrieu An integrated physical-chemical-mechanical approach to study the interfacial compatibility and adhesion in natural fibre thermoplastic composites L.Q. Tran, C.A. Fuentes, C. Dupont-Gillain, A.W. van Vuure and I. Verpoest BepiColombo HGA ARA C/SiC Struts: A thermo - mechanical challenge for support structures in harsh environments F.  Wigger, S. Schmidt-Wimmer, S. Beyer and E. Sperlich
PP.21: Ram/scramjet Experimental	TuA09 Room: Holiday Inn - Forum 12 Chair: Jörg Riccius CoChair: Dmitry Davidenko Rapporteur: to be confirmed
Numerical and Experimental Investigation of a Central Strut Injector with Perpendicular Injection for Scramjet Applications K. Makowka, M. Gurtner, D. Paukner, T. Sattelmayer and H. Kau Preliminary investigation of ignition and flame stabilization using catalytic treatment of propellants for scramjets D. Paukner, M. Gurtner and H.P. Kau Simulation of combustion by cold air injection in a generic scramjet model in the H2K blow down facility J. Riehmer and A. Gülhan Ignition Length Study of JP-8+100 in a Supersonic Duct M.L. Bateup Experimental Investigation of a Pipe-connected Solid Fuel Scramjet in an Arc-heated Facility V. Chernov and A. Gany The performance of dual combustion ramjet based on free-jet experiments J. Tan and J. Wu Experimental and numerical simulating studies on a solid-fuel rocket scramjet Z. Lv, B. Liu, Z.X. Xia and L.Y. Huang
FP.03: Flow Control I	TuA10 Room: Holiday Inn - Forum 14 Chair: Viktor Kozlov CoChair: Allan Grosvenor Rapporteur: to be confirmed
Computational Investigation of C-130 Afterbody Drag Reduction by Finlets H. Telli, E. Ayan and Y.V. Pehlivanoglu Aerostrakes suppressing asymmetric lee-vortices on a slender body at high angles of attack(*) O. Wysocki, C. Schnepf and E. Schülein Numerical Investigations of Dynamic Stall Phenomenon for Vertical Axis Wind Turbine F. Frunzulica, H. Dumitrescu and A. Dumitrache Investigation of an active flow control system by multi-physics simulation and experimental validation. M. Kurowski, M. Matejka, P. Doerffer and B. Peeters Experimantal and numerical study of pulsating transversal jets (*) M.A. Goldfeld, N.N. Fedorova, I.A. Fedorchenko, K.Y. Timofeev, Y.V. Zhakharova and G.A. Pozdnyakov Propagation of disturbances in hypersonic boundary layer on wing with mass transfer through the surface G.N. Dudin and A.V. Ledovskiy Tomography of thermal plasma flows by mean of single CCD camera Y. Babou, F. Cannat and D. Lequang Heat flux control by tangential air blowing at high supersonic speeds. V. Borovoy, E.B. Vasilevskiy, I.V. Egorov, V.E. Mosharov, V.N. Radchenko, P.V. Chuvakhov and V.V. Shtapov Comparison of mixing processes in a compressible accelerated nozzle flow with subsonic and supersonic injection A. Wohler, K. Mohri, C. Schulz and B. Weigand
FP.10: CFD I	TuA11 Room: Holiday Inn - Forum 15 Chair: Vitaly Soudakov CoChair: Jean Muylaert Rapporteur: to be confirmed
The effects of actuation frequency on the separation control over an airfoil using a synthetic jet Y. Abe, K. Okada, T. Nonomura and K. Fujii Treatment of surface intersections for gradient-based aerodynamic shape optimization M.J. Martin, E. Valero, C. Lozano and E. Andres Assessment of Implicit Implementation of the AUSM+ Method and the SST Model for Viscous High Speed Flow S. Colonia, R. Steijl and G. Barakos Development of advanced CFD tools and their application to simulation of internal turbulent flows K. Volkov, V. Emelyanov and A. Karpenko
FP.17: Launchers Aerodynamics	TUA12 Room: Holiday Inn - Forum 16 Chair: Doyle Knight Rapporteur: to be confirmed
Numerical and Experimental Investigations of a Generic Rocket Launcher Configuration with Cold Plume in Hypersonic Flow (*) K. Osswald, V. Hannemann, K. Hannemann, S. Stephan and R. Radespiel Experimental and Numerical Investigation of the Turbulent Wake Flow of a Generic Space Launcher Configuration V. Statnikov, D. Saile, J.H. Meiß, A. Henckels, M. Meinke, A. Gülhan and W. Schröder Numerical and experimental investigation of a transonic space launcher wake. S. Scharnowski, V. Statnikov, M. Meinke, W. Schröder and C.J. Kähler Effect of Separation Motor Firing on the Aerodynamics of a Typical Launch Vehicle using CFD S. Kumar Saha and D. Dipankar Aerodynamic and Heat Problems of New-Generation Multi-Stage Launch Vehicles. S. M.. Drozdov, V.N. Brazhko, V.N. Radchenko, A.S. Skuratov and D.S. Fedorov An essential requirement of developing the launch vehicle system in 2013 S. Thangavel, K. Praveen and N. Balaji
PP.03: LRE Systems	TuA13 Room: Holiday Inn - Forum 10 Chair: Oliver Knab CoChair: William Anderson Rapporteur: to be confirmed
Keynote Lecture Liquid Rocket Hydrocarbon Booster Engines (LRHCBE’s) for Launch Vehicles R.L. Sackheim Pulse-mode Performance Characteristics of a Small Liquid-monopropellant Rocket Engine (*) J.H. Kim, H. Jung and J.S. Kim Status of development of the LYRA Program L. Arione, R. Tontini, M. Rudnykh, A. Gurtovoi, S.D. Lobov, A.V. Shostak, A. De Lillis and E. D‘Aversa Disruptive propulsive technologies for European space missions C. Koppel, D. Valentian , R. Blott, F. Jansen, C. Ferrari, C. Bruno, G. Herdrich and R. Gabrielli Chemical Propulsion System for a Versatile Lander Demonstrator Platform D. Fiot, F. Girard, P. Gambach, M. Plischke, P. Martin and L. Souverein Preburner Development for the SCORE-D Liquid Rocket Engine within the Future Launcher Preparatory Programme FLPP R. Strunz, Th. Fuhrmann, D. Feyhl, G. Dantu, E. Humbert and Ph. James The VINCI Upper Stage Engine: the Demonstration of Maturity P. Alliot, J-F. Delange , E. Edeline and A. Lekeux
PP.10: SRM Metals	TuA14 Room: Holiday Inn - Forum 11 Chair: John Zevenbergen CoChair: Stany Gallier Rapporteur: to be confirmed
Model of Heterogeneous Condensed Systems Microstructure and Problem of Agglomeration Process Description V.A. Babuk and A.A. Nizyaev Numerical simulation of a single aluminum droplet burning in a propellant environment O. Orlandi, S. Gallier, Y. Moonsamy and N. Cesco Detailed Analysis of a Quench Bomb for the Study of Aluminum Agglomeration in Solid Propellants S. Gallier, J.G. Kratz, N. Quaglia, G. Fouin, N. Cesco and E. Robert High Performance Solid ADN Propellants for Space Applications N Wingborg FP7 HISP program: Selection of reference missions and definition of propellant requirements M. Calabro Advanced aluminum powders for solid propellants F. Maggi, S. Dossi, M. Fassina, A. Reina and L.T. DeLuca Comparing ballistics of AP- vs. ADN-based composite solid rocket propellants J.F. Zevenbergen, I.  Palmucci, S. Dossi and L.T. DeLuca Combustion of Metallised ADN/GAP Solid Rocket Propellants with Focus on Agglomeration Effects V. Weiser, A. Franzin, V. Gettwert and L.T. DeLuca
17:20 - 18:00 PLENARY SESSION	TuAP Room: Holiday Inn - Forum 1 Chair: to be confirmed Rapporteur: to be confirmed
Materials for Competitive Aero Engines C. Quillien
Wednesday, July 3rd
08:30 - 11:50 TECHNICAL SESSIONS
SI.10/FD.08: Space Debris 3-GNC&RDV for ADR	WeM01 Room: Holiday Inn - Forum 1 Chair: Charles Vallet CoChair: Luciano Anselmo Rapporteur: to be confirmed
Advanced image processing in space applications: the new trend to increase the success rate of exploration space missions P. Prinetto, D. Rolfo, P. Trotta, P. Lanza, A.  Martelli and A. Tramutola Recognition method of spacecraft docking ring based on monocular vision and laser range finder K. Zhai, X. Qu, Z. Li and X. Chen Stereo vision system for capture and removal of space debris P. Prinetto, D. Rolfo, P. Trotta, F. Rosso, F. Gallo, W. Allasia, E. Licata, A. Favetto, M. Paleari and P. Ariano Covariance Analysis Tool for Far Non-cooperative Rendezvous L. de Mijolla, B. Cavrois, A. Profizi, C. Renault and A. Cropp LIDAR-based pose estimation for non-cooperative rendezvous. M. Dardelle and C. Renault GNC challenges for heavy active debris removal using blow effect P. Brun Control of a space vehicle pulling a debris D. Losa, C. Bakouche and C. Le Peuvédic The Removal of Large Space Debris Using Tethered Space Tug V.S. Aslanov and V.V. Yudintsev
FP.22: CFD II	WeM02 Room: Holiday Inn - Forum 2 Chair: Ivan Egorov CoChair: Maxim Ustinov Rapporteur: to be confirmed
Dynamics of Molecules in a Supercooled Water Nanoparticle during the Ice Accretion on the Aircraft Surface (*) I.A. Amelyuskin and A.L. Stasenko PyFly: Fast, Friendly Framework for Aerodynamic Simulation M. Ghommem, N. Collier and V. Calo Validation of numerical modeling of supersonic spatial flows A. Kharitonov, A.E. Lutsky and A.M. Shevchenko Verification of discontinuous Galerkin scheme for linearized Euler equations S. Mikhaylov, A. Morozov, V. Podaruev, V. Vlasenko and A. Wolkov Experimental Study of the Galloping Stability of Prismatic Beams (*) F Gandia-Aguera, J Meseguer and A Sanz-Andres
PP.18: PDE RDE Detonation	WeM03 Room: Holiday Inn - Forum 3 Chair: Sergey Frolov CoChair: Steve Heister Rapporteur: to be confirmed
Pulsed Detonation Rocket Engine Combustion B. Kan and S. Heister Three-dimensional numerical simulation of a continuously rotating detonation in the annular combustion chamber with a wide gap and separate delivery of fuel and oxidizer S.M. Frolov, A.V. Dubrovskii and V.S. Ivanov A computer-based tool for preliminary design and performance assessment of Continuous Detonation Wave Engines S.A. Doekhie, E. Dumont, A. Cervone and R. Noomen Improving accuracy and performance of Rotating Detonation Engine simulations M. Folusiak, K. Swiderski, J. Kindracki, A. Kobiera, B. Lukasik and P. Wolanski Measurement techniques for investigation on heat transfer characteristics of gaseous rotating detonation engine K. Sobczak, P. Wolanski and J. Kindracki Research on Application of Continuously Rotating Detonation Combustion Chamber to Turbine Engine P. Wolanski, W. Balicki, P. Kalina, J. Kindracki, B. Lukasik, W. Perkowski and A. Rowinski Mathematical modeling of detonation initiation via flow cumulation effects I. Semenov, P. Utkin and I. Akhmedyanov
PP.32: Propellant Injection	WeM04 Room: Holiday Inn - Forum 6 Chair: Yu Daimon CoChair: Dimitry Suslov Rapporteur: to be confirmed
Temperature measurement of cryogenic nitrogen jets at supercritical pressure H. Tani, S. Teramoto, T. Toki, S. Yoshida, K. Yamaguchi and K. Okamoto Design, analysis and testing of a 3.5 kN coaxial pintle demonstrator engine L. Souverein, P. Martin, A. Dahlhaus, C. Hoeglauer, V. Kaufmann, C. Maeding, K. Seeliger, E. Receveur and D. Fiot Numerical simulations of mixing under supercritical pressures of a shear coaxial injector using a high-order method: effect of outer jet temperature H. Terashima and M. Koshi Large Eddy Simulation of Kerosene/LOx Supercritical Mixing Characteristics of a Swirl Injector using Various Cubic Equations of State J.Y. Heo, K.J. Kim and H.G. Sung Large-Eddy Simulation of Trans- and Supercritical Injection (*) H. Müller, C.A. Niedermeier, M. Jarczyk, M. Pfitzner, S. Hickel and N.A. Adams Numerical coupling strategies for the “separated-to-dispersed” transition within the liquid phase of cryogenic rocket engines C. Le Touze, A. Murrone and E. Montreuil
PP.25: New Chem Ingr & Handling	WeM05 Room: Holiday Inn - Forum 7 Chair: Thomas Klapoetke CoChair: Filippo Maggi Rapporteur: to be confirmed
Progress in the Development of High Energy Dense Oxidizers based on CHNO(F)-compounds Q. J.  Axthammer, M A.  Kettner, T. M.  Klapötke, R. Moll and S. F.  Rest Thermal Characterization of Ammonium Dinitramide (ADN) - Hydroxylammonium nitrate (HAN) mixture A. Rahman, J.K. Chin and T.F. Wahida Ku Chik Microscale Electrolytic Decomposition of Hydroxylammonium Nitrate (HAN) Solution in micro-combustion chambers J.K. Chin , K.S.  Koh and T.F.W. Ku Chik Research and Development on Thrusters with HAN (Hydroxyl Ammonium Nitrate) Based Monopropellant (*) N. Azuma, K. Hori, T. Katsumi, R. Amrousse, T. Nagata, K. Hatai, T. Kobayashi, Y. Nakayama, T. Matsumura and S. Fujiwara Combustion characteristics of GAP fules for ducket engine S. Ruiqi , H. Aijun, Y. Yinghua, W. Lizhi, H. Yan and Z. Peng Activation of micrometric aluminum-metal oxides mixtures by mechanical milling S. Dossi, F. Maggi, L. Facciolati and L.T. DeLuca Preparation, transformation and characterization of different aluminum hydride AlH3 phases (alanes) W. Cong , L. Potet, N. Herault, R. Brahmi, Y. Batonneau , C. Kappenstein, G. Jacob, C. Perut, Y. Guelou and E. Labarthe
SI.04: Design and Operation Methodologies applied to Space Programs	WeM06 Room: Holiday Inn - Forum 9 Chair: Jacques Gigou CoChair: Alessandro Mancini Rapporteur: to be confirmed
Challenges for Concurrent Engineering on Launcher Design D. Haerens , G. Collange , D. Denier-Gegu , G. Hericher , A. Huet and A. Matthyssen System Integration of Future Space Infrastructure with involvement of Modern Expert Analysis Techniques. O. Saprykin, A. Kulchitsky, A. Botvinko and A. Kuznetsova Algorithm For Space Related Multi - Objective Optimization Problems (*) A. Mancini and M. Di Giacinto Open Space architecture (*) O. Saprykin ISS-RS: Analysis of Operational Experience and Updating Prospects A Uspensky Alternative concepts for the handling of hazardous, liquid media in biological experiments P. Kern and T. Eisenberg A Decision Support System (DSS) for Developing Programs of Scientific and Applied Research and Experiments on the Russian Segment of the ISS (*) B.V. Zagreev, V.P. Osipov and V. Sudakov
FD.4: Avionics/Platforms	WeM07 Room: Novotel Tegernsee Chair: Corbin Juliien Rapporteur: to be confirmed
Model Predictive Control real time performance in a rendezvous&capture scenario for Mars Sample&Return M. Saponara, C. Philippe and A. Tramutola Mission Oriented Sensor Arrays – An Approach towards UAS Usability Improvement in Practical Applications (*) N.M. Figueira, O. Trindade, A.L.P. Mattei and L. O. Neris Analytical and experimental stability investigation of a hardware-in-the-loop satellite docking simulator (*) M. Zebenay, T.  Boge, R. Krenn and D. Choukroun Robotic Relative Motion Reproduction for Air to Air Refuelling Simulation P. R Thomas, T. S Richardson and J. L. du Bois VEGA LV Qualification Process: GNC aspects on HWIL Testing and Analysis M. Giannini and I. Cruciani
MS.4: Structural Dynamics I	WeM08 Room: Novotel Chiemsee Chair: Bernard Troclet CoChair: Sergey Vorozhtsov Rapporteur: to be confirmed
Integrated and Distributed Adaptive Metacomposites for vibroacoustic control of Aerospace Structures M. Collet, M. Ouisse, F. Tatéo and M.N Ichchou Composite materials usage in acoustic absorption constructions of aircraft engines A.N. Anoshkin and A.A. Tashkinov PAYLOAD COMFORT – A Challenge for launcher’s design V. Le Gallo Pyro-Technique Shock Loads in Launch Vehicles J. Albus and B. Kotzias
PP.27: Electric & Nuclear Propulsion	WeM09 Room: Holiday Inn - Forum 12 Chair: N. N. CoChair: N. N. Rapporteur: to be confirmed
Stationary plasma thruster for small space satellites (*) A.I. Bugrova, G.E. Bugrov, A.V. Desyatskov, M.V. Kozintseva, A.S. Lipatov, A.A. Safronov, M.I. Shaposhnikov, P.G. Smirnov and V.K. Kharchevnikov Modelling of plasma-chemical propellant interaction in electrodeless helicon plasma thruster F. Bosi, G. Parissenti, M. Pessana and D. Pavarin Concept of Electric Propulsion Realization for High Power Space Tug L.E. Zakharenkov, A.V. Semenkin and A.E. Solodukhin New Kind of Resistojet with Power System Based on Supercapacitors L. Mezyk, A. Kobiera, L. Boruc, P. Biczel and P. Wolanski The special features of the combined operation of the energy conversion system and electric propulsion integral with the nuclear power propulsion system A.V. Karevskiy and S.A. Popov Assesment of a small reactor at 10kWe E. Cliquet Moreno, J.M. Ruault, J.P. Roux, B. Cazale and L Manifacier Numerical Investigation of MHD Impact on Argon Plasma Flow by Variable Magnetic Field for Space applications P.P. Upadhyay, U. Bauder, G. Herdrich, S. Fasoulas and H-P. Röser
FP.04: C.A. Aircrafts	WeM10 Room: Holiday Inn - Forum 14 Chair: Volf Borovoy Rapporteur: to be confirmed
Experimental and computational investigations aimed at improving stability and controllability of a “flying wing” aircraft configuration A.A. Pavlenko, G.A. Fedorenko, A.N. Petrushkin, K.A. Osipov and N.D. Ageev Aerodynamic studies for moderate capacity long-range aircraft A.L. Bolsunovsky, N.P. Buzoverya, I.L. Chernyshev, B.I. Gurevich and A.P. Tsiganov Study on a concept of a business jet with high passenger comfort A.L. Bolsunovsky, N.P. Buzoverya, I.L. Chernyshev, V.G. Sudakov and A.V. Voyevodin Studies on Dynamics of an Unmanned Aerial Vehicle With Variable-Span and Variable-Sweep Wing (*) J. Guo and G.T. Yang Simulation of unsteady aerodynamic characteristics of aircraft at high angles of attack using neural networks. D. Ignatyev Wind tunnel two-dimensional parametric investigation about biplane configurations (*) M.A. Barcala-Montejano, A.A. Rodríguez-Sevillano, M.E. Rodríguez-Rojo and S. Morales-Serrano
FP.15: Shock Interaction	WeM11 Room: Holiday Inn - Forum 15 Chair: Ferry Schrijer CoChair: Richard Schwane Rapporteur: to be confirmed
Three-Dimensional Shock-Wave/Boundary-Layer Interaction on Sharp and Blunted Flat Plate V. Borovoy, I.V. Egorov and N. Palchekovskaya A conservative turbulence model for shock-dominated flows. K. Sinha and S. J. Balasridhar Experiments on shock induced laminar-turbulent transition on a flat plate at Mach 6 S. Willems and A. Gülhan Computational analysis of shock wave laminar boundary layer interactions in non-equilibrium hypersonic flow G. Pezzella and R. S. Donelli A New Configuration Of Irregular Reflection Of Shock Waves L.G. Gvozdeva and S.A. Gavrenkov Conical flows near V-shaped wings with attached shock waves on leading edges. F.A. Maximov, N.A. Ostapenko and M.A. Zubin Influence of leading edge bluntness on hypersonic flow in a generic internal-compression inlet V. Borovoy, V. Mosharov, V. Radchenko, A. Skuratov and I. Struminskaya
FP.18: Shear layers and separated flows	WeM12 Room: Holiday Inn - Forum 16 Chair: Dominik Saile CoChair: Francesco Nasuti Rapporteur: to be confirmed
Investigations on a Backward-Facing Step by Means of a Microphone Array and IR-Thermography D. Saile, A. Gülhan and A. Henckels Numerical study of transverse helium injection into plane channel with backward facing step (*) N.N. Fedorova, I.A. Fedorchenko, S.A. Valger, D. Daub and U. Gaisbauer Transonic base-flow buffeting: characterisation of the large scale flow unsteadiness using POD FFJ Schrijer, A Sciacchitano and F Scarano An Investigation of Dynamic of Ordered Structure in Excited Jet using PIV - based phase-averaging technique (*) A. Mironov, S.Y. Krasheninnikov, V. Maslov and D. Zakharov Mean flow and fluctuations around shallow cavity at high subsonic velocities V. Lebiga, D. Mironov, A. Pak and V. Zinoviev Experimental investigation of a dynamic layer at the ramp for supersonic separated flow V.I. Zapryagaev, I.N. Kavun and I.I. Lipatov Flow Separation in Out-of-Round Nozzles, a Numerical and Experimental Study C. Génin, R. Stark and S. Jack Effect of local suction or blowing on the wake behind a cylinder in compressible subsonic flows V.N. Zinovyev, V.A. Lebiga and A.Y. Pak
PP.04: LRE Cooling 2	WeM13 Room: Holiday Inn - Forum 10 Chair: N. N. CoChair: Christoph Kirchberger Rapporteur: to be confirmed
Experimental Investigation of Velocity and Temperature Distributions in Turbulent Cross Flows over Transpiration Cooled C/C Wall Segments (*) S. Schweikert, J. von Wolfersdorf, M. Selzer and H. Hald Wall heat fluxes in rocket combustion chamber with porous injector head V.P. Zhukov and D. Suslov Numerical investigation of heat transfer in flat vortex channels N.V. Kukshinov and M.S. Frantsuzov RANS Simulations of Chemical Reactions in Cooling Films G. Frank, F. Ferraro and M. Pfitzner ZBO system concepts adapted for European Long Term Cryogenic Propulsion J. Lacapere, J. Tanchon , T. Misuri and T. Tirolien Heat transfer in porous media applied to liquid rocket engines Y. Khamis, D. Suslov and B. Desmet
PP.11: HRE Systems	WeM14 Room: Holiday Inn - Forum 11 Chair: Arif Karabeyoglu CoChair: Ognjan Bozic Rapporteur: to be confirmed
Advanced Hybrid Rockets for Future Space Launch Arif Karabeyoglu A Theoretical Prediction of Regression Rates in Swirl Injection Hybrid Rocket Engines K. Ozawa and T. Shimada Paraffin-based and metal-loaded HTPB fuel regression-rates study in a lab-scale hybrid rocket fed with N2O (*) F. Scaramuzzino, C. Carmicino, G. Festa, A. Viviani and A. Russo Development of 20 kN hybrid rocket booster A. Bettella, F. Moretto, E. Geremia, N. Bellomo, D. Petronio and D. Pavarin An approach to improve hybrid rocket performance L. Galfetti, F. Nasuti, D. Pastrone and A. Russo Sorge Design of the feed system of a Hybrid Rocket Engine M. Demoly, J. Fissette, O. Vielpeau, A. Treilhes, N. Rizzo, J. Rèbre, J. Mulpas, V. Jacaranda-Lakiss-Marques, E. Jean-Bart and R. Mercier Experimental Evaluation of a High Test Peroxide Catalyst Chamber for a Hybrid Rocket Engine O. Bozic, D. Lancelle, S. May and D. Porrmann Numerical and experimental evaluation of the performance of a cavitating valve for the control of oxidizer flow in a hybrid rocket engine. P. Dvorak and R. Tijsterman
11:50 - 12:30 PLENARY SESSION	WeAP Room: Holiday Inn - Forum 1 Chair: to be confirmed Rapporteur: to be confirmed
Clean Sky progress and Clean Sky 2 proposal E. Dautriat
12:30 - 14:00 Lunch Break III	Room: Restaurant Holiday Inn and Novotel
14:00 - 17:20 TECHNICAL SESSIONS
M1.0: DESIREH Programme Eccomas/Eucass	WeA01 Room: Holiday Inn - Forum 1 Chair: Jochen Wild Rapporteur: to be confirmed
Overview on the DESIREH project Keynote Lecture J. Wild Acceleration of URANS for Application to Separated High-Lift Flows P. Eliasson, C. Marongiu and S. Bosnyakov Comparison of Grid Adaptation techniques for High Lift Flows Applications J. Ponsin, M. Meheut, L. Tysell and T. Sucipto Progress in Optical Measurement Methods in Cryogenic Conditions J. Quest, R. Konrath and U. Henne Optimization Strategies for High-Lift Design P. Iannelli, M. Minervino, E. Benini, R. Ponza and D. Romano Adjoint Methods in High-Lift Design Optimization S. Kleinveld and O. Amoignon Design of a High-Lift System for a Laminar Wing P. Iannelli, J. Wild, M. Minervino, H. Strüber, F. Moens and A. Vervliet Experimental Verification of the DESIREH High-Lift Wing at Aircraft Flight Conditions D. Meissner, F. Cusset, J. Wild and M. Schulz CFD-based Analysis of Wind Tunnel Installation Effects H. Maseland and F. Moens Contributions of DESIREH towards ACARE Vision 2020 H. Strüber, S. Kleinveld and E. Jesse
FD.10: CEAS/Eucass-GNC Robustness	WeA02 Room: Holiday Inn - Forum 2 Chair: Daniel Chouckroun Rapporteur: to be confirmed
Spacecraft Attitude and Rate SDRE Estimation and Control Using the SDRE Method (*) D. Choukroun and O. Tekinalp Fault-tolerant Spacecraft Magnetic Attitude Control D. Choukroun An Autonomous Collision Avoidance Strategy for Unmanned Air Vehicle Guidance Y.I. Jenie and E. van Kampen Fault-tolerant Control for a Civil Transportation Aircraft L. G. Sun, C. C de Visser and Q.P. Chu Fault Detection and Isolation in Inertial Navigation Systems with SDRE non-linear filter (*) I. Vitanov and N. Aouf Chance constrained optimization for launcher GNC validation G. Maurice, M. Ganet-schoeller, R. Lebrun and S. Bennani
PP.19: Plasma Systems	WeA03 Room: Holiday Inn - Forum 3 Chair: N. N. CoChair: Daniele Pavarin Rapporteur: to be confirmed
Detailed Characterization of Flow Disturbances Caused by SDBD Plasma Actuator S. Leonov, V. Soloviev, A. Frolov, I. Moralev, R. Miles and D. Opaits Plasma Catalysis Burning Viscous Hydrocarbons O.A. Nedybaliuk, V.Y. Chernyak, L.Y. Vergun, S.G. Orlovska, E.V. Martysh, L.V. Simonchik and S.V. Dragnev Plasma-liquid system with pulsed discharge for the creation and focusing of acoustic waves (*) V.V. Iukhymenko, V.Y. Chernyak, E.V. Martysh, O.A. Fedorovich, O.A. Nedybaliuk, E.Y. Gavryliuk, T.E. Lisitchenko, V.O. Andriuschenko and V.E. Marchuk Plasma-Liquid System with Rotational Gliding Arc and Liquid Electrode O.A. Nedybaliuk, O.V. Solomenko, V.Y. Chernyak, E.V. Martysh and I.I. Fedirchyk Plasma Catalysis Conversion of Hydrocarbons in Flow of Air/CO2 O.A. Nedybaliuk, O.V. Solomenko, V.Y. Chernyak, E.V. Martysh, T.E. Lisitchenko, L.V. Simonchik, V.I. Arkhipenko, A.A. Kirillov, A.I. Liptuga and S.V. Dragnev Novel Air-Breathing Plasma Jet Propulsion for Solar Powered High Altitude Flight Platforms B. Goeksel, I. Mashek, V. Lashkov, A. Lyublinsky, S. Korotkov, F. Behrendt, I. Rechenberg, C. Paschereit and M.  Tajmar Application of an integrated CFD model to the metallic nanoparticle production in an Inductively Coupled Plasma reactor S. Lopes, P. Proulx, J.B. Gouriet and P. Rambaud
PP.33: Gelled Propellant Systems	WeA04 Room: Holiday Inn - Forum 6 Chair: Helmut Ciezki CoChair: Karl Wieland Naumann Rapporteur: to be confirmed
Control Characteristics of a Gel Propellant Throtteable Rocket Motor P. Cardoso Caldas Pinto, J. Ramsel, K. Schmidt, K.W. Naumann, H. Niedermaier and A. Thumann Application of Green Propulsion Systems Using Rocket Motors and Gas Generators with Gelled Propellants K.W. Naumann, J. Ramsel, K. Schmid, P. Caldas-Pinto, H. Niedermaier and A. Thumann Overview on Gel Propulsion Activities at DLR Institute of Space Propulsion H. Ciezki and M. Negri Progress in Understanding the Combustion Physics for Gelled Hypergolic Propellants S. Heister and T. Pourpoint Comparative Study of Rheological Properties of Ethanol and UDMH based Gel Propellants B.V.S. Jyoti, M. Varma and S. W. Baek
PP.26: Advanced AB/Green Propellants II	WeA05 Room: Holiday Inn - Forum 7 Chair: Lucien Vingert CoChair: Keiichi Hori Rapporteur: to be confirmed
Conceptual Study of a Rocket Dual Combustion Ramjet Combined-Cycle Engine for a Near Space Plane W. Jiping, T. Jianguo, C. Jian and W. Zhenguo Modeling of Aluminum Combustion in Air-breathing Combustor J.S. Shin, D.H. Han and H.G. Sung Development and Testing of Catalysts for Hydrogen Peroxide Decomposition (*) C. Boffa, L. Micoli, G. Festa, A. Russo Sorge and M. Turco Simulations with a one-dimensional two-fluid model of a hydrogen peroxide catalyst bed (*) R-J. Koopmans, J.S. Shrimpton and G.T. Roberts ERBURIGH Test Facility - The Next Step of Material Testing for H2O2 Rocket Combustion Chambers K. Bubenheim, C. Wilhelmi, S. Beyer and S. Schmidt-Wimmer Impact of Characteristic Length L* on a Green 1-Newton Bi-Propellant Thruster which is based on HTP and Kerosene (*) S. Schuh, A. Woschnak and C. Scharlemann
SI.05: Space Systems Concepts	WeA06 Room: Holiday Inn - Forum 9 Chair: Paulo Moraes CoChair: Kazuhisa Chiba Rapporteur: to be confirmed
Propulsion and Vehicle Study for Future Space Transportation at JAXA M. Yoshida, S. Ishimoto, T. Kimura, S. Tomioka, M. Kodera and K. Tani Technology maturation for the next generation reignitable cryogenic upper stage M. Güthler, M.  Rossmann, B.  Hürmann, M. Brünger and T.  Renk Improving the Brazilian Satellite Launch Vehicle P. Moraes, L. Potolski and H. Schlingloff Conceptual design of single-stage hybrid rocket in view of multidiscipline using design informatics K. Chiba, M. Kanazaki, K. Kitagawa, M. Nakamiya and T. Shimada Space mini-vehicle with the laser propulsion system Y.A..A Rezunkov, M.S. Egorov and A.A. Schmidt
FD.5: Control	WeA07 Room: Novotel Tegernsee Chair: Daniel Chouckroun CoChair: Philippe Tatry Rapporteur: to be confirmed
Nonlinear Model Predictive Control of Space Redundant Manipulators M. Wang, R. Lampariello and U. Walter Performance Comparison of Single- and Two-Loop Control Systems on a Rotary Table B Özkan TVC Control, First Bending Mode and Aero-elastic Effects: Post flight reconstruction of VEGA LARES mission C. Roux and I. Cruciani RACS Stability Analysis for VEGA FPSA Program F. Sciuto, I. Cruciani and C. Roux Precise margins to operational limits of the RACS taking into account the PWM implementation (*) K. Damo and G. Cuciniello Study of Rigid Body Launch Vehicle Dynamics A. Graciano da Silva, W.C. Leite Filho and A. Garro Brito VUT 700 SPECTO project overview P. Zikmund and J. Pejchar
MS.5: Loads and Aeroelasticity	WeA08 Room: Novotel Chiemsee Chair: Jean-Pierre Grisval CoChair: Wolfgang Lüber Rapporteur: to be confirmed
High and low fidelity finite element modelling in aircraft composite fuselage structural analysis and optimisation WJ Vankan, BAT Noordman and K Kueres Elastic body impact on sandwich panels at low and intermediate velocity(*) C. Kralovec, M. Schagerl and K.U. Schröder On the use of lyophobic heterogeneous systems (LHS) in payload comfort(*) M. Michelin-Jamois, L. Guillemot, T. Abensur, E. Charlaix and G. Vigier Aeroelastic tailoring of a blended wing body (BWB) aircraft structure using FSI simulation F. Stroscher, A. Hermanutz, N. Maghaldadze and H. Baier Stand with artificial airflow simulation and flutter tests results of dynamically scaled model V.I. Smyslov, M.M. Bogatyrev, P.G. Karlke and G.V. Liseykin Aeroelastic Rotor Blade Dynamics for Helicopter Flight Mechanics Applications I. Goulos, V. Pachidis and P. Pilidis Fuselage damping characteristics and fatigue blade impact on the stability of helicopter (*) A. Nour, S. Lecheb, A. Chellil and H. Kebir
PP.28: Environmental Impact	WeA09 Room: Holiday Inn - Forum 12 Chair: Niklas Wingborg CoChair: Christiane Voigt Rapporteur: to be confirmed
Ice formation in the exhaust plume from an Ariane5 rocket C. Voigt, U. Schumann and K. Graf Heterogeneous condensation of water vapour and carbon dioxide in rocket engine plumes, operated in the upper atmosphere (*) Y. Platov and L.T. DeLuca CFD-assisted particle size distribution measurements in the Keldysh Research Centre experimental set-up at ONERA J. Hijlkema and P. Prévot The potential impact of solid rocket propellants on the atmosphere: An overview N.A. Slavinskaya, M. Wiegand and U. Riedel Flow characteristics passing past an open cavity containing two mass injection slots. Application to the Trapped Vortex Combustor concept. P. Xavier, A. Vandel, G. Godard, B. Renou, G. Cabot and M.A. Boukhalfa
FP.05: C.A. Aircraft Subsystems	WeA10 Room: Holiday Inn - Forum 14 Chair: Doyle Knight Rapporteur: to be confirmed
The Turbulent Flight Environment Close to the Ground and Its Effects on Fixed and Flapping Wings at Low Reynolds Number S. Watkins, A. Fisher, A.  Mohamed, M. Marino, M. Thompson, R. Clothier and S. Ravi Aerodynamic performance analysis of a non-planar C-Wing using experimental and numerical tools. M.P. Rajaprakash, M.K. Balraj and L.N. Arunachalam Calculation of Tumbling Boundaries of a Generic Wing-Only Airliner A.N. Khrabrov and M.E. Sidoryuk Vortical flow patterns for high lift for high speed aircraft concepts (*) J-E. Lombard, P.  Leyland, M. Gaffuri and Y. Wohlhauser Case study of the challenging installation of a turboprop flow evacuation system V. Ibanez Colas, D. Perdones Diaz and E.J. Angel Blasco The analysis of a reverse jet influence on an engine inlet flow parameters and particles ingestion (*) S.Y. Krasheninnikov and D.E. Pudovikov
FP.12: Wind tunnel and measurement techniques II	WeA11 Room: Holiday Inn - Forum 15 Chair: Ivanov Misha Rapporteur: to be confirmed
Experimental investigation of a newly designed supersonic wind tunnel(*) J. Wu and R. Radespiel Visualization in a water channel as a preliminary design tool (*) A.A. Rodríguez-Sevillano, M.A. Barcala-Montejano and C. Delgado-Obrero Experimental characterization of UV radiation in a high enthalpy plasma torch facility P.J. Bertrand, C.J. Casses, C.M.  Jacobs, M.E.  MacDonald and C.O. Laux
FP.19: Rarefied flows and real gas effects III	WeA12 Room: Holiday Inn - Forum 16 Chair: Pénélope Leyland Rapporteur: to be confirmed
Computational analysis of the flowfield past a capsule returning at super-orbital speed A. Viviani and G. Pezzella Fundamental relations on airframe/propulsion integration for supersonic aircraft (*) A.A. Gubanov Reynolds number and surface roughness effects on damping derivatives of the Exomars capsule (*) A. Guelhan, J. Klevanski, M. Dormieaux, P. Tran, J. Merrifield, S. Portigliotti, P. Venditto, L. Walpot and O. Bayle Radiation-ablation coupling for capsule reentry heating via simulation and expansion tube investigations P. Leyland , T. Mcintyre, R. Morgan, F. Zander, U. Sheikh, T. Eichmann, O. Joshi, E. Fahy, G.  Duffa and D. Potter Compressibility effects on the aerodynamic surface quantities of hypersonic gap flows (*) L. Paolicchi and W. Santos Computational analysis of a rarefied hypersonic flow over combined gap/step geometries (*) P. Leite and W. Santos A blunted cone in a supersonic high-enthalpy nonequilibrium supersonic air flow (*) E.B. Vasilevskiy, B.E. Zhestkov, V. Sakharov and V.V. Shtapov
PP.05: Thrust Nozzles	WeA13 Room: Holiday Inn - Forum 10 Chair: Guenter Langel CoChair: David Hirndorf Rapporteur: to be confirmed
Supersonic Splitline Cold Ball &Socket Nozzle for booster and cruise stages J.M. Larrieu and A-L. Ceccarelli Shape optimization of Herschel small nozzles towards a smaller plume divergence G. Markelov A Procedure for Altitude Optimization of Parabolic Nozzle Contours Considering Thrust, Weight and Size W.B.A. van Meerbeeck, B.T.C. Zandbergen and L. Souverein Simulation of Unstable Rarefied Gas Flow in Channels and Nozzles O.A. Aksenova and I.A. Khalidov
PP.12: HRE Modeling	WeA14 Room: Holiday Inn - Forum 11 Chair: Luciano Galfetti CoChair: Olivier Orlandi Rapporteur: to be confirmed
Numerical Simulation of Ignition Process on Boundary Layer Combustion with Chemical Reaction Model S. Yamanaka and T. Shimada Modeling of Liquefying Fuel Regression Rates in Hybrid Propulsion JY Lestrade, J. Anthoine and G. Lavergne Object oriented techniques for the numerical simulation of combustion processes in hybrid rockets A. Mazzetti and P. Barbante Numerical Simulation of Combustion Processes in Hybrid Rocket Engines using OpenFOAM and COOLFluiD codes L. Merotto and A. Mazzetti Nonsteady combustion simulation of 2d hybrid rocket flame F. Maggi, C. Spoto and L. Galfetti Numerical simulation of hybrid rocket engine flowfields D. Bianchi, A. Urbano, B. Betti and F. Nasuti Vortices generation on the wall blowing surface with chemical reactiions (*) K. Mon, C. Lee and H. Koo Analysis of Fluid-dynamic Systems to Increase Combustion Efficiency in Hybrid Rockets M. Lazzarin, N. Bellomo, M. Faenza, F. Barato, A. Bettella and D. Pavarin
17:20 - 18:00 PLENARY SESSION	WeAP Room: Holiday Inn - Forum 1 Chair: to be confirmed Rapporteur: to be confirmed
The Future of Electric Propulsion Systems K. Kreiner
19:30 - 23:30 Conference Dinner+Award
Thursday, July 4th
08:30 - 11:50 TECHNICAL SESSIONS
SI.06: Environment, Energy & Power System Optimization	ThM01 Room: Holiday Inn - Forum 9 Chair: Artur Mirzoyan CoChair: Guillaume Taton Rapporteur: to be confirmed
Thermal Simulation for Cryogenic Storage Systems M. Stubenrauch, V. Gratzl and M. Huber Integration of Novel Electric-Wheel-Driven Hybrid-Electric Propulsion Systems on Standard Short Range Passenger Airplanes (*) M.C. Schwarze Estimation of main parameters for solar-powered long endurance airplane at the preliminary design stage. S.V. Serokhvostov and T.E. Churkina Design of Hybrid-Electric Propulsion Systems for Small Unmanned Aerial Vehicles (*) J Schoemann and M Hornung Digital Integrated Pyrotechnic System L. Renaud , G. Taton, C. Rossi and V. Dubois
FD.6: Launchers and Spacecrafts Guidance	ThM02 Room: Novotel Tegernsee Chair: Alexander V. Nebylov Rapporteur: to be confirmed
Guidance and control law for D-SEND#2. H. Suzuki , T. Ninomiya and J. Kawaguchi Adaptive Guidance Law for Trajectory Control of a Reusable Launch Vehicle during Air-Breathing Ascent Phase V. Brinda, K. Sivan and S. Dasgupta Ascent Trajectory Guidance for an Impulsive Orbit Injection (*) A.L. Nepomuceno Real-time impact control of a solid rocket motor stage during launcher ascent(*) L. Perrot and S. Hervouet Day-of-launch wind biasing trajectory optimization impact on launch vehicles pre-dimensioning methodologies D. Delorme, J. Desmariaux, B.  Carpentier and A. Espinosa Analtical techenquis in astrodynamics W. A Rahoma and F. Deleflie Robust Autonomous Aerobraking Strategies T. Chabot, G. Bonnéry, S. Val Serra, S. Kemble, H. Scheer, F. Forget, T. Voirin, S. Salehi and D. Gherardi
MS.6: Ceramic Matrix Composites and associated Technologies	ThM03 Room: Novotel Chiemsee Chair: Michel Berdoyes Rapporteur: to be confirmed
Advanced Design Concepts for Ceramic Thrust Chamber Components of Rocket Engines M. Ortelt, H. Hald, A. Herbertz and I. Mueller Technology Status of Fuel Cooled Ceramic Matrix Composites for Dual-Mode Ramjet (DMR) and Liquid Rocket Engine (LRE) S. Beyer, S. Schmidt-Wimmer, F. Wigger, K. Quering, M. Bouchez, B. Le Naour, C. Wilhelmi and M. Steinhilber Investigation of heat-resistant materials in supersonic high-temperature flow (*) A.A. Alexeev and P.K. Tretyakov Assessment of uncertainties propagation in a launcher structural sizing chain J. Thay-nam and G. Pinaud Towards a consideration of the uncertainties in flight loads M. Gonzalez, N. Binaud, C. Espinosa, C. Gogu, J. Morlier and S. Quoniam
FP.06: C.A. &.Optimization	ThM04 Room: Holiday Inn - Forum 14 Chair: Jean-Christophe Robinet CoChair: Norman Wood Rapporteur: to be confirmed
Improvement of the cruise performances of a wing by means of aerodynamic optimization. Validation with a far-field method J. Jiménez-Varona and J. Ponsin-Roca Gradient Calculation for Arbitrary Parameterizations via Volumetric NURBS: The Control Box Approach M.J. Martin, E. Andres, E. Valero and C. Lozano Aerodynamic Optimization Design of Airfoil Based on Directly Manipulated FFD Technique J. Bai and S. Chen Conceptual Aerodynamic Design of Martian Airplane K. Manokaran, G. Vidya, S.M. Aravindh Kumar and A.E. Sivaramakrishnan On optimal configuration of lifting bodies taking into consideration the convective heat flux V.I. Lapygin, A.B. Gorshkov, D.M. Fofonov, T.V. Sazonova and V.A. Mikhalin Mathematical model of flight dynamics, internal and external aerodynamics, heating and radiation of hypersonic vehicles E.S. Chuvasheva and S.N. Chuvashev
FP.13: Rarefied flows and real gas effects-I	ThM05 Room: Holiday Inn - Forum 15 Chair: Valeriy Zapryagaev Rapporteur: to be confirmed
Study of catalytic heating effects on metals and quartz for EXOMARS entry conditions (*) A.F. Kolesnikov, A.N. Gordeev and S.A. Vasilevskii Experimental and Numerical Modelling of Heterogeneous Recombination for Martian Entry Conditions R.V. Kovalev, V.I. Vlasov and G.N. Zalogin Influence dispersion in gas-solid interaction for moving body E.V. Prozorova and A.V. Shadrin Hypersonic Flow Analysis Including Finite Rate Ablation Thermochemistry D. Bianchi, F. Nasuti, R. Paciorri and M. Onofri Analytical Model of Translational Nonequilibrium Flow with Internal Degrees of Freedom M.M. Kuznetsov, I.I. Lipatov and L. Smotrova Extension of Lighthill’s gas model for multi-component air (*) R Gartz and H Olivier Ab-initio analysis of the contributions of ER and LH mechanisms in the atomic oxygen recombination on the Al2O3 coating. V.L. Kovalev, A.A. Krupnov and A.A. Buchachenko
FP.20: Wing aerodynamics, wake and vortices	ThM06 Room: Holiday Inn - Forum 16 Chair: Konstantin Volkov CoChair: Jean Muylaert Rapporteur: to be confirmed
Calculations of unsteady flows around high-lift configurations based on a zonal approach S. Bosnyakov, I.A. Kursakov, S. Mikhaylov and V.V. Vlasenko Applying surrogate modelling for dynamic stall simulation V.P. Surpin, A.V. Bernstein and Y.N. Sviridenko Analysis of blowing jets flows on Coanda surfaces to increase the lift of wing or generated power of wind turbine A. Dumitrache, R.  Bogateanu, F. Frunzulica and H. Dumitrescu Application of wavy surface for flow separation elimination on swept wing at low Reynolds number A.V. Kryukov, V.V. Kozlov and I.D. Zverkov Simulations of the vortex development for a steady and unsteady Lambda – wing wind tunnel model S. Wiggen and G. Voß Experimental methods of the study of vortex structures excited by point injection on the leading edge of the oblique wing S.N. Tolkachev, V.N. Gorev, G.M. Zharkova and V.N. Kovrizhina Hypersonic vortex wake behind the wing and its interaction with shock waves A. Shevchenko, A. Kharitonov and A. Shmakov
PP.06: Combustion Stability 1	ThM07 Room: Holiday Inn - Forum 10 Chair: Michael Oschwald CoChair: Changjin Lee Rapporteur: to be confirmed
Numerical simulation of the acoustical properties in rocket combustion chamber. R. Pongratz and D. Redmann Impact of Axial Gradients on Combustion Chamber Acoustics R. Kaess, S. Koeglmeier, R. Behr, B. Kniesner and T.  Sattelmayer Determination of the nozzle admittance in frequency domain for a generic test case M. Schulze, J. Gikadi and T. Sattelmayer Response Characterization of a LOX-GH2 Flame to Forced Acoustic Pressure Fluctuations T. Ramcke, M. Schmid and T. Sattelmayer On the Reflection, Transmission, Coupling and Damping of Non-Plane Acoustic Modes by Resonator Rings (*) A. Cárdenas Miranda and W. Polifke Stability behaviour of a cylindrical rocket engine combustion chamber operated with liquid hydrogen and liquid oxygen (*) S. Gröning, D. Suslov, M. Oschwald and T. Sattelmayer Cryogenic oxygen jet response to transverse acoustic excitation with 1T and 1L1T modes J.S. Hardi and M. Oschwald
PP.13: HRE Solid Fuel	ThM08 Room: Holiday Inn - Forum 11 Chair: Toru Shimada CoChair: Carmine Carmicino Rapporteur: to be confirmed
Experimental study of fragmentation of novel fuel for hybrid rocket (*) K. Kitagawa, Y. Wada, Y. Nakayama, T. Matsumura, K. Wakabayashi, R. Toda, T. Morita and T. Shimada Formulation of a mechanically improved paraffin fuel N. Gerbal, G. Durand, M. Avril, L. Lefranc, A. Ansart, J.  Diakuma, M. Deroo, P. Le Moguedec, G. Sire and G. Poirey Pure paraffin waxes analysis for hybrid rocket solid fuels: rheological, thermal and mechanical characterization M. Boiocchi, E. Toson, S. Gelosa, A. Sliepcevich, L. Galfetti and L.T. DeLuca A wide characterization of paraffin-based fuels mixed with styrene-based thermoplastic polymers for hybrid propulsion M. Boiocchi, P. Milova, A.K. Golovko, L. Galfetti and L.A. Di Landro Ignition and Combustion of HTPB-based Solid Fuels Loaded with Micron-sized Metals (*) Z. Qin, C. Paravan, G. Colombo, L.T. DeLuca and R. Q. Shen Regression Rate Measurements in Lab-Scale Hybrid Burners (*) P. Tadini, C. Paravan, F. Maggi, M. Boiocchi, G.  Colombo and L.T. DeLuca Numerical and Experimental Activities in Support of the Development of Hybrid-Rocket Engines for softlanding applications M. Faenza, F. Moretto, F. Barato, A. Bettella and D. Pavarin Solid fuel regression in hybrid rockets F.M Favarò, M. Manzoni, A. Coronetti, L.T. DeLuca and W.A. Sirignano
11:50 - 12:30 PLENARY SESSION	ThAP Room: Holiday Inn - Forum 12-14 Chair: to be confirmed Rapporteur: to be confirmed
Future energy, Propulsion Operational Challenges – Opportunities for a Disruptive Approach L. Joergensen
12:30 - 14:00 Lunch Break IV	Room: Restaurant Holiday Inn and Novotel
14:00 - 14:40 PLENARY SESSION	ThAP Room: Holiday Inn - Forum 12-14 Chair: to be confirmed Rapporteur: to be confirmed
The European Space programme and its challenges to enabling sciences F. Ongaro UAV, perspectives in Europe and research needs C. Bréant
14:40 - 18:00 TECHNICAL SESSIONS
SI.07: STERN/SL	ThA01 Room: Holiday Inn - Forum 9 Chair: Karsten Lappöhn Rapporteur: to be confirmed
STERN - A Rocket Programme for German Students K. Lappöhn, D. Regenbrecht and D. Bergmann Progress Update of the DLR STERN Project at the University of Stuttgart T. Willerding, M.  Kobald, C. Schmierer, N. Sultesz, K. Tomilin, R. Spiegelhalder, P. Jaworski, S. Schlechtriem and H-P. Röser DECAN (Deutsche CanSat-Höhenrakete) – A Sounding Rocket Project at TU Berlin M. Schmid, P. Fleischer, F. Sliwowski, H. Adirim and N. Pilz SMART Rockets - A contribution to the DLR STERN program by Dresden University of Technology J. Sieder, C. Bach, O. Przybilski and M. Tajmar "AQUASONIC"- A Project in the Frame of the DLR "STERN" Programme U. Apel and J. Beyer The propulsion system of the ZEpHyR - ZARM Experimental Hybrid Rocket: A contribution to the DLR STERN Project by the University of Bremen P. Rickmers, M. Drinkewitz and F. Orlowski Progress report regarding hybrid propulsion rocket development at WARR S. Althapp, C. Blum, A. Chemnitz, D. Eiringhaus, B. Wagner and C. Bauer Using Composite Materials for Hybrid Propelled Ballistic Experimental Rockets M.O. Ellerbeck and T.G. Dirlich Development of a Supersonic Research Rocket with Hybrid Rocket Engine S. May, G. Poppe, M. Pöppelmann, H.P. Sültrop and P. Vörsmann
FD.7: Missiles and Spacecrafts Guidance	ThA02 Room: Holiday Inn - Forum 10 Chair: Daniel Chouckroun Rapporteur: to be confirmed
Spacecraft in High Elliptical Orbit by "Star"-Configured Thrusters V.A. Obukhov, A.I. Pokryshkin, G.A. Popov and V.V. Svotina Low Orbit Operations of ESA’s Gravity Mission GOCE M. Romanazzo, C. Steiger, V.D. Tran, A. Piris Niño, P.P. Emanuelli, R. Floberghagen and M. Fehringer Studies on Guidance Law for Interception Problem of Small Velocity Ratio J. Guo, S.J. Tang and J.H. Xiong Dynamic Modeling of Two-Part Missiles B Özkan, M K Özgören and G Mahmutyazıcıoğlu Firing Control Optimization of Lateral Propellant Impulse Thrusters for Trajectory Correction Rockets G. Min, Z. Yongwei and Y. Suochang The Estimator is the Key Element in Interception Endgames (*) J. Shinar and V. Turetsky
MS.7: Plasticity, Fatigue, Damage and Corrosion	ThA03 Room: Novotel Chiemsee Chair: Anh-Vu Phan Rapporteur: to be confirmed
A plasticity and damage model for fiber reinforced polymers U. Hofer Analysis of the wing box with spliced skin and estimation of the fatigue life for the wing box T. Narendranath Babu and V. Prasanth A prediction methodology for the high cycle fatigue life of hydrogen-loaded structures W. Bouajila, J. Riccius, M. Bruchhausen and B. Fischer Damage identification in composite structures using full-field strain data G. Labeas and C. Katsikeros Structure and mechanical properties of aluminum after shock-wave compaction S.A. Vorozhtsov, S.N. Kulkov and V.F. Komarov Advanced Cryo-Tanks Research in CHATT M. Sippel, A. Kopp, D. Mattsson, A. Fraters and S. Koussios Modelling of corrosion damage of real aircraft structure. V. Jeníček, M. Pazderová, L. Diblíková and J. Macák
FP.07: C.A. Helicopters & others	ThA04 Room: Holiday Inn - Forum 14 Chair: Volf Borovoy CoChair: Ivan Chernyshev Rapporteur: to be confirmed
Aerodynamic Analysis of a Helicopter Fuselage with rotating rotor head R. Reß, M. Grawunder and C. Breitsamter Numerical and experimental investigation of slot-blowing air over a cylinder(*) W. Runge, F. Buysschaert, J. Hayez, F. Carlier, H. Antoine, P. Hendrick, G. Dimitriadis and G. Degrez Helicopter Drag Fuselage- Combined CFD and Experimental Studies V.  Zherekhov , A.  Kusyumov, S. Mikhailov, V.  Pakhov, A. Sungatullin, M.  Valeev, G. Barakos and A. Batrakov Investigation on Wing rock of square section missile T. Yang, Z. Zhong-liang, W. Xi, W. Junqiang and L. Hao On some methods of improvement of aerodynamic characteristics of supersonic flying vehicles (*) A.N. Kravtsov, V.Y. Lunin, T.Y. Melnichuk and A.V. Panushkin Analytical approach to the problem of slender body separation from a cavity or solid surface to a freestream (*) V. Shalaev Integrative Numerical Simulation by Aerodynamics, Flight Dynamics and Flight Control Coupling L. Hao, Z. Zhong-liang, W. Jun-chang and T. Yang Analysis of jet in cross flow interaction with different investigation techniques (*) T. Gawehn, P. Gruhn and A. Gülhan
FP.14: Rarefied flows and real gas effects II	ThA05 Room: Holiday Inn - Forum 15 Chair: Piotr Doerffer CoChair: Louis Souverein Rapporteur: to be confirmed
DSMC Modeling of Rarefied High-Enthalpy CO2/N2 Flows (*) A.N. Shumakova, Y.A. Bondar, A.V. Kashkovsky, M.S. Ivanov and A. Gülhan Scattering kernels analysis based on molecular dynamics computation results A.N. Yakunchikov and V.L. Kovalev Heat Flux and stress tensor in plasma flows with electronic excitation. V.A. Istomin, E.V. Kustova and M.A. Mekhonoshina Vibrational - Chemical Coupling in High-temperature Air Mixture. O.V. Kunova, E.A. Nagnibeda and I.Z. Sharafutdinov Prediction of UV Radiation for Soyuz Descent Vehicle Reentry A.B. Gorshkov Numerical simulation of rarefied two-phase plume flows J. Li, Y.Z. Shi, L. Yan and W. Huang Application of Gaussian Random Field Model of Surface Roughness in Gas Flow Simulation in Channels O.A. Aksenova and I.A. Khalidov Modeling of High-Temperature Weakly Ionized Flows with SMILE++ Software System (*) A.A. Shevyrin, Y.A. Bondar, A.V. Kashkovsky and M.S. Ivanov The Chemical Elemental Demixing in the Simulation of Air Plasma and CO2 Plasma Flows in the Inductive Plasmatron Chamber V.I. Sakharov and D.Yu Khanukaeva
FP.21: Flow Control II Plasmas	ThA06 Room: Holiday Inn - Forum 16 Chair: Ralf Stark CoChair: Vladimir Statnikov Rapporteur: to be confirmed
Investigation of Bow Shock Dispersion on a Blunt body by Counterflow Pulsed Plasma Jets G Matsoukas and N.A. Ahmed Effect of Variation of Thermodynamic Property with Temperature on Modeling of Near-Surface Discharge (*) H. Yan and S. Wang Investigation of flow separation control by nanosecond pulsed dielectric barrier discharge actuators N. Grech, P. Peschke, S. Bustamante, P. Leyland and P. Ott MHD - Control of a Shock - Wave Structure at a Hypersonic Flow (*) V.M. Fomin, V.P. Fomichev and M.A. Yadrenkin Investigation of Multi DBD Plasma Actuators B. Goeksel Comparison of plasma actuator effects under rarefied flow conditions applied to a flat plate and a cylinder V. Lago, A Kudryavtsev and J. D Parisse
PP.07: Combustion Stability 2	ThA07 Room: Holiday Inn - Forum 10 Chair: Thomas Sattelmayer CoChair: Gérard Ordonneau Rapporteur: to be confirmed
Experimental investigation of acoustic energy dissipation in a rectangular combustion chamber S. Webster, J.S. Hardi and M. Oschwald An Experimental Study on the Dynamic Behavior of Premixed Propane/Air Flame Propagating under the Potential Field of Ultrasonic Standing Wave (*) S. S. Lee, H. S. Seo and J. S. Kim Development of Combustion Response Functions in a Subscale High Pressure Transverse Combustor M. Wierman and W. Anderson Modelling Acoustic Excitation of High Frequency Combustion Instability Experiments S. Beinke, J.S. Hardi, M. Oschwald and B. Dally The equations of state of methane, oxygen, and their mixtures: Calculation of the temperature and pressure of the mixture in the combustion chamber of liquid rocket engine before ignition S.M. Frolov, V.V. Kozynda and N.M. Kuznetsov
PP.14: HRE Lab Scale	ThA08 Room: Holiday Inn - Forum 11 Chair: Jouke Hijlkema CoChair: Elisa Cliquet Moreno Rapporteur: to be confirmed
Investigation of a laboratory scale HTP/HTPB hybrid rocket motor P. Wolanski, P. Surmacz, G. Rarata and K. Sobczak Student hybrid thruster testing and research G. Costa, W. Kitsche and L. Padoan Regression rate study in a small Hybrid Rocket Engine using N2O/Paraffin propellant. K. Boughaba and P. Hendrick Rheological, optical and ballistic investigations of paraffin-based fuels for hybrid rocket propulsion using a 2D slab-burner (*) M.  Kobald, E. Toson, H. Ciezki, S. Schlechtriem, S. Di Betta, M. Coppola and L.T. DeLuca Rheological and ballistic investigations of paraffin-based fuels for hybrid rocket propulsion using a 2D radial micro-burner E. Toson, M. Kobald, S. Di Betta, L.T. DeLuca, H. Ciezki and S. Schlechtriem
Friday, July 5th
09:00 - 13:30 Technical Tours	FrMP Room: to be decided Chair: to be confirmed Rapporteur: to be confirmed
Technical Tours to Astrium (Ottobrunn), MTU (Dachau) and MT Aerospace (Augsburg)