•  DOI: 10.13009/EUCASS2019-3
 -  ANALYTICAL MODELING OF CAPILLARY BIPHASIC DEVICES FOR AERONAUTICAL APPLICATIONS
  •  DOI: 10.13009/EUCASS2019-13
 -  A study on effect of transition on High Lift Configuration Aerodynamics
  •  DOI: 10.13009/EUCASS2019-20
 -  Flight Test Analysis and Flight Manual Modelling of the Rolling and Braking Resistance over Unpaved Runways
  •  DOI: 10.13009/EUCASS2019-25
 -  Aerodynamically Generated Acoustic Resonance (AGAR) Model Revisited and Refurbished
  •  DOI: 10.13009/EUCASS2019-32
 -  Design and analysis of an innovative multifunctional cylinder
  •  DOI: 10.13009/EUCASS2019-33
 -  A New Spacecraft Attitude Stabilization Mechanism Using Deep Reinforcement Learning Method
  •  DOI: 10.13009/EUCASS2019-35
 -  Research on Mechanical Environment Prediction Method for Structure Considering Random Uncertain Elastic Joint
  •  DOI: 10.13009/EUCASS2019-38
 -  Design, Development, Validation and Verification of GNC technologies
  •  DOI: 10.13009/EUCASS2019-39
 -  HERA vision based GNC and autonomy
  •  DOI: 10.13009/EUCASS2019-45
 -  Adaptive fast fuzzy integral sliding mode attitude control for reentry vehicle with control input constraints
  •  DOI: 10.13009/EUCASS2019-49
 -  Numerical Study of Hypersonic Wake Flow over Apollo Command Module
  •  DOI: 10.13009/EUCASS2019-50
 -  A novel external thermal protection coating for aerospace vehicles
  •  DOI: 10.13009/EUCASS2019-54
 -  The aerodynamic interference characteristics of TSTO vehicle stage separation
  •  DOI: 10.13009/EUCASS2019-61
 -  Experiments and optimization design of light-weight multilayer TPS
  •  DOI: 10.13009/EUCASS2019-62
 -  Concept Study of S4TD based on Reliability Based Design Optimization
  •  DOI: 10.13009/EUCASS2019-63
 -  Influence of Oscillator Phase Noise in Frequency-Based Location Methods for Mobile Exploration Robots
  •  DOI: 10.13009/EUCASS2019-69
 -  A Landing Buffer System for Vertical Takeoff and Vertical Landing Reusable Launch Vehicle
  •  DOI: 10.13009/EUCASS2019-72
 -  Research on the fatigue life testing for composite wings
  •  DOI: 10.13009/EUCASS2019-77
 -  Analysis of the 3-dimensional draping and permeability characteristics of woven fabric and optimization of the technological process for the complex shape aerospace structures
  •  DOI: 10.13009/EUCASS2019-78
 -  Numerical Simulation of Pitch-Damping Dynamic Derivatives
  •  DOI: 10.13009/EUCASS2019-79
 -  Combustion Modeling in Solid Rocket Motor Plumes
  •  DOI: 10.13009/EUCASS2019-81
 -  Planetary Exploration of Saturn moons Dione and Enceladus
  •  DOI: 10.13009/EUCASS2019-83
 -  Numerical simulation of ice accretion and consequent power loss estimation in wind turbine blades
  •  DOI: 10.13009/EUCASS2019-85
 -  DIAMOND WINGS IN SUPERSONIC FLOW WITH SLIP
  •  DOI: 10.13009/EUCASS2019-86
 -  Simulation of Inflation Driving Deployment of Rolled Elastic Thin Wall Boom with Velcro Constraints
  •  DOI: 10.13009/EUCASS2019-91
 -  Numerical investigation of transpiration cooling in supersonic nozzles
  •  DOI: 10.13009/EUCASS2019-92
 -  Investigation on the supplementary combustion scheme for the divergent section of a solid rocket engine nozzle
  •  DOI: 10.13009/EUCASS2019-93
 -  Wake Measurements of a MAV with Morphing Geometry
  •  DOI: 10.13009/EUCASS2019-94
 -  Differential Game Guidance Law on Evader in Bearing-only Information Applications
  •  DOI: 10.13009/EUCASS2019-95
 -  Structural design and analysis of a composite wing with high aspect ratio
  •  DOI: 10.13009/EUCASS2019-96
 -  Research on Unsteady Plasma Plume by DSMC/PIC Hybrid Algorithms
  •  DOI: 10.13009/EUCASS2019-97
 -  Technology acceleration process for the THEMIS low cost and reusable prototype
  •  DOI: 10.13009/EUCASS2019-99
 -  Estimation and measurement of base heating on Test Launch Vehicle
  •  DOI: 10.13009/EUCASS2019-100
 -  Modeling of the evolution of multiphase flow of combustion products in the chamber of propulsion system
  •  DOI: 10.13009/EUCASS2019-103
 -  Diffusion Effects on Catalytic Measurements in Plasma Wind Tunnels
  •  DOI: 10.13009/EUCASS2019-105
 -  Numerical Simulations of an Isochoric Hybrid Rocket Combustion Chamber and Comparison with Tests
  •  DOI: 10.13009/EUCASS2019-108
 -  Design and optimization of a ducted fan VTOL MAV controlled by Electric Ducted Fans
  •  DOI: 10.13009/EUCASS2019-111
 -  Feature Extraction Algorithms Applied to Turbulent Channel Flow Databases: The Effect of Agglomeration Strategies
  •  DOI: 10.13009/EUCASS2019-117
 -  How to correct the Bréguet range equation taking into account the fuel flow rate of the aircraft?
  •  DOI: 10.13009/EUCASS2019-118
 -  Numerical Simulation of BTI Broadband Noise Reduction with Wavy Leading Edge for Sweep Blade?
  •  DOI: 10.13009/EUCASS2019-119
 -  CHEOPS – first ESA small scientific mission Ready to launch
  •  DOI: 10.13009/EUCASS2019-121
 -  Generation of non-adiabatic flamelet manifolds: comparison of two approaches applied on a single-element GCH4/GO2 combustion chamber
  •  DOI: 10.13009/EUCASS2019-122
 -  Thermo physics process peculiarities of modern air breathing engines
  •  DOI: 10.13009/EUCASS2019-123
 -  Drag reduction control in turbulent channel using spanwise traveling wave of blowing and suction methods
  •  DOI: 10.13009/EUCASS2019-128
 -  Lateral-Directional Aerodynamics of a Re-usable Re-entry Vehicle
  •  DOI: 10.13009/EUCASS2019-129
 -  Multidisciplinary Design of Reusable Re-Entry Vehicles by Optimization and Computational Fluid Dynamics
  •  DOI: 10.13009/EUCASS2019-130
 -  AERODATABASE OF VEGA-C LAUNCHER DEVELOPMENT AND INTEGRATION
  •  DOI: 10.13009/EUCASS2019-131
 -  Aerospace system of preservation of parametric and speech information for the investigation of flight accidents
  •  DOI: 10.13009/EUCASS2019-135
 -  Wind-tunnel investigation of a twin-engine medium transport model equipped with an external blown flap
  •  DOI: 10.13009/EUCASS2019-137
 -  Modelling and Control of Transition Flight of an eVTOL Tandem Tilt-Wing Aircraft
  •  DOI: 10.13009/EUCASS2019-140
 -  Numerical study of side loads generation in over-expanded conical nozzles
  •  DOI: 10.13009/EUCASS2019-141
 -  Design of a Dual-Frequency Patch Antenna for Small Satellites
  •  DOI: 10.13009/EUCASS2019-142
 -  Experimental and Theoretical Analysis of the Combustion Efficiency and the Heat Loads on a N2O/C2H4 Green Propellant Combustion Chamber
  •  DOI: 10.13009/EUCASS2019-144
 -  Experimental investigation of a single element LOX/GCH4 heat-sink combustion chamber
  •  DOI: 10.13009/EUCASS2019-145
 -  Fatigue Behaviour of New Eco-7175 Extruded Aluminium Alloy
  •  DOI: 10.13009/EUCASS2019-147
 -  Comparisons of Different Propeller Wake Models for a Propeller-Wing Combination
  •  DOI: 10.13009/EUCASS2019-150
 -  EXPERIMENTAL AND NUMERICAL INVESTIGATION OF LIQUID FILM COOLING IN SMALL ROCKET ENGINES
  •  DOI: 10.13009/EUCASS2019-152
 -  Oscillating Boundary Layer in Hybrid Rocket Combustion
  •  DOI: 10.13009/EUCASS2019-157
 -  Aerodynamic Database Design and Flight Data Analysis of a Waverider Vehicle
  •  DOI: 10.13009/EUCASS2019-159
 -  A blade configuration study of vertical axis wind turbines using a CFD approach
  •  DOI: 10.13009/EUCASS2019-160
 -  Longitudinal Flight Dynamics Modeling and Stability Analysis of the Flapping Wing Aircraft with Folding Wing
  •  DOI: 10.13009/EUCASS2019-161
 -  MAX Modeling of Integrally Bladed Rotors with Blends, Mistuning, and Prestress
  •  DOI: 10.13009/EUCASS2019-163
 -  Adaptive Control Allocation-based Control Design for Non-affine Morphing Aircraft System
  •  DOI: 10.13009/EUCASS2019-164
 -  L1 Adaptive Backstepping Control of Aircraft under Actuator Failures
  •  DOI: 10.13009/EUCASS2019-165
 -  Analysis of accident precursor data for Mid Air Collision occurrences using expert-build Bayesian Network model and Information Theory
  •  DOI: 10.13009/EUCASS2019-167
 -  Architectured materials for space applications: a computational tool for the parametric optimization of a three-dimensional lattice subjected to stiffness constraints
  •  DOI: 10.13009/EUCASS2019-168
 -  Missile System Design Integrated with System Engineering Methodology
  •  DOI: 10.13009/EUCASS2019-170
 -  Composite Grid Technology Applied to VEGA-C Interstage 2/3
  •  DOI: 10.13009/EUCASS2019-172
 -  Feasibility study of reusable space plane landing with WIG-craft assist
  •  DOI: 10.13009/EUCASS2019-173
 -  Study on atomization characteristics of kerosene jet in crossflow
  •  DOI: 10.13009/EUCASS2019-174
 -  New design methods and results for automatically controlled WIG
  •  DOI: 10.13009/EUCASS2019-175
 -  Multi Objective Horizontal Tail Optimization of a Jet Trainer Aircraft
  •  DOI: 10.13009/EUCASS2019-176
 -  Modelling and Simulation of Very Low Earth Orbits
  •  DOI: 10.13009/EUCASS2019-178
 -  CATAPULT LAUNCHING TESTS OF AN UNMANNED AERIAL VEHICLE WITH A RAMJET PULSED DETONATION ENGINE
  •  DOI: 10.13009/EUCASS2019-180
 -  A Study on the Design of GNSS Using 2-D Lattice Flower Constellation Pattern
  •  DOI: 10.13009/EUCASS2019-181
 -  Influence of Radial Stratification on Eigenfrequency Computations in Rocket Combustion Chambers
  •  DOI: 10.13009/EUCASS2019-183
 -  Study of a Hydro-Pneumatic Buffer with a Variable Damper for Launch Vehicle Landing Legs
  •  DOI: 10.13009/EUCASS2019-184
 -  Turbulence in a supersonic spatial flow over a flat plate
  •  DOI: 10.13009/EUCASS2019-186
 -  Electromechanical Thrust Vector Control Systems for the Vega-C launcher
  •  DOI: 10.13009/EUCASS2019-190
 -  Scaling for Icing Wind Tunnel Tests and Validation with Numerical Simulations
  •  DOI: 10.13009/EUCASS2019-191
 -  Internal Ballistics of a Boron Containing Solid Fuel Ramjet
  •  DOI: 10.13009/EUCASS2019-192
 -  Using Pulsed Laser Ranging to Drastically Improve LEO Orbit Ephemerii
  •  DOI: 10.13009/EUCASS2019-193
 -  Fire Resistance of Aeronautical Composite Materials under Reduced Pressure Conditions
  •  DOI: 10.13009/EUCASS2019-194
 -  Perspectives of electromagnetic railgun application as plasma engine for spacecrafts
  •  DOI: 10.13009/EUCASS2019-195
 -  Hypersonic Entry Guidance and Bézier Curves
  •  DOI: 10.13009/EUCASS2019-197
 -  FROG, a Rocket for GNC demonstrations: Firsts flights attempts of the FROG turbojet version and preparation of the future mono-propellant rocket engine
  •  DOI: 10.13009/EUCASS2019-198
 -  Inspection schedule adjustments through Monte Carlo Analysis
  •  DOI: 10.13009/EUCASS2019-199
 -  Reaction time evaluation for events governed by wear out process
  •  DOI: 10.13009/EUCASS2019-200
 -  Experiments on Görtler vortices of controllable intensity in a hypersonic compression corner flow
  •  DOI: 10.13009/EUCASS2019-201
 -  Effect of pressure gradient on stability of small disturbances in supersonic boundary-layer flows
  •  DOI: 10.13009/EUCASS2019-202
 -  Computational study of Al droplet combustion in a burning solid propellant environment
  •  DOI: 10.13009/EUCASS2019-204
 -  Modulation of the Spray Jet of a Swirl Injector
  •  DOI: 10.13009/EUCASS2019-206
 -  Microstructural study of nickel-based superalloys through open source software of image analysis.
  •  DOI: 10.13009/EUCASS2019-208
 -  FLPP ETID: TRL6 reached for Enabling Technologies for Future European Upper Stage Engines
  •  DOI: 10.13009/EUCASS2019-209
 -  HERA autonomous Guidance, Navigation and Control experiments: enabling better asteroid science & future missions
  •  DOI: 10.13009/EUCASS2019-211
 -  Drag and Entropy Variables
  •  DOI: 10.13009/EUCASS2019-214
 -  Characterization of miniature Hall thruster plume in the 50-200 W power range
  •  DOI: 10.13009/EUCASS2019-215
 -  Optimal multi-impulse space rendezvous considering limited impulse using a discretized Lambert problem combined with evolutionary algorithms
  •  DOI: 10.13009/EUCASS2019-216
 -  Control law design for the Callisto demonstrator
  •  DOI: 10.13009/EUCASS2019-217
 -  Aerodynamic design of a Martian micro air vehicle
  •  DOI: 10.13009/EUCASS2019-218
 -  GNC Operations for the BepiColombo Mission to Mercury: First In-flight Experience
  •  DOI: 10.13009/EUCASS2019-220
 -  Optimization of allocation of areas for the falling of the worked-off stages boosters of the launch vehicle based on zoning and classification of the existing impact areas of Baikonur cosmodrome
  •  DOI: 10.13009/EUCASS2019-222
 -  Component tests of a LOX/methane full-expander cycle rocket engine: Electrically actuated valve
  •  DOI: 10.13009/EUCASS2019-223
 -  Component tests of a LOX/methane full-expander cycle rocket engine: Injector and regeneratively cooled combustion chamber
  •  DOI: 10.13009/EUCASS2019-224
 -  Simulating vibrated fluids and vibroequilibria in the CFVib microgravity experiment
  •  DOI: 10.13009/EUCASS2019-228
 -  Investigation of a European Reusable VTVL First Stage Jascha Wilken
  •  DOI: 10.13009/EUCASS2019-229
 -  Multiphase Baer-Nunziato type models for the simulation of self-pressurizing tanks
  •  DOI: 10.13009/EUCASS2019-230
 -  The Verifications and Demonstrations of Self-disintegration Fuel Concept for Hybrid Propulsion
  •  DOI: 10.13009/EUCASS2019-231
 -  Multipurpose solenoid valve for pneumatic and hydraulic systems of launch vehicles liquid propellant engines
  •  DOI: 10.13009/EUCASS2019-232
 -  Optimal guidance for Toss Back concepts of Reusable Launch Vehicles
  •  DOI: 10.13009/EUCASS2019-234
 -  A point of view about the control of a reusable engine cluster
  •  DOI: 10.13009/EUCASS2019-235
 -  Interaction of Energy Discharge and Hypersonic Vehicle
  •  DOI: 10.13009/EUCASS2019-236
 -  Mathematical modeling of transient processes during startup of main liquid propellant engine under hot test conditions
  •  DOI: 10.13009/EUCASS2019-238
 -  3D printed acoustic igniter of oxygen-kerosene mixtures for aerospace applications
  •  DOI: 10.13009/EUCASS2019-240
 -  The Influence of Meteorological Conditions on the Icing Performance Penalties on a UAV Airfoil
  •  DOI: 10.13009/EUCASS2019-241
 -  Integrated Navigation using MEMS-based Inertial, GPS and Sun Vector Measurements
  •  DOI: 10.13009/EUCASS2019-242
 -  Novel gelled fuels containing nanoparticles as hypergolic bipropellants with HTP
  •  DOI: 10.13009/EUCASS2019-243
 -  Launcher Vehicle Aerothermodynamics and Fairing Separation Altitude Effects on Payload Temperature
  •  DOI: 10.13009/EUCASS2019-244
 -  Optimization of the base bleed to control trailing edge flows in a wide range of Mach numbers
  •  DOI: 10.13009/EUCASS2019-246
 -  Effects of Cavities on Pressure Fluctuation Characteristics of Hypersonic Vehicle Wall Plate
  •  DOI: 10.13009/EUCASS2019-247
 -  Experimental Study on Thermal Decomposition of Several Kerosene Fuels
  •  DOI: 10.13009/EUCASS2019-248
 -  Derivation of Buckling Knockdown Factors Using The Equivalent Model for Isogrid-Stiffened Cylinders
  •  DOI: 10.13009/EUCASS2019-251
 -  3D Conjugate Heat Transfer Analysis of a 100 kN Class Liquid Rocket Combustion Chamber
  •  DOI: 10.13009/EUCASS2019-252
 -  Wall-Modeled Large Eddy Simulation for Predicting Wall Heat Flux in a Rocket Combustion Chamber
  •  DOI: 10.13009/EUCASS2019-254
 -  Combined experimental and calculation method for sonic boom investigation
  •  DOI: 10.13009/EUCASS2019-257
 -  Characterization under Uncertainty of Catalytic Phenomena in Ceramic Matrix Composites Materials for Spacecraft Thermal Protection Systems
  •  DOI: 10.13009/EUCASS2019-258
 -  Fragmentation and formation of the condensed products during combustion of titanium particles in air
  •  DOI: 10.13009/EUCASS2019-259
 -  Near-field sonic boom signature measurement system for AVIC ARI’s FL-60 wind tunnel
  •  DOI: 10.13009/EUCASS2019-260
 -  Combustion characteristics of model composite propellants containing boron and its compounds
  •  DOI: 10.13009/EUCASS2019-261
 -  Some aspects of transonic flutter of aircraft with laminar wings
  •  DOI: 10.13009/EUCASS2019-262
 -  Reusable Structures for CALLISTO
  •  DOI: 10.13009/EUCASS2019-264
 -  Numerically Efficient Fatigue Life Prediction of Rocket Combustion Chambers using Artificial Neural Networks
  •  DOI: 10.13009/EUCASS2019-268
 -  Composite Optimization Techniques for Aircraft Components Structural Sizing
  •  DOI: 10.13009/EUCASS2019-269
 -  A Sliding Mode Control in a Backstepping Setup for Rendezvous Mission on a Circular Orbit
  •  DOI: 10.13009/EUCASS2019-270
 -  3D Printed Control Surface for UAVs
  •  DOI: 10.13009/EUCASS2019-274
 -  ZDES of an Ariane 6 PPH configuration with incidence angle using Zonal Immersed Boundary Conditions
  •  DOI: 10.13009/EUCASS2019-275
 -  New Control Functionalities for Launcher Load Relief in Ascent and Descent Flight
  •  DOI: 10.13009/EUCASS2019-276
 -  Advanced Propellants for Space Propulsion – A Task within the DLR Interdisciplinary Project "Future Fuels"
  •  DOI: 10.13009/EUCASS2019-279
 -  Atomization and combustion of a single unlike-triplet spray of storable bipropellants: hydrogen peroxide with ethanol or alkanes
  •  DOI: 10.13009/EUCASS2019-280
 -  Development of a Bonded Eurofighter Airbrake Flight Demonstrator
  •  DOI: 10.13009/EUCASS2019-282
 -  Filter design using an iterative Hilbert transform scheme
  •  DOI: 10.13009/EUCASS2019-283
 -  Modeling and Control of Propellant Slosh Dynamics in Observation Spacecraft with Actuator Saturations
  •  DOI: 10.13009/EUCASS2019-284
 -  Guidance and Control Strategy for the CALLISTO Flight Experiment
  •  DOI: 10.13009/EUCASS2019-288
 -  Numerical Analysis of Aerodynamic Instability for HAYABUSA Type Reentry Capsule
  •  DOI: 10.13009/EUCASS2019-289
 -  Simulations of turbulence screens for flow and noise control in tandem cylinders
  •  DOI: 10.13009/EUCASS2019-290
 -  Advanced methodologies for conceptual design of commercial aircraft empennages
  •  DOI: 10.13009/EUCASS2019-291
 -  Anomalous Mesh Dependence of Adjoint Solutions Near Walls in Inviscid Flows Past Configurations with Sharp Trailing Edges
  •  DOI: 10.13009/EUCASS2019-293
 -  Cooling effect of gas injected through a non-symmetric slit of the wedge leading edge in a high speed flow
  •  DOI: 10.13009/EUCASS2019-295
 -  Multirow flutter in low pressure turbines: Comparison of different blade configurations
  •  DOI: 10.13009/EUCASS2019-297
 -  Experimental determination of thermodynamic properties of Hydrazine, MMH and NTO along the saturation line up to the critical point
  •  DOI: 10.13009/EUCASS2019-300
 -  Numerical investigation of jet-wake interaction for a generic space launcher with a dual-bell nozzle
  •  DOI: 10.13009/EUCASS2019-301
 -  Component tests of a LOX/methane full-expander cycle rocket engine: Single-shaft LOX/methane turbopump
  •  DOI: 10.13009/EUCASS2019-302
 -  An Automation Language for Increasing Repeatability in Scaled Flight Testing of New Aircraft Configurations
  •  DOI: 10.13009/EUCASS2019-303
 -  Implementation of market price and raw material cost analysis in an MDO environment for unmanned aircraft
  •  DOI: 10.13009/EUCASS2019-306
 -  2019 BRAIA SCHOLARS’ WORKSHOP UAV influence in the emissions of airborne cargo transportation
  •  DOI: 10.13009/EUCASS2019-307
 -  SABRE TECHNOLOGY DEVELOPMENT: STATUS AND UPDATE
  •  DOI: 10.13009/EUCASS2019-308
 -  Improvement of the Aerospace Composite Manufacturing Process using MWCNTs Fibres
  •  DOI: 10.13009/EUCASS2019-310
 -  Contactless suspension for cryogenic applications
  •  DOI: 10.13009/EUCASS2019-311
 -  Investigation of RANS turbulence models for cryogenic rocket combustion chambers
  •  DOI: 10.13009/EUCASS2019-313
 -  Standardization of Thermal Interface for Future Space Missions
  •  DOI: 10.13009/EUCASS2019-314
 -  Ideal Geometries and Potential Benefit of Variable Pitot Inlets for Subsonic and Supersonic Business Aviation
  •  DOI: 10.13009/EUCASS2019-315
 -  Development of the liquid oxygen and methane M10 rocket engine for the Vega-E upper stage
  •  DOI: 10.13009/EUCASS2019-318
 -  Experimental Investigations for the Thermal Qualification of High Speed Missile Radomes
  •  DOI: 10.13009/EUCASS2019-320
 -  Reverse Engineering with LsDyna and Nastran SOL 400 for an unexpected structural event during a Test Flight campaign for Parachutist drop tests
  •  DOI: 10.13009/EUCASS2019-322
 -  Vortex Generators and Active Flow Control in the aft-deck of a Frigate
  •  DOI: 10.13009/EUCASS2019-323
 -  Methodology for the thermal analysis of instrumentation in Long Duration Balloon missions
  •  DOI: 10.13009/EUCASS2019-324
 -  Additive Manufacturing (AM). Status in Airbus Defence and Space (Spain)
  •  DOI: 10.13009/EUCASS2019-326
 -  CHARACTERIZATION OF THE WIND FLOW ON THE FLIGHT DECK OF A FRIGATE
  •  DOI: 10.13009/EUCASS2019-327
 -  Adaptive transonic wings – a new challenge in designing and testing
  •  DOI: 10.13009/EUCASS2019-328
 -  A Combined Experimental and Computational Study of Jet Engine Combustion – Baseline Engine Operation
  •  DOI: 10.13009/EUCASS2019-329
 -  The numerical and experimental studies on the over-wing-engine configurations aerodynamics
  •  DOI: 10.13009/EUCASS2019-330
 -  Experimental investigation of the aluminum combustion in SRM representative gas species: effect of CO2 / CO
  •  DOI: 10.13009/EUCASS2019-331
 -  Imperfection sensitivity analysis for Buckling of thin cylindrical shell submitted to axial harmonic compression
  •  DOI: 10.13009/EUCASS2019-332
 -  Simulations and linear stability analysis of vortex shedding angle in solid rocket motors
  •  DOI: 10.13009/EUCASS2019-333
 -  Roll angle effects on the asymmetric flow over axisymmetric bodies
  •  DOI: 10.13009/EUCASS2019-334
 -  Numerical Study of Variable-Camber Wing via Drag Decomposition Method
  •  DOI: 10.13009/EUCASS2019-335
 -  Sizing and Optimization of the Horizontal Tail of a Jet Trainer
  •  DOI: 10.13009/EUCASS2019-337
 -  3DoF simulation model and specific aerodynamic control capabilities for a SpaceX’s Starship-like atmospheric reentry vehicle
  •  DOI: 10.13009/EUCASS2019-338
 -  Numerical results of modal coupling in the UPMSat-2 structure
  •  DOI: 10.13009/EUCASS2019-342
 -  Gas injection effect on heat transfer and boundary layer instability for space vehicles
  •  DOI: 10.13009/EUCASS2019-345
 -  Interface Designs between TPS and Cryogenic Propellant Tank of an RLV Booster Stage
  •  DOI: 10.13009/EUCASS2019-346
 -  Development of a functionally graded material for new combustion chambers at ultra-high temperature under oxidising atmosphere
  •  DOI: 10.13009/EUCASS2019-348
 -  Lift Forces, Heat Fluxes and Self-Sustained Oscillations over Supersonic Bodies under Asymmetric Energy Deposition
  •  DOI: 10.13009/EUCASS2019-349
 -  Health Monitoring for Cryogenic Tank Foam Insulations on Reusable Rocket Launch Vehicles
  •  DOI: 10.13009/EUCASS2019-350
 -  First Wind Tunnel Data of CALLISTO Reusable VTVL Launcher First Stage Demonstrator
  •  DOI: 10.13009/EUCASS2019-351
 -  Performance and robustness trade-off capabilities for the VEGA launcher TVC system
  •  DOI: 10.13009/EUCASS2019-352
 -  Laminar to Turbulent Transition with Transport Equation on 2D and 3D Incompressible Flows
  •  DOI: 10.13009/EUCASS2019-353
 -  Simulations of turbulent combustion and wall heat transfer in single and multi injectors GCH4/GOx rocket combustors
  •  DOI: 10.13009/EUCASS2019-354
 -  Optimal Design and Process Simulation for Additive Manufacturing
  •  DOI: 10.13009/EUCASS2019-355
 -  The effect of pressure on transcritical jets: a DNS study
  •  DOI: 10.13009/EUCASS2019-357
 -  Preparation, evaluation and characterization of catalytic beds for a trigas chemical propulsion thruster
  •  DOI: 10.13009/EUCASS2019-358
 -  MIURA1: The Reusable Sounding Rocket. Recovery and Reusability Strategies
  •  DOI: 10.13009/EUCASS2019-359
 -  Computational Analysis of Urban Air Mobility Vehicles
  •  DOI: 10.13009/EUCASS2019-360
 -  Numerical Investigation of a Resonance Ignition System
  •  DOI: 10.13009/EUCASS2019-362
 -  Numerical Solution of Supersonic Gas-Solid Two Phase Flow
  •  DOI: 10.13009/EUCASS2019-366
 -  Collision avoidance multi-vehicle distributed cooperative guidance strategy with high performance communication
  •  DOI: 10.13009/EUCASS2019-368
 -  The effect of single defect of RDX crystal on shock sensitivity of RDX/Al mixtures by ReaxFF-MD simulations
  •  DOI: 10.13009/EUCASS2019-370
 -  The Epsilon Guidance and Control System Contributing to the High Accuracy Injection into the Orbit of the Flights
  •  DOI: 10.13009/EUCASS2019-371
 -  Nonlinear random response analyses of composite panels under combined supersonic aerodynamic, thermal, and acoustic loads
  •  DOI: 10.13009/EUCASS2019-373
 -  The confirmation of thermal boundary parameters of the Gas Oxygen Kerosene Rich Fueled rocket engine wall
  •  DOI: 10.13009/EUCASS2019-379
 -  Investigating the Aerodynamic Interference of Control Surfaces by Artificial Neural Networks
  •  DOI: 10.13009/EUCASS2019-380
 -  Experimental and Computational Analysis of Single Crystal Piezoelectrical Driven Synthetic Jet Actuator
  •  DOI: 10.13009/EUCASS2019-381
 -  Assessment of 4D-trajectories predictability and reliability
  •  DOI: 10.13009/EUCASS2019-382
 -  Implementation of CCSDS Hyperspectral Image Compression Algorithm on FPGA on board a nanosatellite
  •  DOI: 10.13009/EUCASS2019-384
 -  Influence of the plate leading-edge shape and thickness on the boundary layer laminar-turbulent transition at Mach number M=5
  •  DOI: 10.13009/EUCASS2019-385
 -  Focused research on RLV-technologies: the DLR project AKIRA
  •  DOI: 10.13009/EUCASS2019-386
 -  Experimental comparison of attitude controllers for nanosatellites
  •  DOI: 10.13009/EUCASS2019-388
 -  Chance-Constrained Optimal Altitude Control of a Rocket
  •  DOI: 10.13009/EUCASS2019-398
 -  Quasi-Static and Dynamic Response of a 1U Nano-Satellite during Launching
  •  DOI: 10.13009/EUCASS2019-400
 -  The Research of the Application of Spatial Interpolation Methods in the Two-Body Proximity Test Data of TSTO
  •  DOI: 10.13009/EUCASS2019-403
 -  Design of Experiment Method in Objective Space for Machine Learning of Flow Structures
  •  DOI: 10.13009/EUCASS2019-404
 -  Fast Homotopy Method for Binary Asteroid Landing Trajectory Optimization
  •  DOI: 10.13009/EUCASS2019-411
 -  Comparison of Various Parachute Deployment Systems for Full Rocket Recovery of Sounding Rockets
  •  DOI: 10.13009/EUCASS2019-413
 -  Evaluation of Probe-Material Thermal Interaction in Plasma Wind Tunnel Tests by Means of IR Thermography and Thermal Inverse Modelling
  •  DOI: 10.13009/EUCASS2019-416
 -  Industrial benchmark simulations of detached flows using XFlow
  •  DOI: 10.13009/EUCASS2019-418
 -  Investigation of Flashing LN2-Jets in Terms of Spray Morphology, Droplet Size and Velocity Distributions
  •  DOI: 10.13009/EUCASS2019-419
 -  An Autonomous Maneuvering Decision Algorithm of UAV Based on Deep Deterministic Policy Gradient under Endpoint Constraints
  •  DOI: 10.13009/EUCASS2019-420
 -  Secondary resonances due to the solar radiation pressure in the vicinity of the global navigation satellites regions
  •  DOI: 10.13009/EUCASS2019-421
 -  Reusable stage concepts design tool
  •  DOI: 10.13009/EUCASS2019-422
 -  Vibration Reduction Simulation of Lift-offset Compound Helicopters Using Active Vibration Control System
  •  DOI: 10.13009/EUCASS2019-423
 -  A DNS study of DBD plasma actuators to generate a spatially oscillated spanwise body force to reduce the drag in channel
  •  DOI: 10.13009/EUCASS2019-424
 -  A Multi-UAV Collaborative Real-time Path Planning Method Under Time-space Constraints
  •  DOI: 10.13009/EUCASS2019-425
 -  Characterization of dynamic hydroplaning speed for large transport aircraft equipped with a multi-row main landing gear
  •  DOI: 10.13009/EUCASS2019-427
 -  UV and VUV emission measurements in an ICP torch facility
  •  DOI: 10.13009/EUCASS2019-428
 -  Post-Flight Evaluation of the Guidance and Control for Re-entry Capsule “HSRC”
  •  DOI: 10.13009/EUCASS2019-429
 -  Unmanned vs manned Aircraft Systems accidents investigation: post-accident analysis, benchmarking and improvements
  •  DOI: 10.13009/EUCASS2019-430
 -  A Convex Approach to Rocket Ascent Trajectory Optimization
  •  DOI: 10.13009/EUCASS2019-432
 -  Use of ROM Based Methods in the Determination of Gas Turbine Engines Health Condition.
  •  DOI: 10.13009/EUCASS2019-434
 -  The High Level of Maturity of the elsA CFD Software for Aerodynamics Applications
  •  DOI: 10.13009/EUCASS2019-436
 -  Mission Analysis and Preliminary Re-entry Trajectory Design of the DLR Reusability Flight Experiment ReFEx
  •  DOI: 10.13009/EUCASS2019-438
 -  A Systematic Comparison of Reusable First Stage Return Options
  •  DOI: 10.13009/EUCASS2019-439
 -  An Investigation into Injector Architecture for SubNewton Monopropellant Propulsion
  •  DOI: 10.13009/EUCASS2019-441
 -  Design of a low-thrust assisted trajectory to Saturn
  •  DOI: 10.13009/EUCASS2019-442
 -  Collection and stabilization of low-orbit small satellites in the formation
  •  DOI: 10.13009/EUCASS2019-444
 -  Efficiency of the thermal energy storage made of lunar regolith
  •  DOI: 10.13009/EUCASS2019-445
 -  Laminar boundary layer self-induced separation in transonic flow
  •  DOI: 10.13009/EUCASS2019-447
 -  Flow visualization at extremely low Reynolds number
  •  DOI: 10.13009/EUCASS2019-448
 -  Design of Multiple Winglets for Enhancing Aerodynamics in a Micro Air Vehicle.
  •  DOI: 10.13009/EUCASS2019-449
 -  Experimental study of the effect of the reduced frequency in the airfoil`s aerodynamic characteristics
  •  DOI: 10.13009/EUCASS2019-453
 -  Iterative Learning Control for Precise Aircraft Trajectory Tracking in Continuous Descent Approaches
  •  DOI: 10.13009/EUCASS2019-454
 -  Conceptual design of a Two-Stage-To-Orbit vehicle using SABRE engines
  •  DOI: 10.13009/EUCASS2019-455
 -  Two-phase gas-particle flow over bodies: modelling and simulation of random effects
  •  DOI: 10.13009/EUCASS2019-457
 -  CONCEPTUAL DESIGN OF NEW HEAVY TRANSPORT AIRCRAFT
  •  DOI: 10.13009/EUCASS2019-460
 -  IEMN/LEMAC-LICS Magneto-mechanical micro-actuators and active flow control: review of the last 15 years results
  •  DOI: 10.13009/EUCASS2019-461
 -  Application of CFD to WIG-craft motion control system design
  •  DOI: 10.13009/EUCASS2019-462
 -  Combustion Instability for Hybrid Rocket Motors with a Diaphragm
  •  DOI: 10.13009/EUCASS2019-464
 -  Thermal pressure high temperature gradient micro-sensor for aerodynamic measurements
  •  DOI: 10.13009/EUCASS2019-465
 -  ACTiVE – Experimental set up and first results of cold gas measurements for linear aerospike nozzles with secondary fluid injection for thrust vectoring
  •  DOI: 10.13009/EUCASS2019-466
 -  MEMS calorimetric transducers for flow separation detection and control
  •  DOI: 10.13009/EUCASS2019-469
 -  Impulsive Multi-Rendezvous Trajectory Design and Optimization
  •  DOI: 10.13009/EUCASS2019-473
 -  Experimental Investigation of Showerhead injectors on Performance of a 1-kN Paraffin-Fueled Hybrid Rocket Motor
  •  DOI: 10.13009/EUCASS2019-476
 -  Finding the Parameters of Surface Roughness in Rarefied Gas Flow Solving the Inverse Problem
  •  DOI: 10.13009/EUCASS2019-479
 -  Direct Numerical Simulation of heat transfer in SMSP regenerative combustion chamber
  •  DOI: 10.13009/EUCASS2019-480
 -  ReFEx launch with a sounding rocket – a challenging mission on a reliable carrier
  •  DOI: 10.13009/EUCASS2019-482
 -  Tunable Diode Laser Absorption Tomography for characterization of chemical species in aeronautical flames
  •  DOI: 10.13009/EUCASS2019-483
 -  Improving safety requirements of the launch complex by developing modified launch vehicle control algorithms at the initial flight part
  •  DOI: 10.13009/EUCASS2019-485
 -  Compressive response and failure of a micromechanical model for confined unidirectional fiber-reinforced composites
  •  DOI: 10.13009/EUCASS2019-488
 -  THEORETICAL PERFORMANCE ANALYSIS OF HYBRID ROCKET PROPELLANTS AIMING AT THE DESIGN OF A TEST BENCH AND A PROPULSIVE SYSTEM
  •  DOI: 10.13009/EUCASS2019-490
 -  Modified-Polygon Method for Point-in-Polygon Problem
  •  DOI: 10.13009/EUCASS2019-492
 -  Optimisation in Active Flow Separation Control in Low-Pressure Turbines
  •  DOI: 10.13009/EUCASS2019-494
 -  Cessna Citation X Static Cruise Improvement using Morphing Wing Application on its Horizontal Tail
  •  DOI: 10.13009/EUCASS2019-495
 -  STUDY OF THE SHIELDING PERFORMANCE OF WHIPPLE SHIELD ENHANCED BY IMPEDANCE-GRADED MATERIALS
  •  DOI: 10.13009/EUCASS2019-496
 -  Methodology to Identify a Mathematical Model for Predicting Cessna Citation X Cruise Performance in Cruise Regime using Flight Manual Data
  •  DOI: 10.13009/EUCASS2019-502
 -  Development of Computational and Experimental Methods for Determining Dynamic Characteristics of Aircraft Landing Gear
  •  DOI: 10.13009/EUCASS2019-503
 -  Role of combustion modeling in the prediction of heat transfer in LRE thrust chambers
  •  DOI: 10.13009/EUCASS2019-504
 -  Computational Design of a CubeSat Compatible Re-entry Capsule
  •  DOI: 10.13009/EUCASS2019-505
 -  Three-dimensional adaptive neural network guidance law against maneuvering targets
  •  DOI: 10.13009/EUCASS2019-507
 -  Application of hybrid numerical schemes in prediction of high-speed laminar-turbulent transition
  •  DOI: 10.13009/EUCASS2019-508
 -  Development of new analytical models for pressure and heat flux distributions on space debris afterbodies
  •  DOI: 10.13009/EUCASS2019-509
 -  Lithium-sulphur batteries: opportunities and challenges for space applications
  •  DOI: 10.13009/EUCASS2019-510
 -  Design of the trajectory of a tether mission to Saturn
  •  DOI: 10.13009/EUCASS2019-512
 -  A Timescale-Augmented Spalart-Allmaras Turbulence Model for Flamelet Combustion Applications
  •  DOI: 10.13009/EUCASS2019-514
 -  Experimental Study on Jet Acoustics of Subscale Rocket Nozzles with a Different Divergent Contour Design
  •  DOI: 10.13009/EUCASS2019-515
 -  DLR Project TAUROS: TAU for Rocket Thrust Chamber Simulation
  •  DOI: 10.13009/EUCASS2019-516
 -  Experimental Flow Path Analysis of a Hydrogen Transpiration Cooled Model Scramjet Combustor
  •  DOI: 10.13009/EUCASS2019-517
 -  NEMS and MEMS technologies in RLV maintenance operations
  •  DOI: 10.13009/EUCASS2019-518
 -  Smart Operations in ATEX RLV Environment
  •  DOI: 10.13009/EUCASS2019-519
 -  Reynolds number influence on the hysteresis behavior of a dual-bell nozzle
  •  DOI: 10.13009/EUCASS2019-521
 -  Development of a Reliable Performance Gas Generator of 75 tonf-class Liquid Rocket Engine for the Korea Space Launch Vehicle II
  •  DOI: 10.13009/EUCASS2019-522
 -  Numerical Simulation of Instabilities Evolution in a High-Speed Boundary Layer with Crossflow Jet Injection
  •  DOI: 10.13009/EUCASS2019-525
 -  Definition of a Configuration Module for a Concurrent Design Facility
  •  DOI: 10.13009/EUCASS2019-528
 -  Transient Model of API Injector Using EcoSimPro for Expander Bleed Engine Application
  •  DOI: 10.13009/EUCASS2019-530
 -  Experimental Study of the Natural Disturbance Evolution in a Swept Wing Boundary Layer with Periodic Spanwise Roughness at Mach 2 and 2.5
  •  DOI: 10.13009/EUCASS2019-532
 -  Semi-analytical Method for Active Removal of Space Debris with Electrodynamics Tether System
  •  DOI: 10.13009/EUCASS2019-533
 -  Optimal large-scale object selection and trajectory planning for active space debris removal missions
  •  DOI: 10.13009/EUCASS2019-536
 -  Strategies for high performance GNSS/IMU Guidance, Navigation and Control of Rocketry
  •  DOI: 10.13009/EUCASS2019-537
 -  Sensitivity of Spin Parameters to Uncertainties of the Aerodynamic Model of a Light Aircraft
  •  DOI: 10.13009/EUCASS2019-538
 -  Theoretical and Experimental Study of Combustion Instability in Hybrid Rocket Motors
  •  DOI: 10.13009/EUCASS2019-541
 -  Testing 1kN Paraffin-Based Hybrid Rocket Engine
  •  DOI: 10.13009/EUCASS2019-544
 -  Optimal 4D Trajectory Planning for Multiple Aircraft in Continuous Descent Operations
  •  DOI: 10.13009/EUCASS2019-546
 -  Optimization and Model Order Reduction on Launch Vehicle Aerodynamic Design
  •  DOI: 10.13009/EUCASS2019-547
 -  Solid Rocket Motors for the De-Orbiting of Satellites
  •  DOI: 10.13009/EUCASS2019-548
 -  Boundary layer evolution in channel behind the shock wave
  •  DOI: 10.13009/EUCASS2019-549
 -  Autonomous multi-target rendezvous mission planning using artificial intelligence
  •  DOI: 10.13009/EUCASS2019-550
 -  A hybrid genetic algorithm with local search approach for composite structures optimization
  •  DOI: 10.13009/EUCASS2019-551
 -  Optimization and Application of Cryogenic/Thermal Insulation Design for a Liquid-propellant Rocket Engine
  •  DOI: 10.13009/EUCASS2019-552
 -  Preliminary results concerning the development of a waterpropellant vaporizing liquid microthruster for small satellites
  •  DOI: 10.13009/EUCASS2019-553
 -  Non-Linear Model Identification Analysis for a TVC Electro-Hydraulic Actuator
  •  DOI: 10.13009/EUCASS2019-555
 -  An application of HODMD to predict flutter using NeoCASS
  •  DOI: 10.13009/EUCASS2019-559
 -  Influence of numerical model setup on the response of acoustically forced LOx/H2 flames
  •  DOI: 10.13009/EUCASS2019-562
 -  Nanosatellite Development Methodology and Preliminary Design Guides for the NANOSTAR Project
  •  DOI: 10.13009/EUCASS2019-563
 -  Atomization chill-down demonstrator for the next generation cryogenic rocket engines: experiments and first results
  •  DOI: 10.13009/EUCASS2019-564
 -  Investigation of controlled disturbances development from two sources in supersonic boundary layer
  •  DOI: 10.13009/EUCASS2019-565
 -  Data analysis for damage identification in CFRP stiffened structures using guided Lamb waves with PZT sensors
  •  DOI: 10.13009/EUCASS2019-574
 -  Performance Characteristics of the Hundreds-Newton Class Thruster Using Gaseous Methane and Liquid Oxygen as Propellants
  •  DOI: 10.13009/EUCASS2019-575
 -  Investigation of laminar-turbulent transition of 2D supersonic boundary layer by scanning constant temperature hot-wire anemometer
  •  DOI: 10.13009/EUCASS2019-576
 -  Supersonic Flow past a Blunt Cone under the Action of Plasma Formation
  •  DOI: 10.13009/EUCASS2019-577
 -  Output feedback control for optimal propellantless formation keeping using Electrostatic forces
  •  DOI: 10.13009/EUCASS2019-578
 -  Assessment of aircraft conceptual design tools towards the synthesis of Remotely Piloted Aircraft platforms
  •  DOI: 10.13009/EUCASS2019-581
 -  Extension of a Non-Adiabatic Flamelet Combustion Model for Composition Predictions in Thermal Boundary Layers
  •  DOI: 10.13009/EUCASS2019-583
 -  Laser Ignition and Combustion Study of KNO3-Sorbitol based Solid Propellant
  •  DOI: 10.13009/EUCASS2019-584
 -  ReFEx: Reusability Flight Experiment – A Project Overview
  •  DOI: 10.13009/EUCASS2019-586
 -  Experimental validation of an aeroelastic reduced order model dedicated to high aspect ratio flexible composite wing
  •  DOI: 10.13009/EUCASS2019-590
 -  Evaluation of Nonlinear Elements Effects on Aircraft Pilot Coupling for Highly Maneuverable Aircraft
  •  DOI: 10.13009/EUCASS2019-591
 -  Transient growth analysis of a compressible boundary layer using two-dimensional linear stability theory
  •  DOI: 10.13009/EUCASS2019-592
 -  Evaluation of Thermo-Acoustic Stability Behavior in Full-Scale Liquid Rocket Propulsion Systems
  •  DOI: 10.13009/EUCASS2019-593
 -  Experimental analysis of aluminum-droplet combustion in solidpropellant conditions using deep learning
  •  DOI: 10.13009/EUCASS2019-597
 -  CARMEN, The Liquid Propulsion Rocket Engine Simulation Platform, Development Status and Perspectives
  •  DOI: 10.13009/EUCASS2019-598
 -  Retro-Jet Experimental Study for Reusable Rockets in a Hypersonic Flow
  •  DOI: 10.13009/EUCASS2019-600
 -  A fan rotation influence on inlet aerodynamic characteristics at the crosswind regime
  •  DOI: 10.13009/EUCASS2019-602
 -  Conceptual model for a profitable return on investment from space debris as abiotic space resource
  •  DOI: 10.13009/EUCASS2019-603
 -  Relationship between metallographic observation, tensile and yield strength in 7449 aluminium alloy thick plates
  •  DOI: 10.13009/EUCASS2019-604
 -  Design and optimization of glide-back reusable launch vehicle architectures
  •  DOI: 10.13009/EUCASS2019-605
 -  Analysis of high-speed Al-PLIF images to study aluminum droplet combustion in solid propellant flames
  •  DOI: 10.13009/EUCASS2019-606
 -  Steps for Flying Additive Manufacturing Hardware in Space
  •  DOI: 10.13009/EUCASS2019-607
 -  An overview of climatic wind tunnel for anti-icing performance testing of superhydrophobic coatings for aeronautical applications
  •  DOI: 10.13009/EUCASS2019-608
 -  Assessment of the effect of heat-shield ablation on the aerodynamic performance of re-entry capsules in hypersonic flows
  •  DOI: 10.13009/EUCASS2019-613
 -  Prediction of Subscale Rocket Engine Acoustic Emissions Using CAA Hybrid Methods
  •  DOI: 10.13009/EUCASS2019-614
 -  Experimental and numerical characterizations of acoustic damping rates in a coupled-cavity configuration
  •  DOI: 10.13009/EUCASS2019-616
 -  ATHENA/X-IFU: DCS Cryostat Harness baseline design and road map test
  •  DOI: 10.13009/EUCASS2019-617
 -  Low-order Modeling of Combustion Instability Applied to Cryogenic Propellants
  •  DOI: 10.13009/EUCASS2019-618
 -  Influence of Heating Rate on Pyrolysis Process of Paraffin oil for Rocket Fuel
  •  DOI: 10.13009/EUCASS2019-621
 -  The HYPROB Demonstrator Line: Status of the LOX/LCH4 Propulsion Activities
  •  DOI: 10.13009/EUCASS2019-624
 -  Travelling wave mathematical analysis and efficient numerical resolution for a realistic model of solid propellant combustion
  •  DOI: 10.13009/EUCASS2019-625
 -  Large eddy simulation of a transverse hydrogen jet in supersonic crossflow
  •  DOI: 10.13009/EUCASS2019-626
 -  2nd qualification test series results of the upper stage engine LE-5B-3 for H3 rocket
  •  DOI: 10.13009/EUCASS2019-628
 -  Thermal control and fire safety system for test launch vehicle of KSLV-II
  •  DOI: 10.13009/EUCASS2019-629
 -  Modes Reconstruction of Hybrid Combustion Flame
  •  DOI: 10.13009/EUCASS2019-631
 -  Inclusion of structure and loads objectives in the definition of probability for Flight Control System failures in the frame of FTB#2 Clean Sky 2
  •  DOI: 10.13009/EUCASS2019-632
 -  Towards a streamlined stacking sequence optimisation methodology for blended composite aircraft structures
  •  DOI: 10.13009/EUCASS2019-633
 -  Space Rider Mission Engineering
  •  DOI: 10.13009/EUCASS2019-634
 -  Fuel Regression Modelling for Hybrid Rocket CFD Simulations
  •  DOI: 10.13009/EUCASS2019-637
 -  Karhunen-Loève Expansion of Ensemble Weather Forecasts for Aircraft Trajectory Planning
  •  DOI: 10.13009/EUCASS2019-638
 -  Reusable Payload Fairings: Mission Engineering and GNC Challenges
  •  DOI: 10.13009/EUCASS2019-639
 -  VULCAIN®2.1, the European reference for Ariane 6 Lower stage cryogenic propulsive system
  •  DOI: 10.13009/EUCASS2019-641
 -  Analytical and Simulation-based V&V techniques applied to the ExoMars 2020 Cruise GNC
  •  DOI: 10.13009/EUCASS2019-644
 -  Aerodynamic Design of a Reusable Booster Stage Flight Experiment
  •  DOI: 10.13009/EUCASS2019-646
 -  Development and Testing of Spray-on Thermal Protection System Materials based on Cork and Aerogels
  •  DOI: 10.13009/EUCASS2019-648
 -  CARBON NANOTUBES FILLED POLYETHERETHERKETONE (PEEK) COMPOSITES
  •  DOI: 10.13009/EUCASS2019-649
 -  A new method to correlate Thermal Mathematical Models of space instruments and payloads
  •  DOI: 10.13009/EUCASS2019-650
 -  Simulation of Unstable Rarefied Gas Flow in a Channel in Transition from Continuum to Free-Molecular Regime
  •  DOI: 10.13009/EUCASS2019-651
 -  Design aspects and characterisation of a resonance igniter for oxygen/methane in-orbit propulsion systems
  •  DOI: 10.13009/EUCASS2019-652
 -  Structural Radar Research of Airbus Defense and Space as Clean Sky Partnership
  •  DOI: 10.13009/EUCASS2019-653
 -  Study on hypergolic ignition of ionic liquid solutions
  •  DOI: 10.13009/EUCASS2019-656
 -  Discontinuous carbon fibre reinforced polymers: manufacturing and characterization
  •  DOI: 10.13009/EUCASS2019-657
 -  Design of an On-board Flight Safety System for Space Microlaunch Vehicles
  •  DOI: 10.13009/EUCASS2019-658
 -  ExoMars 2020 Cruise GNC formal verification of stability and robustness
  •  DOI: 10.13009/EUCASS2019-660
 -  Experimental Tests Results of Transpiration Cooling Subscale Injector Head in the frame of LYRA Program
  •  DOI: 10.13009/EUCASS2019-661
 -  Development of a MATLAB® Plume Impingement Tool for Fast System Analysis.
  •  DOI: 10.13009/EUCASS2019-663
 -  A New Design of an Embedded System for Online Harness Monitoring in Reusable Launch Vehicles Using Reflectometry
  •  DOI: 10.13009/EUCASS2019-664
 -  Analysis of subsonic premixed turbulent reacting flow in a backward-step combustor using PaSR models
  •  DOI: 10.13009/EUCASS2019-667
 -  Influence of Operating Parameters on the Ballistics of a Lab-Scale Vortex Flow Pancake Hybrid Rocket Engine
  •  DOI: 10.13009/EUCASS2019-668
 -  A BGK model for high temperature rarefied hypersonic flows
  •  DOI: 10.13009/EUCASS2019-669
 -  Experimental study of energetic ionic liquid decomposition
  •  DOI: 10.13009/EUCASS2019-670
 -  In-flight transition of a Dual-Bell nozzle transonic vs. supersonic transition
  •  DOI: 10.13009/EUCASS2019-671
 -  Elastic waves simulation and damping characterization on composite structures for structural health monitoring applications.
  •  DOI: 10.13009/EUCASS2019-673
 -  Planetary Transits and Oscillation of Stars (PLATO) Focal Plane Assembly (FPA): Preliminary Model Philosophy and Prototype test results.
  •  DOI: 10.13009/EUCASS2019-674
 -  Research of Hypersonic Boundary Layer Instability with Thermal-Chemical Non-equilibrium Effects
  •  DOI: 10.13009/EUCASS2019-675
 -  Multi-Disciplinary Modeling Environment for Reusable Launch Vehicle Dynamics and Control System Design
  •  DOI: 10.13009/EUCASS2019-677
 -  Additive manufacturing of Scalmalloy® satellite parts
  •  DOI: 10.13009/EUCASS2019-678
 -  Assessment of numerical aspects using LES in particle separation devices
  •  DOI: 10.13009/EUCASS2019-679
 -  Aerodynamic Database Simulation Implementation Based On Neural Network and Neural Network Parameter Selection Using Genetic Algorithms
  •  DOI: 10.13009/EUCASS2019-680
 -  CFD KINETIC SCHEME VALIDATION FOR LIQUID ROCKET ENGINE FUELLED BY OXYGEN/METHANE
  •  DOI: 10.13009/EUCASS2019-681
 -  Femtosecond Laser Energy deposition in a M=3 Supersonic Flow: Parametric Study
  •  DOI: 10.13009/EUCASS2019-682
 -  Advancing Europe’s Hybrid Rocket Engine Technology with Paraffin and LOX
  •  DOI: 10.13009/EUCASS2019-683
 -  Plasma actuation for lifted flame stabilization in coaxial methane-air flow
  •  DOI: 10.13009/EUCASS2019-685
 -  Autonomous assembly of large structures in space: a technology review
  •  DOI: 10.13009/EUCASS2019-686
 -  Roughness corrections applied to the simulation of turbulent hypersonic flows
  •  DOI: 10.13009/EUCASS2019-687
 -  Continued airworthiness assessment of evolving usage patterns in military transport aircraft
  •  DOI: 10.13009/EUCASS2019-688
 -  MIURA 1 Avionics Development And Qualification
  •  DOI: 10.13009/EUCASS2019-690
 -  Flight Instrumentation for the Reusability Flight Experiment ReFEx
  •  DOI: 10.13009/EUCASS2019-694
 -  An efficient Two-Layer wall model for accurate numerical simulations of aeronautical applications.
  •  DOI: 10.13009/EUCASS2019-697
 -  Development of a Calibration Satellite for a CMB Telescope Flying in Formation about L2 Libration Point
  •  DOI: 10.13009/EUCASS2019-698
 -  Design Simulation and Software Validation for On-board and Real-Time Optimal Guidance
  •  DOI: 10.13009/EUCASS2019-702
 -  Design of a Model-Based Failure Detection Isolation and Recovery System for Cubesats
  •  DOI: 10.13009/EUCASS2019-703
 -  Reliability-Based Design Optimisation of Composite Structure using Multi-fidelity Modelling
  •  DOI: 10.13009/EUCASS2019-706
 -  Feature extraction from micro-tomography analysis of solid propellants
  •  DOI: 10.13009/EUCASS2019-710
 -  Vega Launchers’ Trajectory Optimization Using a Pseudospectral Transcription
  •  DOI: 10.13009/EUCASS2019-713
 -  Using Differential Flatness for solving the Minimum-Fuel Low-Thrust Geostationary Station-Keeping Problem
  •  DOI: 10.13009/EUCASS2019-714
 -  Design of a Flight Control System (FCS) applying airworthiness requirements of MIL-STD-1797A
  •  DOI: 10.13009/EUCASS2019-715
 -  Plasma reforming for oxygen production on Mars
  •  DOI: 10.13009/EUCASS2019-718
 -  An Innovative Strategy for Paraffin-based Fuels Reinforcement: Part I, Mechanical and Pre-Burning Characterization
  •  DOI: 10.13009/EUCASS2019-719
 -  A Comparative Study of the Aging Behavior of Different Nano-sized Aluminum Powders
  •  DOI: 10.13009/EUCASS2019-722
 -  3D-Printed On/Off Sensors for Resin Flow Monitoring in Composite Manufacturing Processes
  •  DOI: 10.13009/EUCASS2019-723
 -  Design of low-thrust control in the geostationary region for station keeping
  •  DOI: 10.13009/EUCASS2019-724
 -  JUST-IN-TIME COLLISION AVOIDANCE MISSION: REACTIVE SYSTEM FOR BRAKING SPACE DEBRIS
  •  DOI: 10.13009/EUCASS2019-725
 -  Basalt fibre reinforced geopolymer made from lunar regolith simulant
  •  DOI: 10.13009/EUCASS2019-727
 -  Hybrid composites for the Space industry
  •  DOI: 10.13009/EUCASS2019-728
 -  An Innovative Strategy for Paraffin-based Fuels Reinforcement: Part II, Ballistic Characterization
  •  DOI: 10.13009/EUCASS2019-730
 -  Investigation of uncertain parameters for characterizing welded structures using Vibration-Based Methods
  •  DOI: 10.13009/EUCASS2019-731
 -  Large-Eddy Simulation of a Multi-Element LOx/CH4 Thrust Chamber Demonstrator of a Liquid Rocket Engine
  •  DOI: 10.13009/EUCASS2019-733
 -  Investigations on Rheology, Spray and Combustion Processes of Gelled Propellants at DLR Lampoldshausen
  •  DOI: 10.13009/EUCASS2019-734
 -  Comparison of efficiency characteristics of jet engines with detonation and slow combustion based on low and high fidelity computational tools
  •  DOI: 10.13009/EUCASS2019-735
 -  Preliminary Design of the Hybrid Navigation System (HNS) for the CALLISTO RLV Demonstrator
  •  DOI: 10.13009/EUCASS2019-736
 -  On the UPMSat-2 Attitude, Control and Determination Subsystem’s design
  •  DOI: 10.13009/EUCASS2019-738
 -  Concept Development of a Cryogenic Tank Insulation for Reusable Launch Vehicle
  •  DOI: 10.13009/EUCASS2019-739
 -  Overview of Flight Guidance, Navigation, and Control for the DLR Reusability Flight Experiment (ReFEx)
  •  DOI: 10.13009/EUCASS2019-740
 -  Design And Development Of A Nitrous Oxide / Alcohol Sounding Rocket Technology Demonstrator
  •  DOI: 10.13009/EUCASS2019-741
 -  Aerodynamic design and preliminary optimization of a commercial PrandtlPlane aircraft
  •  DOI: 10.13009/EUCASS2019-742
 -  Generating Aerodynamic Database from Closed Loop Simulated Flight Data
  •  DOI: 10.13009/EUCASS2019-743
 -  PROMETHEUS: Precursor of new low-cost rocket engine family
  •  DOI: 10.13009/EUCASS2019-745
 -  RUAG’s approach to develop a modular low shock separation and jettison system
  •  DOI: 10.13009/EUCASS2019-747
 -  Development of an enhanced fairing acoustic protection system to increase payload comfort
  •  DOI: 10.13009/EUCASS2019-749
 -  Development of Innovative Heat Sinks for Power Electronics Cooling within the More Electrical Aircraft
  •  DOI: 10.13009/EUCASS2019-750
 -  Highly Efficient RLV-Return Mode “In-Air-Capturing” Progressing by Preparation of Subscale Flight Tests
  •  DOI: 10.13009/EUCASS2019-751
 -  Absolute and Convective Instabilities in High Enthalpy Jets
  •  DOI: 10.13009/EUCASS2019-753
 -  NUMERICAL PREDICTION OF THE NOISE REDUCTION IN A WING MOCK-UP CONFIGURATION USING DBD PLASMA ACTUATORS.
  •  DOI: 10.13009/EUCASS2019-755
 -  Computational Aerothermodynamics for HTV Small Re-entry Capsule Project
  •  DOI: 10.13009/EUCASS2019-756
 -  Effect of microstructure and temperature on the impact toughness of forged Ti-6Al-4V
  •  DOI: 10.13009/EUCASS2019-757
 -  Ignition Study at Small–Scale Solid Rocket Motor
  •  DOI: 10.13009/EUCASS2019-762
 -  Experimental approach to characterize base region Coanda flow topology induced by pulsating blowing
  •  DOI: 10.13009/EUCASS2019-764
 -  Proba-3: Challenges and Needs for Sub-Millimetre Autonomous Formation Flying
  •  DOI: 10.13009/EUCASS2019-766
 -  Analysis of satellite vibration response using techniques of digital image correlation
  •  DOI: 10.13009/EUCASS2019-767
 -  Thermal System Oriented Simulation of Aircraft Electrical Environmental Control Systems Including its Electric Coupling
  •  DOI: 10.13009/EUCASS2019-769
 -  Ceramics from wet-processing of Martian soil simulant using slip casting or Additive Manufacturing for in-situ resource utilization on Mars
  •  DOI: 10.13009/EUCASS2019-770
 -  Reconfigurable Nonlinear Controller Under Turbulence Flight Condition
  •  DOI: 10.13009/EUCASS2019-771
 -  Vega C Light, a flexible and low cost solution for small satellites
  •  DOI: 10.13009/EUCASS2019-772
 -  Auto-Coded Flight Software for the GNC VTVL Demonstrator EAGLE
  •  DOI: 10.13009/EUCASS2019-775
 -  Experimental investigations of flow field around hypersonic vehicle and re-entering spacecraft with the hypersonic rarefied wind tunnel MARHy
  •  DOI: 10.13009/EUCASS2019-776
 -  Main Performances of the Unsteady Constant Volume Combustion Thermodynamic Cycle
  •  DOI: 10.13009/EUCASS2019-777
 -  Assessment of LES techniques for mitigating the Grey Area in DDES models
  •  DOI: 10.13009/EUCASS2019-778
 -  Challenges, strategies and methodologies to build-up and maintain space objects catalogues
  •  DOI: 10.13009/EUCASS2019-779
 -  TUPEX-7: Expanding CubeSat Capability
  •  DOI: 10.13009/EUCASS2019-780
 -  Multiscale structural simulation of metamaterials under large strains. Generation of the RVE behaviour
  •  DOI: 10.13009/EUCASS2019-781
 -  Assessment of the effect of the fuel savings scheme in Formation Flight Planning using Switched Optimal Control Techniques
  •  DOI: 10.13009/EUCASS2019-783
 -  Advances in continuous carbon fibre reinforced Aluminium matrix composites
  •  DOI: 10.13009/EUCASS2019-786
 -  Plasma flow control in a rarefied Mach 20 Flow over a flat plate
  •  DOI: 10.13009/EUCASS2019-787
 -  Particulate phase evolution inside solid rocket motors: preliminary results
  •  DOI: 10.13009/EUCASS2019-789
 -  Investigations on the Crew Injury Biomechanics and Spaceship Seats Safety Design for Human Space Flight
  •  DOI: 10.13009/EUCASS2019-790
 -  Ensuring Numerical Reproducibility for Model-Based Software Engineering
  •  DOI: 10.13009/EUCASS2019-791
 -  Activated and Nano-sized Aluminum as Metal Fuels in Solid Rocket Propellants
  •  DOI: 10.13009/EUCASS2019-792
 -  Optimization of composite materials using 3D printed cores
  •  DOI: 10.13009/EUCASS2019-793
 -  Mechanically Activated Al/Mg Powders for Solid Rocket Propellants
  •  DOI: 10.13009/EUCASS2019-795
 -  Numerical analysis of catalysis and ablation effects for carbon-based ablative materials in nitrogen and air plasma environments
  •  DOI: 10.13009/EUCASS2019-796
 -  How could nature inspire solutions for aeronautics and space sciences?
  •  DOI: 10.13009/EUCASS2019-797
 -  Printed electronics for the functionalization of composite parts
  •  DOI: 10.13009/EUCASS2019-800
 -  Numerical analysis on the sublimation of low-temperature ablator models undergoing shape change in a supersonic
  •  DOI: 10.13009/EUCASS2019-802
 -  Overall Preliminary Sizing and Optimization of the Metallic Structures of a PrandtlPlane Civil Transport Aircraft
  •  DOI: 10.13009/EUCASS2019-805
 -  Electric Thruster Selection Criteria
  •  DOI: 10.13009/EUCASS2019-806
 -  Acoustic Streaming in High-speed Turbulent Channel Flow
  •  DOI: 10.13009/EUCASS2019-809
 -  Benefits of Rotating Rig Facility for the Study of Droplet Deformation and Breakup in the Vicinity of Aerodynamic Surfaces
  •  DOI: 10.13009/EUCASS2019-811
 -  Numerical modelling of mechanical behaviour of weft-knitted carbon fiber composites
  •  DOI: 10.13009/EUCASS2019-813
 -  Open-source AI Assistant for Cooperative Multi-agent Systems for Lunar Prospecting Missions
  •  DOI: 10.13009/EUCASS2019-814
 -  Particle size in SRM plume: assessment of collection method
  •  DOI: 10.13009/EUCASS2019-815
 -  A new approach to acoustic insulation materials characterisation based on X-ray tomographic images and LBM simulations
  •  DOI: 10.13009/EUCASS2019-816
 -  Data Fusion Method for Constructing Fighter Aircraft Aerodynamic Database Using Variable Fidelity and Space Mapping Techniques
  •  DOI: 10.13009/EUCASS2019-818
 -  Trade-off analysis of a new liquid rocket engine
  •  DOI: 10.13009/EUCASS2019-825
 -  CNES/DLR cooperation for the preparation of future reusable launcher cryogenic engines
  •  DOI: 10.13009/EUCASS2019-826
 -  Aircraft Ditching Impact Loads and Floatation Analysis
  •  DOI: 10.13009/EUCASS2019-827
 -  Sensor Integration and Data Exploration of Structural Health Monitoring Network integrated on an Unmanned
  •  DOI: 10.13009/EUCASS2019-830
 -  ALTAIR Semi-Reusable Air-Launch System Current Design and Status of Flight Experiments
  •  DOI: 10.13009/EUCASS2019-831
 -  Sensitivity computations by automatic differentiation of a CFD code based on spectral differences.
  •  DOI: 10.13009/EUCASS2019-834
 -  Design and development of 270 VDC Power Distribution Unit for Feeding essential loads
  •  DOI: 10.13009/EUCASS2019-837
 -  Plasma Jet Pack Technology : Electric Propulsion for Small satellites
  •  DOI: 10.13009/EUCASS2019-839
 -  The Hyperfine Structure of the OH
  •  DOI: 10.13009/EUCASS2019-840
 -  Emergence and evolution of longitudinal structures on blunt cone nosetip in hypersonic flow
  •  DOI: 10.13009/EUCASS2019-841
 -  SWING – COMPARISON OF PROPELLANT SLOSHING AND EQUIVALENT PEDULUM MODELES WITH A MULTI-COPTER
  •  DOI: 10.13009/EUCASS2019-842
 -  Thermal testing campaign of the UPMSat-2
  •  DOI: 10.13009/EUCASS2019-843
 -  ACARE and Flight Path 2050 Goals for Maintaining and Extending Aviation Industrial Leadership
  •  DOI: 10.13009/EUCASS2019-844
 -  Ensuring 2050 European Aviation Safety and Security Goals: Are We Doing the Right Research?
  •  DOI: 10.13009/EUCASS2019-845
 -  Objectives and results of the project PARE: Perspectives for Aerospace Research in Europe
  •  DOI: 10.13009/EUCASS2019-846
 -  Meeting Future European Aviation Societal and Market Needs
  •  DOI: 10.13009/EUCASS2019-847
 -  PARE preliminary analysis of ACARE Challenge 3 environmental impact goals (towards quieter and cleaner environment in aviation sector)
  •  DOI: 10.13009/EUCASS2019-849
 -  Research, education: a priority to safeguard the long-term competitiveness of European aviation
  •  DOI: 10.13009/EUCASS2019-850
 -  Long-range air transport market
  •  DOI: 10.13009/EUCASS2019-851
 -  Emerging Aviation Technologies – Progress in the Electrification of Aircraft
  •  DOI: 10.13009/EUCASS2019-852
 -  Cooperation in aviation beyond Europe´s Borders
  •  DOI: 10.13009/EUCASS2019-853
 -  Attracting young talent to aeronautics
  •  DOI: 10.13009/EUCASS2019-854
 -  Increasing the Participation of Women in Aerospace – A Review
  •  DOI: 10.13009/EUCASS2019-856
 -  Design and development of direct-injection gas-hybrid rocket using glycidyl azide polymer for small satellite thruster
  •  DOI: 10.13009/EUCASS2019-860
 -  The AVUM Orbital Module for the Space Rider System
  •  DOI: 10.13009/EUCASS2019-862
 -  Comparison of LOX/Methane and LOX/Hydrogen cryogenic spray combustion with simultaneous optical diagnostics
  •  DOI: 10.13009/EUCASS2019-863
 -  Multidisciplinary Design Optimization of a Reusable Lunar Vehicle
  •  DOI: 10.13009/EUCASS2019-866
 -  Numerical and Experimental Study of a 230 N Paraffin/N2O hybrid rocket
  •  DOI: 10.13009/EUCASS2019-867
 -  Enhancing operational efficiency of Terminal Maneuvering Areas through Continuous Climb Operations
  •  DOI: 10.13009/EUCASS2019-869
 -  Supersonic vortex wake at a wide distance from the wing and influence of acoustic type waves
  •  DOI: 10.13009/EUCASS2019-870
 -  Surrogate modelling for aerodynamic coefficients prediction in aeronautical configurations
  •  DOI: 10.13009/EUCASS2019-875
 -  Lift to Drag Ratio, Pitching Moment and Hinge Moment Based Airfoil Optimization
  •  DOI: 10.13009/EUCASS2019-878
 -  A Novel Multiplicative Quaternion Estimator from Vector Observations
  •  DOI: 10.13009/EUCASS2019-879
 -  On cup anemometers signal processing for better measurements and maintenance
  •  DOI: 10.13009/EUCASS2019-880
 -  Battery weight optimization for hovering aircraft
  •  DOI: 10.13009/EUCASS2019-882
 -  Analysis of the trends in air traffic and CO2 emissions within the European Union.
  •  DOI: 10.13009/EUCASS2019-883
 -  Performance improvement of hybrid electrolyte technology batteries for electrical propulsion in aerospace industry
  •  DOI: 10.13009/EUCASS2019-885
 -  The impact of large constellations on space debris environment and its Countermeasures
  •  DOI: 10.13009/EUCASS2019-886
 -  Aerodynamic Database Generation with Optimized Artificial Neural Network and a Design of Experiment Technique
  •  DOI: 10.13009/EUCASS2019-887
 -  Thermoelectric generators for long duration lunar missions
  •  DOI: 10.13009/EUCASS2019-891
 -  Direct numerical simulations of swirled jet sprays
  •  DOI: 10.13009/EUCASS2019-892
 -  Dynamics of generation of nanooxides during the burning of aluminum and titanium microparticles
  •  DOI: 10.13009/EUCASS2019-899
 -  Ground System Studies for landing the CALLISTO vehicle at sea
  •  DOI: 10.13009/EUCASS2019-900
 -  Multidisciplinary Overall Aircraft Design and Optimization of Blended Wing Body Configurations
  •  DOI: 10.13009/EUCASS2019-902
 -  Euclid AOCS Highest pointing stability for Dark Universe Investigation
  •  DOI: 10.13009/EUCASS2019-906
 -  Stability of a Flying Wing UAV in Icing Conditions
  •  DOI: 10.13009/EUCASS2019-907
 -  CALLISTO : ITS FLIGHT ENVELOPE AND VEHICLE DESIGN
  •  DOI: 10.13009/EUCASS2019-908
 -  Safety Motion Planning for Spacecraft Autonomous Proximity Maneuver
  •  DOI: 10.13009/EUCASS2019-910
 -  Nonlinear system identification for the thermal management of communication satellites
  •  DOI: 10.13009/EUCASS2019-917
 -  Microwave processing of regolith – a 1D-printing cavity for enabling lunar construction technology
  •  DOI: 10.13009/EUCASS2019-919
 -  Analytical models for Li-ion batteries developed at the IDR/UPM Institute
  •  DOI: 10.13009/EUCASS2019-920
 -  Cooperative Formation Flying Control Laws for Automatic Air to Air Refuelling
  •  DOI: 10.13009/EUCASS2019-921
 -  Decision-making modelling: application to autonomous Air to Air Refuelling
  •  DOI: 10.13009/EUCASS2019-925
 -  System Identification and Testing for a VTVL vehicle
  •  DOI: 10.13009/EUCASS2019-926
 -  Liquid Rocket Propulsion Launcher Design System to Train AxSTREAM.AI. Reusability Aspects.
  •  DOI: 10.13009/EUCASS2019-929
 -  Formation of graphene aerosol micro-flakes by thermal shock followed by shock wave
  •  DOI: 10.13009/EUCASS2019-933
 -  Lunar ISRU Energy Storage and Electricity Generation
  •  DOI: 10.13009/EUCASS2019-934
 -  Modelling and Simulation of the Primary Power Distribution of a Lunar Habitat
  •  DOI: 10.13009/EUCASS2019-935
 -  Slew Maneuver Control of Flexible Spacecraft
  •  DOI: 10.13009/EUCASS2019-936
 -  Experimental and numerical investigation of LOX/Methane Cryogenic Combustion at low mixture ratio
  •  DOI: 10.13009/EUCASS2019-938
 -  Numerical simulation of three-dimensional cylinder flare at hypersonic flows
  •  DOI: 10.13009/EUCASS2019-940
 -  Analysis of scalable distributed on-board computer architecture for suborbital rockets and micro launchers
  •  DOI: 10.13009/EUCASS2019-941
 -  Design of CALLISTO Tilt and Reentry flight sequences
  •  DOI: 10.13009/EUCASS2019-943
 -  All-source navigation algorithm for Hypersonic Vehicle based on ERAIM
  •  DOI: 10.13009/EUCASS2019-944
 -  Catalytic Ignition of Hydrogen Peroxide for Storable Bipropellant Thrusters
  •  DOI: 10.13009/EUCASS2019-947
 -  Fault-tolerant trajectory reconfiguration for sub-orbital spacecraft reentry guidance
  •  DOI: 10.13009/EUCASS2019-949
 -  Ariane Next, a vision for a reusable cost efficient European rocket
  •  DOI: 10.13009/EUCASS2019-950
 -  Study on Aerodynamic Stability of a Deployable Aerobraking Re-entry Capsule
  •  DOI: 10.13009/EUCASS2019-952
 -  Thermal Challenges Related to Lunar In-Situ Resources Utilization: Analysis of a Regolith Mining System
  •  DOI: 10.13009/EUCASS2019-956
 -  Concept of Operations CALLISTO demonstrator
  •  DOI: 10.13009/EUCASS2019-960
 -  Guidance Algorithm for Low-lift Skip Entry Based on Linear Pseudospectral Model Predictive Control
  •  DOI: 10.13009/EUCASS2019-961
 -  Multispectral Sensing for Relative Navigation
  •  DOI: 10.13009/EUCASS2019-962
 -  Laser propulsion: preliminary definition of a demonstrator
  •  DOI: 10.13009/EUCASS2019-963
 -  Development of an LNG Electro-Pump for a cryogenic launcher stage
  •  DOI: 10.13009/EUCASS2019-964
 -  Next steps towards future medium-range electric/hybrid aircraft
  •  DOI: 10.13009/EUCASS2019-965
 -  CASE STUDY OF THE INSTALLATION OF THE A400M ENGINE CONTROL UNIT - Abstract
  •  DOI: 10.13009/EUCASS2019-967
 -  A diffusion model in velocity space to describe the electron dynamics in an ECR plasma thruster with magnetic nozzle
  •  DOI: 10.13009/EUCASS2019-971
 -  LAUNCH VEHICLES SYSTEM STUDIES IN THE “FUTURE LAUNCHERS PREPARATORY PROGRAMME”: THE REUSABILITY OPTION FOR ARIANE EVOLUTIONS.
  •  DOI: 10.13009/EUCASS2019-972
 -  Experimental and Numerical Investigation of Aluminum Particle Combustion in Solid Rocket Combustion Chambers
  •  DOI: 10.13009/EUCASS2019-973
 -  Preparing the Future of European Space Transportation: Reusable Technologies and Demonstrators
  •  DOI: 10.13009/EUCASS2019-975
 -  TAXONOMIES for CORPORATE INTELLIGENCE in the AERONAUTICAL and SPACE SECTORS
  •  DOI: 10.13009/EUCASS2019-977
 -  Trade-off Study, Review and Anatomical Study of Launch Vehicles in use and under-development
  •  DOI: 10.13009/EUCASS2019-978
 -  Passively Safe Relative Orbit Configurations over Long Time Intervals for Heterogeneously Distributed Spacecraft Clusters
  •  DOI: 10.13009/EUCASS2019-979
 -  Scalability analysis of additively manufactured grain for 4 kN High Test Peroxide Hybrid Rocket Motor
  •  DOI: 10.13009/EUCASS2019-981
 -  Aerospace exploration in Central America. A hub for the world and outer space. Costa Rica as a pioneer in the region.
  •  DOI: 10.13009/EUCASS2019-983
 -  Constellation Design and Orbit formation for SmallSat Platform for Earth Observation Mission
  •  DOI: 10.13009/EUCASS2019-985
 -  Multi-Step Ice Accretion Simulation Using The Level-Set Method
  •  DOI: 10.13009/EUCASS2019-987
 -  Vega Space System
  •  DOI: 10.13009/EUCASS2019-990
 -  Space Rider Aerodynamics and Aerothermodynamics from hypersonic to subsonic flight
  •  DOI: 10.13009/EUCASS2019-991
 -  From IXV to Space Rider : CMC Thermal Protection System evolutions
  •  DOI: 10.13009/EUCASS2019-994
 -  Space Debris Mitigation using dedicated Solid Rocket Motor
  •  DOI: 10.13009/EUCASS2019-996
 -  A RE-USABLE HIGH RELIABILITY COMPUTER FOR AUTONOMOUS MISSIONS
  •  DOI: 10.13009/EUCASS2019-1000
 -  Space Rider – Payload and Landing Control Center / Landing Sites
  •  DOI: 10.13009/EUCASS2019-1002
 -  Space Rider’s inspection by a CoBot
  •  DOI: 10.13009/EUCASS2019-1004
 -  Design and development of a COTS battery for space missions at the IDR/UPM Institute
  •  DOI: 10.13009/EUCASS2019-1008
 -  Optimization Design of Structure Shape and Dimension of Anti-sway Plate in Propellant Tank of Liquid Launch Vehicle
  •  DOI: 10.13009/EUCASS2019-1010
 -  Evaluation of a ramjet model in a supersonic high-enthalpy tunnel
  •  DOI: 10.13009/EUCASS2019-1015
 -  The Reattachment Process in Laminar Hypersonic Flow
  •  DOI: 10.13009/EUCASS2019-1016
 -  The Design of the GNC of the Re-entry Module of Space Rider
  •  DOI: 10.13009/EUCASS2019-1020
 -  Numerical Simulation of the Subsonic Jet Noise with Installation Effect
  •  DOI: 10.13009/EUCASS2019-1022
 -  High-order large eddy simulation of particle-laden flow in a T106C low-pressure turbine linear cascade
  •  DOI: 10.13009/EUCASS2019-1024
 -  Symposium "System Integration" – Poster 1024 - Phylogenetic approach applied on Aircraft
  •  DOI: 10.13009/EUCASS2019-1026
 -  On modelling the finite strain anisotropic elastoplasticity with application to the prediction of springback in sheet metal forming
  •  DOI: 10.13009/EUCASS2019-1034
 -  Numerical Efficiency Analysis of Multi-pole Time-domain Impedance Boundary Conditions
  •  DOI: 10.13009/EUCASS2019-1036
 -  A Study on the Vibration Modal Testing and Analytical Model Updating of Liquid Rocket Engine of KSLV-II
  •  DOI: 10.13009/EUCASS2019-1038
 -  Deployment of CubeSats From Low-Earth Orbit to Near-Earth Asteroids
  •  DOI: 10.13009/EUCASS2019-1040
 -  Engine Re-start Transient Simulation Tool for Cryogenic Liquid Rocket System
  •  DOI: 10.13009/EUCASS2019-1049
 -  Space Rider Aerodynamic Surface Control System
  •  DOI: 10.13009/EUCASS2019-1050
 -  A GNSS RTK Positioning Algorithm Utilizing MCAR and AEKF for Medium Baseline
  •  DOI: 10.13009/EUCASS2019-1051
 -  Ignition and Flame Propagation Dynamics in a Scramjet Cavity-Based Flame Holder
  •  DOI: 10.13009/EUCASS2019-1052
 -  An Energy-Based Approach to Satellite Attitude Control in presence of disturbances
  •  DOI: 10.13009/EUCASS2019-1054
 -  Increased capabilities at Esrange –Tests of reusable motors and stages
  •  DOI: 10.13009/EUCASS2019-1056
 -  Analysis and forecast on changes in the level of harmful substance emissions from aviation gas turbine engines
  •  DOI: 10.13009/EUCASS2019-1057
 -  Spectral Analysis of Rocket Wake Flow–Jet Interaction by Means of High-speed Schlieren Imaging
  •  DOI: 10.13009/EUCASS2019-1058
 -  MIXED-HYBRID FUEL FORMULATIONS: COMPOSITION, REGRESSION RATE AND CONDENSED COMBUSTION PRODUCTS
  •  DOI: 10.13009/EUCASS2019-1060
 -  3D density reconstruction of a screeching supersonic jet by synchronized multi-camera Background Oriented Schlieren
  •  DOI: 10.13009/EUCASS2019-1061
 -  Successful collaboration & knowledge transfer amongst student space clubs – the SERA rockets
  •  DOI: 10.13009/EUCASS2019-1062
 -  NEW ADVANCES IN SHORT-PULSE LASER FOR LEO ENVIRONMENT: EXPERIMENTAL INVESTIGATION IN LASER/MATERIAL INTERACTIONS FOR SPACE DEBRIS REMOVAL
  •  DOI: 10.13009/EUCASS2019-1064
 -  Towards an Ontology of Sustainable Space Logistics

 

The conferences are subdivided into five parallel symposia, on topics:

  • SI      SYSTEM INTEGRATION on Aircraft and Space Launch Vehicles
  • FP     FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re- Entry Bodies
  • SM   STRUCTURES AND MATERIALS for Aeronautics and Space Systems
  • FD    FLIGHT DYNAMICS/ GNC and AVIONICS for Aeronautics and Space Applictions
  • PP     PROPULSION PHYSICS for Air-Breathing and Rocket Engines

Poster sessions are also organised.

 

Since 2017, papers effectively submitted and presented have received a DOI.

All papers published since 2005 are now "open access" and retrievable using our search engine.

The search engine will also allow you to explore the many papers published in Europe and whose contents have been reported in our newsletter.

 

EUCASS Search Engine

 

 

A few plenary presentations are available as well in pdf format.

Plenary Presentations EUCASS 2017

 

 


Eucass operates three different series of conferences:

 

Collections of selected & refereed papers

Our publications are available at the Eucass EDP Science website here, where selected, reviewed and refereed papers are compiled together.

Eucass 2013 Selected, Reviewed and Refereed Papers Available

Our colleagues at www.eucass-proceedings.eu have published the 7th volume of their collection in Progress in Flight Physics.

The book contains thirty-five papers selected from over 140 papers presented in the Flight Physics sessions at EUCASS 2013 (see archive here at the main eucass webserver) in Munich, Germany.

These papers were reviewed by experts, revised, and throughly edited to provide state-of-the-art knowledge in their respective fields.

The book is organized in eight chapters:

  1. Aerodynamics
  2. Experimental Facilities
  3. Flow Control
  4. Inlets, Nozzles, and Internal Flows
  5. Jets and Wakes
  6. Non-equilibrium and Rarefield Flows
  7. Shock Waves
  8. Stability and Transition

The volume was prepared as a reference for research scientists and practicing engineers in the field of flight physics.

The articles are of Open Access type, and are available for you on the eucass-proceedings website here.


Aerospace Thematic Workshops

 

The prime objective of the Aerospace Thematic Workshops is to provide an international forum to facilitate and develop contacts between research scientists and engineers of the aeronautics and space community. Each Aerospace Thematic Workshop is devoted to a specific topic which highlights advances in key aerospace sciences (flight physics, flight dynamics, propulsion physics, structures and materials, system integration, etc.). Novelty and, to the extent possible, interdisciplinarity, are key characteristics.

The format of Aerospace Thematic Workshops encourages extensive formal and informal discussion among the attendees. The lecturers are allocated one hour for their presentations, including a minimum of fifteen minutes for discussions. Lectures are organised in one morning session and one evening session, both to be introduced by a short review from the chairman. Afternoons are available for discussion or leisure. The Aerospace Thematic Workshops last four full days and begin either on Sunday evening or on Monday morning.

The emphasis is placed on “off the record” presentations of yet unpublished scientific results. In order to promote open communication, each participant of a thematic school should agree that any information presented is a private communication not available for public release. Each participant is expected to take part actively in the discussions. In view of the multidisciplinary character of the workshop and of the presence of young scientists, lecturers should, wherever needed in their presentation, pay attention to pedagogy. One or two poster sessions are to be organised for late communications and for presentations of work conducted by students and other young scientists.

The location of Aerospace Thematic Workshops also is expected to concur to the general atmosphere of warm and lively scientific exchange. Large cities or cities with many opportunities for distraction are not suitable sites.

The operation of Aerospace Thematic Workshops is placed under the responsibility of a Steering Committee composed of prominent experts who are undisputed leaders in their field and are responsible for keeping the highest standards of excellence. Each school is organised under the authority of a Chairman who receives delegation from the Steering Committee. If necessary the Chairman can be assisted by a Vice-Chairman.

Chairman and, eventually, Vice-Chairman, are responsible for contacting their peers, obtaining from them promising proposals for lectures, and for assembling a balanced and challenging scientific programme. They are also responsible for making the atmosphere as friendly and stimulating as possible and for launching debates over potentially promising issues.

The Workshops are the trademark of European aerospace science, serving the cause of aerospace worldwide and must focus on long-term innovation and on break-through science. They must distinguish themselves by their tradition of excellence, by their cult for novelty, and by their style of lively exchange; multidisciplinarity, which is also considered to be an asset, should be encouraged whenever possible. They are not at the service of any particular interest or commercial group.

 

The Aerospace Thematic Workshops are managed by the Programme Committee of the EUCASS conference.
This Committee:

  • evaluates and selects the eligible topics to be treated each year on the basis of proposals made by any qualified aerospace personnel;
  • procures partial financial assistance;
  • selects suitable conference sites;
  • procures secretarial help and assists in solving problems.

 

Each conference is placed under the authority of a Chairman and a vice-Chairman.
Responsibilities are delegated to each one of them according to the following guidelines:

 

  • Chairman

The chairman is responsible for preparing the conference programme and establishing a tentative budget. His task is also to raise the funds necessary for partial or total defrayment of speakers in the need and of a limited number of PhD students.

 

  • Vice Chairman

The vice Chairman assists the Chairman and has special responsibility over the preparation of the poster sessions. Normally, he has been nominated by his peers on the occasion of the preceding event and is expected to take charge of the Chairmanship on the following one.

  • Local Organisation

Local organisation is, for the moment, placed under the responsibility of the Chairman. It is envisaged to have it promptly taken up by the association (still in the process of being founded) in charge of EUCASS.

 

  • Budget, Registration fees and Support to participants

ATWs are not for profit. A fixed fee may be charged to all participants in order to cover local expenditures (rental of facilities and equipment, etc.), regardless of the time spent at the meeting. The Chairmen are encouraged to seek complementary financial support from Agencies, Research Establishments and Industry. Part of the budget is left at their discretion for partially covering travel and living expenses of invited lecturers if they require assistance. Support may also be given to other participants.

 


Personal data

This website does not offer any user registration, it is used only as a showcase of the association activities, as such there is no need or means of collecting any personal information as name, email, address etc. etc.

The only information collected about a visitor is the link visited, the time and the originating IP address. 

This information is used only to detect possible hacking attempts (i.e. brute forcing the website administrator password) and only for a short period of time, typically a few days.

For example, if an IP address (typically a computer) is trying repeatedly to guess the administrator password, security measures will be taken in order to stop accepting requests from this address. 

Even when contact forms are used intentionally to contact the website administrator, the email and name used are shortly stored on the system logs that register any activity regarding email activity on the system for security reason and are purged in a few days.  

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