EUCASS 2019 Full Papers

  •  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

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