List of Abstracts
You can search and sort the table to your convenience by using the SEARCH area above the table, and the pagination system at the bottom. You will see the session number you will present at on the far right column.
With this information, you can then check the Technical Sessions detailed planning HERE.
| AUTHORS | ABSTRACT TITLE | ORGANIZATION | KEYWORDS | TOPIC | TYPE | SESSION |
|---|---|---|---|---|---|---|
| Shon Mori; Guillaume Arnoult; Mathieu Balesdent; Loïc Brevault; Sylvain Dubreuil; Cédric Liauzun | Multi-fidelity Multidisciplinary Analysis Methodology for Preliminary Design of Ultra-high Aspect Ratio Strut Braced Wing Aircraft | ONERA | Multi-fidelity Simulation; Multidisciplinary Analysis; Aircraft Design; Ultra-high Aspect Ratio Wing; Strut-braced Wing | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 6 |
| Allen Chan; Mitchell Galletly; Dries Verstraete | Design Optimisation of Hybrid Propellant Launch Vehicles | University of Sydney | Multidisciplinary Design Optimisation; Hybrid Rocket Propulsion; Launch Vehicle | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| R. Stark; S. Bartel; F. Ditsche; T. Esch | Design Study of a 30kN LOX/LCH4 Aerospike Rocket Engine for Lunar Lander Application | German Aerospace Center | aerospike engine; lunar lander | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 19 |
| Kolja Michel; Christian Schallert | Multi-Objective Controller Optimization and Robustness Analysis by the Example of Electro-Mechanical Flight Surface Actuation | German Aerospace Center (DLR) | optimization; control; robustness; worst-case search; EMA; control surface; actuation | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Wei Zhang; Haiming Xie; Zhiwen Wang Lirong Bao; Ruiqi Shen | Design, fabrication and characterization of electrically controlled solid microthruster | Nanjing University of Science and Technology | Electrically controlled solid microthruster; controllable ignition and extinguishment; thrust test; multiple ignition and extinguishment | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| Saeed HOSSEINI; Mohammad Ali VAZIRY-ZANJANY; Hamid Reza OVESY | Multi-Objective Multidisciplinary Design Optimization of Regional Truss-Braced Wing Jet Aircraft | Amirkabir University of Technology | Truss-Braced Wing; Aircraft Design; Optimization; DOC; Emission | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 6 |
| Jianbing Xu; Zehua Zhang; Fuwei Li; Jian Cheng; Yinghua Ye; Ruiqi Shen | Design, Fabrication and Performance of Planar Solid Propellant Micro-thruster Based on SU-8 Photoresist | Nanjing University of Science and Technology | Planar Solid Propellant Micro-thruster (PSPMt); SU-8 photoresist; miniature combustion chamber with laval nozzle; lithography process; impulse | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 |
| Dr Raj Nangia; Mr Les Hyde; Prof. Jonathan Cooper | Developing Certifiable Liquid Hydrogen “Gondola” Airliner, Design Innovations & Challenges | nangia | SUSTAV; AEROFLIPHY; CFDMPS | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 4 |
| Marco Grossi; Gianluca Cocirla; Alessio Sereno; Daniele Bianchi;Bernardo Favini1 | Multiphase and Multidimensional Effects on Solid Rocket Nozzle Performance | Sapienza University of Rome | SRM;CFS | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Mark GUETHLER; Andreas Schmieder; Christian Dröge; Francois Gori; Guillaume Gouverne; Alexander Milke | Development and Qualification of the Avionic Support Structure of the Ariane 6 Upper Liquid Propulsion Module | ArianeGroup GmbH | Ariane 6; ULPM; Qualification; Testing | NEWSPA - New systems for future space operations | Oral | 1 |
| Fabien THOLIN | Multiphase MHD model for electric explosions: Application to lightning protection systems | ONERA | MHD; Plasma; CFD; Lightning; Explosion; Phase transition | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Akan Selim; ?brahim Özkol | Multi-phase Robust Optimization of a Hybrid Guidance Architecture for Launch Vehicles | ROKETSAN Inc. | Robust trajectory | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Thomas Greenslade; Minkwan Kim | Multi-physics Atmospheric Entry Simulations in Pursuit of Magnetic Shielding Techniques | University of Southampton | Multi-physics; Numerical Simulation; Atmospheric Entry; Re-entry; Capsule; Magnetic Shielding; Plasma | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Moongeun HONG | Development of a dual-position oxidizer main valve | Korea Aerospace Research Institute | Main oxidizer valve; Dual-position; Partial opening | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 2 |
| Giorgio Guglieri; Francesco Marino; Afshin Zeinaddini Meymand | Navigation in Non-Static Environments with Autonomous Drones: A Kalman Filter Reinforcement Learning Approach | Politecnico di Torino | UAV; Autonomous Navigation; Reinforcement Learning; Non-Static Environments; Dynamic Environments | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Robin Bonny; Martin Simik; Juliette Challot; Hannes Bartle | Development of a Modular Half-Duplex Frequency-Agile X-Band Transceiver for CubeSats and Robotic Spacecraft | EPFL | SDR; transceiver; X-band; student team; new space; frequency agility; CubeSat | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| Yiyuan Ma; Ali Elham | Next steps in aerostructural design of ultra-high aspect ratio wings | Technische Universität Braunschweig | High aspect-ratio wings; conceptual design; aerostructural optimization | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 6 |
| Mansur Tisaev; Andrea Lucca Fabris | Development of a neutraliser for air-breathing electric propulsion in very-low Earth orbit | University of Surrey | Air-breathing electric propulsion; VLEO; AETHER; AMPCAT | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Maxim KURILOV; Lukas WERLING; Christoph KIRCHBERGER | Nitromethane as a Green Propellant: First Results of a Combustion Test Campaign | DLR Deutsches Zentrum für Luft- und Raumfahrt | Green propellant; nitromethane; energetic material | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 14 |
| E. Onillon; A. Iglesias; G. Perruchoud; S. Liberatoscioli | Development of a novel capture system | Centre Suisse D'electronique et de Microtechnique | Capture; Servicing; Gripper; Stewart platform; Loads | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 |
| Simone La Luna; Davide Zuin; Filippo Maggi; Luca Magni; Nicola Foletti | N2O Mass Flow Modelling: State-of-the-Art and The New Dual SPC Model | Politecnico di Milano | green propellant; mass flow rate; self-pressurization; propulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 14 |
| Georgii Oblapenko; Tobias Ecker; Stefan Fechter; Tim Horchler; Sebastian Karl | Development of a photon Monte Carlo radiative heat transfer solver for CFD applications | German Aerospace Center (DLR) | Re-entry; hypersonic; radiation; Monte Carlo; heat transfer | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Zhaoxiang Zhang; Yuelei Xu; Linhua Ma | Non-Cooperative Target Pose Estimation Based on Dynamic Region-Aware Convolution Neural Network | The university of tokyo | pose estimation; non-cooperative target; deep learning | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 |
| Raphael Aubry; Gines Rodriguez Castro; Elouan Maitre; Angeliki Parisi Ploumpi; Jacob Amaler | Development of an injector sizing tool for a 4kN LOX/Ethanol student-built liquid rocket engine | ISAE Supaéro | Space propulsion; liquid rocket injector; propellant atomization; student rocketry | STUDENT - Space Student Projects | Oral | 1 |
| Rabiya BIYIKLI; Raziye TEKIN; Ilkay YAVRUCUK | Nonlinear Dynamic Inversion Autopilot Design for Thrust Vector and Aerodynamic Controlled Aerial Vehicles | Roketsan Missiles Inc. | Nonlinear Dynamic Inversion; Thrust Vector Control; Aerodynamic Control; Non-minimum Phase; Output Redefinition | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 1 |
| Cheulwoong Kim*; Keejoo Lee; Jaesung Park; Hyungjoon Choi; Jisung Yoo; and Sangyeon Ji | Development of Liquid Oxygen/Liquid Methane Pressurization Systems for Launch Vehicles | Korea Aerospace Research Institute | Liquid Rocket Engine; Pressurization; Autogenous Pressurization; VTVL; | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Sangmin Lee; Hyeonggwan Kang; Youdan Kim | Nonlinear model predictive guidance for tilt-rotor UAV performing terrain-following flight for mine detection | Seoul National University | Terrain-following flight; Mine detection; Tilt-rotor UAV; Model predictive control | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Christoph Karl; Joao Esteves; Alberto Sanchez Cebrian; Thomas Knodel | Development of low-shock separation systems for payload fairings | Beyond Gravity | payload fairings; separation systems; low-shock | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 |
| Micha? Kawalec1; Witold Perkowski; Adam Bilar; Maksymilian Augustyn and Piotr Wola?ski | Development of the hollow detonative chamber for the RDE applications | Lukasiewicz-Institute of Aviation | Detonation; Rotating Detonation Engine (RDE); Jet fuel-air mixtures. | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 3 |
| Zvicka DEUTSCH; Florian HELBER; Hannah LINNE; Friedrich DUNGERN; Peter MIDDENDORF | Novel Scalable Infusion Approach, Utilizing Automated Preforming and Smart Mold with Microvibrations for Manufacture of Integral Aerospace Structures | IAI | Composite Materials; Dry Fiber Placement; Binder Materials; Microvibrations; Vacuum Infusion; Integral Heating | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 5 |
| Pawe? St??ycki; Piotr Wola?ski | Development of the Liquid Green Propellants at the ?ukasiewicz-Institute of Aviation | Institute of Aviation | hydrogem; fuel; HTP; propellants | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 13 |
| Hong Yeong Park; Yun Hyeong Kang; Jae Won Lee; Jong Hyun Kim; Jeong Soo Kim | Numerical Analysis on the Film-cooling Effect with Varying Coolant Flow-rate in GCH4-LOx Liquid Rocket Engines | Pukyong National University | Film-cooling; Methane; Liquid Rocket Engine; Computationl Simulation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| X. Zhou; L. Dong; M. Giglio; C. Sbarufatti | Diagnosis and Prognosis of Structural Damage Growth with Parameter Sharing in Fleet Maintenance Digital Twins | Politecnico di Milano | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 | |
| T. Ecker ; J. Martinez Schramm; L. Schmidt ; D. Surujhlal ; A. Wagner; Tim Horchler | Numerical and experimental investigation of the shockwave boundary layer interaction of laminar/transitional flow past a sharp fin | German Aerospace Center (DLR) | Shock; SBLI; CFD | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 4 |
| Hanqing Xia; Yi Wu*; Ningfei Wang; Junsen Yang | Diode Laser Ignition Characteristics of ABS and Oxygen hybrid rocket motor | Beijing Institute of Technology | Laser Ignition; hybrid rocket motor; Combustion characteristic; | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 18 |
| Jonas Peichl; Markus Selzer; Tatjana Cziep; Patrick Pfannes; Hannah Böhrk; Andreas Schwab; Jens von Wolfersdorf; Patrick Palmetshofer; Daniel Eiringhaus | Numerical Framework for the Investigation of a Transpiration Cooled LOx/LH2 Rocket Engine Combustion Chamber | Deutsches Zentrum für Luft-und Raumfahrt | Rocket engine; Transpiration Cooling; Combustion Chamber Cooling | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Leandro Germes Martinez; Benjamin Duret; Julien Réveillon; François-Xavier Demoulin; Amauric Jarry | Direct numerical simulation of sloshing and phase change in LH2 tanks | CNRS UMR 6614 – CORIA | Direct numerical simulation; Sloshing; phase change; interface resolution; hydrogen | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| YANIK Umutcan; OZTURKMEN Musa Onur; TURGUL Doruk | Numerical Investigation of Liquid Film Cooling Performance on An Experimental Rocket Nozzle | ROKETSAN | heat transfer; liquid film cooling; internal flow; multiphase flow; injector; CFD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 13 |
| Juan Manuel Jiménez García | Disruptive and efficient rear fuselage for dual use high speed Rotary Wing platforms | Airbus Helicopters España SAU | Gyrodine; disruptive; RACER; efficient; OoA; additive | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 6 |
| Yannik Feldner; Moritz Ertl; Sebastian Karl; Tobias Ecker | Numerical Investigation of the Effects of Post-Combustion due to Fuel Outflow in Bleed Engine Cycles of a Retro Propulsion-Assisted Launch Vehicle | German Aerospace Center (DLR) | RLV; VTVL; CFD; RANS; Post-Combustion; Retro Propulsion; Bleed Engine; Chemistry Modeling; Turbulence Modeling | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Sean McDaniel; Rui Fu; Matthew Beck; Alexandre Martin | Numerical Investigation of the Effects of Structural Property Variability on the Material Response of a Fibrous Ablator | University of Kentucky | Ablation; Variability; Structural response | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Jascha Wilken; Steffen Callsen; Dennis Daub; Alexander Fischer; Martin Liebisch; Carolin Rauh; Thomas Reimer | DLR project TRANSIENT: Testing reusable cryogenic insulation and thermal protection systems | DLR | RLV; TPS; Cryogenic insulation; cryogenic propellant; Test | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 4 |
| Sasi Kiran Palateerdham; Lakshmi Narayana Phaneendra Peri; Antonella Ingenito; Ashish Vashishtha | Numerical investigation of the impact of injectors location on fuel mixing in the HIFiRE 2 Scramjet combustor | Sapienza University of Rome | SCRAMJET; COMBUSTION; HYPERSONIC PROPULSION; AEROSPACE; CFD; COMBUSTION CHEMISTRY; GREEN TRANSPORTATION | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 |
| Tiziano Santese; Daniel Martinez Sanchis; Chiara Manfletti | DNS of turbulent ribbed channel flow with heat transfer and comparison with current RANS capabilities | TUM | Roughness; DNS; Cooling Channels; Heat Transfer | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| Ibraheem Nasser; Chiara Manfletti; Tiziano Santese ; Oskar Haidn | Numerical investigation on heat transfer of Rocket Engine Cooling Channel for different LNG Under Trans and Super-Critical Conditions | TUM | Cooling Channel; LNG; Supercritical Pressure; Liquid Rocket Engine | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 30 |
| Mariasole Laureti; Sebastian Karl | Dr. | DLR - Institute of Aerodynamics and Flow Technology | Reusable Launch Vehicle; Retro-Propulsion; Aerothermal Loads; CFD; RANS | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Jakub Glowacki | Numerical modelling of supersonic magnetic nozzles | Victoria University of Wellington | in-space propulsion; electric thrusters | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 11 |
| Zhiwen Wang; Ruiqi Shen; Luigi T. DeLuca; Wei Zhang* | Dynamic combustion characteristics of electrically controlled solid propellant with transient voltage | Nanjing University of Science &Technology | Electrically controlled solid propellant; controllable propulsion; multi-stage transient voltage | HEPAEM - Hybrid Electric Propulsion | Oral | 2 |
| Xinying Liu; David Anderegg; Anil Yildirim; Righi Marcello; Leonardo Manfriani | Numerical optimisation of single-/multi-element aerofoils using gradient-based methods | ZHAW Centre for Aviation | aerofoild design; numerical optimisation; wind energy | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 2 |
| Hideto Takasawa; Tomoya Fujii; Koshiro Hirata; Takahiro Moriyoshi; Yusuke Takahashi; Yashnori Nagata; Kazuhiko Yamada | Dynamic Instability of a Thin-Shell type Aeroshell Capsule with Pitching Motion in Transonic wind tunnel | Graduate School of Engineering, Hokkaido University | Reentry Capsule; Dynamic Stability; Transonic | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 4 |
| Carlo E.D. Riboldi; Marco Tomasoni | Dynamic Simulation, Flight Control and Guidance Synthesis for Fixed-Wing UAV Swarms | DAER - Politecnico di Milano | swarm; uav; formation flight; coordination; leader-follower; nonlinear simulation; stability augmentation; guidance; beam tracking; altitude tracking; fixed-wing uav; drone | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 15 |
| Yann BLAIRON; Olivier MONTAGNIER; Annie LEROY | Dynamic stall models for post flutter analysis of an aeroelastic wing section | École de l'Air et de l'Espace | aeroelasticity; non-linear aerodynamics; flutter | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Poster | 4 |
| L. CUtrone; A. Schettino; A. French | Numerical rebuilding of a free-flying ring interfering with a two-dimensional shock wave | CIRA | CFD; Aerothermodynamics; Design for Demise | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| J.S. Sonneveld; T. van den Berg; G. la Rocca; S. Valencia-Ibáñez, B. van Manen; A.M.R.M. Bruggeman | Dynamic workflow generation applied to aircraft moveable architecture optimization | TU Delft | DEFAINE; MDO | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 9 |
| Alessa Sperber; Christian Korn; Clemens F. Kaiser; Johannes W. Oswald; Georg Herdrich | Numerical Rebuilding of Plasma Wind Tunnel Experiments for Investigation of Magnetohydrodynamic Flow Interactions within the EU Project MEESST | Institute of Space Systems | Re-Entry; Numerical Simulation; Magnetohydrodynamics (MHD); MEESST | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Chloe BERENGUER; Konstantinos KATSONIS | Earth atmosphere remnants as an electric propulsion propellant | DEDALOS Ltd | Electric propulsion; Air breathing; Optical diagnostics | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Adrien Langenais; Juliette Aubrée; Pierre Doublet; Stéphane Langlois; Claire Lavigne; Valérie Rialland | Numerical simulation of flight effect on the afterburning plume exhausting from a solid rocket motor | ONERA | Solid rocket motor; plume afterburning; firing experiments; CFD; combustion modelling | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| U. Lommatzsch; B. Schneider; K. Thiel; F. de la Escalera | Eco-efficient manufacturing of horizontal tail plane (HTP) structures for next-generation aircrafts – the role of surface pretreatment for adhesive joints | Fraunhofer | surfaces; adhesive bonding; pretreatment | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 8 |
| Annafederica Urbano; Marie Bibal; Maxence Deferrez; Sébastien Tanguy | Numerical simulation of phase change induced by pressure variations in cryogenic tanks | ISAE SUPAERO | cryogenics; phase change; compressible two phase flows; refuelling; tanks; depots | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| V. Desangles; F. Boni; R. Ferrand; E. Gourcerol; R. Pioch; P-Q. Elias; D. Packan | ECRA Thruster latest development at ONERA | ONERA | electric propulsion; plasma propulsion; ECR Thruster; microwave thruster; magnetci nozzle thruster | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| P. Nair; V. Narayanan | Numerical simulation of the effect of different divergent angle of pylon | Indian Institute of Technology Gandhinagar | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 | |
| Martina FORMIDABILE; Woutijn Baars; Ferry Schrijer | Effect of aeroelasticity on the acoustic imprint of TOP contoured nozzles in overexpanded conditions | Delft University of Technology | Aeroacoustics; Vibroacoustics; Aeroelasticity; Fluid-Structure Interaction; Overexpanded nozzle flows; Rocket noise | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Prasanth P Nair; Vinod Narayanan | Numerical simulation of the effect of different divergent angle of pylon | IIT Gandhinagar | scramjet; cavity-based; pylon; DMD; IDDES | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 35 |
| Stany GALLIER; Mathieu PLAUD | Effect of flame radiation on aluminum particle combustion | ArianeGroup | Aluminum combustion; Radiation; Aluminum oxide | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Sang Gon Lee; Sang Hun Kang | Numerical Study on the Ducted Scramjet Combustor | Konkuk Univ. | AEROFLIPHY; FLOCON | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Domenico Fiorini; Anne Gosset ; David Seveno; Johan Steelant; Miguel Alfonso Mendez | On the capillary rise of cryogenic liquids in microgravity: numerical analysis and experiments | von Karman Institute | Dynamic Wetting in Microgravity; Volume Of Fluid; Interface dynamics in capillary tubes | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| Olivier Orlandi; Mathieu Plaud | Effect of molted or machined surfaces on small scale SRM igntition | ArianeGroup | SRM; ignition; propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 15 |
| Carlo E.D. Riboldi; Alberto Rolando; Stefano Cacciola; Gregory Regazzoni; Ilaria Spadafora | On the Optimal Preliminary Design of High-Altitude Airships: Automated Procedure and the Effect of Constraints | DAER - Politecnico di Milano | Airship design; stratospheric airship; optimal design; preliminary design; high-altitude airship; high-altitude pseudo-satellite; HAA; HAPS; LTA | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 2 |
| Laurent FRANCOIS; Gérald PORTEMONT | Effect of nozzle seal rupture on internal motor dynamics | ONERA | nozzle seal; seal rupture; solid rocket motor; ignition | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| Davide Duri | On the recovery of CH4 on the launch pad: cryogenic challenges towards an environmentally responsible access to space | CEA | methane; recovery; thermal hydraulics | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| Kakeru Mizukoshi; Noritaka Sako; Jun Hayashi; Yu Daimon; Hiroshi Kawanabe | Effect of surface roughness on jet impingement cooling of a superheated wall | Kyoto University | Jet impingement cooling; Liquid film; Surface roughness; Heat transfer | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 36 |
| Behrad Vatankhahghadim; Marco Lovera | Effects of Flexibility on Reorientation of Multibody Spacecraft Using Internal Torques | Politecnico di Milano | multibody systems; flexible spacecraft; attitude and shape dynamics; nonholonomic control; geometric phases | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Yu Daimon; Kohji Tominaga; Go Fujii; Taiichi Nagata; Yoshiki Matsuura; Yasuhito Kano; Erika Uchiyama | One-dimensional Modeling of Ignition Timing for Hypergolic Bipropellant Thrusters | Japan Aeropace Exploration Agency | Chemical propulsion; Hypergolic propellant; Ignition; System simulation | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| A. Caldarelli; F. Filleul; C. Charles; R. Boswell; J. Carter; N. Rattenbury | Effects of magnetic nozzle configuration on ion beam generation for RF electrode-less plasma thrusters | The University of Auckland | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 11 | |
| Riccardo Gelain; Artur Elias De Morais Bertoldi; Patrick Hendrick | Optical investigation of paraffin-based fuel combustion in a hybrid rocket slab burner | Université libre de Bruxelles | Hybrid rocket; slab burner; paraffin; optical investigation | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 18 |
| Juan Manzanero; Diego Lodares; Miguel Sabaris Boullosa; Francisco Asensio Nieto | Optimal control of a combat aircraft with thrust vectoring during take off | Airbus Defence and Space | Flight Control Laws; Optimal Control; Thrust vectoring | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Teng ZHOU; Huijing CAO; Ben ZHAO; Qing'an LI | Effects of the reduced frequency on aerodynamic characteristics of a pitching NACA0012 airfoil under moderate Reynolds number | Chinese Academy of Sciences | Pitching airfoil; unsteady aerodynamics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 1 |
| Yeonhi Kim; Jungsun Park | Optimal design of three-dimensional woven composite aircraft wing with genetic algorithm | three-dimensional woven composite; aircraft wing; optimal design; genetic algorithm | STRMAT - Structures & Materials for Aeronautic and Space Systems | Poster | 46 | |
| Jeongsik SHIN; Kyun Ho LEE; Jung-Won KUK; Han Seo KO | Electric field simulation of FEEP thruster for cubesat application | Sejong University | FEEP Thruster; Electric Propulsion; Cubesat; Electric-field Simulation | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Heekun ROH; Taehyeun KIM; Yongjun MOON; Hyunwook WOO; Chang-Hun LEE | Optimal Time Terrestrial Mapping Scheduling for Spaceborne Push-broom Imagers | Korea Advanced Institute of Science and Technology (KAIST) | Optimization; Earth Observation; Scheduling | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Philippe Saunois; Jean-Christophe Verdier; Nicolas Luquet; Alexandre Delcausse; Nicolas Salvat | Electromechanical TVC using direct engine deflection measurement feedback for reusable stages | ArianeGroup | Electromechanical TVC;multi-engine bay; reusable; engine; deflection measurement; feedback | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Sascha Dengler; Adrian Wagmann Y Otero; Chiara Manfletti | Optimising ConOps of Water Electrolysis Propulsion systems using Deep Q-Learning | Technical University Munich, Chair of Space Propulsion and Mobility | Water Electrolysis Propulsion; ConOps; AI; Reinforcement Learning; In-Space Propulsion | NEWSPA - New systems for future space operations | Oral | 1 |
| Sergio Cuevas del Valle; Pablo Solano-López; Hodei Urrutxua | Embedding Pontryagin’s Principle in Neural Networks for Optimal Asteroid Landing | Universidad Rey Juan Carlos | AI; Neural Networks; Optimal Control; Asteroid Landing | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Theodora ANDREESCU; Simona DANESCU; Alexandru CANCESCU; Dan IFRIM | Optimization of Wave-Plasma Interaction in RF Powered Propulsion Technology based on Ultra-Compact Helicon Reactor | COMOTI | helicon plasma source; magnetic nozzle; electrodeless architecture; radiofrequency | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| Yann Tincelin; Agata Jozwicka-Perlant; Daniel Chipping; Antonio Caiazzo; Irene Huertas; Gianfranco Visentin; Ross Findlay; Andrew Wolahan | Enabling a European In-Space Transportation ecosystem | European Space Agency - ESA | In-space transportation; Space logistics; In-Orbit Demonstration; IOD-IOV; Orbital; Rendezvous; Docking; Refuelling; Ecosystem; Interfaces; Standardization | NEWSPA - New systems for future space operations | Oral | 2 |
| Faycal BAHRI; Qiangqiang Sun; Mark JABBAL; Richard Jefferson-Loveday; Wit Stryczniewicz; Wien Stalewski ; Bruno STEFES; Alexander BUESCHER. | Optimized Active Flow Separation Control in the Slat-cut Region Using Low Duty Cycle Pulsed Jets. | University of Nottingham | flow separation; turbulent boundary layer control; pulsed-jets; Aerofoil. | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 1 |
| Nicola Puca; Giorgio Guglieri | Enabling Single-Pilot Operations technological and operative scenarios: a state-of-the-art review with possible cues | Politecnico di Torino | Single Pilot Operations; Cognitive Human Aircraft Interface; Pilot Monitoring; Certification; Digital Flight Assistant; Pilot Workload | HUMANF - Human factors in Aviation and Space | Oral | 2 |
| Nicola Cimmino; Annarita Argirò; Roberto Opromolla; Giancarmine Fasano; Giorgio Isoletta | Optimized multi-satellite manoeuvring strategy for responsive Earth observation | University of Naples Federico II | responsive space; agile manoeuvring; multi-objective optimization; Earth observation | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 5 |
| Taha Soleymani | Energy harvesting from a rotary sandwich structure with magnetorheological core under aerodynamic pressure | Aviation | Energy Harvesting; Sandwich Structure; Rotary Structure; Smart structure; piezoaeroelasticiy | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 |
| Andriy BORSHCHAK KACHALOV; Pablo SALGADO SÁNCHEZ; Dan GLIGOR; Úrsula MARTÍNEZ; José Miguel EZQUERRO; Jeff PORTER | Optimizing the thermocapillary-driven melting of phase change materials in microgravity | E-USOC, UPM | Phase change materials; thermocapillary effect; microgravity | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| CHEOL-GOO Jung; Chang-Hun Lee; Tae-Hun Kim; Hyung-Sik Choi | Entry Vehicle Trajectory Optimization using Convex Programming and Post-correction technique | KAIST | entry guidance; convex programming | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Dabo Krempus; Fabio Beltrame; Matteo Majer; Carlo Maria De Servi; Matteo Pini; Roelof Vos; Piero Colonna | Organic Rankine Cycle Waste Heat Recovery for Turboshaft Engines of Turboelectric Aircraft | Delft University of Technology | PROPHY; SYSINT; HEPAEM | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 21 |
| Felix Brenner; Jonas Mangold; Dominik Eisenhut; Andreas Strohmayer | Environmental and Economic Assessment of Alternative Fuels and Power Trains on Aircraft Level | University of Stuttgart | Alternative Fuels; Alternative Power Trains; Aircraft Design | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 2 |
| Markus Selzer; Jonas Peichl; Ivens Daniel Hoffmann; Dmitry Suslov | Outflow measurements on porous injector elements | German Aerospace Center | porous media; Injector; outflow distribution | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| Thimo Bielsky; Nils Kuelper; Frank Thielecke | Overall Parametric Design and Integration of On-Board Systems for a Hydrogen-Powered Concept Aircraft | Hamburg University of Technology | Aircraft; Hydrogen; Systems; Secondary Power | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 3 |
| Filippo MAGGI; Sebastian Manuel CERVELLI; Alessandro FINAZZI; Alessandro MURGIA; Stefano DOSSI; Tobias LIPS; Kobye BODJONA; Geert SMET | ESD sensitivity analysis of thermites for satellite demise | Politecnico di Milano | design for demise; thermite sensitivity; electrostatic discharge; experimental characterization | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| Bartosz Ko?cianek; Maciej Mikulski; Konrad Wojciechowski; Karol Bresler | Overview of the Twardowsky Hybrid Sounding Rocket Avionics Design | ISAE-SUPAERO | avionics; avionics system; electronics system; sounding rocket; hybrid rocket | STUDENT - Space Student Projects | Oral | 2 |
| Nora M. Bierwagen; Stefan May; Thino Eggers; Andreas Ohndorf; Christian Mundt | Particle-based modeling of the unsteady flow in a high-test peroxide catalytic chamber | German Aerospace Center (DLR) | hybrid rocket engine; catalytic chamber; high-test peroxide | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| Victor Chernov | Estimating peak soot volume fraction and temperature in a laminar flame using artificial neural networks | Braude College | Soot; Diffusion Flames | SUSTSP - Sustainable Space: Logistics and Space Debris | Reject | |
| Burak Ergöçmen; Umut Tilki | Path generation with RRT* and Path Following during an Emergency for a Fixed Wing Aircraft | Turkish Army Aviation | GNC; Autopilot; Path Generation | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Reject | |
| Kohji Tominaga; Yu Daimon; Go Fujii; Taiichi Nagata; Yoshiki Matsuura; Yasuhito Kano; Erika Uchiyama | Estimation of Hard Start Mechanism by Visualization Test of Hypergolic Bipropellant Thruster | Japan Aerospace Exploration Agency (JAXA) | Hard Start; Detonation; Hypergolic Bipropellant Thruster; Visualization Test | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Roberto Andriani; Antonella Ingenito | Performance Analysis of a Hybrid Thermal-Electric Turboprop Engine | Politecnico di Milano | Hybrid; Thermal; Electric; Turboprop | HEPAEM - Hybrid Electric Propulsion | Poster | 21 |
| Nisheet Singh; Dr. Peter Weiss; Mohamed Makthoum Peer Mohamed; Thibaud Gobert | EUROHAB: A Secondary Habitat concept for the South Pole of the Moon | SPARTAN SPACE | Space habitat; safe haven; inflatable; moon; secondary habitat; ARTEMIS | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Giuseppe GUIDOTTI; Federico TROVARELLI; Giuseppe GOVERNALE; Nicole VIOLA; Ingrid DIETLEIN; Steffen Callsen; Kevin Bergmann; Junnai ZHAI; Roberto GARDI; Barbara TISEO; Ysolde PREVEREAUD; Yann DAUVOIS; Giovanni GAMBACCIANI; Giada DAMMACCO | European Flexible Heat Shields: Advanced TPS Design and Tests for Future In-Orbit Demonstration - 2 | Politecnico di Torino | Inflatable Heat Shields; Re-entry; Reusability; Reusable launchers | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 4 |
| Sevket Utku AYDINLI; Ali Turker KUTAY | Performance Comparison of Deep Reinforcement Learning-Based Quadcopter Guidance Algorithms | Middle East Technical University | Deep Reinforcement Learning; Model Predictive Control; Proportional Navigation; Missile Guidance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 2 |
| Thorben Hammer; Stefanie de Graaf | Evaluation of hybrid electric powertrain topologies and their integration in future aircraft concepts for general aviation | German Aerospace Center (DLR) | Electrified Propulsion; Hybrid-electric; Propulsion architecture; General aviation; future aviation | HEPAEM - Hybrid Electric Propulsion | Oral | 1 |
| Robson H. S. Hahn; Tobias Traudt; Anirudh M. Saraf; Jan Deeken; Michael Oschwald; Stefan Schlechtriem | Performance estimation of supersonic impulse turbine at transient conditions | DLR - German Aerospace Center | Turbine; Supersonic; Transient; Turbopump; LUMEN | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| Arthur Berlet Déchauffour; Stéphanie Dreyer; Michel Duvergey; Sandra Boujnah | PERSEUS and Minerva: Firing tests | ArianeGroup | PERSEUS; MINERVA; Firing Tests | STUDENT - Space Student Projects | Oral | 1 |
| Magdeleine Airiau ; Robin Devillers; Adrien Chan Hon Tong ; Le Besnerais Guy | Evolution of aluminum droplets in solid-propellant combustion by image analysis using deep learning | ONERA | Deep learning; aluminium combustion; solid-propellant; computer vision | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Tobias Ott; Marcel Pfeiffer | PIC schemes for multi-scale plasma simulations | Institute of Space Systems | plasma simulation; particle in cell | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Victor Maldonado; Jack Hicks; Guilherme Fernandes | E-VTOL Concept Design with a New Underwing ‘FanFoil’ Ducted Fan Concept to Improve Aerodynamic Efficiency | Texas Tech University | eVTOL design; ducted fan; distributed propulsion | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 2 |
| Kaltham Alrowahi; Shaima Alshamsi; Ahmed Alhafeiti; Shaaban Ali; Sobers Lourdu | Pilot’s Awareness Sensor System (PASS) | Abu Dhabi Polytechnic | Sensor System; Integration System | HUMANF - Human factors in Aviation and Space | Oral | 1 |
| Julius Stegmüller; Andreas Molz; Christian Breitsamter | Experimental analysis of the flow field over an aeroelastic wind tunnel model for tail buffeting analysis | Technical University of Munich | Flexible Wind Tunnel Model; Aeroelasticity; Tail Buffeting | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| T. Silva; V. Guerra; N.Pinhão ; O.Guaitella; C. Guerra-Garcia; F. J. J. Peeters; M.N. Tsampas and M. C. M. van de Sanden | Plasmas for in-situ resource utilization on Mars: fuels, life-support and agriculture | IPFN | INSITU; MARS; PLASMA; CO2; OXYGEN PRODUCTION | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 3 |
| ARNOULT Guillaume; ANTONAKIS Aristeidis; ATINAULT Olivier; BARETTER Alberto; DELVA Jérôme; MEHEUT Michaël; NOWINSKI Vianney; TOUSSAINT Clément | Experimental and numerical investigations on large fuselage configurations | ONERA | Large Fuselage; Experimental; numerical | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 4 |
| Vishal Youhanna; Leonard Felicetti; Dmitry Ignatyev | Parametric Analysis of Battery-Electric Rotorcraft Configurations to Fly on Mars | Cranfield University | Mars Explorataion; Space Drone; Martian Aerobot; Rotorcraft | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| S. Gumruk Tokgoz; B. Sümer; B. Yazici; S. Uslu | Experimental and Numerical Study of Supersonic Flow in Scramjet Combustor in Expansion Tube | Tubitak SAGE | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 | |
| Francisco José Blázquez Plaza; Mick Wijnen; Andrés Barrado Bautista | Power converter with high gain, high performance for space thrusters based on electrospray technology | Universidad Carlos III de Madrid | High-gain; high-performance; electrospray; DC/DC; FF-CW | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 11 |
| Sujit Sinha; Rick Fu; Jesse B. Hoagg; Sean C. Bailey; Alexandre Martin | Precision Meteorological Prediction Employing A Data-Driven, Adaptive, Real-Time (DART) Approach | University of Kentucky | UAV; weather; forecast; meteorology | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Till Hörger; Lukas Werling; Günther Waxenegger-Wilfing; Stefan Schlechtriem | Experimental and Simulative Evaluation of a Reinforcement Leaning Based Cold Gas Thrust Chamber Pressure Controller | German Aerospace Center DLR - Deutsches Zentrum für Luft- und Raumfahrttechnik | Control; Reinforcement Learning; Machine Learning; Orbital Propulsion | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 2 |
| Moritz Zieher; Christian Breitsamter | Prediction of Aerodynamic Coefficients for Multi-Swept Delta Wings via a Hybrid Neuronal Network | Technical University of Munich | Neuronal Network; Aerodynamic Design; Machine Learning; Hybrid-delta wing | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 2 |
| Malte Christopher Schwarze | Advanced Hybrid-Electric Propulsion Systems and Integrations in Airliner | Advanced Aircraft Design | Hybrid-electric Propulsion; electric thrust; single aisle; hybrid-electric aircraft; flettner; magnus | HEPAEM - Hybrid Electric Propulsion | Oral | 1 |
| Yoshiki Matsuura | Experimental estimation of the amount of residual slag remaining inside orbital insertion stage solid rocket motor | IHI Aerospace | Solid Rocket; Slag; Debris | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Yujie Guo; Yuhang Chen; Fangyin Huang; Haotian Zhu | Predictions of wing structural responses by physical-based machine learning framework | Nanjing University of Aeronautics and Astronautics | structural analysis; machine learning; PINNs; Wing Structure | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Mariangela De Maio; Beatrice Latini; Francesco Nasuti; Sergio Pirozzoli | DNS of flow inside pipes with large relative roughness height | Università di Roma Sapienza | Pipe flow; Roughness; Heat Transfer; Turbulence; DNS | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Alexander Bee; Michael Börner; Justin Hardi | Experimental Investigation of a LOX/Methane Liquid Centered Swirl Coaxial Injector During Ignition, Startup and Subcritical Operation | German Aerospace Center (DLR) | Swirl Coaxial Injector; LOX/Methane; Liquid Rocket Propulsion; Throttleable Injector | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 6 |
| Francesco Bonelli; Davide Ninni; Gianpiero Colonna; Giuseppe Pascazio | Preliminary analysis of a CFD code implementing H2/He State-to-State kinetics for Gas and Ice Giants entry conditions | Politecnico di Bari | Hypersonics; Thermochemical non-equilibrium; Gas/Ice Giants; State-to-State kinetics | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Alessia Assonitis; Renato Paciorri; Enrico Cavallini; Simone Illiano; Simone Pizzurro; Simone Ciabuschi | 3D flow simulations of space launchers stage separations through overset approach | University of Rome La Sapienza | space launchers; overset method; stage separation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Poster | 9 |
| Artur Elias de Morais Bertoldi; Riccardo Gelain; Patrick Hendrick | Experimental investigation of paraffin-based fuel doped with MgB2 and MWCNTs in a 1-kN hybrid rocket engine | University of Brasília | hybrid rocket propulsion system; solid fuel regression rate; paraffin-based fuels; magnesium-diboride; carbon nanotubes | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 18 |
| Gabriel Barreau; François Pechereau; Philippe Lalande; Frédéric Alauzet; Guillaume Puigt | 3D modeling of a continuous arc with anisotropic mesh adaptation | ONERA | MHD; CFD; Mesh adaptation; electric arc | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Poster | 5 |
| Diana Luis; Andrea Fagnani; Alan Viladegut; Bernd Helber; Adriano Camps; Olivier Chazot | Experimental measurements of radio signal attenuation and Faraday rotation due to electron number density in a plasma flow | VKI | Plasma flow; inductively coupled plasma wind tunnel; communication blackout; radio signal attenuation; Faraday rotation; electron number density; spectroscopy | TESTING - Testing in Aerospace | Oral | 2 |
| Marcin Chuchla; Tomasz Palacz; Grzegorz Bywalec; Edyta Gierada; Jacek Kurzyna; Maciej Jakubczak; Arsenii Riazantsev | Preliminary Investigation of A High Efficiency Liquid Micro Pulsed Plasma Thruster (L-PPT) | Liftero Sp. z o. o. | Propulsion; PPT; Electric Propulsion; Pulse Plasma Thruster | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| François Pechereau; Fabien Tholin; Julien Vanharen; Guillaume Puigt; Frédéric Alauzet and Philippe Lalande | 3D Modeling of an arc in interaction with composite materials | ONERA | CFD; LIGHTNING; PLASMA; CFRP; MESH ADAPTATION | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Poster | 6 |
| Ruyao Wang; Junwei Li; Deyou Wang; Jiajin Zeng; Ningfei Wang | Experimental study of pulsed triggering oscillation in T-burner | Beijing Institute of Technology | pulse triggering; T-burner; pressure oscillation; solid rocket motor | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 31 |
| Qiuyang Xia; Davide Marchesoli; Pierangelo Masarati; Meng Liu | Preliminary study of tracking vs boundary avoidance task effects on rotorcraft pilot involuntary response | Politecnico di Milano | Input Strategy; Point Tracking; Boundary Avoidance Tracking; Tracking Error; Input Aggression | HUMANF - Human factors in Aviation and Space | Oral | 1 |
| Hongyi Xie; Franco Bernelli-Zazzera | 6-DOF orbit-attitude stabilization around an asteroid by using performance based intermittent event-triggered control | Politecnico di Milano | barrier-based event-triggered control; orbit-attitude coupling; orbital station keeping; asteroid exploration; attitude control | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| Sung-rok Hwang; Hyung Ju Lee | Experimental study of thermal cracking characteristics of hydrocarbon aviation fuels through endothermic reactions | Pukyong National University | Hypersonic vehicle; Scramjet; Regenerative cooling system; Gas chromatography; Conversion ratio | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 |
| Tomasz Palacz; Jacek Cie?lik | Preliminary testing and analysis of the end-burning swirling flow hybrid rocket engine using torch igniter | AGH UST | Hybrid rocket engine; swirling flow; torch igniter | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 18 |
| Jan Sturla Hegre; Adrien Boiron; Jørn-Inge Ruud; Elliott Worsley; Matt Shaw | 6kN green fuel throttleable development engine – Design and Manufacturing | Nammo Raufoss AS | bi-propellant; green; Peroxide; pintle; additive manufacturing; | NEWSPA - New systems for future space operations | Oral | 1 |
| George Lampeas; Evangelos Carelas; Panagiotis Kordas ; Alexandra Karanika; Konstantinos Fotopoulos | Experimental validation of aircraft fuselage sections by testing at the stiffened panel level | UNIV. PATRAS | stiffened panels; fuselage; simulation; validation | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 8 |
| Tamas Bykerk and Sebastian Karl | Preparatory CFD Studies for Subsonic Analyses of a Reusable First Stage Launcher during Landing within the RETPRO Project | DLR | retpro; cfd; subsonic | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Simone Alfano; Matthieu Garcia; Fabien Castanet | A 2023 overview of French in-space chemical propulsion activities supported by CNES | CNES | Green Propulsion; REACH; Hydrazine replacement | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| S. Mazouffre; U. Weller | Experimental validation of the electric sail concept | CNRS | Electric sail; interplanetary | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Manami FUJII; Tetsuya SATO; Atsushi HASHIMOTO; Hideyuki TAGUCHI | Pressure Model of Buzz Oscillation in a Ramjet Intake | Waseda University | Ramjet Intake; Buzz; CFD; supersonic | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 27 |
| Carmelo Rosario Vindigni; Giuseppe Mantegna ; Calogero Orlando ; Andrea Alaimo | A 3D aeroelastic beam modelling approach for time domain non-uniform lifting structures flutter analysis | Kore University of Enna | 3D aeroelastic beam; wing-aileron flutter; variable elastic axis | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Yeontaek Jung; Hanna Lee; Youngjun Lee; Youdan Kim | Explicit Midcourse Guidance Law of Multi-stage Anti-ballistic Missile with Solid Propellant | Seoul National University | Anti-ballistic missile; Midcourse guidance; Solid propellant; Explicit guidance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 10 |
| Agnes CHAN | A cloud-based multi-fidelity solution for debris re-entry prediction | Re CAE | Immersed boundary conditions; unstructured mesh; cloud-based solution; flight mechanics; aerothermodynamics | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Elisabeth RACHITH; Stephan HELLMICH; Belén Yu IRURETA-GOYENA CHANG; Jean-Paul KNEIB | Exploring large astronomical data archives for the characterization of space debris | EPFL | space-debris; machine learning; data processing | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| T. Germani1, E. Bandelier1, Ph. Cloutet; D. Ribéreau; D. Garitta; M. Angelone; A. Ciucci; D. Scoccimarro | PROGRESS OF THE P160C SOLID ROCKET MOTOR DEVELOPMENT, FUTURE COMMON PROPULSIVE SRM FOR ARIANE 6 BLOCK2 AND VEGA-C/VEGA-E EUROPEAN LAUNCHERS | Europropulsion | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 6 | |
| Shuanghou Deng; Sichen Song; Hongyu Qiao | A Conceptual Design Methodology for Hybrid Aircraft using Multiple Disciplinary Optimization | Nanjing University of Aeronautics and Astronautics | conceptual design; hybrid electric; MDO | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| Stefan Gneiger; Daniel Koutny; Sascha Senck; Thomas Klein | Exploring the Benefits and Limitations of Wire-based Direct Energy Deposition of Magnesium Alloys | AIT Austrian Institute of Technology, LKR Light Metals Technologies Ranshofen | Addidive manufacturing; waDED; magnesium; mechanical properties | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 4 |
| Sippel; Singh; Stappert | Progress Summary of H2020-project FALCon | DLR-SART | RLV; in-air-capturing; FALCon | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 3 |
| Simona DANESCU; Dan IFRIM; Alexandru CANCESCU; Theodora ANDREESCU | Exploring the potential of electropump feed systems for extending high thrust and deep throttle performance for CH4/LOX rocket engines | COMOTI - Romanian Research & Development Institute for Gas Turbines | electropump; cryogenic pumps; liquid-propellant; rocket engines; LOX; liquid methane | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| A. Ramy; N. Meyers; E. Humbert; JL. Normand; A. Espinosa; S. Boujnah | PROMETHEUS® tests on T1 Bench in Vernon | ArianeGroup | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 | |
| Xiaojia Zhao; Shanshan Long; Zhenxin Hong | A data driven approach to predict life cycle cost of commercial aircraft | Nanjing University of Aeronautics and Astronautics | Life cycle cost; data driven apporach; MDO; artificial inetlligence | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| P. Simontacchi; E. Humbert; R. Blasi; E. Edeline; A. Espinosa; JN. Caruana | PROMETHEUS®: Precursor of new low-cost rocket Engine Family | ArianeGroup | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 | |
| Sergio Cuevas del Valle; Pablo Solano-López; Hodei Urrutxua | A Dual-Based Linear Programming formulation of Optimal Control: Fuel-Optimal Rendezvous Guidance and Boresight Pointing Applications | Universidad Rey Juan Carlos | Fuel-optimal control; indirect optimization; ADMM; MPC | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Félix Garmirian; Marcel Pfeiffer | Exponential Differencing BGK Method for Multiscale Flow Simulation | Institute of Space Systems - University of Stuttgart | rarefied gas dynamics; numerical simulation; multiscale flow; hypersonic flow; BGK equation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Adrien SAADA; Florian Micco; Emmanuelle David; Jean-Paul Kneib; Mathieu Udriot; Danielle Wood; Scott Dorrington; Francesca Letizia; Stijn Lemmens; Moriba Jah; Simon Potter; Minoo Rathnasabapathy; Nikolai Khlystov | Promoting responsible space practices: A primer on the Space Sustainability Rating | eSpace (EPFL Space Center) | Space Debris; Space sustainability; rating; incentive; guide | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 4 |
| Simon ALLARDET; Cyprien BETHE; Emrys BOUISSON; Antoine HUREAU; Bastien LEPREUX; Hippolyte MALLEVAYS; Elwin SILVESTRI; Julien SENON; Julien SIMON; Hugo VERJUS | A feasibility study of a future European Single-Stage-To-Orbit (SSTO) spaceplane | IPSA | SSTO; Spaceplane; Airbreathing; Hypersonic | NEWSPA - New systems for future space operations | Oral | 3 |
| Sara Bagassi; Marzia Corsi | Extended Reality Safety Nets for Attention Guidance in Airport Control Towers | University of Bologna | Extended Reality; Safety Nets; Attention Guidance; Airport Control Tower | HUMANF - Human factors in Aviation and Space | Oral | 2 |
| Mikaeel Shaikh; Biswajeet Pradhan; Bhavya Wadhwa | Propellant Management Challenges Related to the Operation of the Depot on Orbit | Universitaet Bremen | Propellant; Depot; In-Space; Storage; Transfer; Low Gravity; | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 5 |
| Margherita Piccinin; Andrea Brandonisio; Andrea Colagrossi; Giovanni Zanotti; Stefano Silvestrini; Michèle Lavagna | A finite state machine approach to nano-satellite SW design: the HERMES case study | Politecnico di Milano | on-board software; finite state machine; nano-satellite software design; software verification | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| DILSHAD AHMAD; RAFIC M AJAJ | Fabrication and Testing of Elastomeric Composite skin for 1D Morphing Wing Application | khalifa university | Elastomeric Skin; Morphing Wing; Carbon Fiber; Composite Elastomers | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 5 |
| Seungho Lee; Sunho Lee; Jaehyuk Huh; Sejin Kwon | Proposal of Aerospace-informatics by Design of Ramjet Inlet Using Machine Learning | Korea Advanced Institute of Science and Technology (KAIST) | Aerospace-informatics; Ramjet; Inlet; Machine Learning | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 38 |
| Alexy Tailleur; Kévin Mathis; Ange Rogani; Pablo Navarro; Steven Marguet; Jean-François Ferrero | A global-local defect/damage initiation and propagation model for launcher composite structures pre-sizing | CNES, ICA | FEM; Composites; Submodeling; Pre-sizing; Damage Initiation; Propagation; Matrix cracks; Delamination | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Marco Riccardo Inchingolo; Mario Merino; Jaume Navarro-Cavallé | Faraday Cup design for Electrodeless Plasma Thrusters | Universidad Carlos III de Madrid | Plasma; Electric Propulsion; Faraday cup; Diagnostics | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| Camille Cottenot; Romain Beauchet; Bastien Boust; Lilian Prevost; Marc Bellenoue | Pt/Al2O3 catalyst for 98 w% hydrogen peroxide decomposition: influence of spherical catalyst diameter on performance and longevity | PPrime | hydrogen peroxide; combustion; platinum catalyst; adiabatic decomposition; rocket propulsion; auto-ignition | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| Francesco Walter PRIZIO; Marek Slawomir LUKASIEWICZ; Quiyang XIA; Pierre GARBO; Giuseppe QUARANTA | A haptic device embedded in rotorcraft seats for target acquistition and tracking tasks | Politecnico di Milano | haptics; feedback; simulator; pilot-in-the-loop; human-machine interaction; performance; closed-loop; pressure | HUMANF - Human factors in Aviation and Space | Oral | 1 |
| Hemant Joshi; Peter Thomas | Unsteady Vortex Lattice Method: A Fast and Cost-Effective Solver for Dynamic Analysis of Supersonic Lifting Surfaces | University of Hertfordshire | Unsteady vortex lattice method; heaving; pitching; design optimisation; unsteady supersonic | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 1 |
| Dan IFRIM; Simona DANESCU; Theodora ANDREESCU; Alexandru CANCESCU | Pumps and Turbopumps Test by Similitude | Romanian R&D Institute for Gas Turbines | Turbo; Testing | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| Vincenzo Gulizzi | A high-order accurate framework for thermal fluid-structure interaction | Università degli Studi di Palermo | high-order accuracy; thermal fluid-structure interaction; discontinuous Galerkin method; embedded boundaries | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| David Planas; Eric Nguyen Van; Carsten Döll; Philippe Pastor | Quick-preliminary aerodynamic estimation for a distributed propulsion aircraft with propellers in front of the wing | ISAE-Supaero & ONERA | Distributed propulsion; preliminary estimation; aero-propulsive interaction | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| Fuqiang Duan; Hongyi Xie; Guoqiang Zeng; Franco Bernelli-Zazzera | Fault-tolerant Orbit and attitude control of Solar sail with a rapid inspection and repair strategy of faulty RCDs | Politecnico di Milano | Solar sail; Fault-tolerant Control; RCDs; orbit and attitude control | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 2 |
| Johannes Sebastian Laur; Diana Luis; Alan Viladegut; Vincent Fritzgerald Giangaspero; Andrea Lani; Jorge Luis Gonzales Rios; Jorge Querol; Juan Vasquez Peralvo; Juan Carlos Merlano Duncan; Andreas Hein; Jan Thoemel | Radio Communication Blackout Mitigation: Ray Tracing Analysis and Signal Characterization including Experimental Validation for Non-magnetized Plasmas | University of Luxembourg | Raytracing; Signal characterization; atmospheric entry plasma; plasma wind tunnel validation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Nikolaos Astyrakakis; Papatsaroucha Dimitra; Pityanou Konstantina; Markakis Evangelos; Zotos Nikolaos; Georgios Alexiou; Marinos Kardaris; George Bogdos | A holistic platform utilizing SDR for aiding automated airport and waterdrome inspections that utilize drones. | Hellenic Mediterranean University | UAV; Drones; SDR; mRNAV; NAVAIDS; Flying Platform; Horizon 2020; Aerosafe | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Jonas Ludowicy; Victor Bahrs; Martin Staggat | Feasibility studies for a medium size regional aircraft with battery powered propulsion system | German Aerospace Center (DLR) | Electric aircraft; battery electric; electric powertrain | HEPAEM - Hybrid Electric Propulsion | Oral | 1 |
| Dennis Harries; Alberto Maulu; Emmanuel Scolan; Kathryn Hadler | A large-scale laboratory demonstrator for the production of oxygen from lunar regolith: Challenges and opportunities | Air Liquide Advanced Technologies | ISRU; moon; alchemist | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Marnix VERKAMMEN; Håkan SVEDHEM; Alessandra MENICUCCI; Mathieu UDRIOT; Adrien SAADA; Emmanuelle DAVID; Andrew WILSON | Feasibility study of a single-score Life-Cycle Assessment for Space missions: preliminary results. | Delft University of Technology | Life-Cycle Assessment; sustainability; space mission; environment; sustainability rating; module; methodology; space debris; biosphere | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 4 |
| Mathieu Udriot; Karin Treyer; Orell Bühler; Laszlo Etesi; Emmanuelle David; Valère Girardin | Rapid Life Cycle Assessment Software for Future Space Transportation Vehicles’ Design | Ecole Polytechnique Fédérale de Lausanne | Life Cycle Assessment; Space Transportation Vehicle; environemntal hotspots; design trade-offs; science gaps; technology gaps; ecodesign | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 4 |
| Moritz Ellerbeck; Josef Wiedemann; Keith-Noah Jurke; | A liquid reusable strap-on booster system discussion for future European launch vehicles | MT Aerospace AG | Reusable; Strap-On; Booster; Launch; Vehicle | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 3 |
| Qiao Li; Xingchen Li; Wen Yao | Field reconstruction of the spacecraft from limited sensors based on graph neural networks. | National University of Defense Technology | Field reconstruction; graph neural networks | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 12 |
| Benjamin King Sutton Woods | Recent Progress in Wrapped Tow Reinforced (WrapToR) Composite Truss Structures | University of Bristol | Composites; Truss Structures; Aerospace Structures | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Carlo Alberto Rasoni; Alessia Assonitis; Renato Paciorri; Aldo Bonfiglioli; Enrico Cavallini; Simone Illiano; Simone Pizzurro; Simone Ciabuschi | A local unstructured re-meshing technique for handling multi-body separation in 2D flows. | University of Rome La Sapienza | CFD; multi-body separation; overset methods | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Gaia Letizia Civardi; Michèle Lavagna | Filtering techniques assessment towards pose estimation enhancement for image-based proximity navigation with uncooperative space objects | Politecnico di milano | Filtering Techniques; Pose Estimation; Vision-based navigation | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| Hajer Saada; Ana Garcia Garriga | A MBSE-based framework for aircraft systems design and evaluation | Collins Aerospace | Aircraft systems; systems design; MBSE; systems evaluation; systems integration; hybrid electric platform | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| David Codoni; Craig Johansen; Artem Korobenko | Finite element formulation for the analysis of hypersonic flows in thermal non-equilibrium with two- and three-temperature model | University of Calgary | Hypersonic non-equilibrium; FEM; CFD; Stabilized methods | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Alexandre Fougnie; Thomas Schmitt; Sébastien Ducruix | Reduced Order Modeling for the prediction of combustion instabilities in liquid rocket engines: coaxial injection response and acoustic damping modeling | Laboratoire EM2C | Combustion instabilities; liquid rocket engines; reduced order modeling; acoustic damping; coaxial injection | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Hyunju Lee; Sangchul Lee | A method to generate a constrained terrain following trajectory using circular path | Korea Aerospace University | Terrain following; trajectory; path | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 1 |
| V. Sant'Ana; P. Krus; R.M.Finzi Neto | Reduced-Scale Generic Future Fighter Aerodynamic Model Using Neuro-Fuzzy Hybridized with Differential Evolution | Linköping University | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 | |
| Davide Cavalieri; Jacopo Liberatori; Pasquale Eduardo Lapenna; Pietro Paolo Ciottoli | A multi-component droplet vaporization model for non-ideal fluids | Sapienza Università di Roma | Droplet vaporization; multi-component; non-ideal fluids | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 44 |
| Célian Boyé; Jaume Navarro Cavalle; Mario Merino Martinez | First ignition of a magnetic arch EPT cluster composed of two ECR plasma sources | UNIVERSIDAD CARLOS III DE MADRID | Electric propulsion; ECR; EPT; plume characterization; plasma physics | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| Rickmers; Kottmeier; Wübbels; Bauer | ReFEx: Reusability Flight Experiment – A Demonstration Experiment for Technologies for Aerodynamically Controlled RLV Stages | German Aerospace Center (DLR) | RLV; Flight Experiment; Hypersonics; Aerodynamic | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Tobie van den Berg; Bas van Manen; Ton van der Laan; Ioana Ciobotia; Darpan Bansal; Jente Sonneveld | A multidisciplinary modeling system for aircraft structural components | Fokker Aerostructures B.V. - GKN Aerospace | MDO; KBE; structural design; design automation; trade studies; multidisciplinary models | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 9 |
| Alexander Koehler; Marcus T. Knopp | First operational tests with the optical ground station at Trauen | German Aerospace Center | Free-space optical communications; optical ground station; laser-communication; direct-to-Earth laser link; optical LEO downlinks | NEWSPA - New systems for future space operations | Poster | 25 |
| Divek Surujhlal; Viola Wartemann; Alexander Wagner | ReFEx: Reusability Flight Experiment - Aerothermodynamics | German Aerospace Center (DLR) | aerothermodynamics; shock-shock interactions; SWBLIs; hypersonic | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Bas van Manen; Tobie van den Berg; Ton van der Laan; Bram Timmer | A Multidisciplinary Modeling System for Designing Fuselage Structures: Extending the Multidisciplinary Modeler | Fokker Aerostructures | fuselage; structures; multidisciplinary optimization; multidisciplinary analysis; DEFAINE; GKN Fokker | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 9 |
| Jaap van Muijden; Jos Aalbers | First Order Thermal Analysis Methodology for Hybrid-Electric Propelled Aircraft in Early Design Stages | NLR | Thermal Management System; Predesign; Heat Rejection; Hybrid-Electric Propulsion | HEPAEM - Hybrid Electric Propulsion | Oral | 2 |
| Jose Luis Redondo Gutierrez; Johannes Robens; Björn Gäßler; Pablo Bernal Polo; Paul Acquatella; David Seelbinder; Stephan Theil | ReFEx: Reusability Flight Experiment – Architecture and Algorithmic Design of the GNC Subsystem | German Aerospace Center (DLR) | GNC; ReFEx; Convex Guidance; INDI; EKF | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Xiaodong Yu; Hongsheng Yu; Wei Zhang; Luigi T. DeLuca; Ruiqi Shen | A new combustion phenomenon: penetrative combustion of 3D printed fuel grain for hybrid rocket engine | Nanjing University of Science and Technology | hybrid rocket propulsion; fuels; combustion; 3D printing | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| ?ukasz Jan Kapusta; Bartosz Ka?mierski | Flash-boiling effect on spray formed by two impinging jets | Warsaw University of Technology | spray; injection; atomisation; flash boiling; impinging jets | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| Johannes Robens; Björn Gäßler | ReFEx: Reusability Flight Experiment - Design of an Exoatmospheric Control System | German Aerospace Center DLR | Exoatmospheric Control; Trajectory Design; PD-control; Pulse Modulation | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Chenyu Wu;Yufei Zhang | A New Framework for Data-assisted Turbulence Modeling | Tsinghua University | Turbulence;Discrete-adjoint;Symbolic-regression;Data-driven | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Kolb Sebastien | Flight dynamics analysis and trajectory optimization of some gliding phases | Centre de Recherche de l'Ecole de l'Air | PIO; optimal control; nonlinear analysis; sailplane; space shuttle | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Jonas Hoffmeister; Thorben Bruns; Jens Gerstmann | ReFEx: Reusability Flight Experiment - Development of a cold-gas RCS using off-the-shelf components | German Aerospace Center (DLR) | DLR; ReFEx; RLV; GnC; RCS; ballistic; vacuum; 1D simulation; cold-gas; thrusters; off-the-shelf; testing | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Huaiyuan Gu; Fintan Healy; Djamel Rezgui; Jonathan Cooper | Flight Dynamics of Aircraft Incorporating the Semi Aeroelastic Hinge | University of Bristol | Folding wingtips; high aspect ratio wing; semi-aeroelastic hinge; Flight mechanics; Flight handling quality | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Jose Luis Redondo Gutierrez; Leonid Bussler; Peter Rickmers | ReFEx: Reusability Flight Experiment – Flight Safety Analysis | German Aerospace Center (DLR) | Flight Safety; Safety Regulations; Flight Termination System; ReFEx | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| T. Jeremy P. Karpowski; Federica Ferraro; Katharina Henn; Christian Bauer; Christian Hasse | A numerical study of resonance ignition for space propulsion systems | STFS, TU Darmstadt | resonance ignition; CFD; compressible flow; rocket propulsion; open-source; OpenFoam | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| Wojciech GRENDYSA | Flight efficiency of multirotor, new definitions and function sensitivity in-flight tests. | Warsaw University of Technology | UAV; efficiency; multi-rotor; energy | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| Leonid Bussler; Jose Luis Redondo Gutierrez; Peter Rickmers; Sven Stappert | ReFEx: Reusability Flight Experiment - Trajectory Design | German Aerospace Center | Reusability; hypersonics; reentry trajectory | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Hongyu Qiao; Shuanghou Deng; Fan Qing; Tianhang Xiao | A Numerical Virtual Flight Platform Development and its Application on High Maneuverability Flight Vehicles | Nanjing University of Aeronautics and Astronautics | Numerical Virtual Flight; High Maneuverability | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 18 |
| Giuseppe Di Martino; Jonas Peichl; Fabian Hufgard; Christian Duernhofer; Stefan Loehle | Flight Experiment of Transpiration Cooled Sharp Edge Fins on the Sounding Rocket HIFLIER1 | Deutsches Zentrum für Luft-und Raumfahrt | Transpiration Cooling; Sounding Rocket; Flight Experiment | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 4 |
| Alexander Schmidt; Andreas Kimpe; Philipp Rosenheimer; Sebastian Weiß; Markus Wittkamp | ReFEx: Reusability Flight Experiment-Planning a MORABA Campaign in South Australia | DLR German Aerospace Center | MORABA; Mobile Rocket Base; Telemetry; Ground Infrastructure; Data Handling; Flight Termination; Launch Campaign; South Australia | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 1 |
| Nicolas Tantot; Panagiotis Giannakakis; Henri Yesilcimen; Anthony Binder | A performance modelling approach to open fan propeller module | Safran SA | Propeller; Performance | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 2 |
| Felix Schäfer; Georg Herdrich; Oleksii Balagurin | Flight results of the miniature 1J pulsed plasma thruster PETRUS | Institute of Space Systems, Univerity Stuttgart | Electric Propulsion; Pulsed Plasma Thruster; CubeSat; Flight results | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| Cédric Dupont; Luc Littré; Pascal Barbier; Alexis Paillet; Grégory Navarro | Regenerative Fuel Cell System technologies development | Air Liquide Advanced Technologies | Fuel cell; electrolyzer; energy storage; moon | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Ainardi; Storck; Estejel; Baratte | A prospective market & business perspective on Lunar ISRU for propellant applications | Arthur D. Little | Sustainability; value chain; ecosystem; prospective | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Albert Zajdel; Micha? Welcer; Cezary Szczepa?ski; Mariusz Krawczyk | Flight test verification of Hardware in the Loop simulations of the PZL-130 Orlik aircraft stabilization system that uses trim tabs in the lateral channel | ?ukasiewicz Research Network - Institute of Aviation | Flight stabilization; trim tabs; flight tests; simulations | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Bhaskar Biswas ; Dmitry Ignatyev ; Argyrios Zolotas ; Antonios Tsourdos | Region of Attraction Estimation Using Multiple Shape Functions in Sum-of-Squares Optimization for Aerospace System | Cranfield University, U.K. | Stability; Region of Attraction; Sum-of-Squares; Shape Function | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Fateme Baneshi; Manuel Soler | A Reinforcement Learning Approach to Conflict Resolution of Climate Optimal Trajectories | Department of Aerospace Engineering, Universidad Carlos III de Madrid | Climate impact; Aircraft trajectory optimization; Conflict resolution; Deep reinforcement learning | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Pinar ENEREN; Frederik MERTENS; Yunus Tansu AKSOY; Arthur VANGEFFELEN; Claudia ESPOSITO; Johan STEELANT; Maria Rosaria VETRANO | FLOw boiling REgimes iN microgravity Conditions Experiment (FLORENCE): REXUS-27 sounding rocket campaign | KU Leuven | Flow boiling; Microgravity; Sounding rocket experiment | TESTING - Testing in Aerospace | Oral | 2 |
| Yulia Akisheva; Yves Gourinat; Cédric Dossat; Susanna Guatelli; Steven Robin-Chabanne; Athina Varotsou; Aidan Cowley; Advenit Makaya | Regolith-based Lunar Habitats - an Engineering Approach to Radiation Shielding | Institut Supérieur de l'Aéronautique et de l'Espace (ISAE) | Regolith; radiation protection; habitat | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 3 |
| R?zvan-Ionu? B?LA?A; Marian-Ciprian BÎLU; C?t?lin IORDACHE | A Reinforcement Learning approach to UAV trajectory configuration | National Institute for Aerospace Research "Elie Carafoli" - INCAS | UAV; Reinforcement Learning; Proximal Policy Optimization; Trajectory Optimization | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Poster | 67 |
| Yogeshwaran G; Srisha Rao M V; Jagadeesh G | Flow Characteristics of a Flat Plate Airfoil Resembling Spinning Samara using PIV | Indian Institute of Science, Bangalore | Spinning samaras; Flat plate airfoil; aerodynamic coefficients; PIV | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| Micha? B?a?ejczyk | RelGNCPy: A simulation toolkit for relative Guidance, Navigation and Control in Satellite Formations | AGH University of Science and Technology | guidance; navigation; control; satellite; formation; relative; ptototyping; propagation; Clohessy-Wiltshire; toolkit; simulation; cross-track; synchronisation | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Dominik Reinhardt; Dr. Abdessalem Bouferrouk | A Simplified Digital Twin Framework of a Trainer Aircraft to Enhance Flight Testing | UWE Bristol | FDGNCAV; SUSTAV; UAVFUT | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Poster | 68 |
| Deyou Wang; Ge Jin; Ruyao Wang; Shipeng Li | Flow separation characteristics of supersonic nozzles in water environment | Beijing Institute of Technology | Underwater jet propulsion; Supersonic nozzles; Flow separation; Water environment; Unsteady characteristics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Poster | 1 |
| Gianluca Liggieri; Adrien Boiron; Bjørn Espen Hansen; Henning Josefsen; Elliott Worsley; Anthony Haynes | RELIANCE - Design, Manufacturing and Testing of the Breadboard Engine | Nammo Raufoss AS | liquid rocket propulsion; breadboard engine; hypergolic storable propellants; high performance; throttleable; moon lander | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Patrick Hendrick; Julien Gagnon; Thomas Laporte | A small long endurance LTA with H2 as lift gas and FC propulsion system | ULB | long endurance; drone; LTA; H2 | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 1 |
| Adrien Boiron; Anthony Haynes; Henning Josefsen; Gianluca Liggieri; Nuria Minguez Esteve; Jørn Inge Ruud; Elliott Worsley | RELIANCE, an electric pump-fed main engine for ESA’s lunar lander | Nammo Raufoss AS | bi-propellant rocket engine; moon; exploration; lunar lander | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 2 |
| Bykerk; Tamas | A standard model for the investigation of aerodynamic and aerothermal loads on a re-usable launch vehicle | DLR | reusable; cfd; standard model;aerodynamics; aerothermodynamics | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Michael Linder; Aziz Belkhiria; Robin Bonny; Joaquim Silveira; Santiago Evangelista; Nicolas Bouron; Saverio Nasturzio; Taras Pavliv; Rico Fausch | Four Months to Orbit: Fast-Tracking CubeSat Development for Reliability Through In-Orbit-Demonstrations | EPFL | CubeSat; OBC; IOD; onboard computer; hosted payload; risk reduction | STUDENT - Space Student Projects | Oral | 2 |
| Francesco Tufano; Cesario Vincenzo Angelino; Edoardo Bucchignani | Repeatable and scalable Image Acquisition from Drone equipped with Multispectral and Thermal Sensor for proximal sensing processing of Nature Based Solutions | CIRA | Proximal Sensing; NBS; Multispectral Sensor | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Yi Li; Yu Lei; Yiye Xia; Yiwei Chen | A Study of the Online Atmospheric Flow Field Modelling with Low Cost IMU for a Soaring UAV | Northwestern Polytechnical University | Soaring; atmosphere flow field; UAV | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Reject | |
| Ye Xiao; Xingchen Li; Wen Yao; Yi Xiao | FRA-GRU: A Deep Learning model for vessel trajectory prediction based on satellite AIS data | Hunan University | Automatic Identification System (AIS); maritime transport; gated recurrent unit (GRU); vessel trajectory prediction | NEWSPA - New systems for future space operations | Poster | 24 |
| Elias; Khiar; Severac; Morilhat; Luyssen; Tobeli; Bur; Doudet; Wattellier; Bizet; André; Mahieu; Mysyrowicz; Houard | Repetitive Femtosecond Laser Energy deposition for Supersonic Flow Control | ONERA | Laser; Supersonic; energy deposition; femtosecond | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Poster | 20 |
| Salvatore Esposito; Domenic D' Ambrosio | A Study on Plasma Formation on Hypersonic Vehicles using Computational Fluid Dynamics | Politecnico di Torino | Hypersonics; Plasma | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Dániel G. Kovács; Guillaume Grossir; Grigorios Dimitriadis; Olivier Chazot | Free-flight testing of proximal spheres and cubes in Mach 14 hypersonic flow | von Karman Institute for Fluid Dynamics/University of Liege | Hypersonic; Aerodynamics; Free-flight testing; Proximal bodies; Fragment separation; Longshot | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 |
| Keita Yamamoto; Satoshi Ukai; Mitsuru Shimagaki; Satoshi Kawasaki; Hideyo Negishi | Research Activities on Numerical and Experimental Studies of Cavitation Instabilities in the Rocket Engine Turbopump | JAXA | Rocket engine; turbopump; inducer; cavitation; unsteady phenomena | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| Inrae Kim; Heetae Park; Seungkeun Kim; Xuan-Toa Tran; Hyondong Oh | A Tailless Flapping Wing MAV’s Attitude Stabilization using observer-based sliding mode control | Chungnam National Univ. | Flapping Wing MAV; Finite time Observer; Sliding Mode Control | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Alessandro Munafo’; Sanjeev Kumar; Vincent LeMaout; Vishnu Oruganti; Kelly Stephani; Francesco Panerai; Daniel Bodony; and Marco Panesi* | From First-Principles Physics to Massively Parallel Simulations: A High-Fidelity Plasma Tunnel Model for Hypersonic Flight Conditions | University of Illinois | NLTE Plasmas; ICP; Multiphysics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 |
| Tatsuya HASHIZUME; Toshiki MORITO1; Hiroya ASAKAWA; Toru TSUKANO ;Koichi YONEMOTO | Research and Development of the Small LOX/Methane Propulsion System for an Experimental Reusable Winged Rocket WIRES#015 | JAXA | Methane Propulsion System; Reusable Rocket | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Ceren Cansu Esmek; Assoc. Prof. Dr. Nilay Sezer Uzol | A VERSATILE DYNAMIC ROTOR AND PROPELLER MODEL FOR eVTOL SIMULATION APPLICATIONS | Turkish Aerospace | eVTOL; Dynamic Rotor Model; Dynamic Propeller Model | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| Lukas Werling; Felix Lauck; Julian Dobsuch; Marc Gritzka; Vincent Stratmann | From Lampoldshausen to Orbit: DLR Spin-off GreenDelta and the Development status of Green Propellant Thrusters based on H2O2 and N2O | German Aerospace Center (DLR) | Green Propellants; Nitrous Oxide; Hydrogen Peroxide; Thruster Development; DLR; GreenDelta | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| Henrike Jakob; Justus Albert; Heinz-Peter Schiffer | Research and test activities on sustainable space propulsion systems at TU Darmstadt | Technische Universität Darmstadt | Sustainable space propulsion; miniaturized ignition systems; rotating detonation engines | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 3 |
| Gabriele Guerra; Bastien Haemmeri; Gejr Hovbrender; Christina Klavenes; Turi Røyne Valle; Antonella Viola; Alice Hromadkova; Marco Leonardi; Nicola Ierardo | Achievements and Development Status of the H2O2 based Roll and Attitude Control System for VEGA launchers | Nammo AS | RACS; Green Propellant; H2O2; VEGA; Propulsion | NEWSPA - New systems for future space operations | Oral | 3 |
| Matteo Losacco; Laura Pirovano; Roberto Armellin; Carlos Yanez; Emmanuel Delande; Stéphanie Lizy-Destrez | From short to too-short arcs: admissible states region theory for ground-based observations | ISAE-SUPAERO | Initial orbit determination; admissible regions; short arcs; space debris | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| Yevhen TKACHENKO; Andrea CIARDI; Benjamin KHIAR | Resistive MHD simulations of a self-field Magneto Plasma Dynamic thruster over the 5 to 40 kA current range | Sorbonne University / LERMA | Electric Propulsion; Magneto Plasma Dynamic thrusters; Numerical simulations; Magnetohydrodynamics | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Hernán ASOREY; Mauricio SUÁREZ-DURÁN; Rafael MAYO-GARCÍA | ACORDE: A new method to assess onboard radiation risks related to human factors | Comisión Nacional de Energía Atómica | ACORDE: A new method to assess onboard radiation risks related to human factors | HUMANF - Human factors in Aviation and Space | Oral | 2 |
| Fabien Champalou; David Tchou-kien | From the ground to DREAM ON: ground support equipment to new PERSEUS bi-liquid demonstrator | CT Ingenierie | GROUND SEGMENT; SOUNDING ROCKETS | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| Cédric Dupont; Romain Chauveau; Pascal Barbier; Alexis Paillet; Grégory Navarro | Results of Air Revitalization System study by adsorbent | Air Liquide Advanced Technologies | air revitalisation; purification; CO2 | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 3 |
| Julian Scholl; Lukas Werling; Dominic Freudenmann; Stefan Schlechtriem | Activation Energy Determination of High-Test Peroxide Decomposition in Inconel 718 Crucibles | German Aerospace Center (DLR) | Green Propellants; High-Test Peroxide; Regenerative Cooling; Inconel 718; Differential Scanning Calorimetry | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| Louis-Ashley CAMUS | From Visual Inspections to AI-Driven Checks: Automating Quadrant Star Sensor Calibration Space Operations | OneWeb | Artificial Intelligence; Space operations; Quadrant Star Sensor; Automation | NEWSPA - New systems for future space operations | Poster | 26 |
| Kazuki SAKAKI; Tatsuya HASHIZUME; Toshiki MORITO; Hideaki NANRI; Shinji ISHIHARA; Yasuhiro ISHIKAWA | Results of Hot-fire Testing of 30kN LOX/Methane Full-expander Cycle Engine | Japan Aerospace Exploration Agency | rocket engine; methane; full-expander cycle | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 |
| Jan Sieder-Katzmann; Martin Propst; Ralf Stark; Dirk Schneider; Stephan General; Martin Tajmar; Christian Bach | ACTiVE – Experimental investigation of the pressure distribution of linear aerospike nozzles with aerodynamic thrust vectoring | Technische Universität Dresden | Cold gas experiment; Aerospike nozzle; Aerodynamic thrust vectoring | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 19 |
| Lisa AUDOUARD; Aurélie JULIAN-JANKOWIAK; Jean-François JUSTIN; Pierre BERTRAND; Cécile LANGLADE; Matthieu GARCIA; Lucien VINGERT; Thibaut ARCHER | Functionally Graded Materials designed for thrusters : resistance in combustion environment and under laser thermal flux | ONERA | Functionally Graded Materials; satellites; ultra-refractories | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Frank Neuman | Review of strategies for Stratospheric Airships Low-altitude Return Phase: Challenges and Risk Mitigation Strategy | ULB | HAPS; airships; challenges | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 2 |
| Ulysse Weller; Vaitua Leroi; Fabien Castanet | Activities in space electric propulsion at the French Space Agency – CNES | CNES | Propulsion; Plasma Physics; Thruster; Electric Propulsion; Hall Effect Thruster; | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| Michael Sielemann; Daniel Andersson; Clément Coïc | Fundamentals Of Aircraft Hydrogen Tank Design With System Simulation | Modelon | Cryogenic; boil-off; dormancy; thermal design; mechanical design; insulation | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 1 |
| Kento Kaneko; Akira Oyama; Aiko Yakeno; Shingo Hamada | Riblet surface effect on laminar to turbulent transition by Direct Numerical Simulation | The University of Tokyo | Riblet; DNS; Laminar; Transition | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| Josef Klevanski; Etienne Dumont; Tobias Ecker; Moritz Ertl; Sven Krummen; Bodo Reimann; Johannes Riehmer | Further Progress in Aerodynamic Studies for CALLISTO - Reusable VTVL Launcher First Stage Demonstrator | DLR | Reusability; CALLISTO; Demonstrator; VTVL; Aerodynamics; Aerothermodynamics; Database | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 2 |
| Timothy JØRAHOLMEN; Stian KORSVOLD; Pål SANDVOLD; Øystein LUKTVASSLIMO; Knut Erik NILSBERG | Roadmap Towards a Qualified Aluminium Green Propellant Diaphragm Tank | Nammo | Green propellant; HTP; Diaphragm tank development | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 8 |
| Heinz WIPF | Advanced RNP Helicopter Procedure and Instrument Flight Procedure Design | AIRNAV CONSULTING GmbH | flight trials; Performance Based Navigation (PBN); helicopter operations; Navigation System Error; Total System Error; GPS/SBAS NAV sensor; IFP design; low RNP values | TESTING - Testing in Aerospace | Oral | 2 |
| Angelo Tomassini; Irene Cruciani; Christian Pomponi | GNC Improvements between Vega and Vega-C | Avio spa | GNC; Launcher; Flexibility; Avio; Software; TVC | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Xin Zhang; Jiyuan Sun; Shushi Wang | Robust Adaptive Switching Control of Hypersonic Reentry Vehicle based on Q-learning | Academy of Astronautics. Nanjing University of Aeronautcs & Astronautics | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 14 | |
| T. Effing; P. Mauerer; E. Stumpf | Advancements in the development of a novel wing design method in conceptual aircraft design | RWTH Aachen University | conceptual aircraft design; wing design; variable camber | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Marco SABATINI; Paolo GASBARRI; Giovanni B. PALMERINI | GNSS relative navigation for operations in cislunar space | Scuola di Ingegneria Aerospaziale, Sapienza Università di Roma | Cislunar Operations; Lunar Formation Flying; Lunar GNSS | NEWSPA - New systems for future space operations | Oral | 3 |
| Gianni Pecora; Elisa Capello; Giuseppe Di Pasquale; Manuel Sanjurjo-Rivo | Robust Attitude Control Using Electrospray Thrusters | IENAI SPACE | electric propulsion; robust control | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Kate UNDERHILL; Andreas FLOCK; Stephane DUSSY | Advancements in Upper Stage Technologies and Design within ESA’s Future Launchers Preparatory Programme (FLPP) | ESA | CFRP; Tank; Stage; Mass | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 6 |
| José Manuel Chorro Martínez; Óscar del Rincón Fernández; José Esteban Gómez Viñas; José María Pérez Hernández | Gravel Deflector Aircraft Integration | AIRBUS | Gravel deflector; C295; structural dynamics; system; | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 6 |
| Patrick Wegener | Robust CAD Methodology for CFD optimizations | German Aerospace Center (DLR) | CAD; CFD; DLR-F25 | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| G. Herdrich; P. Maier; K. Papavramidis; J. Skalden; S. Klinkner; S. Fasoulas; A. Wiegand; M. Walther; L. Walpot; E.B. Borras; B. Duesmann | Advancements of a VLEO satellite system study utilizing an RF Helicon-based Plasma Thruster | Institute of Space Systems (IRS), University of Stuttgart | VLEO; ABEP; RF-Helicon Plasma Thruster; Platform Design | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Florian Merz; Marius Wilhelm; Till Hörger; Lukas Bischof; Fabio Addario; Dr. Christoph Kirchberger; Prof. Dr. Stefan Schlechtriem | Green Propulsion Demonstrator “The LÄNDer” | German Aerospace Center (DLR) | Lander; GNC; Green Propulsion; Reinforcment Learning | TESTING - Testing in Aerospace | Oral | 1 |
| Abolfazl Simorgh; Manuel Soler | Robust climate optimal flight planning toward identifying “win-win” solutions: concept of equivalent CO2 emissions | Universidad Carlos III de Madrid | Climate impact; Aircraft trajectory optimization; Meteorological uncertainty; Robustness; Climate policy; Operating cost. | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Shota TANIGUCHI; Atsushi SHINOZUKA; Ryota FUKUCHI; Kanako YASUE; Akira OYAMA | Aerodynamic Analysis of Tandem Tilt-Wing eVTOL Aircraft in Cruise Phase | The University of Tokyo | eVTOL; aerodynamics; CFD; wind tunnel experiment | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| Raul Bajimaya; David MacManus; Chawki Abdessemed; Ioannis Goulos; Jesús Matesanz García; Christopher Sheaf; Vasileios Kyritsis | Heat exchanger integration into an aero-engine bypass duct | Cranfield University | Computational Fluid Dynamics; Embedded Heat Exchanger Systems; Mixed-Fidelity methods; Design Space Exploration | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 3 |
| WILKINS Robbie; BOUFERROUK Abdessalem | Numerical framework for aerodynamic and aeroacoustics of bio-inspired UAV blades | University of the West of England | drone; bio-inspired; CFD; multi-rotor; UAV | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 |
| Serguei PONIAEV; Nikolay Monakhov; Tatiana Lapushkina; Valery Sakharov; Roman Kurakin; Pavel Popov | Heat flux measurement during short run-time shock-tube experiments | Heat flux; experiment; shock tube; sensors | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 | |
| Julia Guimaraes; Waldemar Leite Filho | Robustness analysis for closed-loop model reference adaptive attitude control for a satellite launcher | INPE | model reference adaptive control; satellite launcher attitude control; robustness analysis | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Moritz Ertl; Tobias Ecker | Aerodynamic and aerothermal comparison between the CAL1C and CAL1D geometries for the CALLISTO vehicle | DLR | CFD; RANS; VTVL; CALLISTO; Aerothermodynamics; Landing Legs | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 5 |
| Donato Fontanarosa; Guido Marseglia; Maria Assunta Signore; Angelica Maria Toscano; Johan Steelant; Maria Grazia De Giorgi; Luca Francioso; Maria Rosaria Vetrano | Heat Transfer Assessment in a Vaporizing Liquid Microthruster undergoing Dual Heating Control | Dept. Mechanical Engineering - KU Leuven | micropropulsion; VLM; micro flow boiling; heat transfer enhancement; dual heating control | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 3 |
| Olga AKSENOVA; Iskander KHALIDOV | Rough Surface Calculation in Rarefied Gas Flow Applying the Solution of Inverse Problem | Rough Surface; Rarefied Gas Flow; Numerical Calculation; Inverse Problem | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 | |
| Junhyun Lim; Heetae Park; Jinyoung Suk; Seungkeun Kim | Aerodynamic Parameter Estimation for Fixed-wing UAV Using Iterated Extended Kalman Filter | ChungNam National University | Aerodynamic Parameter Estimation; Unmanned Aerial Vehicle (UAV); Iterated Extended Kalman Filter | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Jinrae Kim; Hanna Lee; Youdan Kim | Safe Attitude Controller Design for Multicopter via High-order Control Barrier Function | Seoul National University | Safe control; High-order control barrier function; multicopter; attitude dynamics | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Victor Maldonado; Dioser Santos | Aerodynamic Performance of a Small Flying Wing UAV Using Passive Bio-Inspired Microfibers | Texas Tech University | Passive flow control; microfibers; UAV; aerodynamics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| Jakub Kocjan; Stanis?aw Kachel; Robert Rogólski | Helicopter main rotor blade structure parametric optimization using graphic programming language | Military University of Technology Warsaw | helicopter; main rotor; rotor blade; geometric modelling; optimisation; CFD | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 6 |
| BOUHAFID Younes; BONNE Nicolas; JACQUIN Laurent | Aerodynamic simulation of the near-field of an aircraft using different mesh adaptation strategies | ONERA | RANS; Near-field Aerodynamics; Mesh Adaptation; Contrails | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Pierre Bernigaud; Dmitry DAVIDENKO; Laurent CATOIRE | Heterogeneous Combustion of AP / HTPB / RDX with Detailed Kinetics | ONERA | AP; HTPB; RDX; Composite propellants; Heterogeneous combustion; Detailed kinetics | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 15 |
| Minho Lee; Changjong Lee; Jungyeom Kim; Hwanil Huh | Safety review of lithium ion battery for space environment through modeling and simulation | Chungnam National University | TESTING; NEWSPA; | TESTING - Testing in Aerospace | Oral | 1 |
| Jiri Cecrdle | Aeroelastic Demonstrator and Methodology for Experimental Investigation of Propeller Aerodynamic Derivatives | Czech Aerospace Research Centre (VZLU) | whirl flutter; aerodynamic derivative; W-STING demonstrator | TESTING - Testing in Aerospace | Poster | 58 |
| Giuseppe Mantegna; Carmelo Rosario Vindigni; Davide Tumino; Calogero Orlando; Andrea Alaimo | Sandwich hybrid structural component for tilt rotor aircraft | University of Enna Kore | Design; Hybrid structures; Lattice; Additive Manufacturing; | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 4 |
| Bara'ah Fraihat; Rafic Ajaj | Aeroelastic tailoring of a composite cantilever stiffened-plate | Khalifa University of Science and Technology | Aeroelasticity; aeroelastic tailoring; flutter; divergence; aeroelastic instabilities | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 5 |
| Ciro Salvi; Lars Steffens; Oliver Hohn; Ali Gülhan; Filippo Maggi | High Enthalpy Flow Characterization Using Tunable Diode Laser Absorption Spectroscopy | DLR | TDLAS; DLAS; Non intrusive; Hypersonic; High Enthalpy; Arc-Heated Wind Tunnel; Mars | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 |
| Pietro Roncioni; Marco Marini; Sara Di Benedetto | Aeropropulsive Assessment of the Scramjet Hypersonic Experimental Vehicle | CIRA | CFD; Aerodynamic; Propulsion | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Joao Felipe de Araujo Martos; Alessandro Marinii; Henrique Gustavo Argentieri | High speed flight experimental test capability development in the UAE | Technology Innovation Institute - TII | High Speed Flight; Ludwieg Tube; Combustor test facility | TESTING - Testing in Aerospace | Oral | 1 |
| Jérôme HILDEBRANDT; Alexandros VIKAS; Fabio SCHNEIDER; Johannes KAUFMANN; Stefanos FASOULAS; Georg HERDRICH; Sabine KLINKNER | Satellite Water Propulsion: 3D Printed Ceramic Thruster & Space Debris Mitigation Concept | Institute of Space Systems, University of Stuttgart | Water electrolysis propulsion; green propulsion; ALM; thruster; ceramics; hydrogen; oxygen; gox; gh2; ALM; space debris mitigation | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 |
| Thomas Decker; Robin Devillers; Stany Gallier | Agglomeration in solid propellants loaded with inert particles – Study of propellant formulation influence using Shadowgraphy Image Processing | ONERA | solid propellant; agglomeration; shadowgraphy; image processing; combustion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 15 |
| Kamil Piecha; Tomasz Palacz; Bart?omiej Krzeczkowski; Jakub Ko?cielniak | High thrust, low power, green propellant electro-thermal resistojet thruster | Liftero | green propellant; resistojet; propulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| Alexandros Vikas; Jérôme Hildebrandt; David Wanke; Stefanos Fasoulas; Sabine Klinkner | Satellite Water Propulsion: Electrolyzer Development & FMEA | Istitute of Space Systems | Water Propulsion; Green Propulsion; Satellite Propulsion; Electrolysis; Hydrogen | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 14 |
| Tobiasz Mayer; Witold W?sowski; Adrian Morawiec; Roman Górecki | Agile component of infrastructure in New Space companies | Sie? Badawcza ?ukasiewicz – Instytut Lotnictwa | Test Facilities; New Space; Rocket Launchpads; Space Economy; Ground Infrastructure | NEWSPA - New systems for future space operations | Oral | 2 |
| Matteo Filippi; Rodolfo Azzara; Erasmo Carrera | High-fidelity multidimensional models for stress and dynamic analyses of advanced helicopter blades | Politecnico di Torino | rotordynamics; stress analysis; vibrations; higher-order models; finite element method | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Maurice F.M. HOOGREEF; Vincent O. BONNIN; Bruno F. SANTOS; Federico MORLUPO; Nicolas F.M. WAHLER; Ali ELHAM | Scalability assessment of hybrid-electric technology application to various aircraft classes – an overview of opportunities and challenges | Delft University of Technology | hybrid-electric aircraft; distributed electric propulsion; aircraft design | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Michael WEINOLD; Philipp ROHRER; Russell McKENNA | Aircraft Fuel Efficiency Improvements: The Pathway to Evidence-Based Forecasts | PSI | sustainable aviation; fuel efficiency; net zero | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Daniel Muradas; Felix Nieto; Santiago Hernandez | High-fidelity RANS simulations of subsonic and supersonic performance of an Experimental HTB aircraft at 0º, 5º and 10º angles of attack | University of Coruña | CFD simulations; Supersonic vehicles; High fidelity models | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Andrea Aprovitola; Luigi Iuspa; Giuseppe Pezzella; Antonio Viviani | Airfoil aerodynamic optimization for Mars exploration aircraft | Department of Engineering at the University of Campania | airfoil aerodynamic optimization; low Reynolds aerodynamics; mars exploration aircraft | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 2 |
| Baptiste LEGRAND; Nicolas CURLIER; Arnaud GAILLARD; David BOUQUAIN | High-level Sizing Method for Hybrid Electric Distributed Propulsion Aircraft | Avions Mauboussin | Sizing; light aircraft; hybrid; distributed propulsion; model-based design; electricity; hydrogen | HEPAEM - Hybrid Electric Propulsion | Oral | 1 |
| Jonathan Cooper; Huaiyuan Gu | Scaling of Aircraft Incorporating the Semi Aeroelastic Hinged Wings | University of Bristol | Sustainable aircraft design; aeroelasticity; folding wing-tips | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Juan Francisco Reyes; Gustavo Alonso | Alignment of national and European R&I aviation funding programmes | Universidad Politecnica de Madrid | research and innovation; funding programmes; aviation | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Andreas Losch; André Galli; Thomas Schildknecht | History, Concepts and Challenges of suggesting an 18th UN Sustainable Development Goal related to Space | University of Bern | SDG18;space;environment;sustainability;development;goal;history | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| Kirill Shilov | All-in-one integrated UAV avionics architecture with AI capabilities and 5G connectivity | Sky-Drones Technologies Ltd | Autopilot; Navigation; UAV; Architecture; Flight controller; Mission Computer; Connectivity; AI; 5G | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 8 |
| Crenguta LEAUA; George LEAUA | Houston We Have a Solution: Alternative Thinkers in Space | The Swiss Institute of Alternative Thinking | Alternative Thinking; Astronauts; Space Workforce Development | HUMANF - Human factors in Aviation and Space | Reject | |
| Ruofan Zhang?Xingchen Li?Wen Yao | Semi-supervised temperature field information fusion method based on taylor modal decomposition for spacecraft application | National University of Defense Technology | spacecraft temperature?information fusion?semi-supervised?taylor modal decomposition | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Mohammad Moniripiri; Pedro P. C. Brito; André V. G. Cavalieri; Ney R. Sêcco; Ardeshir Hanifi | An adjoint-based approach for finding smooth surface waviness tolerances for natural laminar flow design | KTH Royal Institute of Technology | adjoint-based optimization; natural laminar flow; boundary layer transition; manufacturing tolerances; surface waviness | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 2 |
| Yang Xie; Xingchen Li; Ning Wang; Wen Yao | Hybrid Digital Twin for Satellite Attitude Control System Based on FMI Co-Simulation Technology | Chinese Academy of Military Sciences | Hybrid digital twin; Satellite; FMI; Co-simulation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| Andrea De Vittori; Camilla Colombo; Matteo Omodei; Juan Luis Gonzalo; Michele Maestrini; Pierluigi Di Lizia; Pau Gago Padreny; Marc Torras Ribell; Ángel Gallego Torrego; Diego Escobar Antón; Roberto Armellin | Sensitivity analysis of collision avoidance manoeuvre with low thrust propulsion | Politecnico di Milano | Collision avoidance manoeuvres; Conjunction data messages; low thrust; semi analytical methods | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| Irryhl Mohammedi; David Gucik-Derigny; David Henry | An arbitrary order H? interval filter for spacecraft navigation units | IMS Laboratory - Université de Bordeaux | Interval Estimation; H? Filter ; Space Application; Control System | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| SYAHIN ABU TALIB; ZINNYRAH METHAL; MOHD ROSDZIMIN ABDUL RAHMAN; MARK QUINN; SHAN ZHONG; BENZI JOHN; MOHD RASHDAN SAAD | Hybrid Flow Control on Hypersonic Flow Shock Wave Boundary Layer Interactions: Combination of Micro-Ramp and Jet Blowing | NATIONAL DEFENCE UNIVERSITY OF MALAYSIA | hypersonic; mach5; flow-control; micro-ramp; jet-blowing | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 |
| Iñigo Alforja Ruiz; Alberto Sarritzu; Lily Blondel-Canepari; Angelo Pasini; Michèle Lavagna | Sensitivity analysis of GNC strategies to propulsion system parameters for multi-orbits deliveries | Politecnico di Milano | orbital transfer; optimized delivery sequence; mission strategy; propulsion system parameters; system-level choices; iteration loop | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Pierre-Alexis Joumel et al. | An Economically Viable Lunar ISRU Process for Oxygen and Metal Production and Related Benefits for Terrestrial Applications | Air Liquide Advanced Technologies | ISRU; O2 | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Bram van de Kamp; Markus Kleineberg; Andreas Schröder | Hybrid Laminar Flow Control ready for Series Application | DLR | Laminarity; HLFC; CFRP; | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Alessandro Montanari; Paolo Maria Zolla; Simone D'Alessandro; Marco Pizzarelli; Francesco Nasuti; Rocco Carmine Pellegrini; Enrico Cavallini | Sensitivity study on a low order model for the analysis of transverse combustion instability | Sapienza University of Rome | Liquid Rocket Engines; High-Frequency Combustion Instability; Low order modeling; Response Function | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Jakob Balkenhohl; Nicholas Rattenbury; John Cater | An Experimental Setup for the Performance Analysis of Low-Power Hollow Cathodes at High Applied Magnetic Field Strengths | The University of Auckland | Hollow Cathodes; Plasma Diagnostics; Applied-Field Magnetoplasmadynamic Thrusters; Electric Propulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| Antoine Clout; Adrien Langenais; Yann Dauvois; Luc Mieussens; Julien Labaune | Hybrid NS-DSMC simulation of a full scale solid rocket motor reactive exhaust at high altitude | ONERA | Rocket propulsion; Rarefied flow; Numerical simulation; RANS; DSMC; Coupling | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| Stefano Farì; David Seelbinder; Stephan Theil; Pedro Simplicio; Samir Bennani | Sensor fault detection and isolation for electro-mechanical actuators in a reusable launch vehicle TVC system | German Aerospace Center (DLR) | Fault detection and isolation; TVC; Reusable launch vehicles; Electro-mechanical actuators; Fault tolerance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| Jiang Shao; Qingrui Zhou; Dong Ye; Yan Xiao; Franco Bernelli-Zazzera; Zhaowei Sun | An Indirect Estimation Approach of Underactuated Evader Strategy for Orbital Pursuit-evasion Game | China Academy of Space Technology | pursuit-evasion game; underactuated spacecraft; saddle-point strategy pair; differential Riccati equation | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Gabriele MANGIONI; Renato Marocco; Giovanni Maria Crispino; Daniele Bianchi; Stefano Mungiguerra; Raffaele Savino | Hybrid Rocket Engines Design for Materials Characterization | AVIO | Hybrid Rocket Engine; Materials Characterization | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Tânia Ferreira; Juan Alonso; Catherine Gorle | Setting up a framework for the high-fidelity simulations of contrails from future hydrogen-fueled aircraft | Stanford University | CFD; atmospheric flows; ice microphysics; contrails; hydrogen aircraft | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 3 |
| A. Raju Kulkarni; D. Bansal; F. Mendes Fernandes; G. La Rocca; R. Augustinus; B. Timmer | An MBSE approach to support Knowledge Based Engineering application development | Technische Universiteit Delft | MBSE; KBE; Design Automation; EWIS; DEFAINE | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 10 |
| M. Ferri; A. Verga; B. Vercelli; R. Donnini; S. Dossi; A. Murgia; L. Galfetti | Hydrogen generation from aluminum composites hydrolysis for space propulsion | Politecnico di Milano DAER Dep | In-space propulsion; on-board hydrogen generation; micropropulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 |
| Francesca Rossetti; Marco Pizzarelli; Rocco Pellegrini; Enrico Cavallini; Matteo Bernardini | Setup of a numerical methodology for the study of active-pressurization of cryogenic tanks | Sapienza university of Rome | CFD; tank active-pressurization; cryogenic; VOF; turbulence; thermal stratification | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| Immo Huismann; Stefan Fechter | HyperCODA -- Stabilization methods for hypersonic flows | Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR) | CFD; hypersonic flow; finite volume method; numerical software | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Poster | 7 |
| Albina Tropina | Shell models of turbulence in aero-optics | Texas A&M University | Turbulence; shell model; aero-optics; non-equilibrium | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Giuseppe Fiore | An overview on CNES progresses on space turbopumps design-to-additive | CNES | Turbopump; additive manufacturing; material characterization; design-to-fabrication | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Cancelled | |
| Stefania Carlotti; Luca Caffiero; Davide Orlandi; Filippo Maggi | Hypergolic ignition of amine-based fuels with hydrogen peroxide | Politecnico di Milano | liquid rocket; hydrogen peroxide; green fuels; hypergolicity | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 13 |
| Romain Cariou; Maria Planells-Valencia; Julien Gaume; Yannick Roujol; Jean-Baptiste Charpentier; Clément Jamin; Aude Derrier; Magali Davenet; Philippe Voarino | Silicon photovoltaics, a low cost technology to power HAPS and Satellites constellations | CEA | Silicon; Photovoltaics; HAPS; constellations | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 1 |
| Vincent Dubourg; Stéphane Louvel; Stéphanie Venel; François Vacher; Frédéric Thoumieux | An update of the CNES stratospheric balloon activities | CNES | Aerostats; Balloons; CNES; HAPS; Launch campaign; Science | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 1 |
| Sophie C. Ricker; Michael Mauch; Dominic Freudenmann; Stefan Schlechtriem | Hypergolic Propellants with Hydrogen Peroxide: Carbon-Based Nanomaterials as Additives in Ionic Liquid Fuels | DLR (German Aerospace Center) | Green Propellants; Hydrogen Peroxide; Nanoparticles; Hypergolic Fuels; Ionic Liquids | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 13 |
| Gianluca Cocirla; Marco Grossi; Mario Tindaro Migliorino; Daniele Bianchi; Francesco Nasuti | Simplified Numerical Modeling of Film Cooling and Mixture Ratio Bias in Liquid Rocket Thrust Chambers | Sapienza University of Rome | Liquid Rocket Engines; Film Cooling; Mixture Ratio Bias | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 19 |
| George Lampeas ; George Tzoumakis | Analysis and simulation of a cryogenic hydrogen aircraft fuel tank | UNIV. PATRAS | hydrogen; tank; simulation | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 1 |
| Mi Jang; Hyun-Cheol Shin; Jae-Sang Park | Hypervelocity impact simulations between space objects with various shapes and lattice core sandwich panels | Chungnam National University | Space debris; Hypervelocity impact; space shielding system; Lattice Core Sandwich Panel | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| Michael Moroff; Sebastian Wurster; Philip Pietrek | Simulation of heterogeneous Solid Rocket Motors with the Level-Set Method | Fraunhofer | Solid Rocket Motor; Simulation; Volume-Of-Fluid-Method; Level-Set-Method | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 15 |
| Mathilde Ridard; Bruno Van-Ootegem; Grégory Pinaud; Kevin Haras | Analysis of an arc heated air plasma generator for material screening applications | ArianeGroup | arc heated air plasma generator;composite material; ablation; oxidation | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Federica GALLI; Giuseppe FIORE; Vincent SIRCOULOMB; Ghaleb HOBLOS; Philippe WEBER | Identification of degradation profiles for turbopump bearings in reusable liquid propellant rocket engines | IRSEEM-CNES | bearing; degradation trend; fatigue | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| Ancelin Rocamora; Julien Labaune; Fabien Tholin; Aymeric Bourlet; Christophe Laux | Simulation of Plasma Injector Module for Plasma Assisted Combustion in scramjet | ONERA | combustion; plasma; supersonic | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 21 |
| Tim Horchler; Stefan Fechter; Sebastian Karl | Analysis of Detailed-Chemistry Schemes for the Numerical Simulation of Supercritical LOx/CH4 Flames | German Aerospace Center (DLR) | Liquid Rocket Engines; LOx/CH4 combustion; CFD; Detailed Chemistry Schemes | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Leo Basov; Martin Grabe | Simulation of plume impingement on flat plates via the hybrid Fokker-Planck – DSMC approach | German Aerospace Center (DLR) | DSMC; Fokker–Planck equation; Rarefied gas flows; Kinetic models | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| S. Förste; Prof. Dr. S. Fasoulas | Analysis of Novel Concepts for the Return of Upper Rocket Stages | Institute of Space Systems (IRS) | Disposal Missions; Upper Rocket Stages; Deployable Entry System | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 3 |
| Robin Scholl; Dominic Freudenmann; Stefan Schlechtriem | Implementation of Microencapsulated Fuels in Combination with Hydrogen Peroxide for Creation of New Monopropellants | German Aerospace Center (DLR) | Hydrogen Peroxide; Microencapsulation; Interfacial Polymerization; Monopropellant; Green Propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| Olga AKSENOVA; Iskander KHALIDOV | Simulation of Rarefied Gas Flow in a Channel Applying Artificial Neuron Network | Rarefied Gas Flow; Channel; Numerical Calculation; Artificial Neuron Network | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 5 | |
| Betti; Pella; Negro; Scali; Bianchi | Analysis of performance dispersion in pyrotechnic igniters employing BKNO3 pellets | Avio spa | pyrotechnic igniter; solid rocket motor; BKNO3 pellets | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 15 |
| Lennart Lobitz; Hendrik Traub; Prof. Sebastian Heimbs; Prof. Christian Hühne; Prof. Peter Horst | Implications of extended hybrid laminar flow control suction panels on structural wing design | TU Braunschweig | HLFC; structural wing design; TPMS | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| Gobereit; Wollenhaupt; Bollmann; Kallina | Simulation of Safety Relevant Aspects of LH2 Systems | DLR | LH2 propulsin; ground infrastructre for fueling; simulation | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 1 |
| Séverin ASTRUC; Paul-Quentin ELIAS | Analysis of perturbative effects of a momentum flux probe in a plasma plume | ONERA | Electric propulsion; probe; thrust; plasma; simulation | TESTING - Testing in Aerospace | Oral | 2 |
| Frederik Mertens; Balasubramanian Nagarajan; Sylvie Castagne; Maria Rosaria Vetrano; Johan Steelant | Improving cooling channel heat transfer via femtosecond laser texturing | KU Leuven | cooling; heat transfer; flow boiling; enhanced surfaces | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Menno Berger; Nabih Naeem; Patrick Ratei; Prajwal Shiva Prakasha; Thomas Zill; Björn Nagel | Simulation-driven design of Advanced Air Mobility vehicles for European Door-to-Door Mobility | German Aerospace Center (DLR) | System of systems; door-to-door; advanced air mobility; agent-based simulation; conceptual aircraft design | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Cancelled | |
| Davide Zuin; Simone La Luna; Filippo Maggi; Nicola Sicignano; Domenico Borrelli | Analysis of Process Parameters Effects on Final Properties of Additively Manufactured Components for Space Applications | Politecnico di Milano | Additive Manufacturing; Selective Laser Melting; Inconel 718; Quality Assurance; Process Parameters; Standardization | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 4 |
| Sevket Utku AYDINLI; Ali Turker KUTAY | Simultaneous Arrival Strategy by Using Learning-Based Approach | Middle East Technical University | Simultaneous Arrival; Cooperative Guidance; Control Guidance; Deep Reinforcement Learning; Missile Guidance | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 17 |
| Massimiliano Gargiulo; Claudia Savarese; Francesco Tufano; Sara Parrilli; Mariavittoria Verrillo; Vincenza Cozzolino; Alessandro Piccolo; Marco De Mizio | Analysis of Soil Contamination Effects on Maize Plant using UAV-Mounted Multispectral Camera | Centro Italiano Ricerca Aerospaziale | UAV; heavy metals; soil contamination; vegetation indices; remote sensing | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Maxime Szymanski; Georges Ghazi; Ruxandra M. Botez | Single and Multi-Agent Reinforcement Learning Approach to Optimise Aircraft Ground Trajectories in Airports | École de technologie supérieure | airport; trajectory optimisation; reinforcement learning; multi-agent; single-agent | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Steffen Callsen; Jascha Wilken; Martin Sippel | Analysis of sonic boom propagation and population disturbance of hypersonic vehicle trajectories | German Aerospace Center (DLR) | sonic boom; hypersonic vehicles; trajectories; population disturbance; multi-objective optimization; evolutionary algorithms; SpaceLiner; Dream Chaser; Space Rider; Starship | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Alexander Shiryaev; Daniel Choukroun | Single-Frame Attitude Determination from Low Resolution Earth Imaging | Ben-Gurion University of the Negev | Attitude estimation; Image registration | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Daniel Hahn; Lennart Lobitz; Matthias Haupt; Sebastian Heimbs | Analysis of the structural behavior of wings with nonlinear components for passive load reduction | Institute of Aircraft Design and Lightweight Structures, TU BRaunschweig | load reduction; nonlinear; wing design | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Merve Kurt; Zeynep Kap; Sinem Senol; Kerem Emre Ercan; Abel Tetteh Sika-Nartey; Yusuf Kocak; Ahmet Koc; Hac? Esiyok; Burcu Selen Caglayan; Ahmet Erhan Aksoylu; Emrah Ozensoy* | Influence of La And Si Promoters on the Anaerobic Heterogeneous Catalytic Decomposition of Ammonium Dinitramide (ADN) via Alumina Supported Iridium Active Sites | Roketsan Missile Inc. | ADN; Monopropellant; Catalytic; Propulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 14 |
| Reza Moosavi | Smart Blade Dynamic Stall Suppression | University of Hertfordshire | Smart blade; Dynamic stall suppression | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Alejandro Gorgues; Rodrigo Castellanos; Javier Nieto-Centenero; Esther Andrés Pérez | Application of a deep neural network for Cp prediction on multiple wing geometries in a transonic regime | Instituto Nacional de Técnica Aeroespacial | Surrogate model; machine learning; deep neural networks; multi-layer perceptron; pressure coefficients | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 2 |
| Dominik Sedlacek; Ankit Kasi; Christian Breitsamter | Influence of the Leading-edge Radius on Vortex Development at Hybrid-Delta-Wing Configurations | Technical University of Munich | Delta wing; Vortex; | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 1 |
| Bart Van Hove; Martina Lofqvist; Davide Bonetti; Mikhail Kokorich | Sonic boom of commercial hypersonic aircraft | https://destinus.ch/ | Hypersonic; Sonic Boom; Aviation; Acoustics; Aerodynamics | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Abrahim Bahari | Application of LLP in Satellite Supply Chain | LLP; Satellite supply chain | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 5 | |
| Arianna Remiddi; Pasquale Eduardo Lapenna; Giuseppe Indelicato; Mauro Valorani; Rocco Carmine Pellegrini; Enrico Cavallini; Marco Pizzarelli; Francesco Creta | Injection characterization of multi-injector rocket combustion chambers | Sapienza University of Rome | Liquid Rocket Engines; Thermal characterization; Data-driven; URANS | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| Tim A. Bulk; William Clark | Space System Certification for Human Spaceflight-Historical Practices and New Approaches for Safety | SAS International | Human Spaceflight; System Safety; Certification | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Sevket Utku AYDINLI; Yagiz KURT; Halil Ersin SOKEN; Ali Turker KUTAY | Application of Vision Based Target Tracking and Motion Planning Algorithms in Dynamic Environment | Middle East Technical University | Motion Planning; Target Tracking; Mobile Robots; Multi-Robot Systems; Deep Reinforcement Learning | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 16 |
| Eliot SIDOMMO; Washington GEORGES | Innovative propulsion technologies for increased CubeSat efficiency | IPSA ONE | ionic propulsion; plasma; grid thruster; rail launcher | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 32 |
| Xin Jin; Baichun Gong; Shihang Yang; Shuang Li; Xianqiang Li | Space-based passive orbital maneuver detection algorithm via a new characterization | Nanjing University of Aeronautics & Astronautics | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 | |
| Leonard Schlag; Clemens Schefels; Kathrin Helmsauer | Applying Machine Learning to Routine Satellite Ground Segment Operations by Means of Automated Anomaly Detection | DLR | machine-learning; novelty detection; ground segment | NEWSPA - New systems for future space operations | Oral | 2 |
| Eliot DE MAGNEVAL; Issam HRAZMI; Killian BEURET | INSIDeR : Innovative Net & Space Inflatable structures for active Debris Removal | CT INGENIERIE | Active debris removal; sustainable space; new space; kit; ground demonstrator; inflatable structure; net; mission analysis; debris; capture; LEO | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 |
| Redouane Lombarkia; Augustin Gakwaya | SPH Technique for enhancing prediction of crash behavior of plain weave fabric composites coupons | ulaval | Crashworthiness; Plain weave fabric composites; Finite Element Method (FEM); Smoothed Particle Hydrodynamics (SPH). | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Balack; Philip; Atanasov; Georgi; Zill; Thomas | Architectural Trade-offs for a Hybrid-Electric Regional Aircraft | German Aerospace Center DLR e.V. | Conceptual Aircraft Design; Hybrid-Electric; Propulsion Architectures | HEPAEM - Hybrid Electric Propulsion | Oral | 1 |
| Ohad Gur; Avi Ayele; Marek Polcak; Radovan Dite; Jan Hubacek | Installation Effect on Hover Propeller Performance | Ohad Gur Aerospace engineer | Propeller; performane; hover; uam | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| Stoliaroff | Ariane 6 IMA Separation Test | Arianegroup | Separation; test; Ariane 6 | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Poster | 2 |
| Félix POLLET; Scott DELBECQ; Marc BUDINGER; Jean-Marc MOSCHETTA; Thomas PLANES | Integrating Environmental Life Cycle Assessments in the Design Optimization of Electric UAVs | ISAE-SUPAERO | Life Cycle Assessment; Multidisciplinary Design Optimization; UAV | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 2 |
| Yun Hyeong Kang; Chang Han Bae; Hong Yeong Park; Jae Won Lee; Jong Hyun Kim; Jeong Soo Kim | Spray Behavior of Bi-swirl Injector in a LOx/LNG Small Rocket Engine | Pukyong National University | Bi-swirl Injector; Cold-flow Test; Spray Behavior; Flow Visualization | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 6 |
| Francois Peyraud | Ariane 6 ULPM multi boost mission development, a system multi disciplinary challenge | ArianeGroup | Cryogenic; upper stage | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Giorgia Foschi; Fabrice Thouverez; Laurent Blanc; Giuseppe Fiore; Giampiero Pampolini; Patrick Girard | Stability analysis of simplified labyrinth seals model to geometric and flow hypotheses | Ecole Centrale de Lyon | Labyrinth seals; aeroelasticity; strong fluid-structure coupling; stability | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 2 |
| Anton Ivanov;Alexey Simonov;Nidhish Raj | Artificial Intelligence in Planetary Exploration: Enabling Autonomous Decision-Making for Spacecraft | Technology Innovation Institute | autonomy; planetary exploration; artificial intelligence | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| Chris R. Acheson, Jakub Glowacki, Ryota Nakano, Daiki Maeshima, Dominik Saile, Betina Pavri, Ryoyu Mori, Ryohei Takagi, Randy Pollock, Jamal R. Olatunji, Max Goddard-Winchester, Nick Strickland, Daisuke Ichihara, Stuart C. Wimbush and Kiyoshi Kinefuchi | Integration and Testing of a High Temperature Superconductor Magnet with a Central Cathode Electrostatic Thruster | Robinson Research Institute | Superconductor; magnet; plasma; electric propulsion; thruster; CC-EST | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 11 |
| Fernando Montano; Ivano Benedetti; Vincenzo Gulizzi | Stability and flying qualities analysis of flexible aircraft by coupling the Vortex Lattice method and the discontinuous Galerkin method | Università degli Studi di Palermo | flight dynamics; aeroelasticity; Vortex Lattice Method; discontinuous Galerkin method | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Anne-Hermine Allain; Elena Lopez-Contreras; Evandros Theodosiou; | Asclepios Mission III: THIRD ITERATION OF THE STUDENT-LED ANALOG MISSION SIMULATING A HUMAN EXPEDITION TO THE LUNAR SOUTH POLE | Asclepios Mission III | Asclepios; Student; Lunar; Martian; Habitats; AnalogueAstronaut; Analogue; Astronaut | STUDENT - Space Student Projects | Oral | 2 |
| Xuxing Huang; Bin Yang; Shuang Li | Intelligent guidance method for Galilean moon cycling with online error fitting via reinforcement learning | Nanjing University of Aeronautics and Astronautics | Galilean moon cycling; intelliigent guidance; error fitting; reinforcement learning | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 13 |
| Musa Onur ÖZTÜRKMEN; Yusuf ÖZYÖRÜK | Stability Characteristics of a Single Injector Combustor through Acoustic Solutions with Large Eddy Simulated Heat Sources | Middle East Technical University | Helmholtz solver; thermo-acoustic instabilities; flame transfer function | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 34 |
| Yunjia Yang; Jiazhe Li; Runze Li; Yufei Zhang; Haixin Chen | Interactive optimization of fluidic injection for single expansion ramp nozzle based on a modified autoencoder | Tsinghua University | machine learning; single expansion ramp nozzle; fluidic injection; thrust optimization | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 |
| Carlos Neves; Caterina Gennari; Raffaello Mariani | Stall Development Control of a Blended-Wing_Body UAV Using a Bioinspired Leading-Edge Design | KTH Royal Institute of Technology | Aerodynamics; Stall Development; Bioinspired | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| Sebastian Karl | Assessment of neural network-based predictions of chemical production rates in CFD solvers | DLR | CFD; AI; Combustion; Chemistry | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Masashi Miura ; Yuki Sakamoto | Interactive System Modeling for Designing a New Concept Launch Vehicle | JAXA/ISAS | System Model; System Design; Modeling | SYSINT - System-Integration on Aircraft and Space Systems | Poster | 56 |
| Elia Puccinelli; Angelo Pasini | Steady 1D Viscous Non-adiabatic Flow Model for the Determination of Inner Geometry and Power Density Profile of Nuclear Fuel Element | University of Pisa | Nuclear Propulsion; 1D gasdynamic; non-adiabatic flow; viscous flow | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 3 |
| Davide Cavalieri; Giuseppe Indelicato; Arianna Remiddi; Pietro Paolo Ciottoli; Francesco Creta; Pasquale Eduardo Lapenna | Assessment of phase-separation phenomena in LREs cryogenic flows | Sapienza Università di Roma | Phase-Separation; Vapor-Liquid-Equilibrium; Liquid-Rocket-Engines | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Valerio Mosca; Stanislav Karpuk; Ali Elham | Investigating potentials of active flow control via retrofit of commercial aircraft | Institute of Aircraft Design and Lightweight Structures TU Braunschweig | Aircraft design; active flow control; retrofit; sustainability | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Matteo Gemignani; Francesco Mancini; Salvo Marcuccio | Stratospheric Flight of a Balloon-Borne Solar Cell Testing Facility | University of Pisa | High-altitude balloon; stratospheric flight; solar cell; I/V characteristic curve; solar spectrum | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 1 |
| Francesco Antonio D'Aniello; Pietro Catalano | Assessment of RANS methods for low-Reynolds number compressible flows | Italian Aerospace Research Centre | CFD; Aerodynamics; Space Exploration; Mars | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Mihai Vladut HOTHAZIE; Ionut BUNESCU; Mihai Victor PRICOP | Investigating the Effectiveness of Vortex Generators in Aviation through High-Fidelity CFD Analysis | National Institute for Aerospace Research "Elie Carafoli" | control; passive; vortex; generators | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| Ronan Geffrault; David Tchou-kien | Structural design of PERSEUS bi-liquid demonstrator: ASTREOS-1 | CT ingénierie | Sounding rocket; structure and materials; bi-liquid propulsion | STUDENT - Space Student Projects | Oral | 1 |
| Marco Felice Montaruli; Sergio Bonaccorsi; Andrea Muciaccia; Lorenzo Giudici; Pierluigi Di Lizia; Camilla Colombo; Giuseppe Pariti; Damiano Errico | Assessment of the CZ-6A RB and the H-2A DEB fragmentation events | Politecnico di Milano | Fragmentations; Space Surveillance and Tracking; Conjunction Analysis; Kessler syndrome; Space Debris | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| H. S. Saluja; F. Yin; A. G. Rao | Investigating the influence of turbofan engine design on climate for a short-to-medium-range flight network | Delft University of Technology | turbofan engine design; aviation climate impact; aircraft emissions; combustion technology | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 3 |
| Gabriele Luzzani; Irene Buraioli; Danilo Demarchi; Giorgio Guglieri | Study and Development of a Real-Time Pilot Performance Monitoring System Based on Physiological Signals | Politecnico di Torino | Mental Workload; Human Factors; Biosignals; Pilot Monitoring | HUMANF - Human factors in Aviation and Space | Oral | 1 |
| Angelo Pasini; Stefano Calatafimi; Elia Puccinelli; Tommaso Gerbi | Atmospheric Test Campaign of a Hydrogen Peroxide Propulsion System for CubeSats | University of Pisa | Green propellants; chemical propulsion system; hydrogen peroxide; test campaign; CubeSats; monopropellant | TESTING - Testing in Aerospace | Poster | 61 |
| Harika Gurram;Swaroop Kumar Nagnoori;IL Sumanth Varma | Investigating the Noise Reduction techniques for Rotor Drones | TU Delft | Rotor;Dinotail;CFD;Noise Reduction | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 |
| Dmitry DAVIDENKO; Robin DEVILLERS | Study of aluminum droplet ignition in a solid propellant flame | ONERA | solid propellant flame; aluminum droplet ignition; experiment; modeling | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Min-Jea TAHK; Jong-Chan PARK; Boseok KIM; Heekun ROH; Chang-Hun LEE | Augmented Pursuit Guidance for Flight Trajectory Shaping | KAIST | midcourse guidance; pursuit guidance; real-time optimal guidance; trajectory optimization | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 1 |
| Cedric Caruana; Andre Manicolo; Robert Camilleri | Investigating the power and energy flows for a Kinetic Energy Recovery from a landing aircraft | University of Malta | engineless taxiing; kinetic energy recovery; power flow simulation | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 3 |
| Witold Klimczyk; Adam Sieradzki | Study of geometry effects on aerodynamics and aeroacoustics of various scale rotors | Lukasiewicz Research Network - Institute of Aviation | CFD; CAA; propeller design; global optimization | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 |
| Antoni Kopyt; Anna Czapli?ska; Szymon Bogus | Augmented Reality in UAV’s Operator Training | Warsaw University of Technology | UAV simulator; augmented reality; virtual reality; training | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| Sören Heizmann; Armin Herbertz; Juliusz Saryczew; Chiara Manfletti | Investigation of a Cathode-Vapor-Feed Electrolyser for a Water Electrolysis Propulsion System | Technical University of Munich | In-Space Propulsion; Green Propulsion; Water Electrolysis Propulsion; Propellant Production; PEM-Electrolyser; Cathode-Vapor-Feed; GOX/GH2 | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 3 |
| Daniele Bianchi; Matteo Fiore; Marco Grossi; Bernardo Favini; Francesco Nasuti; Nicola Ierardo; Dario Scoccimarro | Study of SRM Nozzle Divergent Performance Improvement Under Fixed Geometrical Constraints | Department of Mechanical and Aerospace Engineering, Sapienza University of Rome | Solid Rocket Motors; CFD; Nozzle | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 16 |
| Valeriy Trushlyakov; Alexey Novikov; Vladislav Urbansky; Vadim Yudintsev | Investigation of a two-phase vortex flow in a tank with liquid residues for its discharge under low-gravity conditions | liquid residues; vortex flow; gasification; discharge; low-gravity | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 | |
| PLIQUE Ronan; LABAUNE Julien; DUPAYS Joël; GRENARD Philippe | Study of the ineteraction between a droplet and an acoustic waves | Onera | fluid mechanics; acoustics; two-phase flows; modeling and numerical simulation; dynamic meshing; applied mathematics | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| J. M. Gambi; C. Phipps; M.L. Garcia del Pino; J. Mosser; E.B. Weinmüller | Autonomous Sweeping of Middle Size LEO Debris with Space-Based Laser Brooms | U. CARLOS III DE MADRID | Space-based laser brooms; middle-size LEO debris targets; autonomous closed-loop control systems; autonomous pointing and shooting actions. | SUSTSP - Sustainable Space: Logistics and Space Debris | Cancelled | |
| Ivens Daniel Hoffmann; Jan Martin; Wolfgang Armbruster; Dmitry Suslov; Jan Deeken; Justin Hardi | Investigation of Different Porous Injection Technologies in a LOX/CH4 Rocket Combustor with Optical Access at Sub-, Trans- and Supercritical Conditions | German Aerospace Center (DLR) | Rocket Combustor; Cryogenics; Porous Injector; Optical Analysis | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 6 |
| Huimin Xiang?Qingzhen Yang?Xufei Wang?Jiazheng Fan | Study on the Influence of Vortex Generator on Aerodynamic and Stealth Characteristics of Serpentine Inlet | Northwestern Polytechnical University | Serpentine inlet; Vortex Generator; aerodynamic performance;electromagnetic scattering characteristics | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Poster | 19 |
| Michele Capriati; Anabel del Val; Thomas Schwartzentruber; Timothy Minton; Pietro Congedo; Thierry Magin | Bayesian calibration of a finite-rate nitridation model from molecular beam and plasma wind tunnel experiments | von Karman Institute | Ablation; Bayesian calibration; gas surface interaction | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Kartika Ahuja ;Srisha Rao MV | Investigation of fluid structure interaction on a flexible cantilevered plate due to shock impingement | Indian Institute of Science | Hypersonic flows; Shock boundary layer interactions ; Fluid-Structure Interactions | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 4 |
| Manan Joshi; Devanshi Gandhi; Akash Marade; Rushikesh Kore | Suborbital Taxi Transfer | MIT ADT University | orbital dynamics; Space flight dynamics | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 5 |
| Ayushi Pandya | Benefits of Boundary Layer Ingestion with Froude's Propeller Theory | ENSMA | Boundary Layer Ingestion | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Poster | 51 |
| Sebastian SOLLER ; Maria Teresa SCELZO ; Jean-Baptiste GOURIET ; Antoine DE CROMBRUGGHE; Cristian DINESCU; Lionel TERMMERMAN; Alexander DOEHRING; Steffen SCHMIDT; Johan STEELANT | Investigation of Heat Transfer and Nucleate Boiling of Ethanol in Additively Manufactured Cooling Channels | ESA | Heat Transfer; Nucelate Boiling | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Tinoco; Brodersen; Keye; Laflin;; Vassberg; Rider; Wahls; Morrison; Pomeroy; Murama; Nangia | Summary Data from the Seventh CFD Drag Prediction Workshop | nangia | AEROFLIPHY; CFDMPS | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| stephane HEINRICH | BFS an atmospheric reentry kit to bring NANOSAT Payloads « Back From Space », | eNOVA Aerospace | Atmospheric ; Reentry ; Kit ; Nanosat; Payload | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 4 |
| Alexander V. Nebylov; Vladimir A. Nebylov | Investigation of heavy ekranoplanes construction concepts | ekranoplane; concepts construction; flight control system; ground effect; low altitude | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 | |
| Malgorzata Holynska; Alice Suarez Kahan; Federica Arena; Mirko Prato; David Duday; Yann Chouard ; Gernot Groemer; Sibylle Schmied; Adrian Tighe; Riccardo Rampini | Surfaces for space exploration | ESA | surface; lunar dust; EVA suit; antimicrobial | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 2 |
| Riccardo Bisin; Vincenzo Pagliacci; Christian Paravan | Boosting Green Propellants: The Sustainable Armored Grain for Hybrid Rocket Propulsion | Politecnico di Milano | Armored Grain; Green Fuels; Hybrid Rocket | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| Guangda Yang; Christian Allen; Annabel Markesteijn; Hussain Ali Abid; Sergey Karabasov | Surrogate Model-Based Acoustic Optimisation of Jet Nozzle Exit Geometries using Large Eddy Simulation | Northwestern Polytechnical University | Jet aeroacoustics; Large eddy simulation; Acoustic optimisation | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 |
| Amsha S; O N Ramesh; N Balakrishnan | Bubble suppression on a high lift wing section using synthetic jet | Indian institute of science | STOL; separation control; high lift section; synthetic jet | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| Antonio ESPOSITO; Calogero Orlando; Andrea Alaimo | Investigation of seated passengers vibration using a full-flight simulator | Università degli Studi di Enna "Kore" | Flight Simulator; Whole Body Vibration; Seated Passengerr | HUMANF - Human factors in Aviation and Space | Oral | 2 |
| Angelina Frolova; Lina Kuhlman; Joaquim Silveira; Santiago Evangelista | Sustainability Aspects of Rapid Prototyping and Frequent IODs with CubeSats | EPFL | CubeSat; In-Orbit Demonstration; Sustainable Space; Low Earth Orbit; Prototyping | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| Paolo Grasso; Siwei Cai | Cabin Air Quality in Commercial Aircrafts with an Adaptive Environmental Control System Strategy | Collins Aerospace | Cabin Air Quality; Aircraft; Environmental Control System; Ventilation | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| Bahri Tu?can Selimhocao?lu; Prof. Dr. Yusuf Özyörük | Investigation of the Entropic Lattice Boltzmann Method in Various Flow Regimes | Middle East Technical University | LBM; CFD; Aerodynamics; Entropic LBM | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Reject | |
| Stamatios Vassilopoulos | Sustainable Aviation Fuels in the European Union: a critical analysis of the ReFuelEU Aviation Initiative | International Institute of Air and Space Law, Leiden University | Sustainable Aviation Fuel; SAF; European Union; EU; ReFuelEu | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 2 |
| Arnaud Biard; Hauke Martens; Yoshimasa Tajima; Yasuhiro Saito; Christophe Chavagnac; Alain Mauries | CALLISTO - Flight Worthiness Process: how to prepare the tripartite go to flight decision? | CNES | Reusable; Demonstrator; CALLISTO; Review; Project organization; Mission; Risk management; Deviations | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 2 |
| Atilla Altintas; Lars Davidson; Shia-Hui Peng | Investigation of the skin-friction drag reduction capabilities of wall- normal created plasma jets in wall-bounded turbulent flow | Chalmers University of Technology | CFD; flow control; plasma force; drag reduction | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| Stephan Hellmich; Mathieu Udriot; Emmanuelle David | Sustainable Space Hub at EPFL: a review of ongoing research projects | Ecole Polytechnique Fédérale de Lausanne | Space sustainability; space debris; environmental impacts; Space Sustainability Rating; data acquisition and analysis | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| Simon Furnes; Paul Flower; Jelena Aronsen; Jim White; Nathalie Cesco; Sebastien Le Martelot | CALLISTO – on repurposing an expendable reaction control system (RCS) for a reusable demonstrator | Nammo | Reusable; RCS; Callisto; repurposing | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 2 |
| Sevinç; Erdem; ?entürk | Investigation of tip flow structures of a transonic axial compressor stage based on the harmonic balance method | TUSA? Engine Industries Inc. | turbomachinery flows; unsteady flow modelling; harmonic balance method; axial compressor | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 2 |
| Bernd M WEISS; Stella Schuebel; Isidora Casas Del Valle Pacheco; Anna Öhrwall Rönnbäck; René Laufer | Can Regulatory Actions Guide or Dictate Sustainability in Space? | Luleå University of Technology | Spacecraft Reuse; Space Sustainability; Sustainable Development Goals; Space4SDG; Circular Economy | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 |
| Kerem KARAHAN; Sertac CADIRCI | Investigation of Various Baffle Design Effects on Center of Gravity Deviation in a Training Aircraft Wing Fuel Tank using CFD and 1D Simulations | Turkish Aerospace | Computational Fluid Dynamics; Flight Mechanics; Sloshing Tank; 1D Simulation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| Frank Neuman | Technical and Regulatory Hurdles for the use of Hydrogen in Lighter-Than-Air carriers | ULB | Airships; Hydrogen; Flying regulations | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 2 |
| A. Belkallouch; L. Dala | Cavity noise reduction with sweeping actuators | University of Blida | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 7 | |
| Ryohei CHINO; Yoshiaki KAWAGOE; Shugo DATE; Kazuki RYUZONO; Tomonaga OKABE | Investigation of weight estimation in conceptual design for composite aircraft development | Tohoku University | Conceptual Design of Aircraft; FSI; Composite Materials; | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Poster | 52 |
| Leandro Magalhães; Ana Ferreira; Mauro Rocha; André Silva | Techno-economic Analysis of Sustainable Aviation Fuels: e-fuels | ISEC-Institute of Education and Sciences | e-fuels; techno-economic analysis; life-cycle analysis | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 2 |
| Matteo Cimini; Francesca Rossetti; Giacomo Della Posta; Fulvio Stella; Matteo Bernardini | CFD Analysis of the Lateral Sloshing Phenomenon inside an Aerospace LH2 Cryogenic Tank | Sapienza University of Rome | CFD; VOF; Sloshing; Cryogenic Tank; CH4 | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 7 |
| Seong Min Jeon | Investigation on Active Axial Thrust Balancing for a Turbopump | Korea Aerospace Research Institute | Rocket engine; Turbopump; Axial thrust; Active balancing | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Poster | 62 |
| Frederik Jacobs; Johan Steelant | JWST Mission Post-Flight Analysis: Evolution of Fairing Environmental Conditions | European Space Agency | boundary layer; transition; trajectory analysis; post-processing | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 6 |
| Craig Anderson; Christopher Nelson | Challenges of developing commercial activity on the moon | N/A | moon colonization; lunar challenges | SPEXPLO - Space Exploration - In Situ Resource Utilization | Poster | 45 |
| Ivens Daniel Hoffmann; Dmitry Suslov; Jan Deeken; Justin Hardi | Investigation on Pressure Loss and Spray Angle on Different 3D-Printed Helical Swirl Injectors | German Aerospace Center (DLR) | Helical Swirler; Pressure Loss; Spray Angle | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 42 |
| Akash Unnikrishnan; Abishek Sarkar; Vinod Narayanan | Chaotic advection of particles between a stationary cylinder and an eccentrically placed inner oscillating cylinder | Indian Institute of Technology Gandhinagar | Chaotic advection; mixing; laminar; turbulence | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Reject | |
| Nikolaus Papenberg; Stefan Gneiger; Alexander Großalber; Clemens Simson | Investigations on forging of low-density Mg-Li alloys | AIT Austrian Institute of Technology, LKR Light Metals Technologies Ranshofen | magnesium; Mg-Li alloy; forging; low-density | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 8 |
| Alexandru-Claudiu C?NCESCU; Dan IFRIM; Simona D?NESCU; Theodora ANDREESCU; Razvan BIMBA?A | Testing of components for a future European heavy launcher | COMOTI | Anti-Vortex Device; AVD; FLPP; SCOUT | TESTING - Testing in Aerospace | Oral | 1 |
| Claudia Jimenez Cuesta; David Pickles; Andrea Cammarano; Hossein Zare-Behtash | Characterisation of the Dust Cloud During Landing on Lunar and Martian Surfaces | University of Glasgow | PSIs; SBLIs; Lunar dust; Martian dust; Dust mitigation; Regolith Interaction | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 3 |
| D. Villegas-Prados; J. Cruz; M. Wijnen; P. Fajardo | Ionic liquids performance for externally wetted electrospray propulsion system | ienai SPACE | Electrospray; microsatellites; propulsion system | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 11 |
| Antje Link; Martin Staggat | Characterisation of thermal management specific heat rejection for electric propulsion architectures | Thermal Management; Electric Propulsion; Specific Heat Rejection | HEPAEM - Hybrid Electric Propulsion | Oral | 2 | |
| Mitchell Galletly; William Giang | Ironbark: Trajectory and Aerodynamic Simulator for High-Power Rockets | University of Sydney | Trajectory Simulation; Aerodynamic Modelling High-Power Rocket; Student Team | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Michaël Méheut; Olivier Atinault; Sébastien Defoort | The Common Inlet Configuration: An Advanced Boundary Layer Ingestion Engine Integration Concept | ONERA | Boundary Layer Ingestion; CFD; Exergy; aircraft performance | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| Noritaka Sako; Kakeru Mizukoshi; Jun Hayashi; Yu Daimon; Hiroshi Kawanabe | Characteristics of a superheated wall cooling through pulsed injection of a liquid jet | Kyoto University | Jet impingement cooling; Pulsed injection; Liquid film; Heat transfer | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Konstantinos KATSONIS; Chloe BERENGUER | ISRU electric propulsion in the Neptune vicinity | DEDALOS Ltd | ISRU; Solar System; H2/He propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 40 |
| Urara Kamon; Shugo Date; Keiichi Shirasu; Yoshiaki Kawagoe; Kazuki Ryuzono; Tomonaga Okabe | The effect of hot/wet environment on the structural weight of aircraft wing using thermoplastic CFRP | Tohoku University | Carbon fiber reinforced plastic; Aircraft wing; Static aeroelasticity | STRMAT - Structures & Materials for Aeronautic and Space Systems | Poster | 47 |
| Laura Pernigoni; Ugo Lafont; Antonio Mattia Grande | Characterization of self-healing polymers under simulated space environment | Politecnico di Milano | Self-healing polymers; Space environment; Space radiation; Experimental characterization; Inflatable structures | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Giorgia DI DIO; Maura COLUCCI; Marco TOMMASI; Yoann BEN HAMOU | Just-in-time Collision Avoidance (JCA) using nanosatellite swarms (nanotugs) | IPSA (engineering school) | JCA (Just in time Collision Avoidance); space debris; swarm of nanotugs; octopus | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 |
| John Cater; Max Goddard-Winchester; Xiyong Huang; Nick Long; Ben Mallett; Jamal Olatunji; Betina Pavri; Randy POLLOCK; Avinash Rao; Nick Rattenbury; Cameron Shellard; Nick Strickland; David Wright | The Hēki Mission: Testing Superconducting Magnet Technology for Space Propulsion on the International Space Station | Robinson Research Institute | Electric Propulsion; High Temperature Superconductors; AF-MPD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 29 |
| Giorgio Isoletta; Francesco Cuomo; Roberto Opromolla; Giancarmine Fasano | Characterization of space objects’ attitude motion using Lomb-Scargle Periodogram | University of Naples "Federico II" | Space object characterization; Space Domain Awareness; Light Curves; Lomb-Scargle Periodogram | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| R. Stark; C. Rieping; T. Esch | The Impact of Guide Tubes on Flow Separation in Rocket Nozzles | German Aerospace Center | rocket nozzle flow; flow separation; guide tube | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 19 |
| Lim Byoungjik; Lee Keejoo; Lee Keum-Oh; Lee Junseong; Park Jaesung | KARI’s Additive Rocket Engine Initiative for Low-Cost and Sustainable Access to Space | Korea Aerospace Research Institute | Liquid Rocket Engine; Methane; Additive Manufacturing; powder bed fusion; directed energy deposition | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Himpu Marbona; Alejandro Martínez-Cava; Daniel Rodríguez; Eusebio Valero | The impact of unsteady inflow conditions and actuation on the instability and transition of separated flows in low-pressure turbines | Universidad Politécnica de Madrid | separated flow; laminar-turbulent transition; low-pressure turbines; hydrodynamic stability; direct numerical simulation | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 4 |
| Alexander Arnold; Robert Luckner; Guido Weber | Classification of Flight Control Law Requirements in the Context of Model-Based Software Development and Verification | Technische Universität Berlin | flight control laws; classification; verification; model-based | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Alberto Broatch; Pablo Olmeda; Jorge Garcia-Tíscar; Andrés Felgueroso | Keeping turbofans cool: Aerodynamic upgrade of bypass surface heat exchangers (EU Project SACOC) | Polytechnic University of Valencia | Thermal management; Heat exchangers; SACOC; SAOHE; Wind tunnel; Experimental Aerodynamics | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 2 |
| Andrea Curatolo; Dario Modenini; Giacomo Curzi; Alessandro Lotti; Daniele Pecorella; Eliseo Strollo; Alfredo Locarini; Andrew Hyslop; Davide Oddenino | The nanosatellite-class attitude control facility at ESA-ESTEC | Alma Mater Studiorum Università di Bologna | ADCS; satellite testing; CubeSats | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 3 |
| Thomas ARNOULT; Colin Leclercq; Charles Poussot-Vassal; Cécile Ghouila-Houri; Aurélien Mazzamurro; Alain Merlen; Eric Garnier; Denis Sipp; Philippe Pernod; Abdelkrim Talbi | Closed-loop control of an open-cavity flow with magnetically actuated microvalves | Centrale Lille Institut | MEMS actuators; Open-cavity; Closed-loop | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 1 |
| ?ukasz KISZKOWIAK; Aleksander OLEJNIK; Adam DZIUBI?SKI | The use of Computational Fluid Dynamics methods to improve aerodynamic properties of a newly designed twin-jet engine aerial target | Military University of Technology | aerodynamic layout; aerial target; CFD; Finite Volumes Method; airplane | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| Ionut BUNESCU; Stefan BOGOS; Teodor-Viorel CHELARU; Mihai HOTHAZIE; Mihai-Victor PRICOP | Coherent solutions to roll damping derivatives evaluation for a generic rocket model | National Institute for Aerospace Research "Elie Carafoli" - INCAS | Roll Damping Coefficient; CFD; Experimental; Basic Finner Model | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 4 |
| Ingo STAACK; Christopher Jouannet; Kristian Amadori; Reinier van Dijk; Max Baan; Robert Braun; Petter Krus | Knowledge-based Integration of Aircraft System Simulation within Aircraft Conceptual System Design | Linköping University | dynamic system integration; aircraft simulation; aircraft conceptual design; KBE; model tuning; XML; multi-fidelity; AI-based model integration; DEFAINE | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 10 |
| Fatouma MAAMAR ; Omar MERTAD ; Abdeldjelil MANKOUR | Thermal effects in optomechanical ssystems for space applications | Satellites development center, Algerian Space Agency, | bonded optic; elastomer; thermal stress; thermo-optic coefficient ; OPDOPD | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Philipp Teuffel; Lukas Werling | Cold flow analysis of spray angle and droplet size distribution of a pintle injector for green hypergolic propellants | German Aerospace Center (DLR) | Cold flow; pintle injector; green hypergolic propellants; spray angle; droplet size; simulants | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 6 |
| Pasquale Eduardo Lapenna; Arianna Remiddi; Giuseppe Indelicato; Mauro Valorani; Rocco C. Pellegrini; Enrico Cavallini; Marco Pizzarelli; Francesco Creta | Large Eddy Simulations of injectors near-field and heat transfer in rocket combustion chambers | Sapienza University of Rome | Turbulent combustion; Injection; liquid rocket engines | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 4 |
| Seongmin Joo; Dokeun Hwang; Donghyuk Kang; Seongchan Heo; Sanghoon Han; Byeongyoung Lee; Wonju Je; Jonggyu Kim | Cold flow test of pintle injector for variable thrust combustion chamber with servo-valve method | Korea Aerospace Research Institute | Cold flow test; Pintle injector; Servo-valve; Variable thrust | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 33 |
| Can Öznurlu; Berke Bayr?; Farhat Asim | Lateral-Directional Control Law Design, Handling Qualities and Uncertainty Analysis for a Re-entry Vehicle HL-20 Flight Control System | Turkish Aerospace | Control; Handling Quality; Flying Quality; Re-entry; Uncertainty | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Poster | 11 |
| Hagen Kellermann; Anais Luisa Habermann; Arne Seitz | Thermal management system design for a regional hybrid electric aircraft | Bauhaus Luftfahrt e.V. | Thermal Management System; Hybrid Electric Propulsion; Heat Exchangers | HEPAEM - Hybrid Electric Propulsion | Cancelled | |
| Florian Courteville; Enrico GIOVANARDI; Elouan PETERAU; Thomas BESSON | Cold gas roll control for a 30kg experimental rocket | SUPAREO SPACE SECTION | Roll control; pneumatic; rocket; cold gas | STUDENT - Space Student Projects | Oral | 1 |
| CIUFFINI Andrea Francesco | Latest advances in characterization of metallic materials for aerospace industry at European Synchrotron Radiation Facility (ESRF) | ESRF | Synchrotron x-ray diffraction; Residual stresses; Synchrotron x-ray nano-computed tomography; Creep; Synchrotron x-ray in-situ laminography; Fracture | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 8 |
| Chang-Min Lee; Chang-Hoon Sim; Jae-Sang Park | Thermal transfer effects on postbuckling behaviors of common bulkhead structures | Chungnam National University | Common bulkhead; Heat transfer; Thermal-structural analysis; Postbuckling analysis; Knockdown factor | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Alberto Sarritzu; Philip Teuffel; Angelo Pasini; Felix Lauck | Cold-Flow Testing of various injector designs for a novel hypergolic and green propellant combination developed at DLR Lampoldshausen | University of Pisa | Green Propellants; Injection; Cold-Flow tests; Energetic Ionic Liquid; Hydrogen Peroxide | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 14 |
| Joshua BENARROCH; Marianne BLIN; Romain GARDON; Washington GEORGES; Théo PODOLSKY | LEONEEDS - A Space Debris Recycling Space Station | Institut Polytechnique des Sciences Avancées | Space station; Space debris; debris; station; recycling; recycler; deorbiting; deorbitation; lunar gateway; circular economy | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 |
| Alessandro Finazzi; Filippo Maggi; Christian Paravan; Dennis Daub; Stefano Dossi; Alessandro Murgia; Tobias Lips; Geert Smet; Kobye Bodjona | Thermite-for-Demise (T4D): Preliminary assessment on the effects of a thermite charge in plasma wind tunnel experiments | Politecnico di Milano | Thermite; arc-heated wind tunnel; test predictions | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 2 |
| Giuseppe SCARLATELLA; Jan Sieder-Katzmann; Felix Weber; Daniele Bianchi; Martin Tajmar; Christian Bach | Cold-Gas Experiments on Advanced Nozzles in Subsonic Counter-Flows | Technische Universität Dresden | Advanced Nozzles; Reusable Launch Vehicles; Clod-flow Test | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 4 |
| Christian Wallace; Nicolas Fezans | Lidar-based Gust Load Alleviation - Results Obtained on a Generic Long Range Aircraft Configuration | DLR (German Aerospace Center) | Gust load alleviation; LIDAR; preview control | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Evandros Theodosiou; Salvador Navarro-Martinez | Thermodynamic Analysis of Martian Habitats | Department of Mechanical Enginnering, Imperial College London | Habitat; Mars; Space; Analysis; Student | STUDENT - Space Student Projects | Oral | 2 |
| Naveed Ahmed | Collaborative Localization Assisted RFI Detection Using Low-Cost COTS GNSS Receivers | Norwegian University of Science and Technology | RFI Detection; RFI Localization; Carrier to Noise Density Ratio; Majority Voting; Reference Detector | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Iklim Akay; Vincent Affatato; Abhinav Batchu; Marco Conenna; Samuele Malta; Sabatino Santangelo; Daniele Torrisi | Lightweight, Cost-effective, and Multi-functional Bio-based Composite Laminate Design for Satellite Applications | Tu Delft | Sustainability; Bio-materials; Composite; Materials; Multifunctional; Solar panels; FEM; Thermal analysis | STUDENT - Space Student Projects | Oral | 2 |
| Alessandro Aimasso; Matteo Davide Lorenzo Dalla Vedova; Paolo Maggiore | Thermomechanical calibration of FBG sensors for aerospace applications | Politecnico di Torino | Optical Fiber; Fiber Bragg Grating; Sensors; Temperature; Strain; Systems monitoring | TESTING - Testing in Aerospace | Oral | 2 |
| Artur Elias de Morais Bertoldi; Christopher Glaser; Jouke Hijlkema; Jean-Yves Lestrade; Jérôme Anthoine; Patrick Hendrick | Combustion Instabilities Induced by Multi-Stepped Hybrid Rocket Fuel Grains | University of Brasília | Hybrid rockets; combustion chamber pressure oscillations; combustion instability; multi-stepped fuel grains | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| Federico Giambelli; Riccardo Bisin; Enrico Bragalli; Christian Paravan | Liquid Film Cooling: Open-Literature Review, Modeling and Efforts Towards Validation | Politecnico di Milano | Liquid Film Cooling; Liquid Rocket Engines; Thermal Analysis; Film Cooled Length | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Rémy Garcia; Igor Kiyanitsyn; Milan Mitrovic; Hajer Saada; Alfred Tang; Michel van Tooren; Laura Mainini | Thermoplastic Induction Welding for Sustainable Aircraft: an Industrial Perspective | Collins Aerospace | Structures and Materials; Sustainable Aviation; Multiphysics Simulation; Multidisciplinary design optimization | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 6 |
| Lucas BARATON; Annafederica URBANO; Loïc BREVAULT; Mathieu BALESDENT | Comparative review of Multidisciplinary Design Analysis and Optimization architectures for the preliminary design of a liquid rocket engine | ISAE SUPAERO | multidisciplinary design optimization; launch systems; liquid rocket engine; variable-size design space problem | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 2 |
| Cheolwoong Kang; Shinwoo Lee; Hadong Jung; Sunwoo Han; Kangyeong Lee; Dongwoo Choi; Changyoung Oh; Kyubok Ahn | Throttling hot-firing tests of methane engine thrust chamber with uni-element shear coaxial injector | Chungbuk National University | Hot-firing test; Methane engine; Recess length; Shear coaxial injector; Thrust control | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 6 |
| Carlo E.D. Riboldi; Alberto Rolando | Thrust-Based Flight Stabilization and Guidance for Autonomous Airships | DAER - Politecnico di Milano | stabilization; SAS; airship; guidance; beam-tracking; altitude-tracking; thrust control; optimal design; optimal lofting; nonlinear simulation; beam tracking; autonomous flight; autonomous airship; UAV airship; low-altitude flight; Lotte airship | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 2 |
| Karol B?ben; Robert G??bocki | Comparison of evolutionary algorithms for optimizing the flight path of a Unmanned Aerial Vehicles swarm | ?ukasiewicz - Institute of Aviation | UAV Swarm; Evolutionary algorithms; Path planning | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Poster | 63 |
| Zawar Haider ; Rafic M. Ajaj Lakmal Seneviratne | Load alleviation using polymorphing wings: The effect of the morphing rate. | Khalifa University | Morphing wing; Aeroelasticity; Morphing rate; Gust load response; Load alleviation. | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Jeongseok Hyun; Minseok Jang; Tuan Anh Nguyen; Jae-Woo Lee | Tilt Angle Control Planning for eVTOL using Trim Analysis | Konkuk University | Transition; eVTOL; Trim Analysis; Tilt Corridor | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 2 |
| Pascal H. Kringe; Jörg R. Riccius; Justin Hardi; Michael Oschwald; Stefanie Reese | Comparison of experimental Fatigue Life Study for two Inner Liner Materials for Liquid Rocket Engines | DLR | thermomechanical fatigue; liquid rocket engine; fatigue life | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Victor Bahrs; Jonas Ludowicy; Martin Staggat | Load Flow Analysis of Hybrid AC-DC Power Systems for the Application in Electrified Aircraft Propulsion | German Aerospace Center (DLR) | Electrified Aviation; Load Flow Analysis; Electric Propulsion System | HEPAEM - Hybrid Electric Propulsion | Oral | 2 |
| Scherezade Barquero; Mario Merino; Jaume Navarro-Cavallé | Time-Resolved 3D Characterization of the Plume of a Low-Power Ablative Pulsed Plasma Thruster | Universidad Carlos III de Madrid | Pulsed plasma thruster; PTFE; plasma diagnostics; plume divergence; electric propulsion; micropropulsion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 8 |
| Ui-Jin Hwang; Jae-Sang Park; Myeong-Kyu Lee | Comparison of Tiltrotor Whirl Flutter Analyses with Gimballed and Hingeless Hub Models | Chungnam National University | Tiltrotor; Whirl Flutter; Aeroelastic Instability | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 7 |
| Bryan Laabs; Nikolai Block; Ralph Paul; Robert Luckner; Flavio Jose Silvestre | Total Energy Control for the Automatic Landing of UAS with Large Aspect Ratio and Low Wing Loading | TU Berlin | HAPS; Autoland; UAS; TECS | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 2 |
| Jan-Steffen Fischer; Stefanos Fasoulas; Céline Brun-Buisson; Dr. Encarna del Olmo | Comparison Study on the Environmental Impact of Different Launcher Architectures | University of Stuttgart, Institute of Space Systems | Life Cycle Assessment; Launcher; Ecodesign | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 4 |
| amaya.espinosa@cnes.fr ; vincent.taponier@cnes.fr | Towards A New Class Of Engine For Future Heavy LIft Launch Vehicles | CNES Direction du Transport Spatial | High Thrust; Staged Combustion; Heavy Lift; Future Launch Vehicles | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Guillaume Hueber; Jérémie Huser | Compliant high support stiffness rocket gimbal for Thrust Vector Control on liquid engine | EPFL | compliant; gimbal; TVC; flexible; mechanism; rocket; liquid engine; | NEWSPA - New systems for future space operations | Oral | 1 |
| Matteo Crachi; Raffaella Sesana; Cristiana Delprete; Marco Pizzarelli; Domenico Borrelli; Nicola Sicignano | Low cycle fatigue and creep properties of a new L-PBF additive manufacturing copper-maraging steel metal matrix composite for liquid rocket engine thrust chambers | Politecnico di Torino | Liquid Rocket Engine; Additive Manufacturing; Metal Matrix Composite; Low Cycle Fatigue; Creep | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 4 |
| Kevin Marangi; Flavio Noca | Computational Fluid Dynamics of a Supersonic Rocket's Ascent | EPFL Rocket Team | Supersonic; CFD; drag minimization; rocket; compressible flows | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Poster | 8 |
| Conall de Paor; Jasmine Rimani; Stéphanie Lizy-Destrez | Low-Cost Uncrewed Lunar Landers: Mission Design and Preliminary Feasibility Assessment | ISAE-Supaero | Cost; System Analysis; Sizing Rules; Lunar Landers | NEWSPA - New systems for future space operations | Oral | 3 |
| Lars Brandt; Dominik Deden; Fabian Schühler; Michael Vistein; Philipp Gänswürger | Towards toolless manufacturing of aerospace CFRP components via thermoplastic AFP | German Aerospace Center (DLR) | AFP; CFRP; Thermoplastics; Manufacturing; Dual Robot | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 5 |
| Berker Özkaraduman | Computational Study for Axisymmetric Nozzle at Transonic and Supersonic Flow Regime | Turkish Aerospace | Axisymmetric Nozzle;Plume;CFD;SU2;ANSYS Fluent;Supersonic;Transonic | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 8 |
| Vint Lee; Sohom Roy | Low-cost, Lightweight Electronic Flow Regulators for Throttling Liquid Rocket Engines | UC Berkeley | liquid rocket engine; reusable rocket; pressure regulator; flow regulator; thrust control; variable-thrust rocket; closed-loop control | STUDENT - Space Student Projects | Poster | 50 |
| Camilla Colombo; Andrea Muciaccia; Lorenzo Giudici; Mirko Trisolini; Juan Luis Gonzalo; Borja Del Campo; Francesca Letizia; Stijn Lemmens | Tracking the health of the space debris environment with THEMIS | Politecnico di Milano | Space debris index; space sustainability; space capacity; space debris mitigations | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 4 |
| Dominik Hübener; Robert Luckner; Guido Weber | Concepts for Independent Monitoring of Flight Control Laws | Technische Universität Berlin | FCL monitor; failure detection; fault tolerance; FCS architecture; common mode error; requirement error | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Arnaud Ruiz; Max Cerf | Trajectory optimization of semi-reusable launchers | ArianeGroup | Trajectory; optimization; reusable launchers | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 3 |
| Boubakr ZEBIRI *; Nassim BRAHMI; Abdellah HADJADJ | Effects of wall temperature on turbulent boundary layer separation in supersonic planar nozzles | INSA Rouen | Nozzle Flow Separation; Heat transfer; Shock-Boundary Supersonic Layer Interaction; Low-frequency shock Oscillations; Large-Eddy Simulation) | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 69 |
| Wonjeong Hyun; Sojung Park; Changjin Lee | Transition of Pressure Oscillations in Hybrid Rocket Combustion using Paraffin Wax Fuel | Konkuk University | Combustion Instability; Supercritical; Paraffin Wax; Post Chamber in Hybrid Rocket | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| Laurent Bovet | Conceptual design optimization of Hybrid-Electric Regional Aircraft using SPPH architecture | ELISA Aerospace | Aircraft design; Hybrid electric aircraft; optimization | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 2 |
| Oh-Sung Kwon; Joong-Youp Lee | LOX recirculation characteristics of propellant feeding system with a filter installed at tank outlet | KARI | LOX Recirculation; Propellant Feeding System; Cryogenic Propellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 28 |
| Christian HESSEL; Torben BIRCK; Bernhard Opl; Stephane Dussy | LUNA NOVA – Advanced Green Propulsion Systems | ArianeGroup | kick stage; propulsion system; green propellants | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 1 |
| Nicholas F Giannelis; Gareth A Vio | Transonic flow oscillations in cavity/store problems | THE UNIVERSITY OF NEWCASTLE | Aeroacoustics; cavity flow; compressible flow | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 2 |
| Benedikt Aigner; Erich Wehrle | Consideration of Technology Scalability in the Design of Electric Propulsion System Architectures | Electric propulsion; scalability; system architectures; MDO | HEPAEM - Hybrid Electric Propulsion | Oral | 1 | |
| Charalampos Kosmas | Lunar cargo (Oversized or Parcels) | LUNAR CARGO P.C. | Lunar Cargo; Oversized Cargo; Parcels | STRMAT - Structures & Materials for Aeronautic and Space Systems | Poster | 48 |
| Yucheng LI; Dingchong LV; Shoujun ZHAO; Jiang’ao ZHAO; Jian FU; Yongling FU | Tribological characteristics of CrN/DLC friction pair on cylinder block/valve plate interface in electrohydrostatic actuator pumps for aerospace | School of Mechanical Engineering and Automation, Beihang Univ. | Aerospace EHA; Hydraulic pump; EHA pumps; Cylinder block/valve plate interface; Boundary lubrication/mixed friction; Hard surface coating | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 5 |
| Alice Dottori; Ivan Troisi; Michèle Roberta Lavagna; Simone Pirrotta; Francesco Latini | Lunar pilot plant payload design toward in situ demonstration of oxygen extraction by carbothermal reduction | Politecnico di Milano | ISRU; carbothermal process; lunar plant; oxygen extraction | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 3 |
| Henk Jan van Gerner; Arne te Nijenhuis; Changmin Cao; Ignacio Castro; Douglas A. Pedroso; Herol Dsouza | Two-phase pumped cooling system for power electronics; analyses and experimental results | NLR | Cooling; thermal control; power electronics; MPL; two-phase; pump | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 1 |
| Jiwon LEE; Hanna LEE; Youdan KIM | Control Design for VTOL Aircraft of Lift+Cruise Configuration using Mode-Switching Algorithm | Seoul National University | Vertical takeoff and landing (VTOL) aircraft; lift+cruise configuration; linear quadratic regulator (LQR) control; control allocation; mode-switching algorithm | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 2 |
| Arrigo AVI; Giuseppe QUARANTA; Riccardo PARIN | UAV icing testing facility for H24 services | Eurac | UAV; Ice tunnel; Ice accretion; system characterization | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Poster | 65 |
| Jean-Daniel LECUYER; Vicky TSIANIKA; Tony FAVALORO; Bruce DE WITT | Convergence of Machine Learning and Finite Element methods, the smart superelements | Hexagon Manufacturing Intelligence | Convergence; Machine; Learning; Finite; elements; superelements | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Hideto KAWASHIMA; Akihide KUROSU; Teiu KOBAYASHI | Maiden flight result of LE-9 engine for H3 launch vehicle | JAXA | liquid rocket engine; expander cycle | NEWSPA - New systems for future space operations | Cancelled | |
| Francisco Torres-Herrador; Mitchell Gosma; Kelly Stephani | Understanding coke deposition on carbon fibers | Von Karman Institute | Pyrolysis; Thermal Protection Systems; Carbon deposition | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 1 |
| Alessio Sereno; Matteo Fiore; Daniele Bianchi; Francesco Nasuti | Cooling system analysis of a clustered module aerospike for upper-stage applications | Sapienza University of Rome | Liquid Rocket Engines; Aerospike; Regenerative Cooling; CFD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 19 |
| Daniel Patton | Managing Space as Global Commons | Sustainability; policy; economics; commons | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 3 | |
| Fulvio SARTOR | Unsteady simulations of an aircraft with installed engine and rotating fan | ONERA | rotating fan; URANS; airframe | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Stefan Fechter; Immo Huismann; Georgii Oblapenko; Sebastian Karl; Tobias Ecker; Martin Grabe | Coupling of particle and continuum methods for the simulation of radiative and particle laden flows | German Aerospace Center | CFD; particle flows; coupled simulation | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Jungpyo Lee; Suhan Ko; Sulhee Kim; Hasang Jeon; Inwoong Lee; and Heejang Moon | Mass Transfer due to Liquid Layer Flow for Paraffin-Based Fuels in Hybrid Rocket Engines | University of Brasilia | paraffin-based hybrid rocket fuels; liquid layer flow; droplet entrainment; liquid melt layer viscosity; regression rate | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 18 |
| F. Olivon; JE. Durand; A. Genot; E. Piot | Unsteady Thermal Throat Position under Acoustic Forcing | ONERA | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 21 | |
| Keejoo Lee; Junseong Lee; Sunghyuck; Im; Mookeun Yi; Keum-Oh Lee; Daeban; Seo | Cryogenic Upper Stage Development for Future Korean Small-Lift Launch Vehicles | KARI | Small-Lift; Launch Vehicle; Upper Stage; Cryogenic | NEWSPA - New systems for future space operations | Oral | 2 |
| Tatiana Perrotin; Stéphane Mazouffre; Jaume Navarro-Cavallé; Pablo Fajardo; Eduardo Ahedo | Measurements of xenon ions velocity in Cylindrical Hall Thruster with Laser-Induced Fluorescence spectroscopy | Universidad Carlos III de Madrid | Electric propulsion; Cylindrical Hall Thruster; laser-induced fluorescence | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 10 |
| Jamel METMATI | Use the AI tools for Space systems delivery | RHEA | AI; Documents; Requirements; Delivery | NEWSPA - New systems for future space operations | Oral | 2 |
| Valery Frolov; Mikhail Medvedsky; Vadym Naumov; Petro Smertenko; Arnolds Ubelis; Vidvuds Beldavs | Current problems of modeling and monitoring of near-earth orbital debris population for the safety of the future space missions | National Academy of Sciences of Ukraine | aerospace technology; space debris; remote sensing; environmental monitoring; mathematical modeling | SUSTSP - Sustainable Space: Logistics and Space Debris | Poster | 54 |
| Ignazio DIMINO; Cristian Vendittozzi; William Reis Silva; Rafael C.F. Mendes; Salvatore Ameduri; Laura Paglia; Francesco Marra | Mechanical design of a deployable morphing aeroshell for 12U CubeSat atmospheric reentry | CIRA, The Italian Aerospace Research Centre | morphing aeroshell; smart materials; re-entry vehicles | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 2 |
| Jose Felix ZAPATA USANDIVARAS; Annafederica URBANO; Michael BAUERHEIM; Bénédicte CUENOT | Data-driven multi-fidelity surrogate models for Rocket Engines injector design | ISAE-SUPAERO/CERFACS | rocket engines injectors; surrogate models; deep learning; transfer learning; CFD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| Carola Glasgow; Christopher Chaffardon; Achim Tobias; Dragan Dislijeski; Henry Ebsen; Florian Ruhhammer | Mechanical Ground Systems within the SAMMA Project - Review and way forward | MT Aerospace AG | Mechanical; Ground systems; SAMMBA; Minilauncher | NEWSPA - New systems for future space operations | Oral | 2 |
| Hongsheng Yu; Xiaodong Yu; Hongwei Gao; Wei Zhang; Luigi T. DeLuca; Ruiqi Shen | Using metal oxides to reduce pyrolysis difficulty for getting weaken-bond HTPB-based hybrid rocket fuels | Nanjing University of Science and Technology | hybrid rocket propulsion; fuel; weaken-bond HTPB; catalysts; combustion | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 43 |
| Wrik Mallik | Deep learning-based model for predicting the unsteady fluid-structure interaction of flapping wings | University of Glasgow | Deep learning; fluid-structure interaction; model reduction; flapping flight | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 4 |
| Philipp Nieke; Vladimir Yotov; Guglielmo S. Aglietti; Nicholas J. Rattenbury; John E. Cater | Mechanical Properties of Additively Manufactured Titanium Alloy Sandwich Structures for Thermal Protection | The University of Auckland | mechanical properties; thermal protection system; additive manufacturing; lattice structure; Ti-6Al-4V; vibration testing; modal analysis | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 4 |
| Konstantinos KATSONIS; Chloe BERENGUER | Using the CO2DGM model to characterize and to diagnose electric thrusters meant for propulsion near Mars or Venus | DEDALOS Ltd | Electric propulsion; CO2 atmospheres; modelling; diagnostics | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 2 |
| Jeongsu Ahn; Jongho Shin; Hyeong-Geun Kim | Deep reinforcement learning based integrated guidance and control for a longitudinal missile system | ?????(Chungbuk Nat'l Univ) | Guidance law; Neural Networks; Deep Reinforcement Learning; Soft Actor-Critic | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 1 |
| Angelo Pasini; Stefano Calatafimi; Elia Puccinelli; Juliusz Saryczew; Thomas Searle | Vacuum Test Campaign of a Hydrogen Peroxide Propulsion System for CubeSats | University of Pisa | Green propellants; chemical propulsion system; hydrogen peroxide; test campaign; ESTEC; ESA; CubeSats; monopropellant | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 12 |
| JaLoettgen; Matteo Ceriotti; Gerardo Aragon-Camarasa ; Kevin Worrall | Deep reinforcement learning for spacecraft attitude tracking manoeuvres | University of Glasgow | Spacecraft Attitdue Control; Deep reinforcement Learning; Attitude Tracking | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 7 |
| Jian Cheng; Jinle Cao; Yinghua Ye; Ruiqi Shen | Microwave controlled ignition, combustion and extinguishment characteristics of ADN-based ionic liquid propellant in single mode resonator | Nanjing University of Science and Technology | ADN; ionic liquid propellant; microwave controlled propulsion; microwave ignition | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 39 |
| Raphaël Chirac; Herimanana Zafiharimalala; Arturo Martinez-Gracida; Franck Cazaurang; Jean-Marc Andre | Validation of a hazard taxonomy with aviation maintenance experts | Human design Group | Aircraft maintenance; hazards taxonomy; safety | HUMANF - Human factors in Aviation and Space | Poster | 23 |
| Max BAAN; Reinier van Dijk; Tobie van den Berg ; Petter Andersson; Robin Augustinus; Ingo Staack; Christopher Jouannet; Gianfranco La Rocca; Bastiaan Beijer; Massimo Panarotto; Peter Edholm | Using ParaPy's single source of truth to accelerate design processes | ParaPy | DEFAINE; front-loading; aircraft design; KBE | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 10 |
| Boseok Kim; Chang-Hun Lee; Min-Jea Tahk; Yongkun Lee; Hong-Gye Sung | Mid-Course Trajectory Optimization of VFDR Missiles via Pseudospectral Sequential Convex Programming | KAIST | Mid-Course Phase; Trajectory Optimization; Variable-flow Ducted Rocket (VFDR); Sequential Convex Programming | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 1 |
| Giuseppe Di Pasquale; David Villegas; Manuel Sanjurjo-Rivo; Daniel Perez Grande | Variable-Performance Electrospray Maneuvers Optimization | IENAI SPACE | optimization; mission analysis; electric propulsion | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 5 |
| Joseph El Rassi; Bernd Helber; Simone del monte; Pierre Schrooyen; Alessandro Turchi; Thierry Magin; Louis Walpot | Demise performance of Composite Overwrapped Pressure Vessels in reentry conditions | Von Karman Institute | Composite material; high enthalpy flow; material charecterization | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 3 |
| Yutaro Ota; Hiroya Asakawa; Ryohei Ishikawa; Tatsuya Hashizume | Verification of the Electrical Thrust Control Valve in the Small LOX/Methane Engine Firing Tests | IHI corporation | Electrical thrust control; Cryogenic valve; LOX/Methane; Rocket engine | FLOCON - Advanced Aerospace Designs by Innovative Flow Control Technologies | Oral | 2 |
| Kaname Kawatsu; Kohji Tominaga; Taiichi Nagata; Go Fujii; Yoshinori Kondoh; Kazutoshi Ombe | Demonstration plan of fault diagnosis in propulsion system during HTV-X experiment mission for future technologies | JAXA | Spacecraft liquid propulsion; Modelica; In-situ health monitoring; HTV-X | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 2 |
| Hadrien AFSA; Gwendal COLLET; Antoine JOLLY 3; Antoine LE GALL; Jean-Luc CHARLES; David TCHOU-KIEN | MINI-APTERROS: A GNC demonstrator for Vertical Landing and Thrust Vector Control systems | MCA Ingénierie | GNC; TVC; AI; PERSEUS | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 2 |
| Keisuke Bando; Toru Kuga; Toru Tsukano; Satoshi Takada; Hiromitsu Kakudo | Verification of Turbopump in the Small Thrust LOX/Methane Engine Firing Tests | IHI Corporation | Turbopump; Rocket engine; LOX/Methane; Full-expander cycle; Firing test | TURBO - Turbomachinery for Aeronautical and Space Applications (Session Organized with EUROTURBO) | Oral | 1 |
| Valeriy Trushlyakov; Vadim Yudintsev; Sergei Onishchuk | Deployment dynamics for rotating space tether systems | Rotating space tether systems; deployment dynamics; tether tension | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 1 | |
| Sylvain Chardon; Timotéo Payre; Hugo Grardel; Yann Quentel; Mathieu Thomachot; Gérald Aigouy; Frank Claeyssen | Miniature Fast Steering Mirrors (FSM) for Space Optical Communication in NanoSats and CubeSats | CEDRAT TECHNOLOGIES | Fast Steering Mirror; Pointing Ahead Mechanism; Optical Communication; Feeder link; Raster Scan; Line Of Sight Stabilization | NEWSPA - New systems for future space operations | Oral | 3 |
| Paolo Bellomi; Federica Zaccardi; Carlo Bianco; Giorgio Gubernari | Vertue, a green orbital module to meet the growing demand for in-orbit operations | Finis Terrae SRL | In-orbit operations; Vega; green propulsion | NEWSPA - New systems for future space operations | Oral | 1 |
| Alison Ponche; Andrés Marcos; Thomas Ott; Ramin Geshnizjani | Derivation and Verification of a Flexible Hexapod Model for Multi-Body Space Observatories | University Carlos III of Madrid | Modelling; Flexible Modes; Pointing Mechanism; Multi-Body Multi-Actuator Spacecraft | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Hyeon Jun Lee; Bo Hoon Moon; Chan Kwag; Aye Aye Maw; Jae-Woo Lee | Mission Planning of Manned-Unmanned Aircraft Teaming based on Reinforcement Learning: Suppression of Enemy Air Defenses(SEAD) Mission | Konkuk University | Reinforcement Learning; Manned-Unmacnned Aircraft Teaming; Centralized Mission Planning; Surppression of Enemy Air Defence; AirSim | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 1 |
| Jean Desmariaux; N. Perbet; J. Herpe1; Y. Saito; Adachi Hirokazu; Minami Yoshinori; D. Terakado; Lars Witte; Silas Eichel; Jens Windelberg | VERVIEW OF CALLISTO VEHICLE DEVELOPMENT STATUS | CNES | CALLISTO; demonstration; System; VTVL; landing; recover; reuse | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 2 |
| Chang-Hoon Sim; Chang-Min Lee; Jae-Sang Par | Derivation of Buckling Knockdown Factors for Hemispherical Shells with Foam Core | Chungnam National University | Buckling Knockdown Factor; Postbuckling Analysis; Hemispherical with Foam Core; Initial Imperfection | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Mingwei SUN; Zhiming YAN; Jian FU | Model-based comparative evaluation of stability performance of hydraulic servo actuators and electro mechanical actuators for flight controls | School of Mechanical Engineering and Automation, Beihang Univ. | Actuation system; flight control; hydraulic servo actuator; electromechanical actuator | SYSINT - System-Integration on Aircraft and Space Systems | Oral | 1 |
| Jinhyuk KIM; Jong Youn PARK; Soon-Young PARK; Indeuk KANG; Iksung CHOI | Vibration test of upper stage engine for KSLV-II | Korea Aerospace Research Institute | Vibration test; upper stage engine; liquid rocket engine; KSLV-II; frequency response function | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 |
| Macheret; Del Pedro | Design and deployment methods for a Martian exploration airship | EPFL | Mars; Airship; Ballon; Exploration; Envelope; Deployment | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 2 |
| Dmitry Chernetsov; Bryan Laabs; Robert Luckner; Ralph Paul | Model-Based Development of a Library with Standard Functions for Safety-Critical Flight Control Laws | Technische Universität Berlin | Flight Control Library; SCADE; Simulink; DO-178C; DO-331; Model-Based software development; safety-critcal software | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 6 |
| Francesca Roncolini; Giuseppe Quaranta | Virtual pilot: a review of the human pilot's mathematical modeling techniques | Politecnico di Milano | HMI; Virtual Pilot; Human Operator's Modeling; Simulation Model | HUMANF - Human factors in Aviation and Space | Oral | 2 |
| Federico Toson; Carlo Bettanini | Design and development of the ATEMO atmosphere monitoring device. | CISAS G. Colombo | Earth Observation; Air Pollution; Light Pollution; Balloons; Drones | AEROST - AEROSTATS – Airships, balloons, lighter than air | Oral | 1 |
| Lining YANG; Baoyan HU; Haolin MA; Jian FU; Lijian WANG | Modeling and position control of electromechanical actuators for the tiltrotor conversion system of eVTOL aircraft | School of Mechanical Engineering and Automation, Beihang Univ. | eVTOL aircraft; electromechanical actuator; synchronization control; transition performance; structural strength simulation | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 2 |
| Mariano Di Matteo; Berten Olivier; Patrick Hendrick | VoF-to-DPM 3D Model for non-reacting gas liquid two-phase flow | Université Libre de Bruxelles | CFD; Two-phase flow; Discrete phase model | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Aaron Nagel; Leo Basov; Martin Grabe | Modeling of polyatomic gas flows within a kinetic Fokker-Planck approach using a direct modeling method | German Aerospace Center (DLR) | DSMC; Fokker-Planck; rarefied flows | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 3 |
| Granger Florian; Airiau Magdeleine; Devillers Robin; Dorey Luc-Henry; Zuzio Davide; Estivalezes Jean-Luc | Volume estimation on ombroscopy images using deep learning and high fidelity simulations | CNES/ONERA | Deep learning; high fidelity simulations; volume estimation; two-phase flows; assisted atomization | TESTING - Testing in Aerospace | Poster | 60 |
| Mathew Denys; Cameron Shellard; Andrew Limmer-Wood; Gennady Sidorov ; Jakub Glowacki and Randy Pollock | Design and testing of a heaterless hollow cathode for a low- current electric thruster | Victoria University of Wellington | in-space propulsion; electric thrusters; cathodes | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 9 |
| Marco Fabiani; Mario Tindaro Migliorino; Daniele Bianchi; Francesco Nasuti; Massimo Franco; Francesco Barato; Nicolas Bellomo; Daniele Pavarin | Modeling of swirl injection effects in a H2O2-HDPE hybrid rocket | Sapienza University of Rome | Swirl; hybrid rocket; CFD | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 17 |
| T. Devo; A. Beaurain; S. Penaherrera; E. Deletombe; Y. Desplanques; P. Dufrénoy | Wear and heat of aircraft materials in case of emergency landing situations | ONERA | Emergency landings; Wear & Heat; Aircraft's structural materials; Friction tests; Tribological Systems | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 2 |
| Nachiket Dighe; Alexis Harvey; Niklas Emil Knöll; Thomas Müller; Andries Nusselder; Claudio Rapisarda; Oliver Ross; Mohamed Sahir Sujahudeen | Design and Testing of a Reefed Disk-Gap-Band Parachute of Huygens Heritage for Sounding Rocket Recovery | Delft Aerospace Rocket Engineering | Parachutes; Reefing; Sounding rocketry; Wind-tunnel testing | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| LI Yubo?XIAO Tianhang?DENG Shuanghou?XIAO Jiliang | Modeling periodic evolution of aero-optical caused by supersonic mixing layer | Nanjing University of Aeronautics and Astronautics | Aero-optical effect; Supersonic mixing layer; LES; Numerical simulation | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 6 |
| JONGMIN KIM | Weight reduction of TPS and insulation material by using thermal conductivity in vacuum condition | Korea Aerospace Research Institute | vacuum; insulation; thermal conductivity; TPS | TESTING - Testing in Aerospace | Poster | 59 |
| Eve Pachoud; Fabien Tholin; Anne Bourdon | Modelisation of plasma discharge for aerospace applications : Streamer to arc transition | ONERA | modelisation; plasma discharge; streamer discharges; electric arcs; | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 5 |
| Longobardi Pasquale; Skaloud Jan | Wind Tunnel Characterization of a Delta-Wing UAV for Model-Based Navigation | EPFL | UAV; Wind Tunnel; Aerodynamics; Autonomous; Model-based navigation Navigation | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Poster | 64 |
| Giuseppe OLIVA; Daniel CANTOS; Pietro MONDINO; Gaston CHAMPAGNE; Lisa BUXTON; Raquel ARRONTES; Giulio PELENGHI | Design and testing of the combustion chamber of a H2O2/ABS student-developed hybrid rocket engine | ISAE-SUPAERO / Supaero Space Section | hybrid propulsion; testing; student project; hydrogen peroxide; ABS | STUDENT - Space Student Projects | Oral | 2 |
| Antoine SALGAS; Scott DELBECQ; Thomas PLANÈS; Gilles LAFFORGUE; Joël JÉZÉGOU | Modelling and simulation of new regulatory measures in prospective scenarios for air transport | ISAE-SUPAERO | Regulations; Costs; Emissions Targets; Scenarios; Low-Carbon Fuels; Carbon Prices | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Oral | 5 |
| Catharina Moreira; Christian Breitsamter | Wind Tunnel Experiments of an eVTOL Wing-Propeller Configuration | Technical University of Munich | Tiltrotor; propeller aerodynamics | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Oral | 3 |
| Alejandro PRADAS GOMEZ; Tobie VAN DEN BERG; Massimo PANAROTTO; Ola ISAKSSON | Design strategies for critical aerospace components during conceptual design phases | Chalmers University of Technology | Design Automation; KBE; Product Development Process | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 9 |
| José Alfredo Macés-Hernández; David Seelbinder; Stephan Theil | Modelling and Stability Analysis of Sloshing on Liquid-Propelled Reusable Launch Vehicles | German Aerospace Center (DLR) | GNC; flight control systems; robust control; H-infinity; flight dynamics; sloshing; multibody dynamics; launch vehicles; reusable launch vehicles | FDGNCAV - FLIGHT DYNAMICS/GNC and AVIONICS for Aeronautics and Space Applications | Oral | 4 |
| R. Maas; A. Pizzi; D. Prederi; A. Graziani | Wing loads models for a tiltrotor from flight data acquired during tests | Royal NLR | Machine Learning; predictive models; tiltrotor | TESTING - Testing in Aerospace | Oral | 1 |
| Alessio Gizzi; Viviana Ferretti; Michele Urbano Martini; Daniele Liuzzi; Daniele Drigo | DESIGN LOOP PROCESS FOR COOLING JACKET OF LIQUID ROCKET ENGINE | AVIO S.p.A | Liquid rocket engine; cooling jacket; design process | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 7 |
| Benjamin Khiar; Fabien Tholin; François Pechereau; Denis Packan | Modelling of MHD flow control for atmospheric re-entry | ONERA | MHD; re-entry; flow control; hypersonic; magnetic field | AEROFLIPHY - AERODYNAMICS and FLIGHT PHYSICS for Aircraft and Launch Vehicles including Re-Entry Bodies | Poster | 3 |
| Mohamed Sereez; Mikhail Goman; Nikolay Abramov | Wing Rock Prediction in Free-to-Roll Motion Using CFD Simulations | Coventry University | Wing Rock; Free-to-Roll; CFD; Overset | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Alessio Gizzi; Viviana Ferretti; Michele Urbano Martini; Daniele Liuzzi; Daniele Drigo | DESIGN LOOP PROCESS FOR INJECTOR DOME OF LIQUID ROCKET ENGINE | AVIO S.p.A | Liquid rocket engine; Injector Head; design process | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 5 |
| Daniel Frank; Christiane Bauer; Caroline Willich | Modelling of the cathode air supply for a pressurized hydrogen fuel cell system in airborne applications | Universität Ulm | Fuel Cell; Air Supply; Modelling | CLINAV - Climate-Neutral Aviation Fuels and Alternative Propulsion Systems (Session Organized with EASN) | Oral | 1 |
| Saeed HOSSEINI; Hamid Reza OVESY; Mohammad Ali VAZIRY-ZANJANY | Wing Structure Optimization of a Truss-Braced Wing Regional Jet Aircraft with Strength, Stiffness, and Stability Requirements | Amirkabir University of Technology | Truss-Braced Wing; Aeroelasticity; Sizing; Loading | STRMAT - Structures & Materials for Aeronautic and Space Systems | Oral | 9 |
| Etienne Gourcerol; Victor Désangles; Denis Packan; Freddy Gaboriau | Design of a 2-axis thrust stand for thrust vectoring diagnostics of an ECR thruster | ONERA | Electric propulsion; ECR thruster; thrust vectoring; 2-axis thrust stand | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Poster | 37 |
| Tomasz Palacz | MOTUS - motorized dispenser for the nanosatellite constellation deployment | AGH UST | OTV; last-mile logsitics; motorized dispenser; motus | SUSTSP - Sustainable Space: Logistics and Space Debris | Oral | 5 |
| Pavol Pecho; Raffaello Mariani; Martin Bugaj; Jakub Jackulia | Design of an Unmanned Return Module for the Conditions of Stratospheric Phenomena Measurements | University of Zilina | UAV; Weather; Balloon; Glider; Stratosphere; Return; Module | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| Amira Saleh Alhosani; Nawal Mohammed Alblooshi ; Najoud Saleh Alhosani; Alreem Mattar Alsaedi; Sheharyar Malik | Moveable Empennage of The Blended Wing Aircraft | Abu Dhabi Polytechnic | moving tail; rotating tail; drag reduction; blended wing; novel idea | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Reject | |
| Raphael Aubry; Antoni Barredo Juan; Alberto Lopez Platero; Andrea Marrazza | Design of the regenerative cooling system for a 4kN LOX/Ethanol student-built liquid rocket engine | ISAE Supaéro | Space propulsion; cooling channel design; student rocketry; PERSEUS | STUDENT - Space Student Projects | Oral | 1 |
| Sultan Alyammahi; Hamad Albalooshi; Talal Alyaqubi; Mohammed Alhammadi ; Mohammed Alhammadi; Sheharyar Malik | Moveable winglets on the wing of the aircraft | Adpoly | Winglets; induced drag; moveable wing tip; drag reduction; novel wing tip Winglets; induced drag; moveable wing tip; drag reduction; novel wing tip | SUSTAV - Sustainable Aviation: Aircraft Design and Flight Operations | Poster | 53 |
| Sara Di Benedetto; Marco Marini; Giuseppe Di Lorenzo; Pietro Roncioni; Paolo Vernillo | Design of the Scramjet Hypersonic Experimental Vehicle | CIRA | Hypersonic vehicle; scramjet engine; experimental flight mission | NEWSPA - New systems for future space operations | Oral | 3 |
| Fu-Yuen Hsiao; Chun-Wai Wong | Design of translunar injection trajectories using phasing loops in a TPBVP | Tamkang University | Translunar Injection (LTI) Trajectories; Phasing Loops; Lunar Exploration; Two-Point Boundary Value Problem (TPBVP) | SPEXPLO - Space Exploration - In Situ Resource Utilization | Oral | 2 |
| Petter Andersson; Marcus Lejon; Saravanan Chidambaranathan; Siva Dasari; Massimo Panarotto; Max Jacobson | Multidisciplinary design space exploration: An electric fan thruster component design use case | GKN Global Technology Center, Sweden | KBE; Multidisciplinary Design; Design Space Exploration; Machine Learning | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 10 |
| Luis Miguel García-Cuevas; Jorge García-Tíscar; Pau Varela; Federico Nahuel | Design of unmanned air vehicles with distributed electric propulsion: range improvement and noise emission | CMT - Motores Térmicos. Universitat Politècnica de València | Unmanned Air Vehicle; Distributed Electric Propulsion; Boundary Layer Ingestion; Aircraft Design; Noise Emissions | UAVFUT - UAVs: Future Applications/Services and Specific Technologies | Oral | 2 |
| Mauricio Jentys; Tim Effing; Christian Breitsamter; Eike Stumpf | Multifidelity aerodynamic analyses of a hybrid laminar flow control and variable camber coupled wing | Technical University of Munich | CFD; Overall aircraft design; Model order reduction; Hybrid laminar flow control; Variable camber wing | CFDMPS - CFD & Multi-Physics Simulation in Aerospace | Oral | 1 |
| Florian Chantre, Marc Bouchez, Olivier Poncelet | HYDROCARBON FUEL BASED ON BALL-MILLED ALUMINIUM AND DODECANE | MBDA | PROPHY - Propulsion Physics for Aeronautic and Space Applications | Oral | 20 | |
| Margot Clauss; Bernd Weiss; René Laufer; Anna Öhrwall Rönnbäck | Circularity and Sustainability in Aerospace: The Case of Spacecraft Materials | Luleå University of Technology | REUSYS - Reusable Systems for Space Access and In-Orbit Operations | Oral | 3 | |
| Mitchell Galletly; Allen Chan; Dries Verstraete | Design Optimisation and Comparison of Propulsion Systems for Sounding Rockets | University of Sydney | SYSINT - System-Integration on Aircraft and Space Systems | Poster | 57 | |
| Brandon Israel Escamilla Estrada;Giuseppe Di Pasquale;Daniel Gonzalez Arribas;Daniel Pérez Grande;Manuel Sanjurjo-Rivo | A Concurrent Methodology for Optimizing Constellation Deployment and Launcher Selection | Universidad Carlos III de Madrid | SUSTSP - Sustainable Space: Logistics and Space Debris | Poster | 55 |
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