session IP

Title: Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
type: interactive
Description: This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Propulsion addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.
Room: IP Area

IPC members

Co-Chair: Dr. Saroj Kumar, Propulsion Research Center, University of Alabama in Huntsville, United States;
Co-Chair: Dr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;
Co-Chair: Prof. Sabrina Corpino, Politecnico di Torino, Italy;

papers
Paper title	Presentation status	Speaker	Affiliation	Country
Visual Observation of Vortex Cooled Methane/Oxygen Combustion in a Transparent Acrylic Thruster		Mr. Yahia Badran	Student	United Arab Emirates
3D Printed Venturi Flowmeter for Student Rocketry Applications		Ms. Brianna Clark	California State University, Long Beach	United States
Large Eddy Simulation of the Scramjet Combustor Using a Developed Density-Based OpenFOAM Solver	confirmed	Mr. Veli Uysal	National Defence University of Türkiye	Türkiye
3D combustion flow field prediction for the forced ignition process of RBCC engines	confirmed	Mr. Jizheng Qiu	Northwestern Polytechnical University	China
Review on Active Thermal Protection and Heat Transfer for Airbreathing Hypersonic Vehicles	confirmed	Mr. Zeki Inanc Genc	Samsun University	Türkiye
Development and Experimental Validation of a Custom Capacitive Level Sensor for Real-Time Nitrous Oxide Inventory Management in Bi-liquid Propellant Tanks	confirmed	Mr. Łukasz Ciorga	Wroclaw University of Science and Technology	Poland
Design and Testing of a Scalable Piston Propellant Tank for a Small Satellite Propulsion System	confirmed	Mr. Daniel Kichma	Space Flight Laboratory (SFL)	Canada
Design and Characterization of an Optimized Miniaturized Ion Propulsion System for CubeSat Missions	confirmed	Mr. Furkan Kaplan	Karadeniz Technical University	Türkiye
INTEGRATED TEST CAMPAIGN FOR THE CHEMICAL PROPULSION SYSTEM OF THE EMIRATES MISSION TO THE ASTEROID BELT	confirmed	Ms. Nourah Alyammahi	UAE Space Agency	United Arab Emirates
Design and Technical Requirements of a Methane Rocket Engine Combustion Test Facility for Future Launch Vehicle Development	confirmed	Dr. Donghyuk Kang	Korea Aerospace Research Institute (KARI)	Republic of Korea
Development of an Annular Chamber Based 1N-Class Induction Heating Thruster for Non-Catalytic Nitrous Oxide Thermal Decomposition	confirmed	Mr. Junseo Hwang	Pusan National University	Republic of Korea
Development of an electrical system for vacuum arc thruster	confirmed	Mr. Dmitriy Myatezhnyy	Bauman Moscow State Technical University	Russian Federation
Comparative Assessment of Analysis Methods for Hot-Gas-Side Heat Transfer Prediction in Preliminary Liquid Rocket Engine Design	confirmed	Mr. Kerem Kizilboga	Istanbul Technical University	Türkiye
Engineering assessment of electrodeless plasma accelerator operating regimes during preliminary design	confirmed	Mr. Artur Andronov	Bauman Moscow State Technical University	Russian Federation
Experimental and Numerical Investigation of Silver Screen Catalyst Beds with High Bed Loading and Capacity for 90% Hydrogen Peroxide Monopropellant Thrusters		Mr. Yuchen Zhang	Beihang University (BUAA)	China
Initial Operation of a Small-Scale Rotating Detonation Engine with Non-Premixed Propellants		Mr. Yahia Badran	Student	United Arab Emirates
Effect of the Carbon Number of Fully Saturated Hydrocarbon Fuels on the Regenerative Cooling of Small Liquid Rocket Engines	confirmed	Mr. Berkay Gurel	Koc University	Türkiye
Multiphysics Simulation of the IACANGA Solid Rocket Motor: CFD, Thermal, and Structural Integration with Experimental Validation	confirmed	Mr. Jorge Miguel Adame Martínez	Instituto Politécnico Nacional	Mexico
Integrated Software Architecture for Autonomous Metrology, Real-Time Signal Processing, and Anomaly Detection in Micro-Newton Thrust Stands	confirmed	Ms. Luana Almeida	University of Brasilia	Brazil
Parametric Analysis-Based Thermal Performance Prediction in Helical Coil Heat Exchangers	confirmed	Mr. Alperen Ada	ROKETSAN Roket Sanayi ve Ticaret A.S.	Türkiye
The effects of different production methods in paraffin fuels on hybrid rocket motor performance		Dr. Melahat Cihan	Samsun University	Türkiye
Watercube IOD Preparation: Functional, Structural, Propulsive & Thermal Qualification Campaign	confirmed	Mr. Dani Kiblawi	Capsule Corporation	Italy
Optical diagnostics of discharge in plasma thruster with closed ring-shaped gas discharge chamber	confirmed	Mr. Lev Scherbakov	Bauman Moscow State Technical University	Russian Federation
Laser Ablation and Pulsed Plasma Micro-Propulsion Systems	confirmed	Mr. Vadim Danilov	Bauman Moscow State Technical University	Russian Federation
thrust profile optimization of solid rocket motors via internal and external ballistic integration	confirmed	Dr. Hanyun Zheng	Beihang University (BUAA)	China
Variable Geometry Thruster Nozzle Inspired by Squid Jet Propulsion for Ion Propulsion Systems	confirmed	Mr. Efe Aras Aykut	Darüşşafaka High School	Türkiye
Development of a Water-Fed Electrodeless Plasma Thruster within the W.E.T Project	confirmed	Ms. Dounia Bartal		Morocco
Optimal magnetic field configuration for ECR Electrostatic Thruster	confirmed	Ms. Amalia Lefeuvre	Osmos X	France
Exploring Recycled Metal Propellants for Magdrive Thrusters via Plume Deposition Characterisation	confirmed	Ms. Emerald Greenwood	Magdrive Ltd	United Kingdom
Multiphysics Modeling & Optimization of Electrospray Arrays	confirmed	Mr. Punya Malaiya Jain	Indian Institute of Technology, Madras	India
Ferrite-Core Pre-Ionization for Enhanced Ignition in RF Ion Thrusters	confirmed	Ms. Gökçe Uluğsu	Boğaziçi University	Türkiye
A Novel Design of an Inductively Coupled Plasma Ion Thruster with Distributed Ferromagnetic Cores	confirmed	Ms. Gökçe Uluğsu	Boğaziçi University	Türkiye
Distributed Ion Thruster Arrays for Scalable and Fault-Tolerant Electric Propulsion Systems	confirmed	Ms. Shahed Alshab	MENA ENGINEERING EDUCATION AND TRAINING	Jordan
Design methods and life-cycle assessment of OPAL, a hybrid autophage thruster for high-Δv in-space mobility	confirmed	Mr. Martin Gros	Alpha Impulsion	France
Promising heat-resistant coatings for uncooled units of rocket and space engineering	confirmed	Dr. Volodymyr Nadtoka	Yuzhnoye State Design Office	Ukraine
graphene-reinforced paraffin-based hybrid rocket fuel for enhanced combustion performance	confirmed	Ms. Senanur Gamlı	Gebze Technical University	Türkiye
Cold-flow characterization of showerhead, vortex and swirl injectors for hybrid rocket motors under two-phase oxidizer conditions	confirmed	Mr. Fırat Aydın	Yildiz Technical University	Türkiye
Static firing of an integrated hybrid autophage engine using the first embedded, flight-representative propellant insertion system	confirmed	Mr. Martin Gros	Alpha Impulsion	France
DEMİRKAZIK-IV: Türkiye's Highest Total Impluse Student-Built Hybrid Motor	confirmed	Mr. Alp Bora Görüşken	Yildiz Technical University	Türkiye
Effects of Solid Oxidizer Additives in Hybrid Rocket Fuels on Oxidizer Tank Sizing and Propulsion System Mass	confirmed	Mr. Huzeyfe Ali Karakuşoğlu		Türkiye
Thermochemical Characterization and Performance Prediction of 3D Printed Polymer Fuels for Hybrid Rocket Engines	confirmed	Ms. Aleksandra Zieleźny	Wroclaw University of Science and Technology	Poland
flow characterisation of a cots breather valve for use in sounding rocket compartment venting	confirmed	Dr. Sarisha Harrylal	University of KwaZulu-Natal (UKZN)	South Africa
Mechanical Design and Chemical Compatibility of Flow Control Elements for High-Performance Hybrid Rocket Propulsion Systems	confirmed	Mr. Semih Tiryakiol		Türkiye
Theoretical–Experimental Correlation of Discharge Coefficient in a 100 N Paraffin/N₂O Hybrid Motor	confirmed	Mr. Levent Berke Duyuk	Koc University	Türkiye
End-to-End Transient Simulation and Experimental Validation of a Nitrous Oxide Feed Line for a Lab-Scale Hybrid Rocket Motor	confirmed	Ms. Rukiyye Melek AYDURMUŞ	Gebze Technical University	Türkiye
Machine Learning-Enhanced MDO Framework for Target-Driven Sizing and High-Fidelity 3-DOF Stochastic Simulation of Experimental Solid Rocket Motors	confirmed	Mr. Alan Nolasco Méndez		Mexico
performance evaluation of 3d-printed abs fuel for low-cost hybrid rocket propulsion	confirmed	Ms. Najihah Abd Razak	International Islamic University Malaysia	Malaysia
Numerical Analysis on Radiative Heat Transfer and Its Impact on Regression Rate in H₂O₂/HTPB Hybrid Rocket Motors		Mr. Jingfei Gao	Beihang University (BUAA)	China
Revisiting the Fuel Heat of Gasification in Hybrid Rocket Engines: Flux-Dependent Correlations for Improved Regression Rate Prediction		Ms. Jiaqi Tian	Beihang University	China
Additive Fabrication Concept for Launcher Engine Nozzle Extension – Next Steps with Large-Scale Laser Powder Bed Fusion	confirmed	Mr. Jonas Öhrman	GKN Aerospace Engine Systems	Sweden
DFT and NEB Analysis of Magnesium-Catalyzed Methane Dissociation for ISRU-Enabled High-Performance Propellants in Interplanetary Missions	confirmed	Mrs. Kinga Wysocka	Embry-Riddle Aeronautical University	United States
A Design Concept for a Combined Full-Flow Staged Combustion and Continuous Detonation Rocket Engine for Mars Missions	confirmed	Mr. Onur Kağan Yıldırım		Türkiye
Solar Wind–Assisted Propulsion Systems (SWAPS)	confirmed	Mr. Sathvik Krishna Velide	CosmoFleet	India
the effect of stabilizer-induced poisoning on lifetime and performance of catalyst used in hydrogen peroxide thrusters	confirmed	Ms. Elif Funda ALTUN	Istanbul Technical University	Türkiye
STREAM Electric Gear Pump Enabling Low-Pressure Propellant Feed Architectures	confirmed	Mr. Adam Hláčik	Stellar Exploration Inc	Czech Republic
Simulation-based Design of an Additively Manufactured Bi-liquid Rocket Engine Coaxial Swirl Injector	confirmed	Mr. Joel Jia Le Tan	ETH Zurich	Switzerland
Overview of LE-9 Engine Turbopump Design and Turbine Blade Vibration Measurement Test	confirmed	Mr. Atsuhiro TSUNODA	Japan Aerospace Exploration Agency (JAXA)	Japan
Experimental Investigation and Flow Rate Reconstruction Method for Liquid Hydrogen Feedline Chilldown Processes	confirmed	Dr. Peisen Lu	China Academy of Launch Vehicle Technology (CALT)	China
Experimental and Numerical Investigation of a Central Body Injector for Methane/Oxygen Space Propulsion	confirmed	Mr. Justus Caspar	TU Braunschweig, Institute of Space Systems	Germany
Development of a GPU-Accelerated High-Order Compact Incompressible Flow Solver	confirmed	Ms. Elif Mihriban Zeyveli	Istanbul Technical University	Türkiye
development of an integrated shadowgraphy system with automated image-processing for testing and characterization of high-speed liquid rocket injector sprays	confirmed	Mrs. Deniz Başar	Koc University	Türkiye
characteristics of taylor cones in non-uniform electric field of circular-emitter ionic liquid electrospray thruster	confirmed	Dr. Cheng Yang	Beijing Institute of Technology	China
characterization of power processing unit integration and its influences on coaxial pulsed plasma thrusters	confirmed	Mr. Dillon OReilly	Southeast Technological University of Ireland	Ireland
Compact, Efficient, and Mission-Adaptable: A 150–250 W Class Hall Effect Thruster Development	confirmed	Mrs. SEDA KAYRA GULLU	TUBITAK Uzay, Space Technologies Research Institute	Türkiye
Design and Experimental Evaluation of MEMS Thrusters in Micro-Powered Space Systems	confirmed	Mr. Umut Şahan		Türkiye
Design and Experimental Validation of a Low-Voltage Ionic Plasma Thruster with Geometric Optimization for CubeSat Propulsion	confirmed	Ms. Merve Koca	Tarsus University (Tarsus Üniversitesi)	Türkiye
Development and Bench-Scale Demonstration of a Novel MEMS-Based Electrospray Thruster Head with High-Impedance Microfluidic Channels	confirmed	Ms. Blanca Pavón-Castillo	Xiroi Aerospace	Spain
Development of EPC-RFT-1, an “Expedient" Radio Frequency Gridded Ion Thruster	confirmed	Mr. Claude Blue	University of Alabama in Huntsville	United States
Integrated MIMO Control Framework for Simultaneous Thrust Vectoring and Power Optimization in Gridded Ion Thrusters	confirmed	Mr. Abdulrahman Al-Essa	Saudi Space Community (SSC)	Saudi Arabia
Linearized Detailed Electron Model for Hybrid PIC–DSMC Hall Thruster Plume Simulations	confirmed	Prof. Sang Hun Kang	Konkuk University	Republic of Korea
Numerical Studies on charged particles behavior in the acceleration region for electrospray/FEEP propulsion	confirmed	Mr. DAMULURI SURAJ BHARAJATHYA	Indian Institute of Technology, Madras	India
Precision thrust control for low-power Hall thrusters: enabling autonomous small satellite operations	confirmed	Mr. Ahmet emir Daştan	Baykar Science High School	Türkiye
Pulsed Electric Propulsion Systems for Interplanetary CubeSats	confirmed	Mr. Kevin Simmons	BLUECUBE Aerospace	United States
Reinforcement Learning for Autonomous Operation of Spacecraft Propulsion Systems	confirmed	Mr. Taiki Achiha	The University of TOKYO, Graduate school	Japan
Research on Vector Propulsion of Cylindrical Hall Thrusters		Mr. Cheng Zhe	Sun Yat-sen University (Guangzhou)	China
STARGATE: An Undergraduate Experimental Gridded Thruster Student Research Project		Mr. Claude Blue	University of Alabama in Huntsville	United States
Toward Cislunar and Deep-Space Applications: Performance Assessment of an RMF-Based Electrodeless Thruster		Dr. Luca Armani	GAUSS S.r.l.	Italy
Two-Phase Flow Modeling and Parameter Analysis of a Xenon Feed System for Hall Electric Thrusters		Mr. Jincheng Wang	Beihang University (BUAA)	China

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