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: Mr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;
Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;

papers
Paper title	Mode	Presentation status	Speaker	Affiliation	Country
Combustion Modelling and Design of Miniature Pulsed Electric Propulsion System Using Electrically Ignited Solid Propellant			Mr. Abishek Shrestha		Australia
Comparative Analysis of Propellants in Ion Thrusters: Performance, Efficiency, and Feasibility			Mr. Patel Jetun		India
Characterization of Biopolymers for Alternative Propellants in Medium-Thrust Propulsion Systems	10	confirmed	Mr. Marco Cárdenas Aldaco	Administración de Sistemas Aeroespaciales Mexicanos - ASAEM	Mexico
Design and Production of Cube Satellite with Ionic Propulsion System			Mr. Muhammed GÜNEŞ		Türkiye
Exploring gyroid infrastructure and micromagnets for advanced ionic propulsion with Xenon gas			Mr. Mohammad Al Amin Shamsol		Brunei Darussalam
IN-HOUSE DEVELOPMENT OF GRID OPTICS FOR MINIATURIZED MICRO ION THRUSTER			Mr. Ahmed Altunaiji	Sharjah Academy for Astronomy, Space Sciences and Technology (SAASST)	United Arab Emirates
Integration of Nuclear and Electric Propulsion Technologies for Long-Duration Space Exploration			Mr. Abdullah Algharrash	Space Generation Advisory Council (SGAC)	Saudi Arabia
Experimental Investigation of Green Hypergolic Propellants for Upper-Stage Propulsion: Drop Test Results and Performance Analysis		confirmed	Dr. Prakhar Jindal	Delft University of Technology (TU Delft), The Netherlands	The Netherlands
Optimization of Ionic Thrusters for Micro- and Nano-Satellite Propulsion			Mr. Jimit Pathak	Vellore Institute of Technology	India
Plasma Propulsion for Interplanetary Travel: Enabling Sustainable Deep-Space Exploration		confirmed	Ms. Tarana Karimova	Azerbaijan State Oil and Industry University (ASOIU)	Azerbaijan
Recent Developments in Electric Propulsion for Spacecraft			Ms. Alsu Guliyeva	Azerbaijan State Pedagogical University (ASPU)	Azerbaijan
Simulation of plasma processes caused by electromagnetic field oscillations in Hall ion sources			Ms. Victoria Kulikova	Bauman Moscow State Technical University	Russian Federation
The Design of a Low Current Heaterless Hollow Cathode and Validation of the 0D HHC Model			Mr. Hakki Onur Dorduncu	Rose-Hulman Institute of Technology	United States
Comparative Analysis of Nuclear Thermal and Nuclear Electric Propulsion Systems for Enhanced Space Missions			Dr. Alexander Bendoyro	University of Alabama in Huntsville	United States
watercube propulsion system engineering model mait campaign and flight model design cdr			Mr. Francesco Marino	Capsule Corporation	Italy
Dry Mechanical Mixing as an Additive Dispersion Technique for Coating Catalysts over Ammonium Perchlorate: A Novel Time-Based Approach to Determine Catalytic Performance			Mr. Satwik Mohanty	Politecnico di Milano	Italy
Experimental and Computational Study of a Hybrid Rocket Engine for Sustainable Space Propulsion		confirmed	Mr. Ahmet Arif Durhan		Türkiye
optimizing hybrid propulsion efficiency: a cooling system for nitrous oxide management			Mr. Gabriel Martinez	Universidad Nacional Autónoma de México (UNAM)	Mexico
Development of novel solid reaction control system for small satellite using electrically controlled solid propellant		confirmed	Mr. JINHA HWANG	Chosun University	Korea, Republic of
Feasibility Analysis of an Innovative Bimodal Ammonia Nuclear Thermal and Electric Rocket (BANTER)			Mr. Elia Puccinelli	University of Pisa	Italy
Visualization Study in Cryogenic Transfer Line Chill-down with a Low-Conductivity Internal Coating Layer			Mr. Hyunjun Kim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
securing the future of nuclear space propulsion: critical materials, supply chain risks, and regulatory challenges			Ms. Ilenia Bruseghello		Italy
Hybrid Nuclear Thermal-Electric Propulsion for Rapid Deep-Space Transit			Ms. Maryam abuqtaish		Jordan
Sail navigation as an alternative to conventional rockets in space exploration			Mr. Pedro Campos Domínguez	University of Guadalajara	Mexico
Propelling Without Fuel: Examining the Potential of Reactionless Propulsion in Deep Space Exploration Missions			Ms. Rishika Awasthi	Collins Aerospace	India
Thermo Structural Assessment of Solid Rocket Nozzle divergent aft end Assembly scheme flown in Successful Rocket Mission			Mr. Paul Murugan J	Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram	India
effects of valve opening sequences on startup characteristics of a 100 tonf-class methane gas-generator cycle engine			Mr. Sung Yoon	University of Science and Technology (UST)	Korea, Republic of
Ground test of nitrous oxide/ethane premixed thruster for satellite flight maneuvering		confirmed	Mr. seungyeop Baek	Chosun University	Korea, Republic of
LSTM-Based Post-Mission Assessment of Reusable Rocket Engines		confirmed	Mr. Tianwen Li	School of Astronautics, Beihang University	China
Model-based Rocket Hopper and Propulsion System Design Optimisation			Mr. Felix Ebert	Technical University of Munich	Germany
Optimization and Performance Analysis of Liquid Bipropellant Injectors for Advanced Propulsion Systems			Mr. Mehmet Kemal Ergin	Koc University	Türkiye
Optimization of Regenerative Cooling Channel Topology for LOX/Methane Engine Throat Section under Extreme Thermal Conditions			Mr. Bowei Jiao	Beihang University (BUAA)	China
study on cryogenic propellant retention technology for the upper stage of launch vehicles			Ms. Jiaqi Li	Beihang University (BUAA)	China
A web-based semi-empirical numerical tool for accessible liquid swirl injector design		confirmed	Mr. Thitut Uhthalye	University of Bristol	United Kingdom
Study on Ignition Shock Prediction in Transient Analysis of Gas-Generator Cycle Liquid Rocket Engines			Dr. Seungjae Yi	Korea Aerospace Research Institute (KARI)	Korea, Republic of
Analysis of Electric Propulsion Systems for Active Debris Removal Missions			Mr. Rosaldo Bellavita	Politecnico di Torino	Italy
application of a nitrogen gas diffuser in the oxidizer tank of a bi-propellant feed system			Ms. Lisa Lopez	University of Southern California	United States
Characterizing the Ignition Boundaries of a Gaseous Oxygen-Methane Augmented Spark Igniter for Reusable Liquid-Propellant Rocket Engines			Ms. Kelly Ash	University of Southern California	United States
Composition Investigation and Basic Combustion Research of Sustainable Rocket Propellant (SRP) Derived from Plants			Mr. Taisei Takaoka	Department of Engineering, The University of Tokyo	Japan
Cryogenic Feed System Flow Optimization Through Pre-Chill: Analysis of Liquid Nitrogen and Liquid Oxygen Testing			Mrs. Emily Hesby	University of Southern California	United States
Small-Scale Resistojet Thruster Performance Utilising a Heat Exchanger and Green Propellants			Ms. Ahoud Alkaabi	United Arab Emirates University (UAEU)	United Arab Emirates
Development and numerical validation of a novel fractal flame arrestor for flashback prevention in premixed NOFB thrusters			Mr. Jingeon Kim	Hanbat National University	Korea, Republic of
Development of a computational tool for solid motor design and rocket flight analysis			Mr. Leonel Gerardo González Pérez	Altum Principia	Mexico
Enhancing Throttle Performance Through Mixture Ratio Control in Liquid Rocket Engines			Mr. Rushabh Pawnikar	University of Southern California	United States
Evaluation of a Closed-Loop Electronic Pressure Regulator for a Bipropellant Rocket Lander Vehicle			Mr. Adrian Johnson	University of Southern California	United States
expanding possibilities: a conceptual study of water and ammonia in nuclear thermal propulsion			Mr. Lukáš Hudáček	Technical University Košice	Slovak Republic
Experimental study on the effect of number of impeller blades on hydraulic and cavitation performance of centrifugal pump used in cryogenic rocket engine			Mr. Jeetendra Kumar	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
Rarefied Gas Simulation in Vacuum Chambers for Gas-Jet Propulsion: Toward Realizing a Numerical Vacuum Chamber			Dr. Keita Nishii	Tokyo Metropolitan University	Japan
Impact of Ethanol Droplet Size and Methane Addition on the Combustion Performance of Ethanol/LOx Bipropellant Systems: Insights from Reactive Molecular Dynamics Simulations			Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
Innovative High-Voltage Testbed for Advancing Power Processing Topologies for Electric Propulsion Thrusters			Mr. Dillon OReilly	Southeast Technological University of Ireland	Ireland
integrated torch ignition unit of reusable methane/lox rocket engine			Mr. Hanmo Shen	LandSpace Technology Corporation Ltd.	China
Investigation into the Frictional Effects on Flow Regulator Dynamics in Liquid Rocket Engine			Mr. xianwei shang	School of Astronautics, Beihang University	China
Investigation of Key Operational Parameters Influencing the Steady-State Performance of a Hydrogen Peroxide Green Monopropellant Thruster			Mr. Ugur Kokal	Istanbul Technical University	Türkiye
Prospective Analysis of Biofuel Production from Waste Cooking Oil for Aviation and Space Applications in Northern Mexico			Ms. VANESSA MONTIEL VIRUEL	Universidad Autónoma de Baja California	Mexico
Low-Cost Non-Invasive Ultrasonic Liquid Propellant Level Sensing for High Performance Spacecraft			Ms. Stephanie Wegner	ispace, inc.	United States
Preliminary Experimental Investigation of a Small-Scale Rotating Detonation Engine with Non-Premixed Propellant			Mr. Azm Najjar	United Arab Emirates University (UAEU)	United Arab Emirates
Performance Optimization and Environmental Impact Assessment of Paraffin-Based Hybrid Rocket Fuels with Advanced Additives			Ms. Shraddha Lamichhane	Mach24 Orbitals	Nepal
pogo analysis and accumulator design for the pr-2 launch vehicle			Mrs. Hongwei Lou	CAS Space	China
OPTIMIZED ELECTROSPRAY PROPULSION DESIGN FOR SUSTAINABLE CUBESAT OPERATIONS			Ms. MEKHALA HEJIB	VIT Bhopal University	India
numerical analysis of central fluid effects on GH2/GO2 coaxial injector			Ms. Weiran Li	School of Astronautics, Beihang University	China
Thermal Shroud Design for Hall-Effect Thruster Thermal Performance Verification Test			Mr. Mustafa Turkmenoglu	TUBITAK Uzay, Space Technologies Research Institute	Türkiye
Multiphysics Simulation of the ORIÓN-1 Experimental Rocket Motor in Ansys: CFD, Thermal, and Structural Integration with Experimental Validation			Mr. Jorge Miguel Adame Martínez	Instituto Politécnico Nacional	Mexico
Validation of Regenerative Cooling Design Tool through Development and Test of a Liquid Rocket Engine			Mr. Nico von Eckartsberg	University of Southern California	United States
valve design for the pressurization system of large liquid rocket			Mrs. Hongwei Lou	CAS Space	China
Additively Manufactured ABS/Al Hybrid Rocket Fuels: Investigating Advanced Grain Geometry Effects on Combustion	10		Mr. Özgür Mert Küçük	Koc University	Türkiye
A Review Study on Green Propulsion for Launch Vehicles and Satellites			Ms. Chilla Sumana	Space Generation Advisory Council (SGAC)	India
Advanced Propulsion System for Pluto Orbit Insertion and Exploration			Mr. Sukhjit Singh	Space Generation Advisory Council (SGAC)	India
Analysis of Hydrogen Peroxide Thermal Decomposition in Small-Scale Monopropellant Thrusters			Ms. Wedemah Alnuaimi	United Arab Emirates University (UAEU)	United Arab Emirates
Electrically Operated and Controlled Solid Divert and Attitude Control Propulsion System for Small Satellite		confirmed	Dr. Myoungjin Kim		Korea, Republic of
end-of-mission strategies for space nuclear reactors: waste management, decommissioning, and governance challenges			Ms. Ilenia Bruseghello		Italy
experimental investigation of helium injection for enhanced natural circulation in cryogenic system		confirmed	Dr. Ao Sun	CAS Space	China
First In - Flight Ignition of Linear Aerospike Engine: Concept to Flight Testing			Ms. Bhavyashree Janardhana	POLARIS Raumflugzeuge GmbH	Germany
modular automated test equipment for propulsion and satellite subsystems based on ni compactdaq: a low-cost data acquisition approach			Dr. abderrahim Nabi	Khalifa University of Science and Technology (KUST)	United Arab Emirates
Integrating Mission and System Analyses in the BANTER Project for Nuclear Bimodal Propulsion			Ms. Julia Grill	Institute of Space Systems, University of Stuttgart	Germany
Resonant Orbital Dynamics and Electrostatic Charge Management for Efficient Propulsion and Sustainable Spacecraft Operations			Mr. Sudarsana Nerella	Virginia Tech	United States
Quantum Space Thruster			Prof.Dr. Shiang-Yi Han		Taiwan, China
Green Propulsion Technologies for Sustainable Space Operation Advancements, Applications, and Future Prospects			Mr. Abdullah Algharrash	Space Generation Advisory Council (SGAC)	Saudi Arabia
Feasibility of a Spring-Based Sustainable Launch System for Space Exploration.			Mr. Romildo Genaro Silva Cuadros	Universidad Nacional Mayor de San Marcos	Peru
Analysis of combustion regimes in a scramjet combustor operating at different dynamic pressures			Mr. Zhen Tao	Northwestern Polytechnical University	China
Design, Analysis, and Experimental Evaluation of a Cold Gas Thruster System for Martian Drone Propulsion			Mr. Akshat Sharma		India
RBCC engine flow field prediction model with "Encoder-Decoder" architecture			Dr. Tong Zhao	Northwestern Polytechnical University，NPU	China
a dual-use propulsion system for extended space exploration			Mr. Isa Guliyev	Azerbaijan State Oil and Industry University (SABAH Groups)	Azerbaijan
Atmosphere-Breathing Electric Propulsion (ABEP) to Extend Spacecraft Lifespan in Very-Low Earth Orbits (VLEOs)			Mr. Rivaldo Carlos Duran-Aquino	Universidad Nacional Mayor de San Marcos	Peru

session IP

Paper title

Mode

Presentation status

Speaker

Affiliation

Country