session IP

Title: Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM
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 (Hall B)

IPC members

Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Mr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;
Co-Chair: Prof. Riheng Zheng, Beihang University, China;

papers
Order	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	A Study of Prediction and Validation of FEEP Crown needle Internal Porosity for small satellites using CNN(Convolutional Neural Network) and random functions	10	confirmed	Mr. Jung-Won Kuk	Soletop CO., Ltd	Korea, Republic of
2	EFFECT OF EXPANDED COOLING CHANNELS ON THE THERMAL AND STRUCTURAL STRENGTH OF THE MATERIALS USED IN HYBRID ROCKET ENGINES	10	confirmed	Mr. Yiğit Kılıçaslan	Samsun University	Türkiye
3	INFLUENCE OF SURFACE AREA AND PROPELLANT MATERIAL ON THE IMPULSE BIT IN ABLATIVE PULSE PLASMA ACELERATOR	10	confirmed	Mr. Denis Egoshin	Bauman Moscow State Technical University	Russian Federation
4	Sprite-Class Satellites Propulsion to Extended Lifespan	10		Mr. gildo di domenico	Research Consortium Hypatia	Italy
5	Advancements in Hall Effect Thruster Design for Optimizing Performance in Space Missions: A Review	10		Ms. Yashika Paharia	University of Petroleum and Energy Studies	India
6	Computational Simulation of Neutral Gas Dynamics in the CubeSat Ambipolar Thruster	10	confirmed	Ms. Thamiris Thomazini Libard	University of Brasilia	Brazil
8	Development and Preliminary Evaluation of Plugim Electrospray Thruster: Focus on the Fuel Management System and Power Processing Unit	10	confirmed	Ms. Blanca Pavón-Castillo	Xiroi Aerospace	Spain
9	Experimental Testing and Numerical Simulation Validation of an Air Intake for Air-Breathing Electric Propulsion (ABEP) Systems	10	confirmed	Mr. Max Amer	Universitat Politecnica de Catalunya (UPC BarcelonaTech)	Spain
10	Fabrication and Testing of Applied Field Magneto Plasma Dynamic Thruster with Argon as Propellant	10	confirmed	Mr. Akash C	Hindustan Univerisity	India
11	Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet	10		Mr. Chenxi Xia	Beihang University (BUAA)	China
13	optimisation and durability assessment of rf helicon-based plasma thruster (k-2) for very low earth orbit air-breathing electric propulsion	10	confirmed	Mr. Adrià Barceló	Universitat Politecnica de Catalunya (UPC BarcelonaTech)	Spain
14	stargate: an undergraduate experimental electric propulsion student research project	10	confirmed	Mr. Claude Blue	University of Alabama in Huntsville	United States
15	Designing a nuclear electric propulsion system for future Pluto missions	10	confirmed	Mr. Sukhjit Singh	Space Generation Advisory Council (SGAC)	India
16	Design and structural analysis of low-cost modular rocket engine test stand.	10	confirmed	Mr. Korneliusz Szalkowski	Warsaw University of Technology (WUT)	Poland
16	Improving rocket nozzle efficiency with rough surfaces	10	confirmed	Mr. Claudio Antonio Morales Benítez	High Technology Unit (UAT) Faculty of Engineering - UNAM	Mexico
17	Power Sustainment in Long-Duration Space Missions through the Utilization of Nitinol Material Implemented in the Design of Solar Sails, Programmed with PID Control.	10	confirmed	Mr. Alan Adan Velazquez Samaniego	Instituto Tecnológico de Durango (ITD)	Mexico
18	A Study on the Optimum Design of Solid Propellant Grain Using Machine Learning.	10	confirmed	Mr. JINSEOK YOO	Inha Univ.	Korea, Republic of
19	Advancements in the development of the subsystems for a student-developed H2O2/ABS hybrid propellant rocket engine	10		Ms. Raquel Arrontes Quiroga	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
20	Alternative thrust-based algorithm for performance analysis of swirled hybrid rocket engines	10	confirmed	Mr. Valerio Santolini	Politecnico di Milano	Italy
21	An Improved Al Particle Combustion Model for Simulating the Aluminized Hybrid Rocket Motor Combustion	10	confirmed	Mr. XIAOTING NIU	Beihang University (BUAA)	China
22	Characterization of Paraffin-LDPE Blended Fuels	10	confirmed	Mr. Rafael Coelho	University of Brasilia	Brazil
23	design of dual-bell nozzle specified for the second stage engine of students' designed sounding rocket	10	confirmed	Mr. Michał Kret	Warsaw University of Technology (WUT)	Poland
24	Analysis of the nozzle impact on the characteristics of the pulse detonation engine	10	confirmed	Mr. Oleksandr Aksonov	Yuzhnoye State Design Office	Ukraine
25	Decomposition mechanism of ammonium dinitramide: a sustainable energetic molecule for green propellant technologies	10	confirmed	Mr. Zakaria Harimech	Chouaib Doukkali University	Morocco
26	Development and Integration of the Engineering Model for a Modular HTP-based CubeSat Propulsion System for future In-Orbit Validation on the UniPi EXCITE CubeSat Platform	10	confirmed	Mr. Matteo Serchi Masini	University of Pisa	Italy
27	Development and Testing of an Electrically-Driven Centrifugal Pressurization System for Hybrid Rockets in Rocket Propulsion	10	confirmed	Mr. Zelalem Bogale	Ethiopian Space Science and Technology Institute (ESSTI)	Ethiopia
28	Development and validation of rocket motor simulation software	10	confirmed	Mr. Michał Tomporowski	Warsaw University of Technology (WUT)	Poland
29	Development of Environmentally Friendly Solid Propellants Using Fused Deposition Modeling Additive Manufacturing	10		Mr. Ishaan Dutta	R V College of Engineering, Bengaluru	India
30	Development of High-Performance Solid Rocket Propellants Using AP-HTPB Composite Matrix AND Different Plasticizers	10		Mr. Om Kiritbhai Daxini	R V College of Engineering, Bengaluru	India
31	Developments in additive manufacturing for \\ solid and hybrid rocket propulsion charges	10	withdrawn	Prof. Filippo Maggi	Politecnico di Milano	Italy
32	Dynamic characteristics of hydrogen peroxide electric pump during pulse ignition process of hybrid rocket engine	10	confirmed	Mr. Xiaoming Gu	Beihang University (BUAA)	China
33	Effect of manufacturing parameters on tungsten microstructures as an emitter for FEEP thrusters	10	confirmed	Mr. Jung Won Kuk	Soletop CO., Ltd	Korea, Republic of
34	Energetic co-crystals containing ammonium nitrate obtained by solvent method as an alternative to solid rocket fuels based on perchlorates	10	confirmed	Mrs. Aneta Krawiec	Wroclaw University of Science and Technology	Poland
35	Fluidic throat technology for hybrid rocket motor based on liquid oxidizer cooling	10	confirmed	Dr. Haizhou Guo	Beihang University (BUAA)	China
36	Hydro-thermal Analysis of Fuel Element of a Nuclear Thermal Engine	10	confirmed	Ms. Nandini Sachdev	University of Petroleum and Energy Studies	India
37	Introduction of Field Emission Electric Propulsion Research in Republic of Korea	10	confirmed	Prof. Kyun Ho Lee	Sejong University	Korea, Republic of
38	INVESTIGATION INTO THE SUITABLE INJECTOR TYPES FOR SMALL-SCALE GASEOUS THRUST CHAMBERS	10	confirmed	Mr. Mousa Aqailan	United Arab Emirates University (UAEU)	United Arab Emirates
39	Investigation of Solid Fuel Pyrolysis Characteristics in Hybrid Rocket Engines Utilizing HTPB with Aluminum Additive	10		Mr. Yudong Lu	Beihang University	China
40	Low-cost Innovative Experimental Setup for Assessing Laser-Driven Propulsion in Near-Ultimate Vacuum Conditions	10	confirmed	Mr. Basel Altawil	Khalifa University of Science and Technology (KUST)	United Arab Emirates
41	Maximizing Reusability in Propulsion System Testing: A modular Data Acquisition System Using National Instruments PXI hardware and LabVIEW	10	confirmed	Dr. abderrahim Nabi	Khalifa University of Science and Technology (KUST)	United Arab Emirates
42	Numerical Computations of Nozzle Performance Losses in Solid Rocket Motors	10	confirmed	Dr. Marco Grossi	Sapienza University of Rome	Italy
43	Numerical Simulation and Experimental Study of the Throat Parallel Segment Length of Variable Area Cavitating Venturi	10	confirmed	Mr. Ruikai Chen	Beihang University (BUAA)	China
44	Optimization of pump-valve combined regulation strategy for electric pump-fed system in a hybrid rocket motor	10	confirmed	Dr. Xintong Li	Beihang University (BUAA)	China
45	Optimizing Launch Systems: Propulsion and Structural Innovations for Enhanced Efficiency in Advanced Vehicles	10	confirmed	Mr. Mohd.Amaan Mukadam	SRM Institute of Science and Technology	India
46	pace hybrid propulsion: a combination of electric and thermonuclear propulsion to optimize satellites	10	confirmed	Mr. Osmar Naim Corona Zamudio	High Technology Unit (UAT) Faculty of Engineering - UNAM	Mexico
47	Performance testing of small scale resistojet thruster with 3D printed heat exchanger	10	confirmed	Mr. Abdallah Alazeezi	United Arab Emirates University (UAEU)	United Arab Emirates
49	research on mechanism for high nozzle closure opening pressure of solid rocket motor in stage separation	10		Mr. WENBO DONG	Shanghai Academy of Spaceflight Technology (SAST), China Aerospace and Technology Corporation (CASC)	China
50	Research on cryogenic line chill-down process of industrial Teflon coated piping	10	confirmed	Mr. Hyunjun Kim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
51	Research on the performance of the modified paraffin-wax-based fuel grains in the use of Student Researched and Developed (SRAD) hybrid rocket motor	10	confirmed	Mr. Maciej Zawadzki	Gdansk University of Technology	Poland
52	research, analysis and experimental development of solid propellant type rnx for rocket engines in environments with humid mountain climate	10	confirmed	Mr. Daniel Cardenas	Universidad de Antioquia	Colombia
53	RMD simulations applied to the study of energetic materials like HMX smokeless solid propellant: a case study of HMX molecular vacancies.	10	confirmed	Prof.Dr. José Rocco	ITA-DCTA	Brazil
54	Systemisation and Performance Testing of Field Emission Electric Propulsion Thruster using Gallium as Propellant	10	confirmed	Mr. Won Gyo Seo	Soletop CO., Ltd	Korea, Republic of
55	development of subcooled liquid oxygen system for liquid rocket engine	10	confirmed	Mr. JANGHWAN LEE	Korea Aerospace Research Institute (KARI)	Korea, Republic of
56	Fatigue Failure Mechanism of Metal Bellows Caused by Flow-Induced Vibrations	10	confirmed	Mr. Zitao WANG	Beijing Institute of Astronautical Systems Enginnering	China
57	Thermal Decomposition of Hydrogen Peroxide (H2O2) in the Lab-scale for Space Applications	10	confirmed	Ms. Hajar Jabri	Chouaib Doukkali University	Morocco
58	design and cfd analysis of a hypersonic inlet and hydrogen combustion for a scramjet engine at mach 7	10	confirmed	Mr. Marco Cárdenas Aldaco	Administración de Sistemas Aeroespaciales Mexicanos - ASAEM	Mexico
59	thermal responsive propellant formulations for variable thrust control for winged space rocket	10	confirmed	Ms. Diana ALjbour	Space Generation Advisory Council (SGAC)	Jordan
60	MULTIDISCIPLINARY DESIGN OPTIMIZATION OF A SUPERSONIC WIND TUNNEL	10	confirmed	Dr. Antonella Ingenito	Sapienza University of Rome	Italy
61	Modelling of Hypersonic Pre-cooled Engine	10	confirmed	Mr. Vincenzo Castrignano	Università degli Studi di Napoli “Federico II”	Italy
62	hybrid propulsion system for spaceplanes: optimizing efficiency and performance	10	confirmed	Ms. Diana ALjbour	Space Generation Advisory Council (SGAC)	Jordan
63	Enhancing the Performance of Solid-Fuel Dual Scramjet through Innovative Design and Numerical Investigation	10		Ms. Laurine Hillion	Hybrid Propulsion for Space (HyPr Space)	France
64	Development of an Air-Breathing Electrostatic Thruster	10	confirmed	Mr. Omar ElSherbiny	Technical University of Munich	Germany
65	Plume characterization of a magnetic nozzle thruster by two-dimensional laser-induced fluorescence measurements	10	confirmed	Mr. Colum Walter	Universität der Bundeswehr München	Germany
67	Swirl injectors in hybrid rocket engine - design, parameters validation and applicability in a N2O/ABS hybrid rocket booster	10	confirmed	Mr. Marek Dzik	Warsaw University of Technology (WUT)	Poland
68	Conceptual development of modular ion thrusters for its use on nuclear electric propulsion systems.	10	confirmed	Mr. Oscar Mejia	Instituto Politécnico Nacional	Mexico
69	Rapid iterative design of a cost-effective e-pump for a liquid-fuelled reusable sounding rocket: a comprehensive approach to in-house design, manufacturing and testing.	10	confirmed	Mr. Alessandro Battegazzore	Delft Aerospace Rocket Engineering (DARE)	The Netherlands
70	SRAD Capacitive Level Sensor for Propellant Measurement of a Liquid Rocket	10	confirmed	Ms. Sheikha Al-Nasser	Propulse NTNU	Norway
71	Propulsion systems for Mars mission: alternatives and opportunities	10	confirmed	Dr. Marcos Fernandez-Tous	Department of Space Studies, University of North Dakota	United States
72	Life evaluation of liquid rocket engine regenerative cooling system: a comparison of hardening models	10	confirmed	Mr. matteo crachi	Politecnico di Torino	Italy
73	Investigation of Hypergolic Ignition of Green Kerosene-based Fuels with HTP	10	confirmed	Mr. Luca Caffiero	Politecnico di Milano	Italy
74	Full rotordynamics analysis of a turbopump rotor system	10	confirmed	Mr. Shayman-Reza Labadlia	Concordia University	Canada
75	Feasibility Study and Preliminary Design of an Innovative Green Propulsion concept based on Self-Pressurized Propellants	10	withdrawn	Mr. Alberto Sarritzu	University of Pisa	Italy
76	Enhancing Reliability in European Rocket Engines: The GTD Approach to Engine Test Bench Control and Monitoring at DLR Lampoldshausen	10	confirmed	Mr. Alejandro Guerra Mentruit	GTD	Spain
77	Durable oxide catalysts free of noble metals for Hydrogen peroxide thrusters	10	confirmed	Dr. Frederic Monteverde	CNR - ISSMC	Italy
78	Design of a Propellant Liquefaction and Storage System for Cryogenic Rocket Engine Propellants	10	confirmed	Dr. Alejandro Hernandez Gonzalez	Technische Universität München	Mexico
79	Cellulose-Based Gel Propellants for Advanced Space Applications: Synthesis, Characterization, and Performance Optimization	10	confirmed	Mr. Shreyansh Dubey	University of Petroleum and Energy Studies	India
80	A novel technique for salvaging a double walled thrust chamber nozzle	10	confirmed	Mr. Vivek S	Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)	India
81	Experimental Investigation on Pressure and Flow Regulation of Variable Area Cavitation Venturi in Pump-feed System	10	confirmed	Mr. Haoran Shi	School of Astronautics, Beihang University	China
82	Geometric characteristics optimization and integrated design analysis of Air-Breathing Electric Propulsion inlet	10	confirmed	Mr. Chenxi Xia	Beihang University (BUAA)	China
83	Experimental study and modelling of rise time in HAN based monopropellant thruster and its effect on chamber pressure oscillations	10	confirmed	Mr. Vishal Singh	Bellatrix Aerospace Private Limited	India
84	optical visualization of fuel injector with flat spray nozzle of throttling test during H2O2/kerosene bipropellant thruster.	10	confirmed	Mr. Vincent Ugolini	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
85	Closed-Loop Thrust Throttling Capabilities on Kero-Lox Liquid Rocket Engine	10	confirmed	Mr. Connor Zook	University of Southern California	United States
86	combustion characteristics of hydroxylammonium nitrate-based electrically controlled gel propellant	10	confirmed	Ms. CHANSONG KIM	Chosun University	Korea, Republic of
87	Regenerative and Liquid Film Cooling: Development of a Unified Thermal Control Strategy in Liquid Rocket Engines	10	confirmed	Mr. Federico Giambelli	Politecnico di Milano	Italy
88	Potential of Radial Turbines in Liquid Rocket Engines: a comparative study with classical axial Turbines	10	confirmed	Mr. Antonio Lioi		Italy
89	Dynamic combustion characteristics of the GOX/GCH4 pintle model combustor with different sizes of the mantle recirculation zone	10	confirmed	Mr. Dae Hwan Kim	Seoul National University	Korea, Republic of
90	Formulation, Rheology and Atomization of Gelled Hydroxylammonium Nitrate (HAN) “Green” Monopropellant Ternary Mixtures	10	confirmed	Mr. Timothy Velthuysen	University of KwaZulu-Natal (UKZN)	South Africa
91	Conceptual Design and Fabrication of 400 N-class Multi-hole Pintle GCH4/LOx Injector	10	confirmed	Mr. YOONHO SONG	Korea Aerospace Research Institute (KARI)	Korea, Republic of
92	Characterization and Testing of a 1N Green Monopropellant Micro-Thruster Produced Using Additive Manufacturing Technique	10		Dr. Djamal DARFILAL	Khalifa University of Science and Technology (KUST)	United Arab Emirates
93	Design, Development and Testing of a Five-Thruster Multidirectional Resistojet Propulsion System for cubsats applications	10		Dr. Djamal DARFILAL	Khalifa University of Science and Technology (KUST)	United Arab Emirates
94	Decomposition characteristics of hydrogen peroxide by external heat source in small scale monopropellant thrusters	10	confirmed	Mr. Adil Mahroof	United Arab Emirates University (UAEU)	United Arab Emirates
95	Catalyst-Driven Green Propellant Development for Hypergolic Systems	10	confirmed	Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
96	Characterization of Engine Cooldown for a Centrifugal Nuclear Thermal Rocket	10	confirmed	Mr. Mitchell Schroll	Propulsion Research Center, University of Alabama in Huntsville	United States
97	Thermal Considerations of Vaporization in Liquid Core Nuclear Thermal Rockets	10		Mr. Dakota Santana	University of Alabama in Huntsville	United States
98	Optimal trajectories for a spacecraft propelled by an E-sail with piecewise inertially-fixed attitude	10	confirmed	Dr. Lorenzo Niccolai	University of Pisa	Italy
99	A Levitated Displacement Interferometer Thrust Stand for Characterization of Propellantless Propulsion Concepts	10	confirmed	Dr. Ryan Weed		United States
100	innovations in nuclear and propellantless propulsion technologies	10	confirmed	Mr. Ali Jafarov	National Aviation Academy - Azerbaijan	Azerbaijan
101	molten salt reactor concepts for advanced nuclear electric propulsion (NEP) systems	10	confirmed	Prof. Pablo Rubiolo	CNRS	France
102	Review of Nuclear Electric Propulsion for Interplanetary Missions	10	confirmed	Mrs. Monica Salunkhe	University of Alabama in Huntsville	United States
103	Preliminary Low Thrust Direct Trajectory Design Using Nuclear Electric Propulsion System for Rendezvous Missions to Jupiter	10	confirmed	Mrs. Monica Salunkhe	University of Alabama in Huntsville	United States
104	Hydrolytic space propulsion: \\ a new opportunity for cubesat missions	10	confirmed	Prof. Filippo Maggi	Politecnico di Milano	Italy
105	Optimising Solar Sail Design for Interplanetary Missions: Balancing Mass, Area, and Trajectory	10	confirmed	Ms. SUHANA ARSH	R V College of Engineering, Bengaluru	India
106	THE GREEN FUTURE OF PROPULSION FOR SATELLITES & SPACE VEHICLES	10		Mr. Sergii Kamenskyi		Spain
107	The features of LVexisting pressurization systems of propellant tanks and prospects of their development	10	confirmed	Mr. Vadym Khomiak	Yuzhnoye State Design Office	Ukraine
108	Preliminary Test of Kerosene Nitrous Oxide Catalytic Decomposition Bipropellant Thruster	10	withdrawn	Mr. Seungho Lee	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
109	Preliminary study on an electrolysis-based satellite micropropulsor for a 12U cubesat	10	confirmed	Mr. Nicolás de Jong		Spain
110	Perspectives on Colloidal Polymeric Nitrogen Monopropellant Engines	10	confirmed	Mr. Davide Negretti		Italy
111	Optimization study of an upper stage based on an e-pump-fed engine	10	confirmed	Mr. Andrea Montaini	Politecnico di Milano	Italy
112	Optimization of thrust control strategy for electric pump-fed rocket engines	10	confirmed	Mr. Tianwen Li	School of Astronautics, Beihang University	China
113	Modeling, Simulation and Testing of an Innovative Engineering Model Water-based Propulsion Unit for Cubesats	10	confirmed	Mr. Francesco Marino	Capsule Corporation	Italy
114	Investigation on an efficient thermal pressurization method for propellant tanks of cryogenic upper stage	10	confirmed	Dr. Wenbing Jiang	Aerospace System Engineering Shanghai, China	China
115	Integrated propulsion control technology for Future Space Transportation Systems	10		Mr. Wang Tempo	China Aerospace Science and Technology Corporation (CASC)	China
116	In house development of novel, thermally stable ceramic composite catalyst for HAN Decomposition	10		Dr. Rekha M	Bellatrix Aerospace Private Limited.	India
117	fault simulation study of full-flow staged combustion cycle engine start-up process	10	confirmed	Mr. Lihao Zheng	School of Astronautics, Beihang University	China
118	Dynamics modeling and simulation analysis of reusable high-pressure supplementary combustion liquid oxygen kerosene variable thrust rocket engine: Part I - Single point operating condition analysis	10	confirmed	Mr. liu yuwei	National University of Defense Technology	China
119	Digital Twin Performance Analysis of a 500 pound-thrust, Throttling, Hypergolic Rocket Engine	10	confirmed	Mr. Clayton Birchenough		United States
120	Development of Atlas: A Liquid Rocket Engine Cryogenic Feed System	10	confirmed	Mr. Rohin Pathak	University of Southern California	United States
121	Design, Modeling and Simulations of a High Pressure Cryogenic System for a Space Propulsion Test Facility	10	confirmed	Mr. Tommaso Zagatti	Telematic Solutions Srl	Italy
122	Design and evaluation of a small scale liquid rocket engine using pineapple’s waste	10	confirmed	Mr. Alvaro Bermudez	University of Costa Rica	Costa Rica
123	Design and Analysis of a LH2-LOX Rotating Detonation Propulsion System	10	confirmed	Mr. Sihan Di	School of Astronautics, Beihang University	China
124	BREAKING BARRIERS WITH BIOFUELS: THE FUTURE OF ROCKET PROPULSION	10	confirmed	Ms. Vanmitha Athimoolam		Malaysia
125	Establishing a Foundation for Rocketry Advancement in Mexico: Development of a Hybrid Rocket Engine.	10	confirmed	Mr. Luis Fernando Gomez Monroy		Mexico
126	Hybrid Rocket Simulation Using CEQUEL for Thermochemistry Calculations	10		Ms. Paige Berg	University of Alabama in Huntsville	United States
129	Fundamental Investigation of Micro-Explosive in Aluminum-Lithium Alloy Particle at the Atomic Scale	10	confirmed	Mr. Yintao Zhou	Beijing Institute of Technology (BIT)	China
131	Performance analysis of Paraffin, Beeswax and Magnesium as a fuel for Hybrid Propulsion	10	confirmed	Mr. Harish Vernekar	University of Arizona	United States
132	Experimental investigation of combustion instability inside lab-scale hybrid rocket motor with swirl injector	10	confirmed	Dr. ANWER HASHISH	Military Technical College	Egypt
133	Conceptual design of a 1 kN hybrid rocket engine manufactured with additive technology	10	confirmed	Dr. Olexiy Shynkarenko	University of Brasilia	Brazil
134	Numerical modelling approach for the development of an orbital-scale hybrid propulsion engine	10	confirmed	Mr. Raphaël Aubry	Hybrid Propulsion for Space (HyPr Space)	France
135	advancing thermal management: heat flow analysis and hotspot identification in solid rocket motors	10		Mr. Kushal Chatterjee	R V College of Engineering, Bengaluru	India
136	Thrust Prediction of Hybrid Rocket Motor Based on Physical Feature Embedding and Residual Learning	10	confirmed	Dr. Weile Xu	Beihang University (BUAA)	China
137	Statistical Thermodynamics Approaches for Advancing Chemical Propulsion Systems	10		Mr. Ishaan Dutta	R V College of Engineering, Bengaluru	India
138	Research on charge integrity simulation of brush charge asymmetric ignition of small solid thruster	10	confirmed	Mr. Yuqing Tang	Nanjing University of Science and Technology	China
139	numerical combustion model and efficiency study of electrically ignited solid propellants for micro to macro propulsion systems	10	confirmed	Mr. Abishek Shrestha		Australia
140	NUMERICAL AND EXPERIMENTAL ANALYSIS OF NEW PROPELLANT FORMULATIONS FOR HYBRID ROCKETS	10	confirmed	Mr. Abdul Rahman	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
141	machine learning-based study on thrust prediction of hydrogen peroxide and polyethylene hybrid rocket motor	10	withdrawn	Mrs. Keren Lin	Beihang University (BUAA)	China
142	H2O2/HDPE Hybrid Rocket: Experimental and Theoretical Investigation	10	confirmed	Mr. Abdul Rahman	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
143	Development of Carbon Fiber Rocket Motors with Insulative Laminate Structure	10		Mr. Ishaan Dutta	R V College of Engineering, Bengaluru	India
144	AI and Classical Approaches to Estimating Solid Fuel Regression Rate in Hybrid Rocket Engines	10	confirmed	Mr. Gabriel Metre Resende	University of Brasilia	Brazil

session IP

Order

Time

Paper title

Mode

Presentation status

Speaker

Affiliation

Country