session 4

Title: Solid and Hybrid Propulsion (2)
type: oral
Description: The session Solid and Hybrid Propulsion (2) is dedicated to Solid and Hybrid Rocket motors, with particular emphasis on sub-systems and specific components (including propellants). The session welcomes manuscripts on all research and development areas: design, testing (including diagnostics and test facilities), analysis and calculations, modelling, applications, science and fundamentals.
Date: 2025-10-01
Time: 10:15
Room: Room C4.11

IPC members

Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Dr. Stefano Mungiguerra, Università degli Studi di Napoli “Federico II”, Italy;
Rapporteur: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;

papers
Order	Time	Paper title	Mode	Speaker	Affiliation	Country
1	10:15	An Overview of Solid Propulsion Application for Space Launchers	20	Mr. Didier Boury	ArianeGroup SAS	France
2	10:35	Effect of Port Geometries on Additively Manufactured Hybrid Rocket Fuel Grains	13	Mr. Andreas Bonitz	RMIT University (Royal Melbourne Institute of Technology)	Australia
3	10:48	Enhancing Combustion Efficiency through Injector Design in Hybrid Rocket Engines	13	Mr. Mauricio Vicencio Molina	Space Generation Advisory Council (SGAC)	Mexico
4	11:01	incorporation of powders in 3d printed cellular structures for hybrid rocket propulsion	13	Mr. Federico Giambelli	Politecnico di Milano	Italy
5	11:14	Microwave Discharge Ignition of Metalized Fuel for Hybrid Rockets	13	Dr. Keita Nishii	Tokyo Metropolitan University	Japan
6	11:27	Numerical and Experimental Demonstration of Residual Thrust Phenomenon in Hybrid Rocket Thrusters under Vacuum Environment	13	Mr. Hinata Kariya	Tohoku University	Japan
7	11:40	Numerical Study of Sloshing Mitigation for Mexican Hybrid Rocket Using Passive Baffles Coupled with a Spring System	13	Mrs. Gema Esmeralda Martinez Gonzalez	Instituto Politécnico Nacional	Mexico
8	11:53	Performance improvement by vortex combustion for a Magnesium-Loaded HTPB/N2O Hybrid Rocket for Small Spacecraft	13	Mr. Tomoya Kanda	Tokyo Metropolitan University	Japan
9	12:06	Performance Testing of a 7 kN Hybrid Rocket Motor under Varying Propellant Conditions	13	Mr. Bernard Genevieve	University of KwaZulu-Natal (UKZN)	South Africa
10	12:19	Scalable Anomaly Detection in High-Speed Combustion Imaging	13	Dr. Hakan Akdag	German Aerospace Center (DLR)	Germany
11	12:32	TNT Synthesis Byproducts in Solid Propellants	13	Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
1*	10:15	Study of potential use of Magnesium/Teflon/Viton Pyrotechnic Composition as an ignitor for solid rocket motors through computational simulations using molecular dynamics (MD).	13	Mr. Vinicius Rossetto	Instituto Tecnológico de Aeronáutica (ITA)	Brazil
2*	10:35	Enhancement of the main sub-systems in Student Researched and Developed (SRAD) Hybrid Rocket Engine (HRE)	13	Ms. Małgorzata Majda	Gdansk University of Technology	Poland
3*	10:48	Designing Advanced Solid and Hybrid Propulsion Systems for Rapid Space Missions: Propellant Enhancements and Thrust Control Innovations	13	Mr. Yuvraj Pagare	University of Hertfordshire	United Kingdom

session 4

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