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: 2026-10-07
Time: 10:15
Room: Hall 7

IPC members

Co-Chair: Dr. Yuji Saito, Tohoku University, Japan;
Co-Chair: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;
Rapporteur: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;
Rapporteur: Dr. Jouke Hijlkema, ONERA, France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	KEYNOTE: Future of Micro Launchers using Hybrid Rocket Propulsion	20	confirmed	Dr. Ozan Kara	Technology Innovation Institute (TII)	United Arab Emirates
2	10:35	High-Precision Direct Measurement of Residual Thrust in Hybrid Thrusters	10	confirmed	Mr. Hinata Kariya	Tohoku University	Japan
3	10:45	Design and Experimental Validation of a Low Environmental Impact Solid Rocket Motor Casing in Peru Using a Lignocellulosic Biocomposite and PALF Reinforcement	10	confirmed	Mr. Italo Paolo Ambrosio Huanay	Universidad Nacional de Ingeniería (Lima, Perù)	Peru
4	10:55	research on composite thermal insulation materials for amateur and student rocket motors	10	confirmed	Mr. Dominik Jaszczyk	Wroclaw University of Science and Technology	Poland
5	11:05	Comparative Collection and Environmental Characterization of Hybrid and Solid Rocket Engine Fire Plumes	10	confirmed	Mr. Huzeyfe Ali Karakuşoğlu	Mechanical and Chemical Industries Corporation	Türkiye
6	11:15	Modeling N2O Discharge Characteristics: An Approach with Experimental Validation	10	confirmed	Ms. Selin Çetin	Deltav Space Technologies,Inc.	Türkiye
7	11:25	State-Transition Thermofluid Modeling and Experimental Validation of Self-Pressurizing Nitrous Oxide Propellant Feed Systems	10	confirmed	Mr. Kotaka Nagayama	Tohoku University	Japan
8	11:35	Nitrous Oxide Decomposition Under Pyrogenic Initiation: Experimental Peak Pressures vs. Analytical Predictions	10	confirmed	Mr. Egemen Aycan	Deltav Space Technologies,Inc.	Türkiye
9	11:45	Investigation of the Effects of Injector Design on Performance in Hybrid Fuel Rocket Motors	10	confirmed	Ms. Fatıme Sevgili	Gebze Technical University	Türkiye
10	11:55	Hydrogen Peroxide Ignition System for an In-Space Hybrid Propulsion Mission	10	confirmed	Mrs. İlknur Akkaya Arslan	Deltav Space Technologies,Inc.	Türkiye
11	12:05	Scaling Effects in Tens-of-Newtons-Class H2O2 Hybrid Rocket Engines through Experimental Investigation	10	confirmed	Mr. Riccardo Guida	Scuola Superiore Meridionale	Italy
12	12:15	Comparison of different methods of paraffin wax fuel grain casting	10	confirmed	Mr. Krzysztof Kondracki	Gdansk University of Technology	Poland

session 4

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