session 3

Title: Solid and Hybrid Propulsion (1)
type: oral
Description: The session Solid and Hybrid Propulsion (1) is dedicated to Solid and Hybrid Rocket motors, with particular emphasis on full systems. 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: 2026-10-06
Time: 10:15
Room: E6

IPC members

Co-Chair: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Co-Chair: Dr. Jouke Hijlkema, ONERA, France;
Rapporteur: Dr. Djamal DARFILAL, Khalifa University of Science and Technology (KUST), United Arab Emirates;
Rapporteur: Dr. Yuji Saito, Tohoku University, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Analytical and Experimental Investigation of the Effects of Fuel Additives on the Regression Correction Coefficients of Hybrid Rockets	10	confirmed	Mr. Emir Han Bulut	Istanbul Technical University	Türkiye
2	10:25	Hardware-in-the-Loop Validation of a Hybrid Rocket Telemetry System	10	confirmed	Ms. Heba Youssef	Technology Innovation Institute (TII)	United Arab Emirates
3	10:35	Hybrid Sounding Rocket Avionics and Telemetry System	10	confirmed	Dr. Ozan Kara	Technology Innovation Institute (TII)	United Arab Emirates
4	10:45	Bench-to-Flight Validation of Thrust Curve and Time-Varying Stability for a Small-Scale Solid-Propellant Rocket	10	confirmed	Mr. Abraham H. Gutierrez	Intinauta Research Center	Peru
5	10:55	Thermo-Structural and Conjugate Heat Transfer (CHT) Analysis of the Combustion Chamber and Nozzle of a Small-Scale Hybrid Rocket Motor	10	confirmed	Ms. Sara AYDOGAN	Samsun University	Türkiye
6	11:05	Design and Optimization of a H2O2 Hybrid Rocket Cluster for Upper-Stage Applications	10	confirmed	Mr. Daniele Iannarelli	Scuola di Ingegneria Aerospaziale "La Sapienza"	Italy
7	11:15	Design of a 100 N Paraffin/N2O Hybrid Rocket Engine and Real-Time Regression Rate Characterization with Longitudinal Wire Array Sensors	10	confirmed	Mr. Levent Berke Duyuk	Koc University	Türkiye
8	11:25	case study - static test of the paraffin/n2o fueled high power hybrid rocket engine	10	confirmed	Mr. Dominik Jaszczyk	Wroclaw University of Science and Technology	Poland
9	11:35	Hydrogen Peroxide-Based Hypergolic Liquid Bipropellant Thruster and Hypergolic Hybrid Rocket Experimental Investigation	10	confirmed	Mr. Ahmet Nihat Karci	University of Southampton	United Kingdom
10	11:45	System Level Hybrid Rocket Engine Modelling Validated Against Ground Tests and Flight Data	10	confirmed	Mr. Guillaume Knight	RMIT University	Australia

session 3

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