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: 2025-09-30
Time: 10:15
Room: Room C3.6

IPC members

Co-Chair: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;
Co-Chair: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;
Rapporteur: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;
Rapporteur: Dr. Yuji Saito, Tohoku University, Japan;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Red Kite Solid Rocket Motor	14		Mr. Markus Kuhn	Bayern Chemie	Germany
2	10:29	Progress and Prospects of Key Technologies in Structural Dynamics of Solid Rocket Motors	14		Mr. Hao LE	Shanghai Space Propulsion Technology Research Institute	China
3	10:43	Pioneering Indonesia’s First Academic Solid Rocket: A Sustainable and Low-Cost Propellant for Future Space Endeavors	14	confirmed	Mr. Afiq Sulistya	PSN	Indonesia
4	10:57	Nitrous Oxide/Polyethylene Based Sounding Rocket Development in UAE	14	confirmed	Dr. Ozan Kara	Technology Innovation Institute (TII)	United Arab Emirates
5	11:11	Static fire test of a piston-fed hybrid autophage engine	14		Mr. Vincenzo Mazzella	Alpha Impulsion	France
6	11:25	A Quest to Indigenous Launch Capability via Hybrid Rocket Propulsion – Lessons Learned from Development of Pescadore Engine	14	confirmed	Mr. Tzu Yu Lin	Taiwan Space Agency (TASA)	Taipei
7	11:39	Flight Test Data from the Phoenix-1D and -1E Hybrid Rockets	14		Dr. Sarisha Harrylal	University of KwaZulu-Natal (UKZN)	South Africa
8	11:53	design and testing of a vortex flow pancake hybrid rocket engine with a green, self-storable liquid oxidizer	13		Mr. Valerio Santolini	Politecnico di Milano	Italy
9	12:06	RAVEN: Insights from the first year testing campaign of a hybrid propulsion system	13		Mrs. Moa Kihlbaum	Luleå University of Technology	Sweden
10	12:19	Design methodology for hybrid rocket engines in Students’ Space Association	13		Mr. Bartosz Hyży	Warsaw University of Technology (WUT)	Poland
11	12:32	Design and Experimental Testing of a Lab-Scale GOX-Paraffin-Based Hybrid Rocket Engine	13	confirmed	Mr. Arbind Yadav	Mach24 Orbitals	Nepal
12*	12:45	Design and Testing of a Hybrid Rocket Motor using Paraffin based Solid Fuel Blended with Bio additives for Performance Enhancement	13	confirmed	Mr. Sunil Bista	Mach24 Orbitals	Nepal
13*	12:45	Time variant nozzle flow efficiency factor for accurate estimation of solid rocket motor thrust	13		Mr. KIRAN PINUMALLA	Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA	India
14*	12:45	Design and Analysis of a Variable Exit Area Nozzle for an Experimental Rocket	13		Mr. Renato Sebastian Gomez Olazo	Universidad Peruana de Ciencias Aplicadas	Peru

session 3

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