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: 2024-10-16
Time: 10:15
Room: Yellow Hall 2

IPC members

Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;
Co-Chair: Dr. Yuji Saito, Tohoku University, Japan;
Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;
Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	KEYNOTE: Hybrid Propulsion System Practices and Safety Considerations both for Launch Vehicles and In-Space Missions	18	confirmed	Dr. Ozan Kara	Technology Innovation Institute (TII)	United Arab Emirates
2	10:33	Nozzle Erosion Avoidance through Regenerative Cooling Systems in Hybrid Rocket Engines: Experimental Campaign and Numerical Modeling	11	confirmed	Mr. Riccardo Cambertoni	Politecnico di Torino	Italy
3	10:44	A new catalytic chamber concept for multi-phase injection of hydrogen peroxide	11	confirmed	Mrs. Nora Bierwagen	DLR (German Aerospace Center)	Germany
4	10:55	Experimental investigation of swirl oxidizer injector effect on 3D printed ABS hybrid rocket fuel regression rate	11	confirmed	Dr. ANWER HASHISH	Military Technical College	Egypt
5	11:06	performance testing of a 7 kn hybrid rocket motor under varying propellant conditions	11	withdrawn	Mr. Bernard Genevieve	University of KwaZulu-Natal (UKZN)	South Africa
6	11:17	The three-dimensional dynamic numerical simulation of star-shaped grains in hybrid rocket motors	11	confirmed	Mr. XIAOTING NIU	Beihang University (BUAA)	China
7	11:28	Scalable Hybrid Rocket Systems for Agile and Affordable In-space Propulsion	11	confirmed	Mr. Toku Sakai	Letara Ltd.	Japan
8	11:39	Green Solid Fuels with Enhanced Mechanical Properties: Use of Sustainable Waxes and Scale-Up Analysis of Armored Grains.	11	confirmed	Dr. Ch Paravan	Politecnico di Milano	Italy
9	11:50	Solid Fuel Analysis in Hybrid Rocket Engine Using Image Processing	11	confirmed	Mr. Felipe Fernandes	Universidade de Brasília	Brazil
10	12:01	Experimental Investigation of a 10 kN class Hydrogen Peroxide - Paraffin Wax Hybrid Motor Demonstrator	11	confirmed	Ms. Lucia Zeni	T4i	Italy
11	12:12	Improving alumina-cap characterisation in aluminized solid-rocket motors with computer vision	11	confirmed	Mr. Andrea Sportillo	Office National d’Etudes et de Recherches Aérospatiales (ONERA)	France
12	12:23	study on the effect of the gap between grain and case on the structural integrity of solid propellant	11	withdrawn	Dr. Qin-liu Cao	Shanghai Space Propulsion Technology Research Institute	China
13	12:34	Challanges in verification process of the Solid Rocket Motor for Direct Deorbitation Engineering Model	11	confirmed	Mr. Arthur Pazik	Łukasiewicz Research Network – Institute of Aviation (ILOT)	Poland

session 4

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