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: 2023-10-03
Time: 10:15
Room: BCC A8

IPC members

Co-Chair: Dr. Marco Di Clemente, Italian Space Agency (ASI), Italy;
Co-Chair: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;
Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Passivation of aluminium particle and its effects in solid propellants: a ReaxFF study	15	confirmed	Prof. Rene Gonçalves	Aeronautic Institute of Technology (ITA)	Brazil
2	10:30	A Conceptual Design of Permeable Nozzle for Altitude Compensation and Thrust Vectoring	15	confirmed	Mr. Ye Wang	CAS Space	China
3	10:45	Design, manufacturing and testing of 50 mm solid rocket motor using non-HTPB composite propellant for potential in-orbit applications.	15	confirmed	Dr. Florin Mingireanu	Romanian Space Agency (ROSA)	Romania
4	11:00	effect of aluminum content on nozzle erosion in a hybrid rocket motor	15	confirmed	Dr. Xianzhu Jiang	School of Astronautics, Beihang University	China
5	11:15	Hybrid autophage propulsion for space launch vehicles: a promising concept	15	confirmed	Mr. Martin Gros		France
6	11:30	Research on Analytical Inverse Kinematics Algorithm for Servo Mechanism of Swinging Nozzle	15	confirmed	Mrs. Guanchao Han	CAS Space	China
7	11:45	In-Situ Propellant Design for Moon and Mars Exploration Using Hybrid Rockets	15	confirmed	Ms. Hessa Almarzooqi	Technology Innovation Institute (TII)	United Arab Emirates
8	12:00	Surrogate Neural Network Model for Integrated Ascent Trajectory Optimization of Throttleable Hybrid Rockets	15	confirmed	Dr. Mario Tindaro Migliorino	Sapienza University of Rome	Italy
9	12:15	Design and testing of the combustion chamber of a H2O2/ABS student-developed hybrid rocket engine	15	confirmed	Mr. Giuseppe Oliva	ISAE - Institut Supérieur de l'Aéronautique et de l'Espace	France
10	12:30	Course and challenges of flight qualification test campaign of the students’ hybrid rocket engine.	15	confirmed	Mr. Marek Dzik	Warsaw University of Technology (WUT)	Poland

session 3

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