session 2

Title: Liquid Propulsion (2)
Description: The session Liquid Propulsion (2) is dedicated to Liquid Rocket Engines (mono-propellant or bi-propellant), 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: Blue Hall 1

IPC members

Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Dr. Annafederica Urbano, ISAE - Institut Supérieur de l'Aéronautique et de l'Espace, France;
Rapporteur: Dr. Christian Bach, Technische Universität Dresden (DTU), Germany;
Rapporteur: Mr. Ulrich Gotzig, ArianeGroup, Germany;
Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	H-IMP: a new propulsion test facility for LOX/LCH4 Liquid Rocket Engines with advanced optics/laser diagnostics	12	confirmed	Mr. Federico De Filippis	CIRA Italian Aerospace Research Centre	Italy
2	10:27	Subsystem and system test results of the 4-ton class rocket engine for rocket startups	12	confirmed	Mr. Ryoma Yamashiro	Japan Aerospace Exploration Agency (JAXA)	Japan
3	10:39	Enhancing Propulsion Efficiency in the Development of Italy's First Private Launcher: The Role of Coaxial Swirl Injector Design	12	confirmed	Mr. Davide Cozzi		Italy
4	10:51	Propulsion System Technology Trades for Starlab Space Station for Unleashing the next Generation of Space Destinations	12	confirmed	Mr. Markus Jaeger	Airbus Defence & Space, Space Systems	Germany
5	11:03	comparison of combustion characteristics in various spray nozzle injector geometries for low-toxic hypergolic thruster	12	confirmed	Mr. Hyeonjun Im	Korea Advanced Institute of Science and Technology (KAIST)	Korea, Republic of
6	11:15	the development of 3D-printed metal on support based catalysts for the decomposition of h2o2 green mono-propellant in monolithic catalytic beds	12	confirmed	Mrs. Shaima Albedwawi	Technology Innovation Institute (TII)	United Arab Emirates
7	11:27	pressure measurement over truncated linear aerospike nozzle in differential throttling configuration	12	confirmed	Mr. JEHANGIR HASSAN	Politecnico di Torino	Italy
8	11:39	Flight Qualification Logic of Additive Manufactured Critical Part in the Ariane 6 Vinci Engine	12	confirmed	Ms. Li Forsberg	GKN Aerospace Engine Systems	Sweden
9	11:51	Studies on the Additive Fabrication Concept for Future Launcher Engine Nozzle Extension Design and Manufacturing	12	confirmed	Dr. Christo Dordlofva	GKN Aerospace Engine Systems	Sweden
10	12:03	AUTOMATION OF ENGINE MEDIUM SUBSTITUTION FOR CRYOGENIC ENGINES TESTING IN HIGH ALTITUTE TEST BAY	12	confirmed	Mr. VINOD P	Indian Space Research Organization (ISRO)	India
11	12:15	CFD Performance Prediction of Cryogenic High-Speed Bearings for Reusable Pump-fed Liquid Rocket Engines	12	confirmed	Mr. Kento Sakai	Waseda University	Japan
12	12:27	Research of Reusable LOX/RP-1 Propulsion System Firing Test	12	confirmed	Dr. Sheng Zhao	China Academy of Launch Vehicle Technology (CALT)	China

session 2

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