session 2
- Title
Liquid Propulsion (2)
- type
oral
- 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, with a significant technical content: design, testing (including diagnostics and test facilities), analysis and calculations, modelling, applications, science and fundamentals.
- Date
2025-10-01
- Time
- Room
- IPC members
Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;
Co-Chair: Dr. Christian Bach, Technische Universität Dresden (DTU), Germany;
Rapporteur: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;
Rapporteur: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;
Order | Time | Paper title | Mode | Presentation status | Speaker | Affiliation | Country |
|---|---|---|---|---|---|---|---|
1 | 10:15 | 12 | Dr. Elizabeth Jens | Jet Propulsion Laboratory - California Institute of Technology | United States | ||
2 | 10:27 | Development and Test Results of an additively printed 250N Class Monopropellant Thruster | 12 | Mr. Ulrich Gotzig | ArianeGroup | Germany | |
3 | 10:39 | Effect of surface roughness on cooling channel fouling in methane fueled rocket engines | 12 | Mr. Jules Heldens | Royal Institute of Technology (KTH) | Sweden | |
4 | 10:51 | 12 | Mrs. Chungman Kim | Perigee Aerospace Inc. | Korea, Republic of | ||
5 | 11:03 | 12 | Mr. Jordan Silver | University of KwaZulu-Natal (UKZN) | South Africa | ||
6 | 11:15 | 12 | Mr. Avinash Chandra | Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC) | India | ||
7 | 11:27 | Numerical Simulation of the DLR LUMEN Thrust Chamber: Impact of Small Injection Asymmetry | 12 | confirmed | Ms. Clara Morris | DLR (German Aerospace Center) | Germany |
8 | 11:39 | 12 | Dr. Taras Koturbash | Royal Institute of Technology (KTH) | Sweden | ||
9 | 11:51 | High-Speed Multispectral Visualization of Bubbly Spray Combustion in Hypergolic Rocket Propellants | 12 | Prof.Dr. Fabio Antonio da Silva Mota | Universidade Federal do ABC - UFABC | Brazil | |
10 | 12:03 | Experimental Investigation of a 10N class Vortex-Cooled Methane/Oxygen Bipropellant Thruster | 12 | confirmed | Mr. Mousa Aqailan | United Arab Emirates University (UAEU) | United Arab Emirates |
11 | 12:15 | 12 | Mr. Krzysztof Pietrzak | Łukasiewicz Research Network – Institute of Aviation (ILOT) | Poland | ||
12 | 12:27 | design, manufacturing and test of china's largest niobium alloy rocket nozzle | 12 | Mr. Hanmo Shen | LandSpace Technology Corporation Ltd. | China | |
1* | 10:15 | Experimental Validation of Numerical Methodologies in Liquid-Liquid Coaxial Swirl Injector Design | 12 | confirmed | Mr. Felix Liu | University of Southern California | United States |
2* | 10:27 | 12 | Dr. Stefano Mungiguerra | Università degli Studi di Napoli “Federico II” | Italy | ||
3* | 10:39 | From Concept to Results: Insights from the HYPROB Demonstrators Line on Methane-based Propulsion | 12 | Dr. Daniele Ricci | CIRA Italian Aerospace Research Center, Capua | Italy | |
4* | 10:51 | Reduced-order Models for Radiative Heat Loads Estimation in Liquid Rocket Engines | 12 | confirmed | Mr. Marco Fabiani | Sapienza University of Rome | Italy |
5* | 11:03 | Development of turbopumps for LE-9, first stage engine of H3 Launch Vehicle | 12 | Mr. Taiichi Motomura | Japan | ||
6* | 11:15 | 12 | confirmed | Mr. Abhishek Sharma | Indian Space Research Organization (ISRO) | India |