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: 10:15
Room: Room C3.6

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;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	10:15	Design, development and testing of a small thruster throttle valve to enable low-cost Mars landed missions	12	confirmed	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	confirmed	Mr. Ulrich Gotzig	ArianeGroup	Germany
3	10:39	Effect of surface roughness on cooling channel fouling in methane fueled rocket engines	12	confirmed	Mr. Jules Heldens	Royal Institute of Technology (KTH)	Sweden
4	10:51	Influence of Fuel Properties on the Ignition Behavior of NaBH4-Promoted Hypergolic Fuels with Hydrogen Peroxide	12	confirmed	Prof. Jongkwang Lee	Hanbat National University	Korea, Republic of
5	11:03	Development and performance testing of a “green” hydroxylammonium nitrate-based monopropellant in a lab-scale thruster	12	confirmed	Mr. Jordan Silver	University of KwaZulu-Natal (UKZN)	South Africa
6	11:15	EXPERIMENTAL STUDIES ON IGNITION PERFORMANCE OF TEA-TEB	12	confirmed	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	Pyrolysis stability of different methane fuel qualities for regenerative cooling rocket engines usage	12	confirmed	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	confirmed	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	Overview of valve developments at Łukasiewicz-ILOT	12	confirmed	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	confirmed	Mr. Hanmo Shen	LandSpace Technology Corporation Ltd.	China

session 2

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