session 1

Title: Liquid Propulsion (1)
type: oral
Description: The session Liquid Propulsion (1) is dedicated to Liquid Rocket Engines (mono-propellant or bi-propellant), with particular emphasis on full engine systems. 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: 2026-10-05
Time: 16:30
Room: E6

IPC members

Co-Chair: Mr. Giuseppe Fiore, CNES, France;
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: Dr. Justin Hardi, German Aerospace Center (DLR), Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	16:30	Deep Throttling Implementation of the TQ-12A Methalox Engine for ZQ-3 Launch Vehicle's Booster Recovery	10	confirmed	Mr. Hua Wei	LandSpace Technology Corporation Ltd.	China
2	16:40	Final Development Results of LE-9 Type2 Engine	10	confirmed	Mr. Shogo Ozaki	JAXA	Japan
3	16:50	A Practical Unsupervised LSTM-Based FDHM Framework for LOX/Methane Rocket Engines Toward ZQ-3 Reusable Missions	10	confirmed	Dr. Jianing Liu	LandSpace Technology Corporation Ltd.	China
6	17:00	numerical dispersion analysis of startup transients in a staged combustion cycle engine	10	confirmed	Dr. Insang Moon	Korea Aerospace Research Institute (KARI)	Republic of Korea
7	17:10	Upper stage rocket engine development in Brazil using high test peroxide	10	confirmed	Mr. Nicolas Miquelin	Bizu Space	Brazil
8	17:20	Development Status of Japan’s Next-Generation Upper-Stage Engine: Preliminary Design and Breadboard Model Test Results	10	confirmed	Mr. Hideo Sunakawa	Japan Aerospace Exploration Agency (JAXA)	Japan
9	17:30	Development of the Nyx Earth Propulsion System	10	confirmed	Mr. Markus Jaeger	The Exploration Company GmbH	Germany
10	17:40	In-orbit Demonstration of the Vyom-2u Propulsion System Enabled by MS289: A Safe, Reliable, and High-Performance Green Monopropellant for Small Satellites	10	confirmed	Mr. Tushar Jadhav		India
11	17:50	Multiscale High-Test Peroxide (HTP) Based Propulsion Systems for Small Satellites: Integrated Development and Experimental Validation	10	confirmed	Ms. Fatima AlHammadi	Khalifa University of Science and Technology (KUST)	United Arab Emirates
12	18:00	Experimental Investigation of Operational Parameters Governing the Steady-State Performance of a Hydrogen Peroxide Monopropellant Thruster	10	confirmed	Dr. Ugur Kokal	Deltav Space Technologies,Inc.	Türkiye

session 1

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