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: 2025-09-29
Time: 15:30
Room: Room C3.6

IPC members

Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;
Co-Chair: Dr. Justin Hardi, German Aerospace Center (DLR), Germany;
Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;
Rapporteur: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;

papers
Order	Time	Paper title	Mode	Presentation status	Speaker	Affiliation	Country
1	15:30	Development Strategy and Early Test Results of a 250 N Green Propellant Thruster	10	confirmed	Dr. Carmine Carmicino	Technology Innovation Institute (TII)	United Arab Emirates
2	15:40	Development Status of a 420 N Liquid Bipropellant Engine Using 98% HTP and TMPDA	10	confirmed	Dr. Pawel Surmacz	Łukasiewicz Research Network – Institute of Aviation (ILOT)	Poland
3	15:50	Designing for Reuse: Technical Challenges and Performance Trade-offs for Reusable Liquid Propellant Rocket Engines	10	confirmed	Ms. Lilly Etzenbach	Massachusetts Institute of Technology (MIT)	United States
4	16:00	The Emirates Mission To The Asteroid Belt: Chemical Propulsion System Architecture And Usage In EMA	10	confirmed	Ms. Nourah Alyammahi	UAE Space Agency	United Arab Emirates
5		Transient conjugate heat and mass transfer analysis of cryogenic propellant tank during ground servicing operations for a manned space mission	10	withdrawn	Mr. Vishnu Viswanath	Liquid Propulsion System centre	India
6	16:10	Tank Head Start Approach for a 80 ton-Class Gas-Generator Cycle Methane/LOX Rocket Engine	10	confirmed	Mr. Hanmo Shen	LandSpace Technology Corporation Ltd.	China
7	16:20	integrated development of an expander cycle liquid rocket engine and upper stage propulsion system	10	confirmed	Dr. Cheulwoong Kim	Korea Aerospace Research Institute (KARI)	Korea, Republic of
8		Investigation of High Frequency Combustion Instability During Cryogenic Rocket Engine Start Transient	10	withdrawn	Mr. M VISWAJITH	Liquid Propulsion System centre	India
9	16:30	H3 launch vehicle launch result and LE-9 Type2 Engine development status	10	confirmed	Mr. Shogo Ozaki	JAXA	Japan
10	16:40	Recent improvements in the LUMEN test bed for oxygen-methane rocket engine technologies	10	confirmed	Dr. Justin Hardi	German Aerospace Center (DLR)	Germany
11		Progress in the Development of South Africa’s SAFFIRE Liquid Rocket Engine	10	withdrawn	Prof. Jean Pitot	University of KwaZulu-Natal (UKZN)	South Africa
12		Development of Additively Manufactured Electric Turbompump Methalox Reusable Engine	10	withdrawn	Dr. Tadayoshi Shoyama	Innovative Space Carrier Inc.	Japan

session 1

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