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  • 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

    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

    Influence of Fuel Properties on the Ignition Behavior of NaBH4-Promoted Hypergolic Fuels with Hydrogen Peroxide

    12

    Mrs. Chungman Kim

    Perigee Aerospace Inc.

    Korea, Republic of

    5

    11:03

    Development and performance testing of a “green” hydroxylammonium nitrate-based monopropellant in a lab-scale thruster

    12

    Mr. Jordan Silver

    University of KwaZulu-Natal (UKZN)

    South Africa

    6

    11:15

    EXPERIMENTAL STUDIES ON IGNITION PERFORMANCE OF TEA-TEB

    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

    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

    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

    Mr. Mousa Aqailan

    United Arab Emirates University (UAEU)

    United Arab Emirates

    11

    12:15

    Overview of valve developments at Łukasiewicz-ILOT

    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

    Mr. Felix Liu

    University of Southern California

    United States

    2*

    10:27

    A Novel Versatile Test Bench for Liquid Bipropellant Rocket Testing and Numerical Combustion Simulations

    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

    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

    Critical Assessment of Open and Closed-end Swirl Injector Dynamics for LOx-Methane Rocket Engine Applications

    12

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India