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  • session 2

    Title

    Liquid Propulsion (2)

    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: design, testing (including diagnostics and test facilities), analysis and calculations, modelling, applications, science and fundamentals.

    Date

    2024-10-16

    Time

    10:15

    Room

    Blue Hall 1

    IPC members
    • Co-Chair: Dr. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

    • Co-Chair: Dr. Annafederica Urbano, ISAE - Institut Supérieur de l'Aéronautique et de l'Espace, France;

    • Rapporteur: Dr. Christian Bach, Technische Universität Dresden (DTU), Germany;

    • Rapporteur: Mr. Ulrich Gotzig, ArianeGroup, Germany;

    • Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    H-IMP: a new propulsion test facility for LOX/LCH4 Liquid Rocket Engines with advanced optics/laser diagnostics

    12

    confirmed

    Mr. Federico De Filippis

    CIRA Italian Aerospace Research Centre

    Italy

    2

    10:27

    Subsystem and system test results of the 4-ton class rocket engine for rocket startups

    12

    confirmed

    Mr. Ryoma Yamashiro

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    3

    10:39

    Enhancing Propulsion Efficiency in the Development of Italy's First Private Launcher: The Role of Coaxial Swirl Injector Design

    12

    confirmed

    Mr. Davide Cozzi

    Italy

    4

    10:51

    Propulsion System Technology Trades for Starlab Space Station for Unleashing the next Generation of Space Destinations

    12

    confirmed

    Mr. Markus Jaeger

    Airbus Defence & Space, Space Systems

    Germany

    5

    11:03

    comparison of combustion characteristics in various spray nozzle injector geometries for low-toxic hypergolic thruster

    12

    confirmed

    Mr. Hyeonjun Im

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    6

    11:15

    the development of 3D-printed metal on support based catalysts for the decomposition of h2o2 green mono-propellant in monolithic catalytic beds

    12

    confirmed

    Mrs. Shaima Albedwawi

    Technology Innovation Institute (TII)

    United Arab Emirates

    7

    11:27

    pressure measurement over truncated linear aerospike nozzle in differential throttling configuration

    12

    confirmed

    Mr. JEHANGIR HASSAN

    Politecnico di Torino

    Italy

    8

    11:39

    Flight Qualification Logic of Additive Manufactured Critical Part in the Ariane 6 Vinci Engine

    12

    confirmed

    Ms. Li Forsberg

    GKN Aerospace Engine Systems

    Sweden

    9

    11:51

    Studies on the Additive Fabrication Concept for Future Launcher Engine Nozzle Extension Design and Manufacturing

    12

    confirmed

    Dr. Christo Dordlofva

    GKN Aerospace Engine Systems

    Sweden

    10

    12:03

    AUTOMATION OF ENGINE MEDIUM SUBSTITUTION FOR CRYOGENIC ENGINES TESTING IN HIGH ALTITUTE TEST BAY

    12

    confirmed

    Mr. VINOD P

    Indian Space Research Organization (ISRO)

    India

    11

    12:15

    CFD Performance Prediction of Cryogenic High-Speed Bearings for Reusable Pump-fed Liquid Rocket Engines

    12

    confirmed

    Mr. Kento Sakai

    Waseda University

    Japan

    12

    12:27

    Research of Reusable LOX/RP-1 Propulsion System Firing Test

    12

    confirmed

    Dr. Sheng Zhao

    China Academy of Launch Vehicle Technology (CALT)

    China

    1*

    10:15

    Development of H3 RCS (Reaction Control System)

    12

    Mr. yoshihiro kishino

    IHI Aerospace Co, Ltd.

    Japan

    2*

    10:27

    Design of an Additively Manufactured Bipropellant Thruster for In-Orbit Satellite Operations

    12

    confirmed

    Mr. Davide Zuin

    Politecnico di Milano

    Italy

    3*

    10:39

    Study on Ignition and Combustion Characteristics of Gaseous Oxygen/Gaseous Methane Igniter

    12

    confirmed

    Dr. Yang Zhang

    Jiangsu University

    China

    4*

    10:51

    Blockage Removal and Requalification of a Regeneratively Cooled, Additively Manufactured Rocket Engine

    12

    confirmed

    Mr. Sebastian Bouckenooghe

    University of Southern California

    United States

    5*

    11:03

    Enhancing Bipropellant Attitude Control Thruster Testing: A Control Theory Approach

    12

    confirmed

    Mr. Lars Osborne

    United States