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

    Date

    2023-10-04

    Time

    10:15

    Room

    BCC A8

    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. Hidenori Hara, Mitsubishi Heavy Industries, Ltd., Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Qualification of a Propulsion System for active Deorbit

    15

    confirmed

    Mr. Ulrich Gotzig

    ArianeGroup

    Germany

    2

    10:30

    Performance Evaluation of Hypergolic Ionic Liquid-based Fuel (ILethCu01) with 95% Hydrogen Peroxide Oxidizer in 50 N Thruster.

    15

    confirmed

    Dr. Vikas Bhosale

    Space Solutions Co. LTD

    Korea, Republic of

    3

    10:45

    Experimental investigation of fuel transverse injection during throttling in a bipropellant thruster.

    15

    confirmed

    Mr. Vincent Ugolini

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    4

    11:00

    Employing carbon-split pore tubes as adsorbents to control the leakage of methane in transport valves

    15

    Ms. Anagha Udupa

    R V College of Engineering, Bengaluru

    India

    5

    11:15

    SOFT FLOW METER FOR MISSION-ONBOARD TO MEASRUE FLOW PARAMETER FOR LIQUID ROCKET ENGINES

    15

    confirmed

    Mr. elayaperumal ezhilrajan

    Indian Space Research Organization (ISRO)

    India

    6

    11:30

    DESIGN AND ANALYSIS OF A NOVEL SWIRL-PINTLE COMBINED FUEL INJECTOR FOR IMPROVED PERFORMANCE OF LIQUID ROCKET ENGINES

    15

    confirmed

    Mr. Sriram Kumar

    Sri Sairam Engineering College

    India

    7

    11:45

    Feasibility of UV induced decomposition of High Test Peroxide in spacecraft propulsion.

    15

    confirmed

    Mr. Damian Grabowski

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    8

    12:00

    Performance testing of 1N Hydrogen Peroxide thruster at FOTEC propulsion test facilities

    15

    confirmed

    Mr. Varun Reddy Nandyala

    FOTEC Forschungs- und Technologietransfer GmbH

    Austria

    9

    12:15

    A novel approach for the design and manufacture of an optimized catalyst bed for hydrogen peroxide

    15

    withdrawn

    Mrs. Natalia Ghisi

    United Arab Emirates

    10

    12:30

    Convective and Radiative Wall Heat Transfer Evaluation in Film-Cooled Liquid Rocket Thrust Chambers

    15

    confirmed

    Dr. Mario Tindaro Migliorino

    Sapienza University of Rome

    Italy