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  • session 1

    Title

    Liquid Propulsion (1)

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

    Date

    2024-10-14

    Time

    15:15

    Room

    Blue Hall 1

    IPC members
    • Co-Chair: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Co-Chair: Mr. Ulrich Gotzig, ArianeGroup, Germany;

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

    • Rapporteur: Dr. Vanniyaperumal Narayanan, Indian Space Research Organization (ISRO), India;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

    Progresses in Applied Research on Liquid Rocket Propulsion by T(H)RUST Research Team at Sapienza University of Rome

    12

    confirmed

    Prof. Francesco Nasuti

    Sapienza University of Rome

    Italy

    2

    15:27

    600 seconds of qualification test on a low-toxic hypergolic bi-propellant thruster

    12

    confirmed

    Dr. Junyeong Jeong

    Satellite Technology Research Center( SaTReC), KAIST

    Korea, Republic of

    3

    15:39

    Esrange Space Center: Developing a Modern, Flexible, and Sustainable Rocket Engine Test Site

    12

    confirmed

    Mr. Casper Liavåg

    Swedish Space Corporation (SSC)

    Sweden

    4

    15:51

    In-Orbit Demonstration Overview of a Nitrous-Based Bipropellant Thruster

    12

    confirmed

    Mr. Davide Zuin

    Politecnico di Milano

    Italy

    5

    16:03

    LUMEN: Liquid Upper Stage Demonstrator Engine - A Versatile Test Bed for Rocket Engine Components: Hot-Fire Test Results

    12

    confirmed

    Mr. Tobias Traudt

    DLR (German Aerospace Center)

    Germany

    6

    16:15

    ENLIGHTEN Project: New Key Technologies for Future Launchers

    12

    confirmed

    Dr. Antonio Accettura

    AZO GmbH

    Germany

    7

    16:27

    study on multi-mode space propulsion of ch4/n2o propellant

    12

    confirmed

    Mr. tae young Lee

    Chosun University

    Korea, Republic of

    8

    16:39

    Design and development of a Green Engine for In-Orbit Servicing and space logistics applications

    12

    confirmed

    Dr. Roberto Bertacin

    Italian Space Agency (ASI)

    Italy

    9

    16:51

    Effect of Fuel Injection Temperature on the Stability of LOx-Methane Supercritical Combustion

    12

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    10

    17:03

    Design and Development of the Largest Student-Built Liquid Rocket Engine for Suborbital Flight: A Comprehensive Overview and Lessons Learned

    12

    confirmed

    Mr. Oleg Khalimonov

    Concordia University

    Canada

    11

    17:15

    On development of green storable liquid rocket engine with thrust variation

    12

    confirmed

    Mr. Dawid Cieslinski

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    12

    17:27

    Capacities and development prospects of the Lleida-Alguaire airport testing facilities for rocket engines, sub-components and prototypes

    12

    confirmed

    Mr. Lluís Montilla Rodríguez

    Institut d'Estudis Espacials de Catalunya (IEEC)

    Spain

    1*

    15:15

    On-orbit demonstration of RUDRA 0.3 HPGP Green Monopropellant thruster system in POEM-3 PSLV C-58 mission.

    12

    confirmed

    Mr. Saagar Malaichamy

    Bellatrix Aerospace Private Limited

    India

    2*

    15:27

    Highly Throttleable Propulsion for FROG-H: A Green Technological Leap

    12

    confirmed

    Mr. Błażej Marciniak

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    3*

    15:39

    Sustainable Spacecraft Propulsion: A 1N Thrust-Level Bi-Propellant Thruster utilizing Nitrous Oxide

    12

    confirmed

    Mr. Varun Reddy Nandyala

    FOTEC Forschungs- und Technologietransfer GmbH

    Austria

    4*

    15:51

    A numerical optimization of high-altitude test facility for upper stage engines

    12

    confirmed

    Dr. chaehyoung kim

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    5*

    16:03

    Experimental investigations into the low toxicity hypergolic ionic liquid-ethanol fuel and hydrogen peroxide oxidizer

    12

    confirmed

    Dr. Vikas Bhosale

    Space Solutions Co. LTD

    Korea, Republic of