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  • session 1

    Title

    Liquid Propulsion (1)

    type

    oral

    Description

    This session is dedicated to all aspects of Liquid Rocket Engines.

    Date

    2021-10-25

    Time

    15:15

    Room

    Ajman D

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

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

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

    • Rapporteur: Mr. Akira Ogawara, Mitsubishi Heavy Industries, Ltd., Japan;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    15:15

    Data-driven emulation models for Rocket Engines injector design

    15

    confirmed

    Mr. Jose Felix Zapata Usandivaras

    ISAE-Supaero University of Toulouse

    France

    2

    15:30

    Design of a conical anti-slosh baffle and its experimental validation for slosh stability for the Indian interplanetary mission

    15

    confirmed

    Mr. Sarath Chandran Nair S

    Indian Space Research Organization (ISRO), Liquid Propulsion Systems Centre (LPSC)

    India

    4

    15:45

    Preliminary Test of Hydrogen Peroxide Thermal Decomposition Monopropellant Thruster

    15

    confirmed

    Mr. Seungho Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    6

    16:00

    Development of an additively manufactured Hydrogen Peroxide / Kerosene 6 kN aerospike breadboard engine

    15

    confirmed

    Mr. Tim Dorau

    TU Dresden

    Germany

    8

    16:15

    Liquid Upper Stage Demonstrator Engine (LUMEN): Overview and Project Progress

    15

    confirmed

    Mr. Tobias Traudt

    DLR (German Aerospace Center)

    Germany

    11

    16:30

    comparison between a 400n electric pump fed hydrogen peroxide/ethanol thruster and the mmh/nto legacy systems

    15

    confirmed

    Ms. Livia Ordonez Valles

    Hochschule Bremen

    Germany

    1003

    16:45

    The results of ground development tests of the RD861K high-altitude liquid-propellant restartable rocket engine

    15

    confirmed

    Mr. Yevgen Strelchenko

    Yuzhnoye State Design Office

    Ukraine

    1005

    17:00

    Ariane 6 Upper Liquid Propulsive Module Qualification

    15

    confirmed

    Mr. Patrick Danous

    ArianeGroup

    France

    1007

    17:15

    Experimental characterization and analysis of passive flow separation control of upper stage rocket nozzle during sea-level testing

    15

    confirmed

    Dr. Ganesh Paramasivan

    ISRO Propulsion Complex, Mahendragiri, India

    India

    1009

    17:30

    Tests to study the influence of the low temperature of structure and propellants on the performance of VEGA Stage 4 main engine

    15

    confirmed

    Mr. Andrii Kovalenko

    Yuzhnoye State Design Office

    Ukraine

    1010

    17:45

    Combined pressurization system and gas-reactive control system of the reusable stage of the launch vehicle

    15

    withdrawn

    Mr. Vladislav Urbansky

    Omsk State Technical University

    Russian Federation

    1012

    18:00

    Experimental & Numerical Investigation of GOX/GCH4 Combustion in 7- Element Sub-scale Combustor

    15

    confirmed

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India