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  • session 2

    Title

    Liquid Propulsion (2)

    type

    oral

    Description

    This session includes all science and technologies supporting all aspects of liquid propulsion. The emphasis in this session is placed, in particular, on components for liquid propulsion.

    Date

    2022-09-20

    Time

    10:15

    Room

    W08

    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. Martin Velander, GKN Aerospace Engine Systems, Sweden;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Characterization of Residual Inconel Particles in Additively Manufactured Rocket Engines

    15

    confirmed

    Mr. Charlie Whitesell

    Viterbi School of Engineering, USC

    United States

    2

    10:30

    Integral Channel Nozzles and Heat Exchangers using Additive Manufacturing Directed Energy Deposition NASA HR-1 Alloy

    15

    confirmed

    Mr. Paul Gradl

    National Aeronautics and Space Administration (NASA)

    United States

    3

    10:45

    Summary of initial feasibility studies on the use of laser powder bed fusion in nozzle extension applications

    15

    withdrawn

    Dr. Christo Dordlofva

    GKN Aerospace Engine Systems

    Sweden

    4

    11:00

    Combustion Performance Enhancement of a Hydrogen Peroxide Bi-propellant Thruster Using the Fluidic Oscillator Kerosene Injector

    15

    confirmed

    Mr. Sangwoo Jung

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    5

    11:15

    Testing of a small HTP Monopropellant Thruster for Space Applications

    15

    confirmed

    Dr. Francesco Barato

    University of Padova - DII/CISAS

    Italy

    6

    11:30

    An efficient numerical approach for thermal characterization in Liquid Rocket Engines

    15

    confirmed

    Ms. Arianna Remiddi

    Sapienza University of Rome

    Italy

    7

    11:45

    Surrogate models based on high fidelity numerical simulations for rocket engines injector design

    15

    confirmed

    Dr. Annafederica Urbano

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    France

    8

    12:00

    Development of a method for the quantitative assessment of fouling by thermo-catalytic fuel decomposition in rocket cooling channels

    15

    withdrawn

    Mr. Jules Heldens

    Royal Institute of Technology (KTH)

    Sweden

    9

    12:15

    Experimental Verification of Flutter Limits for a Mistuned Supersonic Turbine Blisk

    15

    withdrawn

    Dr. Clas Andersson

    GKN Aerospace Engine Systems

    Sweden

    10

    12:30

    Methane-Oxygen space rockets test bench H-IMP Italian facility non-stationary performances numerical simulation

    15

    Dr. Federico De Filippis

    CIRA Italian Aerospace Research Centre

    Italy