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  • session 4

    Title

    Solid and Hybrid Propulsion (2)

    Description

    This session includes all science and technologies supporting all aspects of solid and hybrid propulsion.

    Date

    2022-09-20

    Time

    10:15

    Room

    W05

    IPC members
    • Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;

    • Co-Chair: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;

    • Rapporteur: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

    • Rapporteur: Dr. Arif Karabeyoglu, Koc University, Turkey;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    pressure oscillation in p120c srm: what had to be proved

    15

    confirmed

    Mrs. Severine Larrieu

    ArianeGroup

    France

    2

    10:30

    The Three-Dimensional Combustion Flame of Micron Aluminum Particles Base on Computed Tomography of Chemiluminescence (CTC)

    15

    confirmed

    Dr. Bingning JIN

    Northwestern Polytechnical University

    China

    3

    10:45

    Study of the influence of the electric field on the incidental ignition of aluminized compound solid propellent via electrostatic discharge

    15

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    4

    11:00

    Framework for the design of solid propellants via functionally graded, additively manufactured nanoenergetic materials

    15

    confirmed

    Mr. Connor MacRobbie

    University of Waterloo

    Canada

    5

    11:15

    Experimental Investigation of Different Propellants and Expandable Graphite Additives for Controlling Rocket Motor Thrust

    15

    confirmed

    Ms. Gabriele Muller

    TECHNION - Israel Institute of Technology

    Israel

    6

    11:30

    Centrifugal Casting of Paraffin Wax: Numerical Analysis of the Influence of Casting Tube Aspect Ratio

    15

    confirmed

    Prof. Danielle Wood

    Massachusetts Institute of Technology (MIT)

    United States

    7

    11:45

    Experimental investigation and numerical simulation on throttleable pintle-centrifugal injector for hybrid rocket motor

    15

    confirmed

    Mr. Tianwen Li

    School of Astronautics, Beihang University

    China

    8

    12:00

    static and re-ignition test of hypergolic hybrid rocket using hydrogen peroxide oxidizer

    15

    confirmed

    Mr. Junyeong Jeong

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    9

    12:15

    Prediction Of Hybrid Rocket Nozzle Behaviour Under High Temperature Oxygen Rich Environment

    15

    confirmed

    Ms. Sule Ozturk

    Deltav Space Technologies,Inc.

    Turkey

    10

    12:30

    Cryogenic Pump Design and Testing for Hybrid Rocket Applications

    15

    confirmed

    Mr. Berkay Terzi

    Deltav Space Technologies,Inc.

    Turkey