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  • C4
  • IPB
  • session IPB

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    Date

    2022-09-19

    Time

    12:50

    Room

    IP Area

    IPC members
    • Co-Chair: Dr. Elizabeth Jens, Jet Propulsion Laboratory - California Institute of Technology, United States;

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

    • Co-Chair: Dr. Ozan Kara, Space Generation Advisory Council (SGAC), Turkey;

    • Co-Chair: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Numerical Model for the Prediction of the Regression Rate in Hybrid Rocket Kick-Motors Working with Liquid Nitrous Oxide

    10

    confirmed

    Dr. Giuseppe Gallo

    Hokkaido University

    Italy

    2

    Development of a Low-Cost Permanent Magnet Cylindrical Hall Effect Thruster for CubeSats

    10

    Mr. Kevin Burville

    MDA

    Canada

    3

    Computational Study of Plasma Detachment from Magnetic Nozzles in Applied Field MPD Thrusters using Lattice Boltzmann Method

    10

    confirmed

    Ms. Hamda Al-Ali

    The University of Manchester

    United Kingdom

    4

    Hybrid Rocket Engines as an Option to Future Application for the Brazilian Space Sector

    10

    confirmed

    Dr. Artur Bertoldi

    University of Brasilia

    Brazil

    5

    high- power sounding rockets

    10

    Ms. OLIVIA MWANIKI

    Kenya Space Agency (KSA)

    Kenya

    6

    Thermal Analysis of the Scramjet Engine System with Burning Fuel

    10

    confirmed

    Mr. Lucas Pádua

    UNIVAP University

    Brazil

    7

    Catalytic reactor test with an alternative ADN-H2O2 monopropellant

    10

    withdrawn

    Mr. Ju Won Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    8

    experimental study on the influence of different oscillation amplitude on the combustion characteristics of propellant aluminum particles

    10

    confirmed

    Ms. Jiang Yuan

    Northwestern Polytechnical University

    China

    9

    Advantage of Using Turbopump in Hybrid Rocket Applications

    10

    confirmed

    Mr. Berkay Terzi

    Deltav Space Technologies,Inc.

    Turkey

    10

    The Latest Investigation of Modular Engine – An Economical And Versatile Solution To Future Propulsion System

    10

    withdrawn

    Mr. Takenori Maeda

    Mitsubishi Heavy Industries, Ltd.

    Japan

    11

    Feasibility Study of Orbit Control Methods in CubeSats with Electric Propulsion for an Interplanetary Mission

    10

    confirmed

    Mr. Yassir Debbah

    Université Internationale de Rabat

    Morocco

    12

    Influence of different equations of state on the mixing behavior of a transcritical shear layer

    10

    withdrawn

    Mr. T. Jeremy P. Karpowski

    TU Darmstadt

    Germany

    13

    investigation of parametric dynamics inside a heaterless hollow cathode (hhc)

    10

    confirmed

    Mr. Rohan M Ganapathy

    Bellatrix Aerospace Private Limited.

    India

    14

    Development of a magnetically enhanced laser-ablative plasma thruster

    10

    withdrawn

    Mr. Shaun Andrews

    Alma Mater Studiorum - University of Bologna

    Italy

    15

    research on aerodynamic drag characteristics \\of solid fuel ramjet

    10

    confirmed

    Mr. Kyeongmin Jang

    Pusan National University

    Korea, Republic of

    16

    Fuel regression characteristics of axial-injection end-burning hybrid rockets using Nitrous Oxide

    10

    confirmed

    Ms. Mai FUKADA

    Hokkaido University

    Japan

    17

    Qualification and industrialization of the SWAN SANDWICH NOZZLE for ARIANE6

    10

    withdrawn

    Mr. Marcus Almqvist

    GKN Aerospace Engine Systems

    Sweden

    18

    smc based heading control of a satellite model with duo cold thrusters

    10

    Mr. Prasitthichai Naronglerdrit

    Asian Institute of Technology

    Thailand

    19

    Development of a validated modular design tool for ABS-nitrous hybrid rocket engines

    10

    confirmed

    Mr. Rolf Wubben

    Delft University of Technology (TU Delft)

    The Netherlands

    20

    The operational range of liquid metal and ionic liquid ion sources in the pure ionic regime.

    10

    Mr. Ximo Gallud Cidoncha

    Massachusetts Institute of Technology (MIT)

    United States

    21

    Interstellar space exploration using photon propulsion

    10

    confirmed

    Ms. Rithika S

    Manipal Institute of Technology, Manipal Academy of Higher Education

    India

    22

    STUDY OF EFFECT ON COMBUSTION FLOW-FIELD DUE TO VARIATION OF INLET BOUNDARY CONDITIONS IN DUAL-CAVITY SCRAMJET COMBUSTOR

    10

    confirmed

    Ms. Prisha Asher

    Space Generation Advisory Council (SGAC)

    India

    23

    Experiment and Simulation for Dynamic Characteristics of Dual-mode Space Propulsion System Pressurized by Electric Pump

    10

    confirmed

    Dr. Chuang Zhou

    School of Astronautics, Beihang University

    China

    24

    Modern materials and technologies implementation into the LRE design

    10

    Dr. Andrei Ivanov

    JSC NPO Energomash

    Russian Federation

    25

    RF Helicon-based Plasma Thruster Development for Very-Low Earth Orbit platforms: Progress at IRS

    10

    withdrawn

    Mr. Konstantinos Papavramidis

    Institute of Space Systems, University of Stuttgart

    Germany

    26

    Determination of solid fuels regression rate by reactive molecular dynamics simulations

    10

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    27

    Novel electro-chemical miniaturized thrusters for Distributed Satellite Space Missions

    10

    confirmed

    Mr. Sasi Kiran Palateerdham

    University of Rome “La Sapienza”

    Italy

    28

    Assessing Impurity Effects on LO-x/Methane and LO-x/Natural Gas Mixtures in Rocket Propulsion Systems

    10

    confirmed

    Ms. Jessica Baker

    University of Central Florida (UCF)

    United States

    29

    Atomisation and Combustion of the ONERA / CNES High Performance Green Monopropellant

    10

    confirmed

    Mr. Lorenzo Byrde

    ONERA - The French Aerospace Lab

    France

    30

    Development and Verification of a Thrust Vector Balance for Electric Propulsion Systems

    10

    Dr. Bernhard Seifert

    FOTEC Forschungs- und Technologietransfer GmbH

    Austria

    31

    Challenges and Opportunities for Orbital Propulsion

    10

    confirmed

    Mr. Ulrich Gotzig

    ArianeGroup

    Germany

    32

    Development of FEEP thruster based on annular-slit configured type emitter with indium propellant

    10

    Mr. Chanearl Kwon

    Seoul National University

    Korea, Republic of

    33

    cfd optimization of film cooling in green storable bipropellant rocket thrusters

    10

    confirmed

    Mr. Cezary Chmielewski

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland