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  • session IP

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    Description

    Authors with an abstract accepted for an interactive presentation will be asked to prepare slides and display them for the duration of the congress on plasma screens. Authors will be assigned to interactive sessions in which they must be near the plasma screens to engage in interactive discussions with other congress attendees.

    Date

    2022-09-21

    Time

    13:30

    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

    PEPE: A low cost, reliable, reusable, user- and environment- friend Propulsion System

    10

    confirmed

    Mr. Luciano Battocchio

    Czech Republic

    2

    Optimized orbit transfer of a Gravidyne with low-thrust propulsion

    10

    confirmed

    Mr. David Gil

    United Arab Emirates University (UAEU)

    United Arab Emirates

    3

    Experimental Investigation on Throttling Transient Response of Bipropellant Thruster Using Cavitating Venturi Valve.

    10

    confirmed

    Mr. Vincent Ugolini

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    4

    The Turborocket Engine: An Integrated Pump-Fed Rocket Engine for Propulsion Applications

    10

    withdrawn

    Dr. John Bossard

    United States

    5

    Physical properties and ignition characteristics of hypergolic propellant with oxidizing additives

    10

    confirmed

    Mr. Kyounghwan Lee

    Hanbat National University

    Korea, Republic of

    6

    ignition delay and thermoacoustic coupling in hybrid rocket combustion

    10

    confirmed

    Prof. Changjin Lee

    Konkuk University

    Korea, Republic of

    7

    two-phase, multicomponent hydrogen peroxide blowdown injector modelling and tests comparisons

    10

    confirmed

    Mr. Arthur Bahdur

    Alcântara Launch Center

    Brazil

    8

    Wave Steepening Instability Caused by Hypergolic Detonation of High Test Peroxide-based Hypergol

    10

    withdrawn

    Mr. Kyu-Seop Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    9

    Numerical and experimental investigation of lambda type seals in high-pressure cryogenic bolted joints

    10

    confirmed

    Mr. B Deependran

    Indian Space Research Organization (ISRO)

    India

    10

    Designing a nuclear electric propulsion system for future Pluto missions

    10

    confirmed

    Mr. Maanyash Jain

    India

    11

    ST-40 Hall Thruster Testing with LaB6 Hollow Cathode

    10

    Prof. Olexandr Petrenko

    Flight Control LLC

    Ukraine

    12

    Strategy for Simultaneous Hydrogen Trapping and Metallic Grain Size Control in Cermet Fuels for Nuclear Thermal Propulsion

    10

    confirmed

    Mr. Jonathan Johnson

    The University of Alabama

    United States

    13

    Conceptual Design of a N2O/Paraffin Hybrid Sounding Rocket

    10

    confirmed

    Mr. Riccardo Gelain

    Université Libre de Bruxelles

    Belgium

    14

    Parametric design and testing of explosion-preventive solid propellant rocket engines in the event of unexpected behavior during combustion

    10

    confirmed

    Mr. Nicolás de Jong

    LEEM-UPM

    Spain

    15

    Nuclear Thermal Propulsion for In-Space Applications focusing Beryllium as the Working Fluid and Graphite and FLiBe as Moderator and Coolant and Thorium Blanket

    10

    confirmed

    Ms. Aarya Kulkarni

    International Space University (ISU)

    India

    16

    Propellant grain design for Solid strap-on Booster operating under Martian condition and selecting the appropriate propellant.

    10

    confirmed

    Mr. Mahir Rawal

    India

    17

    The Relativistic Mass Ratio in Ultrarelativistic Photon Rockets

    10

    Prof. Espen Haug

    Norwegian University of Science and Technology

    Norway

    18

    Simulation analysis of multimode propulsion systems for satellites

    10

    withdrawn

    Ms. Sagarika Rao Valluri

    RNSIT Bangalore

    India

    19

    Pulsed Plasma Thruster for Deep Space Exploration

    10

    confirmed

    Dr. Jayakumar Venkatesan

    Valles Marineris International Private Limited

    India

    20

    Electrodeless plasma thruster concepts for high-power propulsion systems

    10

    confirmed

    Dr. Sean Shan Min Swei

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    21

    Aerodynamic analysis on JAXA’s experimental vehicle for hypersonic flight

    10

    Dr. Susumu Hasegawa

    Japan Aerospace Exploration Agency (JAXA)

    Japan

    22

    Dynamic Modeling and Simulation of a Hydrogen Peroxide Monopropellant Thruster

    10

    confirmed

    Dr. Sukmin Choi

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    23

    Three-Dimensional MHD Analysis of Magnetic Plasma Drag with Coils Placed on Three Axes

    10

    confirmed

    Dr. Shoko Arita

    Shizuoka University

    Japan

    24

    Conditions for the long-term existence of spacecraft with air-breathing electric propulsion in ultra-low orbits about planets

    10

    confirmed

    Dr. Egor Loktionov

    Bauman Moscow State Technical University

    Russian Federation

    25

    A Novel Design Usage of Thermoelectric Materials in Aerospike Engines

    10

    confirmed

    Mr. Gautam Arora

    University of Petroleum and Energy Studies

    India

    26

    A Comparison Study on the Feasibility of Two Low Sloshing Configurations for Small Satellite Magnetic Fluid Actuation

    10

    confirmed

    Mr. Priyank Dubey

    Indian Institute of Technology

    India

    27

    The nano-probe by the photon transportation in the Deep Space

    10

    confirmed

    Mr. Jamel Metmati

    THALES Services

    France

    28

    9tonf staged combustion cycle liquid rocket engine startup analysis

    10

    confirmed

    Mrs. BOYEON KHIM

    Korea, Republic of

    29

    Hypergolic ignition characterization of less-toxic bipropellants using Hydrocarbon fuel blend and Hydrogen Peroxide

    10

    confirmed

    Mr. Vignesh G

    ISRO Propulsion Complex, Mahendragiri, India

    India

    30

    Development Status of the SPS-40 Propulsion System

    10

    confirmed

    Mr. Danylo Shcherbak

    Flight Control LLC

    Ukraine

    31

    HYDROGEN-ENRICHED LIQUID METHANE AND LIQUID ETHANOL AS A TRANSITIONAL SOLUTION TOWARDS SUSTAINABILITY IN TERMS OF TECHNICAL FEASIBILITY FOR AEROSPACE MISSIONS

    10

    confirmed

    Mr. ILYES GHEDJATTI

    Beijing University of Aeronautics and Astronautics (BUAA)

    China

    32

    cold-gas experiments on advanced nozzles in subsonic counter-flows

    10

    withdrawn

    Mr. Giuseppe Scarlatella

    Dresden University of Technology (DUT) / Technische Universität Dresden

    Germany

    33

    Development of Ultra High DN Ceramic Ball Bearing for Cryogenic Rocket Engine Turbopump

    10

    confirmed

    Mr. BEN JACOB

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

    India

    34

    The effect of aerodynamic heating to cryogenic propellant discharge

    10

    confirmed

    Dr. Seungwhan Baek

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    35

    preliminary screening of catalytic beds for hydrogen peroxide thrusters with thrust level lower than 0.5 N

    10

    confirmed

    Mr. Rawoof Shaik

    University of Pisa

    Italy

    36

    Numerical Simulation of Flow Atomization caused by Two Impinging Liquid Jets

    10

    confirmed

    Ms. Maryam Ozair

    Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)

    Pakistan

    37

    Rapid Design of a Small Scale KeroLOx Flight Vehicle Propulsion System

    10

    confirmed

    Mr. Nathan Hirsch

    Viterbi School of Engineering, USC

    United States

    38

    FEASIBILITY ANALYSIS FOR ELECTRIC PROPULSION SYSTEMS FOR SHORT TERM INTERPLANETARY MISSIONS

    10

    confirmed

    Ms. Pritha Pal

    University of Michigan

    United States

    39

    Design and development of Latching Solenoid valve for Active Pressure Regulation System

    10

    confirmed

    Mr. Venkata Sunil Sai Nukala

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

    India

    40

    Computational model for performance prediction of a nitrous oxide / eicosane hybrid rocket engine

    10

    confirmed

    Mr. Joel Jean-Philyppe

    McGill University

    Canada

    41

    Common pitfalls of testing hybrid rocket engines at student led facilities

    10

    confirmed

    Mr. Cyril Mani

    McGill University

    Canada

    42

    Vacuum Arc Thruster architecture for green orbit maintenance with small satellite missions

    10

    confirmed

    Mr. José-María Jiménez-Coronado

    Costa Rica Institute of Technology (ITCR)

    Costa Rica

    43

    Experimental & Numerical Investigation of GOx/GCH4 Combustion in a 7-Element Rocket Combustor

    10

    Mr. Abhishek Sharma

    Indian Space Research Organization (ISRO)

    India

    44

    Numerical study on n-decane heat transfer under supercritical pressure in regenerative cooling channel

    10

    confirmed

    Mr. Yuhang Li

    Xi'an Aerospace Propulsion Institute

    China

    45

    Integrated internal and external ballistics for sounding rocket design

    10

    confirmed

    Dr. Jeongmoo Huh

    United Arab Emirates University (UAEU)

    United Arab Emirates

    46

    Numerical estimation of heat loss and thrust performance characteristics in micro propulsion

    10

    confirmed

    Dr. Jeongmoo Huh

    United Arab Emirates University (UAEU)

    United Arab Emirates

    47

    Comparative analysis of numerical models of film and regenerative cooling in thrust chamber at high pressure

    10

    confirmed

    Mr. Dhiyaneshwar L V

    SASTRA University

    India

    48

    multi-scale numerical study on atomization dynamics of gas-liquid pintle injector

    10

    confirmed

    Mr. Pu Shi

    Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University

    China

    49

    Modeling of wall-bounded high pressure flows in Liquid Rocket Engines

    10

    Mr. Giuseppe Indelicato

    Sapienza University of Rome

    Italy

    50

    High Flux Hybrid Motor Development with Distributed Tube Injector

    10

    confirmed

    Mr. Mehmet Kahraman

    Deltav Space Technologies,Inc.

    Turkey

    51

    Research on Acoustic Closed-End Device for Hydraulic Excitation Test of LRE

    10

    confirmed

    Dr. meng dong

    Xi'an Aerospace Propulsion Institute

    China

    52

    RESEARCH ON ELECTRIC SPACE PROPULSION AT ITALIAN AEROSPACE RESEARCH CENTRE: status and future enhancement

    10

    confirmed

    Dr. Marco Invigorito

    CIRA Italian Aerospace Research Centre

    Italy

    53

    Effect of H2O2 concentration and catalytic ratio on the autoignition characteristics of RP-3 kerosene under catalytic ignition engine-like conditions

    10

    confirmed

    Mr. Shutao Han

    Beihang University (BUAA)

    China

    54

    A Review: On the various FEEP thrusters present in the Industry and their Performance Comparison

    10

    confirmed

    Mr. Anirudh Balaji N S

    SASTRA University

    India

    55

    Vacuum testing of 3D printed 1N Hydrogen Peroxide thruster and a novel platinum catalyst

    10

    confirmed

    Mr. Varun Reddy Nandyala

    FOTEC Forschungs- und Technologietransfer GmbH

    Austria

    56

    Lessons learned during SRAD hybrid rocket motor development

    10

    confirmed

    Mr. Norbert Szulc

    Gdansk University of Technology

    Poland

    57

    Using differential pressure sensor to measure nitrous oxide level in a tank

    10

    confirmed

    Mr. Mateusz Czapski

    Gdansk University of Technology

    Poland