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    Title

    Virtual 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.

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

    • Co-Chair: Dr. Vanessa Vial, Safran Aircraft Engines, France;

    • Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Design of a gas filled bellow pogo suppression device for launch vehicles.

    10

    confirmed

    Mr. SUNNY MITRA

    LPSC, ISRO

    India

    2

    Research and application on the innovative design system of LOX Kerosene engine which is available to Additive manufacturing technology

    10

    confirmed

    Mr. WANG Chunmin

    Northwestern Polytechnical University,NPU

    China

    6

    A way to increase rocket efficiency: the aerospike engine

    10

    confirmed

    Mr. Baptiste Laulan--Souilhac

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

    France

    8

    Effect of blade configuration on performance of a high speed axial flow pump inducer

    10

    confirmed

    Mr. AJI M ABRAHAM

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

    India

    11

    influence of inlet air temperature for dilution mixing in turbine-based air-breathing propulsion system

    10

    confirmed

    Mr. Wei Dai

    Beijing institute of Astronautical Systems Engineering, Beijing

    China

    13

    Experimental Studies on the Efficacy of Tabs as Supersonic Jet Control

    10

    confirmed

    Mr. THILLAIKUMAR T

    Indian Institute of Technology Kharagpur

    India

    14

    A technology for improving regenerative cooling in advanced cryogenic rocket engines for space transportation

    10

    confirmed

    Mr. AP Baiju

    LPSC, ISRO

    India

    15

    Assessment and Design of the Active Air Intake for VLEO Operation

    10

    confirmed

    Mr. Anatolii Papulov

    Skolkovo Institute of Science and Technology

    Russian Federation

    16

    MEMS thruster with an alternative ADN based monopropellant

    10

    confirmed

    Mr. Ju Won Kim

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    19

    minimum catalyst bed length for high test hydrogen peroxide thrusters

    10

    confirmed

    Mr. Sangwoo Jung

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    22

    Design and Test of Non-Uniform Spray Swirl Injectors and Its Applications in Injection Plate Design

    10

    confirmed

    Mr. Alexandre Costa Goulart

    Universidade Federal do ABC - UFABC

    Brazil

    23

    Literature studies and experimental characterization of multiple solid propellant regression rates using Crawford bomb method and rocket design analysis

    10

    confirmed

    Mr. Jesús Manuel Muñoz Tejeda

    Imperial College London

    Spain

    24

    Prediction of thermoacoustic instabilities by the linearized Navier-Stokes equations incorporated with the nonlinear n-tau model

    10

    confirmed

    Mr. Yuanzhe LIU

    Northwestern Polytechnical University

    China

    25

    Fission Fragment Rocket: Fuel Production and Structural Considerations

    10

    confirmed

    Mr. Pauli Laine

    Finland

    29

    Mutation of Permanent Magnet Hall Thruster: Central Cathode Configuration

    10

    confirmed

    Ms. Shritu Badoniya

    University of Petroleum and Energy Studies

    India

    30

    Design and Simulation of an Articulated On-board CubeSat Propulsion System

    10

    confirmed

    Ms. Sneha Gayen

    SRM Institute of Science and Technology

    India