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  • session IP

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    type

    interactive

    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. Angelo Cervone, Delft University of Technology (TU Delft), The Netherlands;

    • Co-Chair: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;

    • Co-Chair: Prof. Riheng Zheng, Beihang University, China;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    ROLE OF ACOUSTICS ON UNSTABLE FIRE PHENOMENON IN SPACE PROPULSION

    10

    confirmed

    Mr. Vinayak Malhotra

    SRM University Chennai

    India

    Research on the acoustic characteristics of flow distribution plate in LOX/kerosene staged combustion rocket engine

    10

    confirmed

    Dr. chen cao

    Xian Aerospace Propulsion Institute

    China

    Review on the technology of liquid oxygen kerosene engine for the booster stage of Long March 5

    10

    confirmed

    Prof. Chen Jianhua

    Xi'an Aerospace Propulsion Institute

    China

    Improving rocket nozzle efficiency with rough surfaces

    10

    withdrawn

    Mr. Claudio Antonio Morales Benítez

    High Technology Unit (UAT) Faculty of Engineering - UNAM

    Mexico

    Fusion-Enabled Plasma Propulsion for Enabling Interstellar Missions

    10

    Mr. ravinder singh

    Concordia University

    Canada

    Fabrication and propulsion performance testing of a 100 mN class resistojet thruster

    10

    confirmed

    Mr. Mohamed Elawad

    United Arab Emirates University (UAEU)

    United Arab Emirates

    Sidewall-mounted planar type propulsion system for post mission disposal of Cubesats

    10

    confirmed

    Dr. Daeban Seo

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    pulsed plasma thruster using a metal composite polymer as a propellant

    10

    withdrawn

    Mr. TSUNG-YING YANG

    National Cheng Kung University

    Taipei

    equivalent circuit of vacuum arc thruster with multi-layer electrodes

    10

    withdrawn

    Mr. Ping-Han Huang

    National Cheng Kung University

    Taipei

    Magnetic Octupole Plasma Thruster with a Center-Mounted Hollow Cathode

    10

    confirmed

    Mr. Jordan Hsieh

    National Cheng Kung University

    Taiwan, China

    Effects of Structural Vibration on Spray Pattern of well-functioning and faulty pintle-head injector

    10

    withdrawn

    Mr. Manish Tajpuriya

    Nepal

    Direct thrust measurements of multidirectional plasma thruster operated in Krypton

    10

    confirmed

    Mr. Andrei Shumeiko

    Bauman Moscow State Technical University

    Russian Federation

    Advanced Room Temperature Propellants for Rockets and Spacecrafts

    10

    confirmed

    Mr. Ansh Jaipuria

    SRM Institute of Science and Technology

    India

    Energetic and Sustainable Rocket Propellant for Lower Stage

    10

    confirmed

    Mr. BHUSHAN THOMABRE

    SRM Institute of Science and Technology

    India

    experimental study on oxygenation constant volume combustion characteristics of hydrogen internal combustion engine

    10

    confirmed

    Dr. Liqiang Ai

    China Academy of Launch Vehicle Technology (CALT)

    China

    Magnetically Levitated Test Stand for Thrust Measurement for Micro Propulsion Systems

    10

    confirmed

    Mr. Basel Altawil

    Khalifa University of Science and Technology (KUST)

    United Arab Emirates

    THE EFFECT OF SWIRL INJECTION PARAMETERS ON A VORTEX-COOLED THRUSTER FABRICATED USING THERMOPLASTICS AND METAL

    10

    confirmed

    Mr. Mousa Aqailan

    United Arab Emirates University (UAEU)

    United Arab Emirates

    renewable liquid propellants: decarbonizing space exploration

    10

    confirmed

    Prof.Dr. Nazim Muradov

    University of Central Florida (UCF)

    United States

    Research Progress and Future Prospects of Novel Liquid Propellant

    10

    confirmed

    Mr. Xing Zhang

    China Aerospace of Science and Technology Corporation

    China

    Development of Atlas: A Liquid Rocket Engine Cryogenic Test Stand and Feed System

    10

    confirmed

    Mr. Johannes Reichert

    Viterbi School of Engineering, USC

    United States

    Development of a Small Scale LOx/Kerosene Powered Flight Vehicle: Methods of Mass and Cost Optimization

    10

    withdrawn

    Mr. Danetti Martino

    Viterbi School of Engineering, USC

    United States

    Computational simulation of boron oxidation by atmospheric air oxygen using Reactive Molecular Dynamics

    10

    confirmed

    Prof.Dr. José Rocco

    ITA-DCTA

    Brazil