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  • LBA
  • session LBA

    Title

    Late Breaking abstracts (LBA)

    type

    interactive

    Room

    IP Area (Hall B)

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

    • Co-Chair: Mrs. Elena Toson, Space Generation Advisory Council (SGAC), Italy;

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

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

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Aerospike nozzle design with passive cooling system for improved durability and efficiency at rocket engines.

    10

    confirmed

    "Chaac": Harnessing Machine Learning for Intelligent Combustion Control and Sustainable Propellants in Liquid Propellant Rocketry

    10

    confirmed

    Mr. Angel Vázquez

    High Technology Unit (UAT) Faculty of Engineering - UNAM

    Mexico

    dual flame holder design for enhanced efficiency and blowout control in liquid propellant rocket afterburners

    10

    confirmed

    Ms. Kavya Dichwalkar

    VIT Bhopal University

    India

    Emerging Nuclear Thermal Propulsion Capabilities for Rapid Transit Space Science Missions

    10

    Dr. Michael Eades

    United States

    Erosion Impact on Thrust Alignment in Hybrid Rocket Motor Nozzle Extensions Using Various Materials

    10

    confirmed

    Mr. Mehmet Kemal Ergin

    Deltav Space Technologies,Inc.

    Türkiye

    experimental study of porous-wall expansion-deflection nozzle flow

    10

    confirmed

    Dr. Bocheng Zhou

    Harbin Engineering University

    China

    Impact of Nozzle Throat Length on Erosion and Thrust Misalignment in Paraffin-Based Hybrid Rocket Motors

    10

    Ms. Büşra Kahraman

    Deltav Space Technologies,Inc.

    Türkiye

    Investigating Ignition Lead Times Across Fuel Variations in Hybrid Rocket Motors

    10

    confirmed

    Ms. İlknur Akkaya

    Deltav Space Technologies,Inc.

    Türkiye

    Supercavitating Liquid Oxygen and JET-A Pump Analysis for a 35 KN Rocket Engine Turbopump

    10

    confirmed

    Mr. Hudson Pastuszko

    Concordia University

    Canada

    Numerical Investigation on Combustion Enhancement Strategy in Shock Concentric Bubble Interaction

    10

    confirmed

    Mr. Zhibang Wang

    Harbin Engineering University

    China

    Preliminary Design for Air-Breathing Gridded Ion Thruster

    10

    confirmed

    Mr. Angelo Romano

    CIRA Italian Aerospace Research Center, Capua

    Italy

    Numerical model of rarefied gas interaction with charged particles

    10

    confirmed

    Mr. Tomas Valuch

    TRL Space

    Czech Republic