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  • IAC-26
  • C4
  • LBA
  • session LBA

    Title

    Late Breaking Abstracts (LBA) - IAF SPACE PROPULSION SYMPOSIUM

    type

    interactive

    Description

    Late Breaking Abstracts (LBA) - IAF SPACE PROPULSION SYMPOSIUM This session offers a unique opportunity to deliver your key messages in an interactive presentation on any of the subjects of Space Propulsion addressed in the classic Sessions. The presentation will be displayed on a digital screen in a dedicated location and available for view by all Congress attendees for the entire Congress week. In addition, one afternoon is dedicated exclusively for the attendees to view the Interactive Presentations, and the author will be assigned a specific ten minute slot to personally present the topic and interact with the attendees present. The Interactive Presentation may take advantage of all electronic display capabilities, such as: PowerPoint charts, embedded hot links, pictures, audio and video clips etc. An award will also be presented to the author of the best Interactive Presentation in the C Category at a special ceremony. An Abstract that follows the standard format must be submitted by the deadline for standard IAC abstracts.

    Room

    IP Area

    IPC members
    • Co-Chair: Dr. Saroj Kumar, Propulsion Research Center, University of Alabama in Huntsville, United States;

    • Co-Chair: Dr. Andrei Shumeiko, Bauman Moscow State Technical University, Russian Federation;

    • Co-Chair: Prof. Sabrina Corpino, Politecnico di Torino, Italy;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    CFD and Thermal Management of a Scramjet Hypersonic Demonstrator Vehicle for future experimental campaigns

    Mr. Oreste Russo

    CIRA Italian Aerospace Research Centre

    Italy

    Comparative Heat Transfer Analysis of DEMİRKAZIK-IV Engine : Analytical, Numerical and Experimental Approaches

    confirmed

    Mr. Gökdeniz Yıldırım

    Yildiz Technical University

    Türkiye

    design and optimization of a pyrotechnic ignition system for hybrid rocket motors

    confirmed

    Ms. Umay Akkuyu

    Yildiz Technical University

    Türkiye

    Electric Thruster Plume and Surface Charging Analysis of HALE-1500 for Design Validation of the TÜRKSAT-6A Satellite

    confirmed

    Mr. Arif Armagan Gozutok

    TUBITAK Uzay, Space Technologies Research Institute

    Türkiye

    Geodesic Dome Profile Optimization with Friction-Integrated Winding Kinematics and Progressive Failure Analysis for Hybrid Rocket Motor COPVs

    confirmed

    Mr. Namık Hisar

    Yildiz Technical University

    Türkiye

    Hybrid AI-Driven Thrust Scheduling for Energy-Constrained 3U CubeSats with Ion Propulsion

    confirmed

    Mr. Aymar SUERY

    Ecole Centrale de Lyon

    France