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  • session IPB

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    type

    interactive

    Description

    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

    RAVEN: Reaching 1kN Engine Milestone, Test Bench Updates and Beyond

    10

    confirmed

    Mr. Gustavo Neves

    Giron Space Organisation

    Sweden

    Fast Propellant Margin Estimation for Early-Phase Liquid Rocket Engine Design Under O/F Ratio and Loading Uncertainties

    10

    confirmed

    Mr. Kubilay ÖZÇELİK

    ROKETSAN Roket Sanayi ve Ticaret A.S.

    Türkiye

    Numerical Investigation of Heat Transfer Characteristics and Nozzle Ablation in Hybrid Rocket Motors under Flight Overload

    10

    Mr. Yiming Ke

    School of Astronautics, Beihang University

    China

    Thermal profile of regressing paraffin-based fuels: intrusive measurement development and experiments

    10

    Mr. Valerio Santolini

    Politecnico di Milano

    Italy

    Analysis of Discharge Characteristics of a Hall Thruster Fueled with Multiple Propellants

    10

    Dr. Yu Chen

    Edrive Space Technology Co., Ltd

    China

    Rheology-Informed Design of Gel Propulsion Systems: Modeling Non-Newtonian Hydraulic Behavior and Injector Response

    10

    confirmed

    Mr. Utku Can Yıldız

    ROKETSAN Roket Sanayi ve Ticaret A.S.

    Türkiye

    Preliminary Design Framework for Torch-Type Igniters in Solid Rocket Motors

    10

    confirmed

    Ms. Alexandra Lopez Gutierrez

    Universidad de Costa Rica

    Costa Rica

    Quantitative Fractography for Ductility Prediction in Paraffin Hybrid Rocket Fuels: Transfer Across Manufacturing Scale and Route

    10

    confirmed

    Mr. Hamza Yiğit Yıldız

    Istanbul Technical University

    Türkiye

    Design Considerations for Turbine Exhaust Gas Film Cooling in Gas-Generator Cycle Rocket Engines

    10

    confirmed

    Dr. Insang Moon

    Korea Aerospace Research Institute (KARI)

    Republic of Korea

    Ultra-Lightweight Tensegrity-Based Hybrid Buoyant–Propulsive Aerial Platform for Surface Inspection

    10

    confirmed

    Mr. Wilberth Corrales

    Universidad de Costa Rica

    Costa Rica

    Verification of a Physics-Informed Multiphase Thermal Model using the Centrifugal Nuclear Thermal Rocket

    10

    confirmed

    Mr. Joshua Naudet

    The Ohio State University College of Engineering

    United States