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  • IPB
  • session IPB

    Title

    Interactive Presentations - IAF SPACE TRANSPORTATION SOLUTIONS AND INNOVATIONS SYMPOSIUM

    type

    interactive

    Room

    IP Area (Hall B)

    IPC members
    • Co-Chair: Prof. Sunny Narayanan, Florida State University, United States;

    • Co-Chair: Dr. Jens Lassmann, ArianeGroup, Germany;

    • Co-Chair: Mr. Markus Jaeger, Airbus Defence & Space, Space Systems, Germany;

    papers

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    Prediction of Acoustic Noise Induced by the Launch of Space Vehicles

    15

    withdrawn

    Ms. Maryam Ozair

    Pakistan Space and Upper Atmosphere Research Commission (SUPARCO)

    Pakistan

    An Online Trajectory Planning Scheme for a Class of Long-Range Aerospace Transportation Vehicle

    12

    withdrawn

    Dr. Feng Zhang

    China Academy of Launch Vehicle Technology(CALT)

    China

    Flight Dynamics Simulation and Aerodynamic Database of a Retro-propulsion Assisted Reusable Launcher within the RETPRO Project

    12

    confirmed

    Dr. Josef Klevanski

    DLR (German Aerospace Center)

    Germany

    Conversion Of A Two-Stage Expendable Rocket Into A Reusable System And Analysis Of Its Re-entry Dynamics

    13

    confirmed

    Mr. Alessandro Mazzone

    University of Pisa

    Italy

    Sensors hybridization for distributed launcher system navigation development: first results of the NIBBIO project

    12

    confirmed

    Ms. Alessia Di Giacomo

    Sapienza University of Rome

    Italy

    Comparative Analysis of Airframe Configurations for Scramjet-Powered Hypersonic Vehicle

    13

    confirmed

    Mr. Kohei Omiya

    Kyushu University

    Japan

    New generation pyrotechnics for launchers - Combining heritage and innovation into an integrated approach

    12

    confirmed

    Mr. Florian THIVENT

    PYROALLIANCE

    France

    A novel optimization method of testing process for launch vehicles based on reinforcement learning

    10

    confirmed

    Dr. Hao Zhou

    Beijing Institute of Aerospace Systems Engineering

    China

    Optimizing Reusable Rocket Performance: Harnessing the Potential of Grid Fins for Enhanced Control

    10

    confirmed

    Ms. Sara Altrawneh

    Jordan University of Science & Technology

    Jordan

    Navigating the Space Maze: Optimizing Launch Service Selection

    15

    confirmed

    Ms. Zahra Imanova

    SABAH.HUB

    Azerbaijan

    Cruiser-feeder alternative to render Artemis affordable

    10

    Mr. Giorgio Gaviraghi

    Unispace Exponential Creativity

    Italy

    Research of Joint Launch Vehicle and Satellite Adaptive Coding Technology

    15

    confirmed

    Dr. Yuandong Zhang

    Beijing Institute of Astronautical Systems Enginnering

    China

    Requirement to Thrive: Embracing the New Era in New Space - A Digitalization Approach to Launch Processes and Management

    15

    confirmed

    Ms. Ceyda Yarımbatman

    Plan-S Satellite and Space Technologies

    Türkiye

    reconfigurable software design of model-based launch vehicle simulator for ground control system

    15

    confirmed

    Mr. SungRyoung Lee

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    Automated Model-driven Operation Approach using Open-source Script

    15

    confirmed

    Dr. Kwangsoo Kim

    Korea Aerospace Research Institute (KARI)

    Korea, Republic of

    esa vega-c launch complex water injection system – design of deluge system for an operational launch site

    10

    confirmed

    Mr. Christian Garegnani

    Telematic Solutions Srl

    Italy

    Flyboard Air: Sustainable Transportation Alternative for Explorers on Mars

    10

    confirmed

    Mr. Romildo Genaro Silva Cuadros

    Universidad Nacional Mayor de San Marcos

    Peru

    Real-time adaptive apogee prediction for a suborbital student rocket

    10

    confirmed

    Mr. Jack Johnston

    School of Engineering, University of Glasgow

    United Kingdom

    Comprehensive Simulation of Rocket Flight Trajectories with Active Canard Control for Descent Path Correction

    10

    confirmed

    Mr. Ahmet Nuri Yılmaz

    Istanbul Technical University

    Türkiye

    Optimisation of Categorical Choices in Exploration Mission Concepts of Operations Using Branch-and-Price Method

    10

    confirmed

    Mr. Nick Gollins

    Georgia Institute of Technology

    United States