• Home
  • IAF Digital Library
  • Public Website
  • My papers
  • Home
  • event
  • IAC-23
  • C4
  • IPB
  • session IPB

    Title

    Interactive Presentations - IAF SPACE PROPULSION SYMPOSIUM

    type

    interactive

    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

    Prospects in green propellants and green propulsion systems

    10

    withdrawn

    Prof. Rachid Amrousse

    Chouaib Doukkali University

    Morocco

    Student built cryogenic liquid rocket engine technology demonstrator: Results and learning outcomes

    10

    withdrawn

    Ms. Francesca van Marion

    Delft Aerospace Rocket Engineering (DARE)

    The Netherlands

    Overview of existing launch vehicle fuel tank pressurization systems and development prospects

    10

    Mr. Vadym Khomiak

    Yuzhnoye State Design Office

    Ukraine

    A Trade Study of Mission Architectures for Centrifugal Nuclear Thermal Propulsion

    10

    confirmed

    Mr. William Ziehm

    University of Alabama in Huntsville

    United States

    Toolkit for Liquid Rocket Propulsion System Design

    10

    confirmed

    Mr. Nijat Abdulla

    National Aviation Academy - Azerbaijan

    Azerbaijan

    Design evaluation of the performance capabilities and schematic for the LOx/LNG liquid-propellant rocket engine

    10

    Dr. Volodymyr Shulha

    Yuzhnoye State Design Office

    Ukraine

    A new H2O2 oriented Rocket and Satellite Propulsion Laboratory Center

    10

    confirmed

    Mr. Lukasz Radzikowski

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    Using the intrinsic magnetic susceptibility change of methane combustion to increase maneuverability of RCEs

    10

    Mr. Akash Prasanna

    R V College of Engineering, Bengaluru

    India

    Numerical simulation of a detonation engine

    10

    confirmed

    Ms. Elena Mikhalchenko

    Scientific Research Institute for System Analysis, Russian Academy of Sciences (RAS)

    Russian Federation

    Power converter with high gain, high performance for space thrusters based on electrospray technology.

    10

    Mr. Francisco José Blázquez Plaza

    Universidad Carlos III de Madrid

    Spain

    Green Propellants: Self-Pressurization Behavior Modelling

    10

    confirmed

    Mr. Simone La Luna

    Politecnico di Milano

    Italy

    exploring the complexities of pintle injectors for high performance rocket propulsion an advanced numerical simulation investigation with expansion deflection nozzle

    10

    confirmed

    Mr. Sudarsan Nerella

    University of Petroleum and Energy Studies

    India

    Report on test firing results of 6.5 kN pressure-fed hypergolic storable liquid rocket engine and comparison to the design theoretical calculations.

    10

    confirmed

    Dr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    structural modification and flow analysis of isolator for enhanced efficiency of dual mode ramjet-scramjet engine

    10

    confirmed

    Mr. Greekshith Mahesh Babu

    R V College of Engineering, Bengaluru

    India