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  • session 4

    Title

    Solid and Hybrid Propulsion (2)

    Description

    The session Solid and Hybrid Propulsion (2) is dedicated to Solid and Hybrid Rocket motors, with particular emphasis on sub-systems and specific components (including propellants). The session welcomes manuscripts on all research and development areas: design, testing (including diagnostics and test facilities), analysis and calculations, modelling, applications, science and fundamentals.

    Date

    2024-10-16

    Time

    10:15

    Room

    Yellow Hall 2

    IPC members
    • Co-Chair: Mr. Didier Boury, ArianeGroup SAS, France;

    • Co-Chair: Dr. Yuji Saito, Tohoku University, Japan;

    • Rapporteur: Mr. Jean-Claude Traineau, Office National d’Etudes et de Recherches Aérospatiales (ONERA), France;

    • Rapporteur: Dr. Ozan Kara, Technology Innovation Institute (TII), United Arab Emirates;

    • Rapporteur: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    KEYNOTE: Hybrid Propulsion System Practices and Safety Considerations both for Launch Vehicles and In-Space Missions

    18

    confirmed

    Dr. Ozan Kara

    Technology Innovation Institute (TII)

    United Arab Emirates

    2

    10:33

    Nozzle Erosion Avoidance through Regenerative Cooling Systems in Hybrid Rocket Engines: Experimental Campaign and Numerical Modeling

    11

    confirmed

    Mr. Riccardo Cambertoni

    Politecnico di Torino

    Italy

    3

    10:44

    A new catalytic chamber concept for multi-phase injection of hydrogen peroxide

    11

    confirmed

    Mrs. Nora Bierwagen

    DLR (German Aerospace Center)

    Germany

    4

    10:55

    Experimental investigation of swirl oxidizer injector effect on 3D printed ABS hybrid rocket fuel regression rate

    11

    confirmed

    Dr. ANWER HASHISH

    Military Technical College

    Egypt

    5

    11:06

    performance testing of a 7 kn hybrid rocket motor under varying propellant conditions

    11

    confirmed

    Mr. Bernard Genevieve

    University of KwaZulu-Natal (UKZN)

    South Africa

    6

    11:17

    The three-dimensional dynamic numerical simulation of star-shaped grains in hybrid rocket motors

    11

    confirmed

    Dr. Xiangyu Meng

    Beihang University (BUAA)

    China

    7

    11:28

    Scalable Hybrid Rocket Systems for Agile and Affordable In-space Propulsion

    11

    confirmed

    Dr. Landon Kamps

    Letara Ltd.

    Japan

    8

    11:39

    Green Solid Fuels with Enhanced Mechanical Properties: Use of Sustainable Waxes and Scale-Up Analysis of Armored Grains.

    11

    confirmed

    Dr. Ch Paravan

    Politecnico di Milano

    Italy

    9

    11:50

    Solid Fuel Analysis in Hybrid Rocket Engine Using Image Processing

    11

    confirmed

    Mr. Felipe Fernandes

    Universidade de Brasília

    Brazil

    10

    12:01

    Experimental Investigation of a 10 kN class Hydrogen Peroxide - Paraffin Wax Hybrid Motor Demonstrator

    11

    confirmed

    Ms. Lucia Zeni

    T4i

    Italy

    11

    12:12

    analysis and experiment on the sustained combustion phenomenon of han/pva-based electrically controlled solid propellant

    11

    Mr. CHOI WOOJOO

    Chosun University

    Korea, Republic of

    12

    12:23

    study on the effect of the gap between grain and case on the structural integrity of solid propellant

    11

    confirmed

    Dr. Qin-liu Cao

    Shanghai Space Propulsion Technology Research Institute

    China

    13

    12:34

    Challanges in verification process of the Solid Rocket Motor for Direct Deorbitation Engineering Model

    11

    confirmed

    Mr. Pawel Nowakowski

    Łukasiewicz Research Network – Institute of Aviation (ILOT)

    Poland

    1*

    10:15

    Improving alumina-cap characterisation in aluminized solid-rocket motors with computer vision

    11

    confirmed

    Mr. Andrea Sportillo

    Office National d’Etudes et de Recherches Aérospatiales (ONERA)

    France

    2*

    10:33

    Reactive Molecular Dynamics Simulation of Ammonium Perchlorate-Aluminum Interactions: Effects of Passivation and Initial Decomposition Mechanism

    11

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    3*

    10:44

    Hybrid Rocket Engine Nozzle Deformation using a Level Set Method

    11

    confirmed

    Mr. Jan Erik Zeriadtke

    DLR (German Aerospace Center)

    Germany