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  • session 4

    Title

    Solid and Hybrid Propulsion (2)

    type

    oral

    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

    2023-10-04

    Time

    10:15

    Room

    BCC B6

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

    • Co-Chair: Mrs. Elena Toson, Space Generation Advisory Council (SGAC), Italy;

    • Rapporteur: Mr. Christophe Bonhomme, Centre National d'Etudes Spatiales (CNES), France;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Thermoplastic solid propellant analysis

    12

    confirmed

    Ms. Ana Carolina Buzelim dos Santos

    Brazil

    2

    10:27

    Study of the influence of the electric field on the incidental ignition of aluminized compound solid propellent via electrostatic discharge

    12

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    3

    10:39

    Development of High-Performance Solid Rocket Propellants Using AP-HTPB Composite Matrix and Different Plasticizers

    12

    withdrawn

    Mr. Om Kiritbhai Daxini

    R V College of Engineering, Bengaluru

    India

    4

    10:51

    Measurement of Solid Fuel Port Pressure by Using Exposed HDPE Hydrogen Peroxide Catalytic Decomposition Hybrid Thruster

    12

    confirmed

    Mr. Seungho Lee

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    5

    11:03

    Investigation of the influence of gas phase molecular mass variations on hybrid rocket regression rate

    12

    confirmed

    Dr. Francesco Barato

    University of Padova - DII/CISAS

    Italy

    6

    11:15

    Combustion Characteristics of Axial-Injection End-Burning Hybrid Rockets using Liquid Oxygen

    12

    confirmed

    Mr. Kaii Ri

    Hokkaido University

    Japan

    7

    11:27

    Experimental and numerical assessment of regression rate and propulsive performance of 10N-class hybrid rockets for nanosatellite maneuvering

    12

    confirmed

    Dr. Stefano Mungiguerra

    Università degli Studi di Napoli “Federico II”

    Italy

    8

    11:39

    Ablation Resistance Assessment of Graphite and Carbon-Carbon Composites Under Hybrid Propellant Rocket Free-Jet Exposure

    12

    confirmed

    Mr. Serhan Enes Kalmis

    Deltav Space Technologies,Inc.

    Türkiye

    9

    11:51

    Novel Design of Gas Generator System Using Hybrid Rocket Motor

    12

    confirmed

    Mr. Mehmet Reşat UFUK

    Deltav Space Technologies,Inc.

    Türkiye

    10

    12:03

    Demonstration of centrifugal casted paraffin wax-based hypergolic solid fuel for hydrogen peroxide

    12

    confirmed

    Mr. Junyeong Jeong

    Korea Advanced Institute of Science and Technology (KAIST)

    Korea, Republic of

    11

    12:15

    Development of Hybrid Thruster Ignition System with Low-Toxicity Fuel and Catalytic Reaction

    12

    confirmed

    Dr. Yuji Saito

    Tohoku University

    Japan