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  • session 3

    Title

    Solid and Hybrid Propulsion (1)

    type

    oral

    Description

    The session Solid and Hybrid Propulsion (1) is dedicated to Solid and Hybrid Rocket motors, with particular emphasis on full systems. 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

    2023-10-03

    Time

    10:15

    Room

    BCC A8

    IPC members
    • Co-Chair: Dr. Marco Di Clemente, Italian Space Agency (ASI), Italy;

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

    • Rapporteur: Dr. Adam Okninski, Łukasiewicz Research Network – Institute of Aviation (ILOT), Poland;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Passivation of aluminium particle and its effects in solid propellants: a ReaxFF study

    15

    confirmed

    Prof. Rene Gonçalves

    Aeronautic Institute of Technology (ITA)

    Brazil

    2

    10:30

    A Conceptual Design of Permeable Nozzle for Altitude Compensation and Thrust Vectoring

    15

    confirmed

    Mr. Ye Wang

    CAS Space (Guangzhou Zhongke Aerospace Exploration Technology Co., Ltd.)

    China

    3

    10:45

    Design, manufacturing and testing of 50 mm solid rocket motor using non-HTPB composite propellant for potential in-orbit applications.

    15

    confirmed

    Dr. Florin Mingireanu

    Romanian Space Agency (ROSA)

    Romania

    4

    11:00

    effect of aluminum content on nozzle erosion in a hybrid rocket motor

    15

    confirmed

    Dr. Xianzhu Jiang

    School of Astronautics, Beihang University

    China

    5

    11:15

    Hybrid autophage propulsion for space launch vehicles: a promising concept

    15

    confirmed

    Mr. Martin Gros

    France

    6

    11:30

    Research on Analytical Inverse Kinematics Algorithm for Servo Mechanism of Swinging Nozzle

    15

    confirmed

    Mrs. Guanchao Han

    CAS Space (Guangzhou Zhongke Aerospace Exploration Technology Co., Ltd.)

    China

    7

    11:45

    In-Situ Propellant Design for Moon and Mars Exploration Using Hybrid Rockets

    15

    confirmed

    Ms. Hessa Almarzooqi

    Technology Innovation Institute (TII)

    United Arab Emirates

    8

    12:00

    Surrogate Neural Network Model for Integrated Ascent Trajectory Optimization of Throttleable Hybrid Rockets

    15

    confirmed

    Dr. Mario Tindaro Migliorino

    Sapienza University of Rome

    Italy

    9

    12:15

    Design and testing of the combustion chamber of a H2O2/ABS student-developed hybrid rocket engine

    15

    confirmed

    Mr. Giuseppe Oliva

    ISAE - Institut Supérieur de l'Aéronautique et de l'Espace

    France

    10

    12:30

    Course and challenges of flight qualification test campaign of the students’ hybrid rocket engine.

    15

    confirmed

    Mr. Marek Dzik

    Warsaw University of Technology (WUT)

    Poland