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  • session 4

    Title

    Solid and Hybrid Propulsion (2)

    Description

    This session includes all science and technologies supporting all aspects of solid and hybrid propulsion.

    IPC members
    • Co-Chair: Mr. Jerome Breteau, European Space Agency (ESA), France;

    • Co-Chair: Prof.Dr. Arif Karabeyoglu, Koc University, Türkiye;

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

    • Rapporteur: Dr. Ashley Karp, Jet Propulsion Laboratory - California Institute of Technology, United States;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    A Novel Coordinated Energetic Compound Leading a Promising Concept of Propellant Formula Designing

    10

    confirmed

    Mr. Zhenhao Mi

    The 41st Institute of the Fourth Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    2

    Energetic hybrid rocket propellants for upper stage propulsion

    10

    confirmed

    Mr. Vinayak Malhotra

    SRM University Chennai

    India

    3

    Performance evaluation of modified loose flap venting scheme introduced for the propellant processing of upper stage SRM through hot test

    10

    confirmed

    Mr. Shubham Maurya

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    5

    Development of a Thrust Control System for Rocket Engines

    10

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil

    6

    Experimental and Numerical Study on Feasibility of 5kN Thrust Level Hybrid Rocket Motor using the Low-Melting-Point Thermoplastic Fuel

    10

    confirmed

    Dr. Yo Kawabata

    Japan

    7

    numerical and experimental research on ablation performance of a carbon/carbon composties solid rocket motor nozzle insert

    10

    confirmed

    Dr. Lin Sun

    Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory, Northwestern Polytechnical University

    China

    11

    Study on thermoacoustic oscillation characteristics of carbon nanotubes

    10

    confirmed

    Mr. Yu Liao

    Northwestern Polytechnical University

    China

    13

    Experimental investigation of a flow-oriented throttleable injector designed for throttleable hybrid rocket motor

    10

    confirmed

    Mr. Zeng Zhao

    School of Astronautics, Beihang University

    China