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  • session 3

    Title

    Solid and Hybrid Propulsion (1)

    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

    2024-10-15

    Time

    10:15

    Room

    Blue Hall 1

    IPC members
    • Co-Chair: Dr. Yen-Sen Chen, American Institute of Aeronautics and Astronautics (AIAA), United States;

    • Co-Chair: Dr. Christian Bach, Technische Universität Dresden (DTU), Germany;

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

    • Rapporteur: Dr. Yuji Saito, Tohoku University, Japan;

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

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    10:15

    Preliminary Design and Flight Performance of Paraffin/N2O Sounding Rocket Program in the UAE

    12

    confirmed

    Dr. Ozan Kara

    Technology Innovation Institute (TII)

    United Arab Emirates

    2

    10:27

    Analytical and experimental investigation of a H2O2-HDPE hybrid autophage rocket engine

    12

    confirmed

    Mr. Vincenzo Mazzella

    Alpha Impulsion

    France

    3

    10:39

    Mechanical development and static-fire testing of an orbital-scale hybrid propulsion engine

    12

    confirmed

    Mr. Clément Arrat

    Hybrid Propulsion for Space (HyPr Space)

    France

    4

    10:51

    Impact assessment of long term vertical storage on ballistic performance and validation through hot test of solid rocket booster

    12

    confirmed

    Mr. Arun Raj

    Vikram Sarabhai Space Centre (VSSC)

    India

    5

    11:03

    Research and Development of Hybrid Thruster for ELS-R100: Mission Concept & Firing Test Results

    12

    confirmed

    Dr. Yuji Saito

    Tohoku University

    Japan

    6

    11:15

    Insights into MOUETTE Hybrid Rocket Slab Burner Testing Activities

    12

    confirmed

    Mr. Riccardo Gelain

    Université Libre de Bruxelles

    Belgium

    7

    11:27

    Numerical Modeling of Scale Effects in Paraffin-Hydrogen Peroxide Hybrid Rockets with Swirl Injection

    12

    confirmed

    Mr. Alessio Sereno

    Sapienza University of Rome

    Italy

    8

    11:39

    Experimental Verification of Advanced Hybrids Performance and Scaling Factors

    12

    confirmed

    Mr. Manuel Stella

    T4i

    Italy

    9

    11:51

    Experimental study of water and aluminum combustion aiming for a novel pulsed-chemical micropropulsion system

    12

    confirmed

    Dr. Masaya Murohara

    ZHAW – Zurich University of Applied Sciences

    Switzerland

    10

    12:03

    RAVEN: Results and Insights from the first test campaign of a hybrid rocket engine

    12

    confirmed

    Ms. Zoe Zahariades

    Luleå University of Technology

    Sweden

    11

    12:15

    Propulsive and combustion modelling of SABRE engine in rocket mode to support NOx emissions estimation in conceptual design

    12

    confirmed

    Mr. Alessio Ricca

    Turin Polytechnical University

    Italy

    12

    12:27

    Automatic Outlier Detection for Hybrid Rocket Static Firing Tests

    12

    confirmed

    Mr. Oliver Assenmacher

    German Aerospace Center (DLR)

    Germany

    1*

    10:15

    Three Dimensional and Multiphase Simulations of Aft-Finocyl Solid Rocket Motors

    12

    confirmed

    Mr. Gianluca Cocirla

    Sapienza University of Rome

    Italy

    2*

    10:27

    effect of the electrode shape on the combustion characteristics of electrically controlled solid propellant

    12

    confirmed

    Mr. Myoungjin Kim

    Chosun University

    Korea, Republic of

    3*

    10:39

    Numerical study of an additively manufactured hybrid rocket engine of 1 kN: A CFD Approach

    12

    confirmed

    Dr. Olexiy Shynkarenko

    University of Brasilia

    Brazil

    4*

    10:51

    Preliminary design of a throttleable hybrid rocket engine using the A-SOFT principle

    12

    confirmed

    Mr. Joël Martin

    Deutsch Luft und Raumfahrt Zentrum (DLR)

    Germany

    5*

    11:03

    Thermo structural assessment of Un-submerged Flex Nozzle system (USFN) with 4-D Carbon- Carbon Nozzle liner

    10

    confirmed

    Mr. Paul Murugan J

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India