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  • session 3

    Title

    Solid and Hybrid Propulsion (1)

    Description

    This session is dedicated to all aspects of Solid and Hybrid Rocket motor.

    IPC members
    • Co-Chair: Mr. Stéphane Henry, ArianeGroup, France;

    • Co-Chair: Dr. Toru Shimada, Institute of Space and Astronautical Science (ISAS), Japan Aerospace Exploration Agency, Japan;

    • Rapporteur: Dr. Yen-Sen Chen, National Space Organization, Taiwan, China;

    • Rapporteur: Dr. Mario Kobald, HyImpulse Technologies GmbH, Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    Performance evaluation of SRM Flex Seal realized through alternate moulding process

    15

    confirmed

    Mr. Ahemedulkabeer M S

    Vikram Sarabhai Space Centre, ISRO, Thiruvananthapuram

    India

    2

    Modeling and Simulating Distributed Combustion in SRM

    15

    confirmed

    Ms. Anne Elisa Leal Caselato

    Universidade de Brasília

    Brazil

    3

    Solid Propellant Burning Rate Measurements using Ultrasonic Technique

    15

    Mr. KIRAN PINUMALLA

    Vikram Sarabhai Space Centre, Thiruvananthapuram-695 022, INDIA

    India

    4

    Deviant ablation mechanism of nozzle throat in solid rocket motors under acceleration conditions

    15

    confirmed

    Prof. Weiping Tian

    The 4th Academy, China Aerospace Science and Technology Corporation (CASC)

    China

    5

    A 75 kN LOX-Paraffin Hybrid Rocket Motor for New-Space

    15

    Dr. Mario Kobald

    HyImpulse Technologies GmbH

    Germany

    6

    TiSPACE Hybrid Rocket Launch Vehicle Design for Space Missions

    15

    confirmed

    Dr. Yen-Sen Chen

    American Institute of Aeronautics and Astronautics (AIAA)

    United States

    7

    EXPERIMENTAL AND NUMERICAL INVESTIGATION OF A PARAFFIN-BASED HYBRID ROCKET ENGINE TO BRAKE A 24U MICROSATELLITE IN A MARS ORBIT

    15

    confirmed

    Mr. Caio Henrique Franco Levi Domingos

    Sapienza University of Rome

    Italy

    8

    Understanding Regression Rate Characteristics of CO2 as an oxidizer compound in Paraffin Based Hybrid Rocket Motors

    15

    confirmed

    Mr. Ozan Kara

    Space Generation Advisory Council (SGAC)

    Turkey

    9

    effects of a pre-heater for improvement of combustion efficiency in hybrid rockets using liquid oxygen

    15

    withdrawn

    Prof. Jungpyo Lee

    University of Brasilia

    Brazil

    10

    Experimental study of a Mg/N2O powdered metal fuel rocket engine

    15

    confirmed

    Dr. Liya Huang

    National University of Defense Technology

    China

    11

    Variations and Control of Thrust and Mixture Ratio in Hybrid Rocket Motors

    15

    confirmed

    Dr. Francesco Barato

    University of Padova - DII/CISAS

    Italy

    12

    RMD Simulation and Combustion evaluation of Paraffin/GOX for hybrid rocket motors

    15

    withdrawn

    Prof.Dr. Rene Gonçalves

    Instituto Tecnológico de Aeronáutica (ITA)

    Brazil

    13

    impact assessment of propellant entrapment in loose flap cavity on ballistic performance and validation through hot test of solid rocket booster

    confirmed

    Mr. Arun Raj

    Vikram Sarabhai Space Centre (VSSC)

    India

    14

    Effect of residual strain on structural integrity of SRM grain during ignition

    Prof. Jinxian Li

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

    China

    15

    Investigation of a Dual-Fuel Hybrid Rocket Engine for Missile and Rocket Applications

    confirmed

    Mr. Maurício Gontijo

    University of Brasilia

    Brazil