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  • session 2

    Title

    Propulsion System (2)

    Description

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

    Date

    2019-10-23

    Time

    09:45

    Room

    143A

    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, American Institute of Aeronautics and Astronautics (AIAA), United States;

    • Rapporteur: Dr. Mario Kobald, German Aerospace Center (DLR), Germany;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    09:45

    KEYNOTE: OmegA Launch Vehicle

    25

    confirmed

    Mr. Kent Rominger

    Northrop Grumman Innovation Systems

    United States

    2

    10:10

    Ariane 6 and Vega-C programs: the P120C SRM nozzle qualification

    13

    confirmed

    Mr. ERIC GAUTRONNEAU

    ArianeGroup SAS

    France

    3

    10:23

    Performance evaluation of 4D Carbon-Carbon throat insert through Hot test of Solid Motor

    13

    confirmed

    Mr. Siva kumar Ganesan

    Indian Space Research Organization (ISRO)

    India

    4

    10:36

    Design and Developmental Challenges of Slow Burning Solid Booster for Sub-orbital Hyper Sonic re-entry Experiment

    13

    confirmed

    Dr. ACHUTANANDA PARHI

    Indian Space Research Organization (ISRO)

    India

    5

    10:49

    Performance and environmental impact prediction of SRMs. Road map for reliable dataset of particles in plume

    13

    confirmed

    Ms. Stefania Carlotti

    Politecnico di Milano

    Italy

    6

    11:02

    Analysis of Solid Propellant Combustion Using Image Processing Techniques

    13

    confirmed

    Ms. Sonali Sinha Roy

    Purdue University

    United States

    7

    11:15

    Mars Ascent Vehicle (MAV) Preliminary Architecture Assessment Overview

    13

    confirmed

    Ms. Angie Jackman

    NASA

    United States

    8

    11:28

    A Study on New Hybrid Rocket Engine with Multi-Section Swirl Injection and Aft Counter-Swirl Injection Method

    13

    confirmed

    Prof. Shigeru Aso

    Kyushu University

    Japan

    9

    11:41

    Real-time regression rate measurement of an additive-manufactured functional hybrid rocket fuel

    13

    confirmed

    Dr. Kohei Ozawa

    Kyushu Institute of Technology

    Japan

    10

    11:54

    Cost-Effective Hybrid Rocket Launch Vehicle of Taiwan

    13

    confirmed

    Dr. Yen-Sen Chen

    American Institute of Aeronautics and Astronautics (AIAA)

    United States

    11

    12:07

    Green Fuels for Rocket Propulsion: Current Status and Future Perspectives of Paraffin-based Formulations

    13

    confirmed

    Mr. Riccardo Bisin

    Politecnico di Milano

    Italy

    12

    12:20

    dynamic response of thrust modulation in hybrid rocket for VTVL propulsion system

    13

    confirmed

    Prof. Changjin Lee

    Konkuk University

    Korea, Republic of

    13

    12:33

    Performance Analysis of N2O/CO2 Oxidizer Mixture with Paraffin based Micro-Aluminum Fuel for Mars Ascent Vehicles

    13

    confirmed

    Mr. Ozan Kara

    Space Generation Advisory Council (SGAC)

    Turkey